Date:
April 10th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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 3499)
---------------------------------------
Vector Time (GMT): 2009/098/13:34:46
084
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4157292
47 A = 6737485
44 meter
Y = 5232170
79 meter E =
0015536
Z = -773338
58 I = 51
37961
XDOT = -3362
729842 Wp = 174
80642
YDOT = -3548
212933 meter/sec RA = 303
16496 deg
ZDOT = -5953
383761 TA = 13
65442
MA = 13
61244
Ha = 193
764 n
mi
Hp = 187
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13639410
98 X = -4211733
73
Y = 17165914
66 feet Y = 5185377
06 meter
Z = -2537200
05 Z = -793667
52
XDOT = -11032
578222 XDOT = -3293
882533
YDOT = -11641
118548 feet/sec YDOT = -3585
432498 meter/sec
ZDOT = -19532
098954 ZDOT = -5969
552486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 549013
84 X = 167339
42
Y = 21908755
24 feet Y = 6677788
60 meter
Z = -2616212
87 Z = -797421
68
XDOT = -14245
837101 XDOT = -4342
131148
YDOT = -1973
663072 feet/sec YDOT = -601
572504 meter/sec
ZDOT = -19595
472069 ZDOT = -5972
699887
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 09098
59607907
00010596 00000-0 82463-4 0 9009
2 25544 51
6376 303
6172 0009096 215
2519 144
8042 15
72041062 35000
Satellite: ISS
Catalog Number: 25544
Epoch time: 09098
59607907 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 303
6172 deg
Eccentricity:
0009096
Arg of perigee: 215
2519 deg
Mean anomaly: 144
8042 deg
Mean motion: 15
72041062 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3500
Checksum: 299
Coasting Arc #2 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2009/099/13:34:46
084
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3630285
94 A = 6725860
50 meter
Y = 2124955
63 meter E =
0007614
Z = 5250697
08 I = 51
32395
XDOT = -3724
286679 Wp = 204
59881
YDOT = 6733
021991 meter/sec RA = 298
01385 deg
ZDOT = -156
818586 TA = 246
85670
MA = 246
93694
Ha = 193
741 n
mi
Hp = 188
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11910386
96 X = 3580747
28
Y = 6971639
22 feet Y = 2165274
99 meter
Z = 17226696
45 Z = 5268212
73
XDOT = -12218
788318 XDOT = -3798
537855
YDOT = 22089
967162 feet/sec YDOT = 6690
959673 meter/sec
ZDOT = -514
496674 ZDOT = -175
092211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13493488
45 X = 4112815
28
Y = -2453762
89 feet Y = -747906
93 meter
Z = 17295229
36 Z = 5271585
91
XDOT = 5033
818522 XDOT = 1534
307885
YDOT = 23714
515257 feet/sec YDOT = 7228
184250 meter/sec
ZDOT = -585
379249 ZDOT = -178
423595
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 09099
61319201
00010596 00000-0 82463-4 0 9011
2 25544 51
6367 298
4078 0009171 217
7582 142
2937 15
71983744 35160
Satellite: ISS
Catalog Number: 25544
Epoch time: 09099
61319201 = yrday
fracday
Element set: 901
Inclination: 51
6367 deg
RA of node: 298
4078 deg
Eccentricity:
0009171
Arg of perigee: 217
7582 deg
Mean anomaly: 142
2937 deg
Mean motion: 15
71983744 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3516
Checksum: 331
Coasting Arc #3 (Orbit 3530)
---------------------------------------
Vector Time (GMT): 2009/100/13:34:46
084
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2250219
46 A = 6737598
91 meter
Y = -6331314
27 meter E =
0001947
Z = -483917
76 I = 51
35188
XDOT = 4682
546077 Wp = 41
80917
YDOT = 1208
137473 meter/sec RA = 292
86734 deg
ZDOT = 5982
515329 TA = 312
91352
MA = 312
92986
Ha = 193
574 n
mi
Hp = 188
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7382609
77 X = 2323200
85
Y = -20772028
45 feet Y = -6305742
97 meter
Z = -1587656
69 Z = -472808
45
XDOT = 15362
683981 XDOT = 4639
626058
YDOT = 3963
705621 feet/sec YDOT = 1260
260753 meter/sec
ZDOT = 19627
674965 ZDOT = 6005
159154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8351178
01 X = -2545439
06
Y = -20405205
70 feet Y = -6219506
70 meter
Z = -1544717
76 Z = -470829
97
XDOT = 12516
044466 XDOT = 3814
890353
YDOT = -6611
063593 feet/sec YDOT = -2015
052183 meter/sec
ZDOT = 19716
165967 ZDOT = 6009
487387
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 09100
56671842
00010596 00000-0 82463-4 0 9021
2 25544 51
6372 293
5239 0009272 221
3463 138
6998 15
72060148 35310
Satellite: ISS
Catalog Number: 25544
Epoch time: 09100
56671842 = yrday
fracday
Element set: 902
Inclination: 51
6372 deg
RA of node: 293
5239 deg
Eccentricity:
0009272
Arg of perigee: 221
3463 deg
Mean anomaly: 138
6998 deg
Mean motion: 15
72060148 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3531
Checksum: 311
Coasting Arc #4 (Orbit 3546)
---------------------------------------
Vector Time (GMT): 2009/101/13:34:46
084
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4344430
11 A = 6726039
98 meter
Y = 66715
77 meter E =
0008679
Z = -5140143
76 I = 51
30343
XDOT = 1346
708556 Wp = 118
28548
YDOT = -7471
977450 meter/sec RA = 287
73975 deg
ZDOT = -1240
858982 TA = 139
81966
MA = 139
75546
Ha = 193
236 n
mi
Hp = 188
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14253379
63 X = -4319882
97
Y = 218883
76 feet Y = 18270
94 meter
Z = -16863988
70 Z = -5161189
70
XDOT = 4418
335157 XDOT = 1436
189330
YDOT = -24514
361713 feet/sec YDOT = -7456
417488 meter/sec
ZDOT = -4071
059653 ZDOT = -1234
099027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10232453
08 X = -3118851
70
Y = 9783946
09 feet Y = 2982146
77 meter
Z = -16946154
69 Z = -5165187
95
XDOT = -12695
000243 XDOT = -3869
436074
YDOT = -20251
431818 feet/sec YDOT = -6172
636418 meter/sec
ZDOT = -4045
178621 ZDOT = -1232
970444
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 09101
58380068
00010596 00000-0 82463-4 0 9032
2 25544 51
6376 288
3158 0009113 224
8829 135
1597 15
72092718 35476
Satellite: ISS
Catalog Number: 25544
Epoch time: 09101
58380068 = yrday
fracday
Element set: 903
Inclination: 51
6376 deg
RA of node: 288
3158 deg
Eccentricity:
0009113
Arg of perigee: 224
8829 deg
Mean anomaly: 135
1597 deg
Mean motion: 15
72092718 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3547
Checksum: 328
Coasting Arc #5 (Orbit 3562)
---------------------------------------
Vector Time (GMT): 2009/102/13:34:46
084
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -79663
79 A = 6736357
80 meter
Y = 6515237
67 meter E =
0013343
Z = 1674388
21 I = 51
32993
XDOT = -4986
719838 Wp = 155
05058
YDOT = 1405
013318 meter/sec RA = 282
56848 deg
ZDOT = -5699
757999 TA = 6
36024
MA = 6
34332
Ha = 193
055 n
mi
Hp = 188
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -261364
14 X = -160646
34
Y = 21375451
67 feet Y = 6513894
03 meter
Z = 5493399
63 Z = 1673804
47
XDOT = -16360
629389 XDOT = -4974
371513
YDOT = 4609
623747 feet/sec YDOT = 1349
317936 meter/sec
ZDOT = -18699
993435 ZDOT = -5723
953840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14587933
05 X = 4446401
99
Y = 15626598
84 feet Y = 4762987
33 meter
Z = 5491566
50 Z = 1673829
47
XDOT = -7396
006078 XDOT = -2254
302653
YDOT = 13514
476578 feet/sec YDOT = 4119
212461 meter/sec
ZDOT = -18794
369144 ZDOT = -5728
523715
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 09102
60086699
00010596 00000-0 82463-4 0 9040
2 25544 51
6371 283
1060 0009226 230
0632 129
9720 15
72106303 35635
Satellite: ISS
Catalog Number: 25544
Epoch time: 09102
60086699 = yrday
fracday
Element set: 904
Inclination: 51
6371 deg
RA of node: 283
1060 deg
Eccentricity:
0009226
Arg of perigee: 230
0632 deg
Mean anomaly: 129
9720 deg
Mean motion: 15
72106303 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3563
Checksum: 285
Coasting Arc #6 (Orbit 3578)
---------------------------------------
Vector Time (GMT): 2009/103/13:34:46
084
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4147790
56 A = 6727572
73 meter
Y = -2348473
56 meter E =
0009177
Z = 4752300
51 I = 51
29636
XDOT = 1124
501329 Wp = 186
49921
YDOT = 7169
949419 meter/sec RA = 277
45930 deg
ZDOT = 2553
246225 TA = 238
28919
MA = 238
37869
Ha = 192
833 n
mi
Hp = 188
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13608236
73 X = 4150657
22
Y = -7704965
74 feet Y = -2302074
59 meter
Z = 15591537
09 Z = 4772457
64
XDOT = 3689
308821 XDOT = 1031
838821
YDOT = 23523
456098 feet/sec YDOT = 7182
006106 meter/sec
ZDOT = 8376
792077 ZDOT = 2558
484146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4162141
78 X = 1268620
81
Y = -14992388
45 feet Y = -4569680
00 meter
Z = 15670082
87 Z = 4776241
26
XDOT = 18066
236165 XDOT = 5506
588783
YDOT = 13821
869000 feet/sec YDOT = 4212
905671 meter/sec
ZDOT = 8397
736179 ZDOT = 2559
629987
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 09103
61791899
00010596 00000-0 82463-4 0 9058
2 25544 51
6379 277
8970 0009253 233
7843 126
2464 15
72144489 35796
Satellite: ISS
Catalog Number: 25544
Epoch time: 09103
61791899 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 277
8970 deg
Eccentricity:
0009253
Arg of perigee: 233
7843 deg
Mean anomaly: 126
2464 deg
Mean motion: 15
72144489 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3579
Checksum: 354
Coasting Arc #7 (Orbit 3593)
---------------------------------------
Vector Time (GMT): 2009/104/13:34:46
084
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1974349
87 A = 6734138
97 meter
Y = -5820581
64 meter E =
0004372
Z = -2752071
58 I = 51
31713
XDOT = 4252
273842 Wp = 234
79471
YDOT = -3864
947992 meter/sec RA = 272
27129 deg
ZDOT = 5115
478088 TA = 93
63709
MA = 93
58709
Ha = 192
671 n
mi
Hp = 188
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6477525
83 X = -1895747
23
Y = -19096396
47 feet Y = -5842220
42 meter
Z = -9029106
22 Z = -2761472
27
XDOT = 13951
029665 XDOT = 4270
326015
YDOT = -12680
275563 feet/sec YDOT = -3817
295779 meter/sec
ZDOT = 16783
064594 ZDOT = 5136
179566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18168079
99 X = -5537630
78
Y = -8710915
21 feet Y = -2655086
96 meter
Z = -9066216
63 Z = -2763382
83
XDOT = -63
471753 XDOT = -19
346190
YDOT = -17447
024551 feet/sec YDOT = -5317
853083 meter/sec
ZDOT = 16863
635191 ZDOT = 5140
036006
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 09104
57139231
00010596 00000-0 82463-4 0 9061
2 25544 51
6391 273
0142 0009123 236
9965 123
0320 15
72147917 35947
Satellite: ISS
Catalog Number: 25544
Epoch time: 09104
57139231 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 273
0142 deg
Eccentricity:
0009123
Arg of perigee: 236
9965 deg
Mean anomaly: 123
0320 deg
Mean motion: 15
72147917 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3594
Checksum: 298
Coasting Arc #8 (Orbit 3609)
---------------------------------------
Vector Time (GMT): 2009/105/13:34:46
084
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3109804
87 A = 6729879
00 meter
Y = 4295785
85 meter E =
0001723
Z = -4141679
90 I = 51
30310
XDOT = -3254
739841 Wp = 199
11550
YDOT = -5916
596120 meter/sec RA = 267
17503 deg
ZDOT = -3694
074929 TA = 32
94315
MA = 32
93241
Ha = 192
311 n
mi
Hp = 189
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10202771
87 X = -3137490
29
Y = 14093785
60 feet Y = 4260855
51 meter
Z = -13588188
65 Z = -4156854
55
XDOT = -10678
280318 XDOT = -3170
392325
YDOT = -19411
404593 feet/sec YDOT = -5952
520811 meter/sec
ZDOT = -12119
668402 ZDOT = -3709
681814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3335648
21 X = 1016705
58
Y = 17029356
89 feet Y = 5190547
98 meter
Z = -13647148
87 Z = -4159650
98
XDOT = -20167
713072 XDOT = -6147
118944
YDOT = -5808
304252 feet/sec YDOT = -1770
371136 meter/sec
ZDOT = -12181
028274 ZDOT = -3712
777418
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 09105
58841471
00010596 00000-0 82463-4 0 9070
2 25544 51
6391 267
8059 0009125 241
7309 118
2932 15
72169280 36104
Satellite: ISS
Catalog Number: 25544
Epoch time: 09105
58841471 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 267
8059 deg
Eccentricity:
0009125
Arg of perigee: 241
7309 deg
Mean anomaly: 118
2932 deg
Mean motion: 15
72169280 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3610
Checksum: 314
Coasting Arc #9 (Orbit 3625)
---------------------------------------
Vector Time (GMT): 2009/106/13:34:46
084
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3579934
25 A = 6731479
04 meter
Y = 4360303
36 meter E =
0004412
Z = 3666752
62 I = 51
31127
XDOT = -2661
238301 Wp = 127
45461
YDOT = 5803
290435 meter/sec RA = 261
97837 deg
ZDOT = -4301
834973 TA = 8
26541
MA = 8
25814
Ha = 192
127 n
mi
Hp = 189
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11745191
11 X = 3513098
07
Y = 14305457
23 feet Y = 4399962
50 meter
Z = 12030028
27 Z = 3683981
73
XDOT = -8731
096789 XDOT = -2705
036283
YDOT = 19039
666780 feet/sec YDOT = 5773
286113 meter/sec
ZDOT = -14113
631801 ZDOT = -4314
869576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18439561
41 X = 5620378
32
Y = 973281
73 feet Y = 296656
27 meter
Z = 12097623
68 Z = 3687355
70
XDOT = 8351
980056 XDOT = 2545
683521
YDOT = 17857
917217 feet/sec YDOT = 5443
093168 meter/sec
ZDOT = -14164
127537 ZDOT = -4317
226073
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 09106
60542258
00010596 00000-0 82463-4 0 9086
2 25544 51
6391 262
5969 0009100 245
2471 114
7745 15
72172411 36268
Satellite: ISS
Catalog Number: 25544
Epoch time: 09106
60542258 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node: 262
5969 deg
Eccentricity:
0009100
Arg of perigee: 245
2471 deg
Mean anomaly: 114
7745 deg
Mean motion: 15
72172411 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3626
Checksum: 304
Coasting Arc #10 (Orbit 3641)
---------------------------------------
Vector Time (GMT): 2009/107/13:34:46
084
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1427164
52 A = 6732289
55 meter
Y = -5666842
78 meter E =
0005071
Z = 3342461
93 I = 51
32101
XDOT = 4723
844688 Wp = 127
32177
YDOT = 3927
363357 meter/sec RA = 256
88474 deg
ZDOT = 4633
649469 TA = 272
17169
MA = 272
22976
Ha = 191
876 n
mi
Hp = 189
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4682298
29 X = 1474188
94
Y = -18592003
86 feet Y = -5650620
49 meter
Z = 10966082
45 Z = 3349509
28
XDOT = 15498
178110 XDOT = 4657
067709
YDOT = 12885
050384 feet/sec YDOT = 3979
814736 meter/sec
ZDOT = 15202
262037 ZDOT = 4656
435761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10931351
87 X = -3331876
05
Y = -15732024
21 feet Y = -4795120
98 meter
Z = 10993200
16 Z = 3350727
41
XDOT = 18701
188486 XDOT = 5700
122251
YDOT = -2291
107024 feet/sec YDOT = -698
329421 meter/sec
ZDOT = 15291
540540 ZDOT = 4660
861557
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 09107
62241216
00010596 00000-0 82463-4 0 9090
2 25544 51
6401 257
3878 0009160 249
7393 110
2785 15
72251350 36422
Satellite: ISS
Catalog Number: 25544
Epoch time: 09107
62241216 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 257
3878 deg
Eccentricity:
0009160
Arg of perigee: 249
7393 deg
Mean anomaly: 110
2785 deg
Mean motion: 15
72251350 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3642
Checksum: 302
Coasting Arc #11 (Orbit 3656)
---------------------------------------
Vector Time (GMT): 2009/108/13:34:46
084
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4497923
93 A = 6728748
85 meter
Y = -2418942
04 meter E =
0005754
Z = -4384268
64 I = 51
31685
XDOT = 496
787445 Wp = 180
45422
YDOT = -6929
195450 meter/sec RA = 251
69120 deg
ZDOT = 3307
691740 TA = 122
98914
MA = 122
93383
Ha = 191
588 n
mi
Hp = 189
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14756968
27 X = -4449242
62
Y = -7936161
55 feet Y = -2468968
29 meter
Z = -14384083
46 Z = -4406001
30
XDOT = 1629
880069 XDOT = 558
165770
YDOT = -22733
580874 feet/sec YDOT = -6923
296880 meter/sec
ZDOT = 10852
007022 ZDOT = 3310
254264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15540214
43 X = -4736657
36
Y = 6066148
73 feet Y = 1848962
13 meter
Z = -14469146
65 Z = -4410195
90
XDOT = -15890
648287 XDOT = -4843
469598
YDOT = -14757
007711 feet/sec YDOT = -4497
935950 meter/sec
ZDOT = 10861
509305 ZDOT = 3310
588036
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 09108
57582886
00010596 00000-0 82463-4 0 9108
2 25544 51
6399 252
5052 0009105 254
3727 105
6431 15
72241550 36574
Satellite: ISS
Catalog Number: 25544
Epoch time: 09108
57582886 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 252
5052 deg
Eccentricity:
0009105
Arg of perigee: 254
3727 deg
Mean anomaly: 105
6431 deg
Mean motion: 15
72241550 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3657
Checksum: 312
Coasting Arc #12 (Orbit 3672)
---------------------------------------
Vector Time (GMT): 2009/109/13:34:46
084
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 600833
83 A = 6734584
71 meter
Y = 6252221
25 meter E =
0007382
Z = -2416251
61 I = 51
34743
XDOT = -5325
178469 Wp = 220
88574
YDOT = -1552
938833 meter/sec RA = 246
59173 deg
ZDOT = -5338
820098 TA = 346
48520
MA = 346
50496
Ha = 191
319 n
mi
Hp = 190
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1971239
62 X = 542613
53
Y = 20512536
90 feet Y = 6258614
55 meter
Z = -7927334
69 Z = -2413474
31
XDOT = -17471
057969 XDOT = -5281
482400
YDOT = -5094
943679 feet/sec YDOT = -1612
243880 meter/sec
ZDOT = -17515
813969 ZDOT = -5364
583685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17154155
20 X = 5228586
50
Y = 11426467
64 feet Y = 3482787
34 meter
Z = -7916020
96 Z = -2412803
19
XDOT = -14108
165182 XDOT = -4300
168747
YDOT = 8967
286788 feet/sec YDOT = 2733
229013 meter/sec
ZDOT = -17616
565355 ZDOT = -5369
529120
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 09109
59279034
00010596 00000-0 82463-4 0 9110
2 25544 51
6402 247
2958 0009044 258
4338 101
5809 15
72267270 36739
Satellite: ISS
Catalog Number: 25544
Epoch time: 09109
59279034 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 247
2958 deg
Eccentricity:
0009044
Arg of perigee: 258
4338 deg
Mean anomaly: 101
5809 deg
Mean motion: 15
72267270 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3673
Checksum: 319
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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