ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 10225.71
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 72.1
Monthly MSFC 50% earth geomagnetic index (Kp) : 2.19
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 2209)
---------------------------------------
Vector Time (GMT): 2009/016/12:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 639525.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5128696.28 A = 6737721.70 meter
Y = -2863364.79 meter E = .0003320
Z = -3298061.42 I = 51.66039
XDOT = 4980.607130 Wp = 273.61080
YDOT = -3487.405150 meter/sec RA = 2.81148 deg
ZDOT = -4713.137898 TA = 305.01228
MA = 305.04344
Ha = 193.230 n.mi
Hp = 192.584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16826431.37 X = -5080275.32
Y = -9394241.44 feet Y = -2920445.98 meter
Z = -10820411.48 Z = -3322858.80
XDOT = 16340.574575 XDOT = 5042.128965
YDOT = -11441.617947 feet/sec YDOT = -3431.364932 meter/sec
ZDOT = -15463.050848 ZDOT = -4688.793142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1190467.95 X = -362854.63
Y = -19179707.81 feet Y = -5845974.94 meter
Z = -10917117.93 Z = -3327537.55
XDOT = 17121.298143 XDOT = 5218.571674
YDOT = 7692.969203 feet/sec YDOT = 2344.817013 meter/sec
ZDOT = -15368.487999 ZDOT = -4684.315142
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 09016.54575237 .00010596 00000-0 82463-4 0 9004
2 25544 51.6401 3.1542 0008078 273.4222 86.6015 15.70373981 22104
Satellite: ISS
Catalog Number: 25544
Epoch time: 09016.54575237 = yrday.fracday
Element set: 900
Inclination: 51.6401 deg
RA of node: 3.1542 deg
Eccentricity: .0008078
Arg of perigee: 273.4222 deg
Mean anomaly: 86.6015 deg
Mean motion: 15.70373981 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2210
Checksum: 278
Coasting Arc #2 (Orbit 2225)
---------------------------------------
Vector Time (GMT): 2009/017/12:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 639525.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2780331.06 A = 6732747.47 meter
Y = 3880524.65 meter E = .0004905
Z = 4750979.18 I = 51.61404
XDOT = -7002.566046 Wp = 342.30696
YDOT = -1796.366683 meter/sec RA = 357.65834 deg
ZDOT = -2626.865306 TA = 133.54285
MA = 133.50210
Ha = 193.771 n.mi
Hp = 192.884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9121821.06 X = -2846596.24
Y = 12731380.07 feet Y = 3849062.62 meter
Z = 15587202.03 Z = 4737311.71
XDOT = -22974.298052 XDOT = -6969.197628
YDOT = -5893.591479 feet/sec YDOT = -1874.486732 meter/sec
ZDOT = -8618.324495 ZDOT = -2660.802462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15704076.46 X = -4786602.51
Y = -571177.46 feet Y = -174094.89 meter
Z = 15534228.78 Z = 4734832.93
XDOT = -7898.088749 XDOT = -2407.337451
YDOT = -21182.686088 feet/sec YDOT = -6456.482719 meter/sec
ZDOT = -8750.543518 ZDOT = -2667.165664
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 09017.56392417 .00010596 00000-0 82463-4 0 9015
2 25544 51.6400 357.9537 0008225 277.5404 82.4822 15.70397006 22269
Satellite: ISS
Catalog Number: 25544
Epoch time: 09017.56392417 = yrday.fracday
Element set: 901
Inclination: 51.6400 deg
RA of node: 357.9537 deg
Eccentricity: .0008225
Arg of perigee: 277.5404 deg
Mean anomaly: 82.4822 deg
Mean motion: 15.70397006 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2226
Checksum: 304
Coasting Arc #3 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2009/018/12:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 639525.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6627567.02 A = 6741641.74 meter
Y = 92736.75 meter E = .0009494
Z = 1196501.39 I = 51.61550
XDOT = -1129.838128 Wp = 23.38647
YDOT = 4840.922699 meter/sec RA = 352.58041 deg
ZDOT = 5875.768692 TA = 349.71217
MA = 349.73159
Ha = 193.804 n.mi
Hp = 192.678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21743986.29 X = 6620225.11
Y = 304254.42 feet Y = 166808.92 meter
Z = 3925529.50 Z = 1228680.00
XDOT = -3706.818004 XDOT = -1212.429321
YDOT = 15882.292318 feet/sec YDOT = 4827.826012 meter/sec
ZDOT = 19277.456337 ZDOT = 5870.079695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12143155.07 X = 3701233.67
Y = 18012165.38 feet Y = 5490108.01 meter
Z = 4050799.41 Z = 1234683.66
XDOT = -13908.480593 XDOT = -4239.304885
YDOT = 5040.912809 feet/sec YDOT = 1536.470224 meter/sec
ZDOT = 19255.597463 ZDOT = 5869.106107
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 09018.58208012 .00010596 00000-0 82463-4 0 9026
2 25544 51.6402 352.7528 0008140 280.4070 79.6174 15.70449627 22425
Satellite: ISS
Catalog Number: 25544
Epoch time: 09018.58208012 = yrday.fracday
Element set: 902
Inclination: 51.6402 deg
RA of node: 352.7528 deg
Eccentricity: .0008140
Arg of perigee: 280.4070 deg
Mean anomaly: 79.6174 deg
Mean motion: 15.70449627 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2242
Checksum: 291
Coasting Arc #4 (Orbit 2256)
---------------------------------------
Vector Time (GMT): 2009/019/12:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 639525.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -858073.70 A = 6730283.22 meter
Y = -4099562.39 meter E = .0007378
Z = -5274289.98 I = 51.54855
XDOT = 7514.868812 Wp = 73.99953
YDOT = -1632.662093 meter/sec RA = 347.45571 deg
ZDOT = 48.483893 TA = 196.44975
MA = 196.47371
Ha = 194.185 n.mi
Hp = 192.524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2815202.43 X = -786546.63
Y = -13450007.84 feet Y = -4108757.50 meter
Z = -17304100.98 Z = -5278285.07
XDOT = 24655.081403 XDOT = 7532.331463
YDOT = -5356.502929 feet/sec YDOT = -1548.528836 meter/sec
ZDOT = 159.067889 ZDOT = 85.033082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9325022.02 X = 2842266.71
Y = -10066041.95 feet Y = -3068129.59 meter
Z = -17319894.63 Z = -5279103.88
XDOT = 18024.383283 XDOT = 5493.832025
YDOT = 16190.744961 feet/sec YDOT = 4934.939064 meter/sec
ZDOT = 301.250013 ZDOT = 91.821004
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 09019.53658978 .00010596 00000-0 82463-4 0 9033
2 25544 51.6407 347.8767 0008206 285.3740 74.6514 15.70434464 22573
Satellite: ISS
Catalog Number: 25544
Epoch time: 09019.53658978 = yrday.fracday
Element set: 903
Inclination: 51.6407 deg
RA of node: 347.8767 deg
Eccentricity: .0008206
Arg of perigee: 285.3740 deg
Mean anomaly: 74.6514 deg
Mean motion: 15.70434464 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2257
Checksum: 336
Coasting Arc #5 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2009/020/12:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 639525.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6013259.04 A = 6741769.52 meter
Y = 2833348.16 meter E = .0006120
Z = 1101915.07 I = 51.55944
XDOT = -2952.062691 Wp = 142.18981
YDOT = -3968.588605 meter/sec RA = 342.33170 deg
ZDOT = -5892.782444 TA = 25.75869
MA = 25.72823
Ha = 194.411 n.mi
Hp = 192.345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19728540.16 X = -6049847.93
Y = 9295761.67 feet Y = 2765899.72 meter
Z = 3615206.93 Z = 1072614.37
XDOT = -9685.245048 XDOT = -2878.840112
YDOT = -13020.303823 feet/sec YDOT = -4001.190298 meter/sec
ZDOT = -19333.275736 ZDOT = -5906.945944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19266482.29 X = -5872423.80
Y = -10258639.87 feet Y = -3126833.43 meter
Z = 3501309.95 Z = 1067199.27
XDOT = 3953.754970 XDOT = 1205.104515
YDOT = -14057.313606 feet/sec YDOT = -4284.669187 meter/sec
ZDOT = -19388.645012 ZDOT = -5909.659000
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 09020.55471757 .00010596 00000-0 82463-4 0 9046
2 25544 51.6411 342.6758 0008221 289.4748 70.5525 15.70461968 22735
Satellite: ISS
Catalog Number: 25544
Epoch time: 09020.55471757 = yrday.fracday
Element set: 904
Inclination: 51.6411 deg
RA of node: 342.6758 deg
Eccentricity: .0008221
Arg of perigee: 289.4748 deg
Mean anomaly: 70.5525 deg
Mean motion: 15.70461968 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2273
Checksum: 321
Coasting Arc #6 (Orbit 2288)
---------------------------------------
Vector Time (GMT): 2009/021/12:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 639525.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4051145.45 A = 6732033.17 meter
Y = 2436388.49 meter E = .0001655
Z = 4794511.41 I = 51.50033
XDOT = -5686.645206 Wp = 254.07379
YDOT = 4539.966694 meter/sec RA = 337.24550 deg
ZDOT = 2498.186707 TA = 171.41399
MA = 171.41116
Ha = 194.419 n.mi
Hp = 192.070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13291159.60 X = 4000309.71
Y = 7993400.54 feet Y = 2481405.99 meter
Z = 15730024.30 Z = 4814068.39
XDOT = -18656.972462 XDOT = -5749.124792
YDOT = 14894.903853 feet/sec YDOT = 4476.025721 meter/sec
ZDOT = 8196.150612 ZDOT = 2470.410085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1759885.21 X = 536413.01
Y = 15331231.65 feet Y = 4672959.41 meter
Z = 15806301.91 Z = 4817760.82
XDOT = -22109.800263 XDOT = -6739.067120
YDOT = -5800.014346 feet/sec YDOT = -1767.844373 meter/sec
ZDOT = 8088.283828 ZDOT = 2465.308911
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 09021.57282820 .00010596 00000-0 82463-4 0 9051
2 25544 51.6417 337.4752 0008330 292.4593 67.5686 15.70524395 22895
Satellite: ISS
Catalog Number: 25544
Epoch time: 09021.57282820 = yrday.fracday
Element set: 905
Inclination: 51.6417 deg
RA of node: 337.4752 deg
Eccentricity: .0008330
Arg of perigee: 292.4593 deg
Mean anomaly: 67.5686 deg
Mean motion: 15.70524395 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2289
Checksum: 326
Coasting Arc #7 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2009/022/12:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 639525.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3577146.65 A = 6737872.46 meter
Y = -4746349.46 meter E = .0005605
Z = -3166133.01 I = 51.49259
XDOT = 5878.833905 Wp = 327.60583
YDOT = 1219.799173 meter/sec RA = 332.08209 deg
ZDOT = 4814.122802 TA = 355.46503
MA = 355.47010
Ha = 194.805 n.mi
Hp = 191.868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11736045.44 X = 3645335.48
Y = -15572012.66 feet Y = -4705966.12 meter
Z = -10387575.51 Z = -3148590.43
XDOT = 19287.512812 XDOT = 5841.371253
YDOT = 4001.965792 feet/sec YDOT = 1285.329709 meter/sec
ZDOT = 15794.366148 ZDOT = 4842.590823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19527869.34 X = 5952094.57
Y = -541341.77 feet Y = -165000.97 meter
Z = -10319560.74 Z = -3145402.11
XDOT = 8848.980106 XDOT = 2697.169136
YDOT = 16054.670053 feet/sec YDOT = 4893.463432 meter/sec
ZDOT = 15905.267103 ZDOT = 4847.925413
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 09022.52729564 .00010596 00000-0 82463-4 0 9069
2 25544 51.6414 332.5987 0008337 297.1595 62.8716 15.70498093 23044
Satellite: ISS
Catalog Number: 25544
Epoch time: 09022.52729564 = yrday.fracday
Element set: 906
Inclination: 51.6414 deg
RA of node: 332.5987 deg
Eccentricity: .0008337
Arg of perigee: 297.1595 deg
Mean anomaly: 62.8716 deg
Mean motion: 15.70498093 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2304
Checksum: 333
Coasting Arc #8 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2009/023/12:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 639525.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5772504.40 A = 6736788.66 meter
Y = 477921.44 meter E = .0005050
Z = -3442930.35 I = 51.46520
XDOT = 2241.380255 Wp = 336.21185
YDOT = -5778.148269 meter/sec RA = 327.01198 deg
ZDOT = -4553.168286 TA = 244.57153
MA = 244.62379
Ha = 194.864 n.mi
Hp = 191.419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18938662.73 X = -5760694.80
Y = 1567983.73 feet Y = 413436.34 meter
Z = -11295703.25 Z = -3470943.85
XDOT = 7353.609762 XDOT = 2327.943875
YDOT = -18957.179361 feet/sec YDOT = -5752.599370 meter/sec
ZDOT = -14938.216163 ZDOT = -4542.070246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13265949.59 X = -4043461.44
Y = -13515581.74 feet Y = -4119549.31 meter
Z = -11404738.61 Z = -3476164.33
XDOT = 18350.485300 XDOT = 5593.227919
YDOT = -5423.707944 feet/sec YDOT = -1653.146181 meter/sec
ZDOT = -14895.353929 ZDOT = -4540.103878
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 09023.54537793 .00010596 00000-0 82463-4 0 9074
2 25544 51.6423 327.3973 0008280 301.3322 58.7028 15.70548456 23201
Satellite: ISS
Catalog Number: 25544
Epoch time: 09023.54537793 = yrday.fracday
Element set: 907
Inclination: 51.6423 deg
RA of node: 327.3973 deg
Eccentricity: .0008280
Arg of perigee: 301.3322 deg
Mean anomaly: 58.7028 deg
Mean motion: 15.70548456 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2320
Checksum: 305
Coasting Arc #9 (Orbit 2335)
---------------------------------------
Vector Time (GMT): 2009/024/12:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 639525.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -265970.90 A = 6732770.81 meter
Y = 4894068.93 meter E = .0008313
Z = 4619369.60 I = 51.42762
XDOT = -6728.273038 Wp = 4.33768
YDOT = 2363.073128 meter/sec RA = 321.84236 deg
ZDOT = -2882.497257 TA = 114.34763
MA = 114.26082
Ha = 195.036 n.mi
Hp = 191.316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -872607.95 X = -343116.93
Y = 16056656.60 feet Y = 4890662.90 meter
Z = 15155412.07 Z = 4617890.63
XDOT = -22074.386607 XDOT = -6740.194953
YDOT = 7752.864593 feet/sec YDOT = 2287.767294 meter/sec
ZDOT = -9457.011997 ZDOT = -2915.211128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12798772.11 X = -3901065.74
Y = 9743437.73 feet Y = 2969799.82 meter
Z = 15149951.63 Z = 4617705.26
XDOT = -19526.555942 XDOT = -5951.694251
YDOT = -10703.897237 feet/sec YDOT = -3262.547878 meter/sec
ZDOT = -9584.237032 ZDOT = -2921.275447
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 09024.56344515 .00010596 00000-0 82463-4 0 9086
2 25544 51.6424 322.1965 0008264 304.8880 55.1504 15.70555025 23362
Satellite: ISS
Catalog Number: 25544
Epoch time: 09024.56344515 = yrday.fracday
Element set: 908
Inclination: 51.6424 deg
RA of node: 322.1965 deg
Eccentricity: .0008264
Arg of perigee: 304.8880 deg
Mean anomaly: 55.1504 deg
Mean motion: 15.70555025 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2336
Checksum: 298
Coasting Arc #10 (Orbit 2351)
---------------------------------------
Vector Time (GMT): 2009/025/12:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 639525.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5518481.88 A = 6740935.49 meter
Y = -3554552.54 meter E = .0013173
Z = 1494609.22 I = 51.43314
XDOT = 1559.481147 Wp = 26.38368
YDOT = 4851.428136 meter/sec RA = 316.75374 deg
ZDOT = 5772.061910 TA = 350.11198
MA = 350.13788
Ha = 195.119 n.mi
Hp = 191.068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18105255.50 X = 5550558.99
Y = -11661917.77 feet Y = -3492662.44 meter
Z = 4903573.55 Z = 1521494.89
XDOT = 5116.407964 XDOT = 1477.076916
YDOT = 15916.758977 feet/sec YDOT = 4868.405951 meter/sec
ZDOT = 18937.210991 ZDOT = 5779.437896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20731178.00 X = 6318863.05
Y = 5743126.13 feet Y = 1750504.85 meter
Z = 5008033.29 Z = 1526448.55
XDOT = -8137.449723 XDOT = -2480.294676
YDOT = 12813.464913 feet/sec YDOT = 3905.544106 meter/sec
ZDOT = 18966.231616 ZDOT = 5780.907397
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 09025.58149668 .00010596 00000-0 82463-4 0 9092
2 25544 51.6425 316.9946 0008328 308.9704 51.0715 15.70575315 23525
Satellite: ISS
Catalog Number: 25544
Epoch time: 09025.58149668 = yrday.fracday
Element set: 909
Inclination: 51.6425 deg
RA of node: 316.9946 deg
Eccentricity: .0008328
Arg of perigee: 308.9704 deg
Mean anomaly: 51.0715 deg
Mean motion: 15.70575315 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2352
Checksum: 327
Coasting Arc #11 (Orbit 2366)
---------------------------------------
Vector Time (GMT): 2009/026/12:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 639525.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2789235.47 A = 6729850.05 meter
Y = -3171905.47 meter E = .0009883
Z = -5246477.94 I = 51.37617
XDOT = 5369.525195 Wp = 61.87582
YDOT = -5484.595978 meter/sec RA = 311.60942 deg
ZDOT = 466.467376 TA = 212.54698
MA = 212.60794
Ha = 195.232 n.mi
Hp = 190.724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9151035.02 X = -2728073.70
Y = -10406514.01 feet Y = -3202754.03 meter
Z = -17212854.14 Z = -5259879.29
XDOT = 17616.552476 XDOT = 5428.189831
YDOT = -17994.081294 feet/sec YDOT = -5424.222848 meter/sec
ZDOT = 1530.404776 ZDOT = 492.693942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1515827.91 X = 462024.35
Y = -13708872.54 feet Y = -4178464.35 meter
Z = -17265236.84 Z = -5262444.19
XDOT = 24164.746832 XDOT = 7365.414834
YDOT = 638.011907 feet/sec YDOT = 194.466029 meter/sec
ZDOT = 1632.172090 ZDOT = 497.486053
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 09026.53590543 .00010596 00000-0 82463-4 0 9102
2 25544 51.6431 312.1185 0008312 312.5395 47.5064 15.70613122 23677
Satellite: ISS
Catalog Number: 25544
Epoch time: 09026.53590543 = yrday.fracday
Element set: 910
Inclination: 51.6431 deg
RA of node: 312.1185 deg
Eccentricity: .0008312
Arg of perigee: 312.5395 deg
Mean anomaly: 47.5064 deg
Mean motion: 15.70613122 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2367
Checksum: 279
Coasting Arc #12 (Orbit 2382)
---------------------------------------
Vector Time (GMT): 2009/027/12:30:00.000
Vector Time (MET): N/A
Weight (LBS) : 639525.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3537973.32 A = 6741634.47 meter
Y = 5696142.75 meter E = .0005236
Z = 678613.26 I = 51.39724
XDOT = -4417.394355 Wp = 115.43390
YDOT = -2029.625093 meter/sec RA = 306.47953 deg
ZDOT = -5960.375638 TA = 57.16343
MA = 57.11303
Ha = 195.438 n.mi
Hp = 190.613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11607524.02 X = -3604702.07
Y = 18688132.40 feet Y = 5656205.96 meter
Z = 2226421.45 Z = 661264.40
XDOT = -14492.763632 XDOT = -4365.416841
YDOT = -6658.874978 feet/sec YDOT = -2078.732121 meter/sec
ZDOT = -19555.038182 ZDOT = -5981.708554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21542271.63 X = -6566084.39
Y = 4495115.27 feet Y = 1370111.13 meter
Z = 2159243.02 Z = 658137.27
XDOT = -4782.039479 XDOT = -1457.565633
YDOT = -13429.435898 feet/sec YDOT = -4093.292062 meter/sec
ZDOT = -19638.235421 ZDOT = -5985.734156
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 09027.55392739 .00010596 00000-0 82463-4 0 9113
2 25544 51.6431 306.9170 0008274 315.9930 44.0572 15.70615406 23832
Satellite: ISS
Catalog Number: 25544
Epoch time: 09027.55392739 = yrday.fracday
Element set: 911
Inclination: 51.6431 deg
RA of node: 306.9170 deg
Eccentricity: .0008274
Arg of perigee: 315.9930 deg
Mean anomaly: 44.0572 deg
Mean motion: 15.70615406 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2383
Checksum: 305
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