ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 7534.74
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 74.3
Monthly MSFC 50% earth geomagnetic index (Kp) : 1.63
ET - UTC (sec) : 66.18
UT1 - UTC (sec) : 0.00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
There are no maneuvers.
Coasting Arc #1 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2009/236/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4415707.96 A = 6722127.16 meter
Y = 1177666.16 meter E = .0008163
Z = 4922499.90 I = 51.39335
XDOT = -3995.690952 Wp = 52.91572
YDOT = 6248.870548 meter/sec RA = 315.60994 deg
ZDOT = 2091.804073 TA = 16.77253
MA = 16.74555
Ha = 192.359 n.mi
Hp = 182.938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14487230.84 X = 4378298.33
Y = 3863734.13 feet Y = 1226836.13 meter
Z = 16149934.07 Z = 4943860.49
XDOT = -13109.222284 XDOT = -4075.431519
YDOT = 20501.543793 feet/sec YDOT = 6203.742573 meter/sec
ZDOT = 6862.874256 ZDOT = 2072.199222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10917541.26 X = -3327666.58
Y = -10143632.76 feet Y = -3091779.27 meter
Z = 16233997.55 Z = 4948122.45
XDOT = 20467.578547 XDOT = 6238.517941
YDOT = -11181.583517 feet/sec YDOT = -3408.146656 meter/sec
ZDOT = 6786.061647 ZDOT = 2068.391590
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09236.55118355 .00020000 00000-0 20000-3 0 9002
2 25544 51.6423 315.9047 0008401 10.3667 349.7668 15.73781612 16728
Satellite: ISS
Catalog Number: 25544
Epoch time: 09236.55118355 = yrday.fracday
Element set: 900
Inclination: 51.6423 deg
RA of node: 315.9047 deg
Eccentricity: .0008401
Arg of perigee: 10.3667 deg
Mean anomaly: 349.7668 deg
Mean motion: 15.73781612 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1672
Checksum: 292
Coasting Arc #2 (Orbit 1686)
---------------------------------------
Vector Time (GMT): 2009/237/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2919037.75 A = 6731395.19 meter
Y = -5754706.27 meter E = .0015425
Z = -1891196.17 I = 51.40287
XDOT = 5207.228117 Wp = 24.63748
YDOT = 804.448116 meter/sec RA = 310.42544 deg
ZDOT = 5619.661466 TA = 314.27048
MA = 314.39694
Ha = 192.711 n.mi
Hp = 182.803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9576895.50 X = 2992358.00
Y = -18880269.90 feet Y = -5721653.92 meter
Z = -6204711.85 Z = -1876837.37
XDOT = 17084.081749 XDOT = 5170.546327
YDOT = 2639.265472 feet/sec YDOT = 862.473318 meter/sec
ZDOT = 18437.209533 ZDOT = 5644.869076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17111036.66 X = -5215443.97
Y = 12493527.27 feet Y = 3808027.11 meter
Z = -6148509.48 Z = -1874065.69
XDOT = -13037.304980 XDOT = -3973.770558
YDOT = -8782.613233 feet/sec YDOT = -2676.940514 meter/sec
ZDOT = 18536.384638 ZDOT = 5649.890038
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09237.50367121 .00020000 00000-0 20000-3 0 9016
2 25544 51.6416 311.0157 0008645 13.5652 346.5742 15.73736589 16875
Satellite: ISS
Catalog Number: 25544
Epoch time: 09237.50367121 = yrday.fracday
Element set: 901
Inclination: 51.6416 deg
RA of node: 311.0157 deg
Eccentricity: .0008645
Arg of perigee: 13.5652 deg
Mean anomaly: 346.5742 deg
Mean motion: 15.73736589 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1687
Checksum: 293
Coasting Arc #3 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2009/238/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4621627.45 A = 6722364.69 meter
Y = -242886.01 meter E = .0018737
Z = -4892213.52 I = 51.35358
XDOT = 2696.622057 Wp = 51.38454
YDOT = -6853.084122 meter/sec RA = 305.30791 deg
ZDOT = -2201.404353 TA = 197.07168
MA = 197.13479
Ha = 192.738 n.mi
Hp = 182.438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15162819.71 X = -4594802.49
Y = -796870.12 feet Y = -294417.72 meter
Z = -16050569.28 Z = -4914600.22
XDOT = 8847.185226 XDOT = 2783.748021
YDOT = -22483.871792 feet/sec YDOT = -6822.441734 meter/sec
ZDOT = -7222.455227 ZDOT = -2188.092632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13207703.37 X = 4025707.99
Y = 7298509.04 feet Y = 2224585.56 meter
Z = -16138624.95 Z = -4919052.89
XDOT = -17284.180789 XDOT = -5268.218304
YDOT = 15380.749154 feet/sec YDOT = 4688.052342 meter/sec
ZDOT = -7170.422853 ZDOT = -2185.544886
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09238.51964862 .00020000 00000-0 20000-3 0 9024
2 25544 51.6408 305.7998 0008574 18.0388 342.1078 15.73765675 17037
Satellite: ISS
Catalog Number: 25544
Epoch time: 09238.51964862 = yrday.fracday
Element set: 902
Inclination: 51.6408 deg
RA of node: 305.7998 deg
Eccentricity: .0008574
Arg of perigee: 18.0388 deg
Mean anomaly: 342.1078 deg
Mean motion: 15.73765675 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1703
Checksum: 323
Coasting Arc #4 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2009/239/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1784130.46 A = 6731031.01 meter
Y = 6186837.82 meter E = .0016566
Z = 1953416.11 I = 51.36751
XDOT = -5298.254128 Wp = 79.95649
YDOT = 247.211375 meter/sec RA = 300.11819 deg
ZDOT = -5579.077846 TA = 78.22698
MA = 78.04119
Ha = 192.830 n.mi
Hp = 182.280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5853446.39 X = -1862669.46
Y = 20298024.35 feet Y = 6166447.44 meter
Z = 6408845.50 Z = 1944558.21
XDOT = -17382.723518 XDOT = -5273.522623
YDOT = 811.060943 feet/sec YDOT = 188.101612 meter/sec
ZDOT = -18304.061174 ZDOT = -5604.756623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13892454.25 X = 4234420.06
Y = -15928400.54 feet Y = -4854976.49 meter
Z = 6374299.86 Z = 1942886.60
XDOT = 14848.461371 XDOT = 4525.811026
YDOT = 5528.391095 feet/sec YDOT = 1685.053606 meter/sec
ZDOT = -18405.043713 ZDOT = -5609.857324
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09239.53561561 .00020000 00000-0 20000-3 0 9037
2 25544 51.6413 300.5837 0008830 21.8778 338.2761 15.73828071 17190
Satellite: ISS
Catalog Number: 25544
Epoch time: 09239.53561561 = yrday.fracday
Element set: 903
Inclination: 51.6413 deg
RA of node: 300.5837 deg
Eccentricity: .0008830
Arg of perigee: 21.8778 deg
Mean anomaly: 338.2761 deg
Mean motion: 15.73828071 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1719
Checksum: 299
Coasting Arc #5 (Orbit 1734)
---------------------------------------
Vector Time (GMT): 2009/240/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4597899.30 A = 6722305.86 meter
Y = -679900.74 meter E = .0010372
Z = 4846943.24 I = 51.32401
XDOT = -1347.644316 Wp = 64.98786
YDOT = 7234.695364 meter/sec RA = 294.99939 deg
ZDOT = 2293.744494 TA = 2.60940
MA = 2.60399
Ha = 192.751 n.mi
Hp = 182.139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15084971.45 X = 4581614.89
Y = -2230645.48 feet Y = -628575.54 meter
Z = 15902044.76 Z = 4869240.14
XDOT = -4421.405236 XDOT = -1439.586299
YDOT = 23735.877177 feet/sec YDOT = 7219.111064 meter/sec
ZDOT = 7525.408445 ZDOT = 2286.974583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14608367.91 X = -4452630.54
Y = -4041282.58 feet Y = -1231782.93 meter
Z = 15989708.97 Z = 4873663.29
XDOT = 13412.920875 XDOT = 4088.258283
YDOT = -18820.333890 feet/sec YDOT = -5736.437770 meter/sec
ZDOT = 7499.128254 ZDOT = 2285.734292
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09240.55157381 .00020000 00000-0 20000-3 0 9043
2 25544 51.6409 295.3678 0008754 25.9266 334.2334 15.73828839 17353
Satellite: ISS
Catalog Number: 25544
Epoch time: 09240.55157381 = yrday.fracday
Element set: 904
Inclination: 51.6409 deg
RA of node: 295.3678 deg
Eccentricity: .0008754
Arg of perigee: 25.9266 deg
Mean anomaly: 334.2334 deg
Mean motion: 15.73828839 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1735
Checksum: 318
Coasting Arc #6 (Orbit 1749)
---------------------------------------
Vector Time (GMT): 2009/241/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 555170.74 A = 6730855.56 meter
Y = -6381058.60 meter E = .0015449
Z = -2049863.13 I = 51.34089
XDOT = 5185.429441 Wp = 34.02637
YDOT = -1318.087893 meter/sec RA = 289.80641 deg
ZDOT = 5540.199096 TA = 302.99822
MA = 303.14660
Ha = 193.002 n.mi
Hp = 181.951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1821426.31 X = 636441.35
Y = -20935231.64 feet Y = -6374395.89 meter
Z = -6725272.74 Z = -2046968.93
XDOT = 17012.563782 XDOT = 5172.870081
YDOT = -4324.435346 feet/sec YDOT = -1260.171775 meter/sec
ZDOT = 18176.506219 ZDOT = 5565.359146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9873320.44 X = -3009388.07
Y = 18554456.48 feet Y = 5655398.34 meter
Z = -6714201.31 Z = -2046488.56
XDOT = -15901.688512 XDOT = -4846.834659
YDOT = -1887.390155 feet/sec YDOT = -575.276519 meter/sec
ZDOT = 18275.404163 ZDOT = 5570.343189
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09241.50402714 .00020000 00000-0 20000-3 0 9053
2 25544 51.6406 290.4780 0008905 29.6089 330.5577 15.73822263 17502
Satellite: ISS
Catalog Number: 25544
Epoch time: 09241.50402714 = yrday.fracday
Element set: 905
Inclination: 51.6406 deg
RA of node: 290.4780 deg
Eccentricity: .0008905
Arg of perigee: 29.6089 deg
Mean anomaly: 330.5577 deg
Mean motion: 15.73822263 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1750
Checksum: 287
Coasting Arc #7 (Orbit 1765)
---------------------------------------
Vector Time (GMT): 2009/242/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4416762.49 A = 6722444.57 meter
Y = 1582025.37 meter E = .0019877
Z = -4832959.33 I = 51.30414
XDOT = -35.525983 Wp = 56.36861
YDOT = -7314.460061 meter/sec RA = 284.68666 deg
ZDOT = -2357.982043 TA = 190.46192
MA = 190.50334
Ha = 193.099 n.mi
Hp = 181.641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14490690.57 X = -4410647.33
Y = 5190371.95 feet Y = 1532668.84 meter
Z = -15856165.79 Z = -4854400.82
XDOT = -116.555062 XDOT = 57.722726
YDOT = -23997.572377 feet/sec YDOT = -7314.335896 meter/sec
ZDOT = -7736.161558 ZDOT = -2357.928302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15294340.66 X = 4661715.03
Y = 569219.92 feet Y = 173498.23 meter
Z = -15940426.60 Z = -4858642.03
XDOT = -8864.158384 XDOT = -2701.795475
YDOT = 21168.878219 feet/sec YDOT = 6452.274081 meter/sec
ZDOT = -7736.317912 ZDOT = -2358.029700
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09242.51996764 .00020000 00000-0 20000-3 0 9069
2 25544 51.6411 285.2616 0008926 33.9995 326.1739 15.73828692 17665
Satellite: ISS
Catalog Number: 25544
Epoch time: 09242.51996764 = yrday.fracday
Element set: 906
Inclination: 51.6411 deg
RA of node: 285.2616 deg
Eccentricity: .0008926
Arg of perigee: 33.9995 deg
Mean anomaly: 326.1739 deg
Mean motion: 15.73828692 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1766
Checksum: 336
Coasting Arc #8 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2009/243/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 616007.08 A = 6730651.96 meter
Y = 6370511.56 meter E = .0018855
Z = 2071462.14 I = 51.32525
XDOT = -4860.384471 Wp = 82.93306
YDOT = 2279.448161 meter/sec RA = 279.49128 deg
ZDOT = -5519.516674 TA = 73.83697
MA = 73.62954
Ha = 193.144 n.mi
Hp = 181.529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2021020.60 X = 534662.49
Y = 20900628.49 feet Y = 6376945.27 meter
Z = 6796135.62 Z = 2074257.14
XDOT = -15946.143278 XDOT = -4858.699970
YDOT = 7478.504465 feet/sec YDOT = 2225.105959 meter/sec
ZDOT = -18108.650504 ZDOT = -5543.123985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5629332.48 X = 1715820.54
Y = -20225660.65 feet Y = -6164781.37 meter
Z = 6807460.74 Z = 2074914.03
XDOT = 15992.586089 XDOT = 4874.540240
YDOT = -1724.879131 feet/sec YDOT = -525.743159 meter/sec
ZDOT = -18201.396109 ZDOT = -5547.785534
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09243.53589720 .00020000 00000-0 20000-3 0 9073
2 25544 51.6404 280.0454 0009109 37.4699 322.7097 15.73880657 17820
Satellite: ISS
Catalog Number: 25544
Epoch time: 09243.53589720 = yrday.fracday
Element set: 907
Inclination: 51.6404 deg
RA of node: 280.0454 deg
Eccentricity: .0009109
Arg of perigee: 37.4699 deg
Mean anomaly: 322.7097 deg
Mean motion: 15.73880657 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1782
Checksum: 315
Coasting Arc #9 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2009/244/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4040003.01 A = 6722375.60 meter
Y = -2392479.31 meter E = .0012529
Z = 4799258.10 I = 51.29293
XDOT = 1389.351152 Wp = 75.02690
YDOT = 7189.651803 meter/sec RA = 274.37118 deg
ZDOT = 2412.526471 TA = 351.32209
MA = 351.34374
Ha = 193.123 n.mi
Hp = 181.382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13254603.06 X = 4043142.28
Y = -7849341.56 feet Y = -2347284.03 meter
Z = 15745597.45 Z = 4818891.80
XDOT = 4558.238688 XDOT = 1297.132521
YDOT = 23588.096468 feet/sec YDOT = 7204.672743 meter/sec
ZDOT = 7915.113093 ZDOT = 2419.051786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15052505.67 X = -4588003.73
Y = 2878294.47 feet Y = 877304.15 meter
Z = 15822705.16 Z = 4822760.53
XDOT = 4030.618720 XDOT = 1228.532586
YDOT = -22612.366960 feet/sec YDOT = -6892.249450 meter/sec
ZDOT = 7941.168327 ZDOT = 2420.468106
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09244.55181840 .00020000 00000-0 20000-3 0 9088
2 25544 51.6396 274.8292 0009169 42.1176 318.0691 15.73878466 17980
Satellite: ISS
Catalog Number: 25544
Epoch time: 09244.55181840 = yrday.fracday
Element set: 908
Inclination: 51.6396 deg
RA of node: 274.8292 deg
Eccentricity: .0009169
Arg of perigee: 42.1176 deg
Mean anomaly: 318.0691 deg
Mean motion: 15.73878466 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1798
Checksum: 330
Coasting Arc #10 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2009/245/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1798104.97 A = 6730390.49 meter
Y = -6119770.31 meter E = .0015458
Z = -2135668.49 I = 51.32018
XDOT = 4353.727639 Wp = 44.14506
YDOT = -3184.712348 meter/sec RA = 269.17458 deg
ZDOT = 5495.007517 TA = 291.85644
MA = 292.02077
Ha = 193.199 n.mi
Hp = 181.178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5899294.53 X = -1719164.46
Y = -20077986.58 feet Y = -6139436.46 meter
Z = -7006786.39 Z = -2144211.64
XDOT = 14283.883331 XDOT = 4362.322677
YDOT = -10448.531326 feet/sec YDOT = -3135.978192 meter/sec
ZDOT = 18028.239886 ZDOT = 5516.178600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -996686.68 X = -303790.10
Y = 20891552.14 feet Y = 6367745.09 meter
Z = -7040734.45 Z = -2146015.86
XDOT = -15284.046290 XDOT = -4658.577309
YDOT = 5336.339245 feet/sec YDOT = 1626.516202 meter/sec
ZDOT = 18111.349689 ZDOT = 5520.339385
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09245.50423532 .00020000 00000-0 20000-3 0 9092
2 25544 51.6405 269.9394 0009164 45.8465 314.3450 15.73921460 18138
Satellite: ISS
Catalog Number: 25544
Epoch time: 09245.50423532 = yrday.fracday
Element set: 909
Inclination: 51.6405 deg
RA of node: 269.9394 deg
Eccentricity: .0009164
Arg of perigee: 45.8465 deg
Mean anomaly: 314.3450 deg
Mean motion: 15.73921460 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1813
Checksum: 292
Coasting Arc #11 (Orbit 1828)
---------------------------------------
Vector Time (GMT): 2009/246/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3546396.95 A = 6722385.05 meter
Y = 3116737.19 meter E = .0020646
Z = -4804774.15 I = 51.29403
XDOT = -2665.824853 Wp = 62.24880
YDOT = -6784.558242 meter/sec RA = 264.05425 deg
ZDOT = -2431.847772 TA = 183.81880
MA = 183.83458
Ha = 193.317 n.mi
Hp = 181.019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11635160.59 X = -3557644.81
Y = 10225515.70 feet Y = 3077016.16 meter
Z = -15763694.72 Z = -4822029.82
XDOT = -8746.144531 XDOT = -2577.947284
YDOT = -22259.049349 feet/sec YDOT = -6813.877832 meter/sec
ZDOT = -7978.503189 ZDOT = -2444.584414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14139183.35 X = 4309623.08
Y = -6154870.73 feet Y = -1876004.60 meter
Z = -15831401.24 Z = -4825411.10
XDOT = 941.483502 XDOT = 286.964172
YDOT = 22827.266961 feet/sec YDOT = 6957.750970 meter/sec
ZDOT = -8028.998425 ZDOT = -2447.238720
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09246.52013664 .00020000 00000-0 20000-3 0 9108
2 25544 51.6399 264.7225 0009172 49.0417 311.1538 15.73899030 18294
Satellite: ISS
Catalog Number: 25544
Epoch time: 09246.52013664 = yrday.fracday
Element set: 910
Inclination: 51.6399 deg
RA of node: 264.7225 deg
Eccentricity: .0009172
Arg of perigee: 49.0417 deg
Mean anomaly: 311.1538 deg
Mean motion: 15.73899030 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1829
Checksum: 294
Coasting Arc #12 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2009/247/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2852714.51 A = 6730394.98 meter
Y = 5710195.23 meter E = .0020669
Z = 2117954.40 I = 51.32435
XDOT = -3714.063354 Wp = 87.45970
YDOT = 3911.809148 meter/sec RA = 258.85637 deg
ZDOT = -5496.969889 TA = 68.75026
MA = 68.52964
Ha = 193.353 n.mi
Hp = 180.924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9359299.56 X = 2778361.54
Y = 18734236.32 feet Y = 5741680.37 meter
Z = 6948669.29 Z = 2131631.79
XDOT = -12185.247224 XDOT = -3730.826761
YDOT = 12834.019515 feet/sec YDOT = 3870.182213 meter/sec
ZDOT = -18034.678113 ZDOT = -5515.053643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3424607.82 X = -1043820.46
Y = -20641820.67 feet Y = -6291626.94 meter
Z = 7002814.05 Z = 2134457.72
XDOT = 13803.090774 XDOT = 4207.182068
YDOT = -8484.398180 feet/sec YDOT = -2586.044565 meter/sec
ZDOT = -18105.591629 ZDOT = -5518.584329
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09247.53602773 .00020000 00000-0 20000-3 0 9116
2 25544 51.6385 259.5052 0009339 52.5877 307.6135 15.73932910 18459
Satellite: ISS
Catalog Number: 25544
Epoch time: 09247.53602773 = yrday.fracday
Element set: 911
Inclination: 51.6385 deg
RA of node: 259.5052 deg
Eccentricity: .0009339
Arg of perigee: 52.5877 deg
Mean anomaly: 307.6135 deg
Mean motion: 15.73932910 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1845
Checksum: 307
Coasting Arc #13 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2009/248/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2914405.08 A = 6722320.13 meter
Y = -3697965.56 meter E = .0013925
Z = 4785493.81 I = 51.30348
XDOT = 3855.316723 Wp = 83.51896
YDOT = 6212.522494 meter/sec RA = 253.73628 deg
ZDOT = 2448.239462 TA = 342.45119
MA = 342.49925
Ha = 193.313 n.mi
Hp = 180.889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9561696.46 X = 2932292.77
Y = -12132432.94 feet Y = -3665274.58 meter
Z = 15700439.00 Z = 4799695.68
XDOT = 12648.676912 XDOT = 3773.667621
YDOT = 20382.291646 feet/sec YDOT = 6255.178580 meter/sec
ZDOT = 8032.281701 ZDOT = 2466.769720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12453673.86 X = -3795879.79
Y = 9043086.60 feet Y = 2756332.79 meter
Z = 15756089.14 Z = 4802455.97
XDOT = -5819.526353 XDOT = -1773.791632
YDOT = -22162.785542 feet/sec YDOT = -6755.217033 meter/sec
ZDOT = 8105.556911 ZDOT = 2470.573746
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09248.55190896 .00020000 00000-0 20000-3 0 9128
2 25544 51.6379 254.2881 0009305 56.1551 304.0496 15.73927273 18611
Satellite: ISS
Catalog Number: 25544
Epoch time: 09248.55190896 = yrday.fracday
Element set: 912
Inclination: 51.6379 deg
RA of node: 254.2881 deg
Eccentricity: .0009305
Arg of perigee: 56.1551 deg
Mean anomaly: 304.0496 deg
Mean motion: 15.73927273 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1861
Checksum: 311
Coasting Arc #14 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2009/249/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3845571.18 A = 6730210.28 meter
Y = -5085429.26 meter E = .0015392
Z = -2148134.44 I = 51.34067
XDOT = 2939.487477 Wp = 53.00197
YDOT = -4526.457042 meter/sec RA = 248.54019 deg
ZDOT = 5489.722553 TA = 282.86319
MA = 283.03510
Ha = 193.353 n.mi
Hp = 180.691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12616703.35 X = -3777983.95
Y = -16684479.21 feet Y = -5128054.98 meter
Z = -7047685.16 Z = -2166651.67
XDOT = 9643.987785 XDOT = 2963.216499
YDOT = -14850.580846 feet/sec YDOT = -4493.452847 meter/sec
ZDOT = 18010.900763 ZDOT = 5504.060608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7810015.31 X = 2380492.67
Y = 19378341.27 feet Y = 5906518.42 meter
Z = -7120847.34 Z = -2170434.27
XDOT = -11655.668763 XDOT = -3552.647839
YDOT = 11293.394518 feet/sec YDOT = 3442.226649 meter/sec
ZDOT = 18067.033180 ZDOT = 5506.831713
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09249.50428735 .00020000 00000-0 20000-3 0 9131
2 25544 51.6384 249.3981 0009345 60.0378 300.1712 15.73968457 18761
Satellite: ISS
Catalog Number: 25544
Epoch time: 09249.50428735 = yrday.fracday
Element set: 913
Inclination: 51.6384 deg
RA of node: 249.3981 deg
Eccentricity: .0009345
Arg of perigee: 60.0378 deg
Mean anomaly: 300.1712 deg
Mean motion: 15.73968457 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1876
Checksum: 314
Coasting Arc #15 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2009/250/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 701645.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2227301.98 A = 6722228.97 meter
Y = 4155551.71 meter E = .0021125
Z = -4811429.28 I = 51.32481
XDOT = -4879.537364 Wp = 68.45371
YDOT = -5419.184762 meter/sec RA = 243.42055 deg
ZDOT = -2422.530120 TA = 177.73382
MA = 177.72424
Ha = 193.429 n.mi
Hp = 180.614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7307421.20 X = -2250231.33
Y = 13633699.83 feet Y = 4130516.15 meter
Z = -15785529.15 Z = -4822305.58
XDOT = -16008.980854 XDOT = -4806.808157
YDOT = -17779.477567 feet/sec YDOT = -5473.344145 meter/sec
ZDOT = -7947.933464 ZDOT = -2446.058005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10313101.34 X = 3143433.29
Y = -11470460.07 feet Y = -3496196.23 meter
Z = -15828063.45 Z = -4824393.74
XDOT = 10324.928730 XDOT = 3147.038277
YDOT = 20374.617278 feet/sec YDOT = 6210.183346 meter/sec
ZDOT = -8040.834520 ZDOT = -2450.846362
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09250.52014786 .00020000 00000-0 20000-3 0 9143
2 25544 51.6376 244.1800 0009297 63.1065 297.1048 15.73955341 18921
Satellite: ISS
Catalog Number: 25544
Epoch time: 09250.52014786 = yrday.fracday
Element set: 914
Inclination: 51.6376 deg
RA of node: 244.1800 deg
Eccentricity: .0009297
Arg of perigee: 63.1065 deg
Mean anomaly: 297.1048 deg
Mean motion: 15.73955341 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 1892
Checksum: 296
|
