Date:
December 4th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14692 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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 978)
---------------------------------------
Vector Time (GMT): 2010/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3473902
26 A = 6726295
74 meter
Y = 3343283
53 meter E =
0003073
Z = -4693101
04 I = 51
97408
XDOT = -2611
919184 Wp = 112
14880
YDOT = 6668
192004 meter/sec RA = 93
47338 deg
ZDOT = 2817
250647 TA = 185
54212
MA = 185
54552
Ha = 190
873 n
mi
Hp = 188
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11397317
12 X = 3459057
56
Y = 10968777
97 feet Y = 3382048
03 meter
Z = -15397313
12 Z = -4676260
36
XDOT = -8569
288661 XDOT = -2699
976005
YDOT = 21877
270353 feet/sec YDOT = 6638
491454 meter/sec
ZDOT = 9242
948317 ZDOT = 2804
348126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14302322
41 X = -4359347
87
Y = 6909072
60 feet Y = 2105885
33 meter
Z = -15329659
76 Z = -4672480
30
XDOT = -16956
052313 XDOT = -5168
204745
YDOT = -14710
125325 feet/sec YDOT = -4483
646199 meter/sec
ZDOT = 9190
951011 ZDOT = 2801
401868
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 10335
51100436
00016717 00000-0 10270-3 0 9009
2 25544 51
6454 94
2369 0007884 288
2786 71
7518 15
72736225 9792
Satellite: ISS
Catalog Number: 25544
Epoch time: 10335
51100436 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 94
2369 deg
Eccentricity:
0007884
Arg of perigee: 288
2786 deg
Mean anomaly: 71
7518 deg
Mean motion: 15
72736225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 979
Checksum: 325
Coasting Arc #2 (Orbit 994)
---------------------------------------
Vector Time (GMT): 2010/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1472926
24 A = 6733749
70 meter
Y = -6222148
29 meter E =
0003539
Z = -2105374
08 I = 52
00086
XDOT = 4431
567574 Wp = 238
83984
YDOT = 2934
128461 meter/sec RA = 88
41147 deg
ZDOT = -5566
030761 TA = 324
54350
MA = 324
56702
Ha = 190
922 n
mi
Hp = 188
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4832435
16 X = 1552621
75
Y = -20413872
34 feet Y = -6205231
38 meter
Z = -6907395
28 Z = -2098025
33
XDOT = 14539
263694 XDOT = 4425
467631
YDOT = 9626
405713 feet/sec YDOT = 2983
651230 meter/sec
ZDOT = -18261
255776 ZDOT = -5544
516300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17604814
03 X = 5365947
31
Y = 11426206
53 feet Y = 3482707
75 meter
Z = -6877721
30 Z = -2096329
45
XDOT = -13140
622400 XDOT = -4005
261708
YDOT = 9296
392921 feet/sec YDOT = 2833
540562 meter/sec
ZDOT = -18174
806208 ZDOT = -5539
680932
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 10336
52764540
00016717 00000-0 10270-3 0 9014
2 25544 51
6459 89
0257 0007868 292
8487 67
1844 15
72777151 9958
Satellite: ISS
Catalog Number: 25544
Epoch time: 10336
52764540 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 89
0257 deg
Eccentricity:
0007868
Arg of perigee: 292
8487 deg
Mean anomaly: 67
1844 deg
Mean motion: 15
72777151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 995
Checksum: 346
Coasting Arc #3 (Orbit 1010)
---------------------------------------
Vector Time (GMT): 2010/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4145537
61 A = 6724795
00 meter
Y = -1747579
77 meter E =
0007307
Z = 5002189
33 I = 51
96993
XDOT = 700
940199 Wp = 343
56845
YDOT = -7398
672196 meter/sec RA = 83
27506 deg
ZDOT = -1997
778401 TA = 125
70829
MA = 125
64029
Ha = 191
170 n
mi
Hp = 188
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13600845
18 X = -4149988
03
Y = -5733529
41 feet Y = -1793963
05 meter
Z = 16411382
31 Z = 4982038
85
XDOT = 2299
672570 XDOT = 793
326505
YDOT = -24273
858910 feet/sec YDOT = -7390
317098 meter/sec
ZDOT = -6554
391078 ZDOT = -1994
149496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9797308
99 X = 2986219
78
Y = -11158888
72 feet Y = -3401229
28 meter
Z = 16330393
67 Z = 4977503
99
XDOT = 21451
343029 XDOT = 6538
369355
YDOT = 9233
884637 feet/sec YDOT = 2814
488037 meter/sec
ZDOT = -6539
632241 ZDOT = -1993
279907
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 10337
54425843
00016717 00000-0 10270-3 0 9028
2 25544 51
6468 83
8151 0007873 298
1528 61
8839 15
72815655 10111
Satellite: ISS
Catalog Number: 25544
Epoch time: 10337
54425843 = yrday
fracday
Element set: 902
Inclination: 51
6468 deg
RA of node: 83
8151 deg
Eccentricity:
0007873
Arg of perigee: 298
1528 deg
Mean anomaly: 61
8839 deg
Mean motion: 15
72815655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1011
Checksum: 323
Coasting Arc #4 (Orbit 1026)
---------------------------------------
Vector Time (GMT): 2010/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 264489
98 A = 6734598
39 meter
Y = 6575985
14 meter E =
0012427
Z = 1389498
84 I = 51
99925
XDOT = -4892
732275 Wp = 26
25189
YDOT = -1042
684121 meter/sec RA = 78
20210 deg
ZDOT = 5857
092710 TA = 348
94575
MA = 348
97303
Ha = 191
321 n
mi
Hp = 187
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 867749
29 X = 184186
36
Y = 21574754
41 feet Y = 6578493
66 meter
Z = 4558723
24 Z = 1390589
52
XDOT = -16052
271243 XDOT = -4909
162420
YDOT = -3420
879662 feet/sec YDOT = -1097
490190 meter/sec
ZDOT = 19216
183432 ZDOT = 5833
283288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20820494
66 X = -6346086
77
Y = -5717648
08 feet Y = -1742739
13 meter
Z = 4562946
07 Z = 1390785
96
XDOT = 7728
050503 XDOT = 2355
509793
YDOT = -12859
041405 feet/sec YDOT = -3919
435820 meter/sec
ZDOT = 19120
462081 ZDOT = 5827
916842
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 10338
56084272
00016717 00000-0 10270-3 0 9039
2 25544 51
6474 78
6042 0007896 302
6448 57
3952 15
72856366 10273
Satellite: ISS
Catalog Number: 25544
Epoch time: 10338
56084272 = yrday
fracday
Element set: 903
Inclination: 51
6474 deg
RA of node: 78
6042 deg
Eccentricity:
0007896
Arg of perigee: 302
6448 deg
Mean anomaly: 57
3952 deg
Mean motion: 15
72856366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1027
Checksum: 326
Coasting Arc #5 (Orbit 1041)
---------------------------------------
Vector Time (GMT): 2010/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4273874
43 A = 6723645
90 meter
Y = 77989
32 meter E =
0008140
Z = -5196112
90 I = 51
95580
XDOT = 1305
193210 Wp = 72
10912
YDOT = 7488
647823 meter/sec RA = 73
07731 deg
ZDOT = 1189
896344 TA = 209
19303
MA = 209
23856
Ha = 191
490 n
mi
Hp = 187
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14021897
75 X = 4297926
88
Y = 255870
47 feet Y = 125917
56 meter
Z = -17047614
49 Z = -5175291
64
XDOT = 4282
129954 XDOT = 1215
576353
YDOT = 24569
054538 feet/sec YDOT = 7502
742038 meter/sec
ZDOT = 3903
859397 ZDOT = 1196
020439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4279698
37 X = -1304452
06
Y = 13461471
09 feet Y = 4103056
39 meter
Z = -16963879
99 Z = -5170590
62
XDOT = -23780
226711 XDOT = -7248
213102
YDOT = -2626
355456 feet/sec YDOT = -800
513143 meter/sec
ZDOT = 3928
287371 ZDOT = 1197
341991
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 10339
51386490
00016717 00000-0 10270-3 0 9043
2 25544 51
6476 73
7202 0007955 306
8266 53
2167 15
72920456 10421
Satellite: ISS
Catalog Number: 25544
Epoch time: 10339
51386490 = yrday
fracday
Element set: 904
Inclination: 51
6476 deg
RA of node: 73
7202 deg
Eccentricity:
0007955
Arg of perigee: 306
8266 deg
Mean anomaly: 53
2167 deg
Mean motion: 15
72920456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1042
Checksum: 308
Coasting Arc #6 (Orbit 1057)
---------------------------------------
Vector Time (GMT): 2010/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1987323
53 A = 6734976
81 meter
Y = -6393973
38 meter E =
0003077
Z = -708273
03 I = 51
98372
XDOT = 4739
477937 Wp = 165
82888
YDOT = -808
448338 meter/sec RA = 67
99075 deg
ZDOT = -6008
431767 TA = 21
84429
MA = 21
83117
Ha = 191
540 n
mi
Hp = 187
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6520090
31 X = -1912236
52
Y = -20977602
94 feet Y = -6415776
89 meter
Z = -2323730
41 Z = -717746
10
XDOT = 15549
468297 XDOT = 4777
354095
YDOT = -2652
389559 feet/sec YDOT = -755
235988 meter/sec
ZDOT = -19712
702646 ZDOT = -5985
315244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21954736
82 X = 6691803
78
Y = -619090
66 feet Y = -188698
83 meter
Z = -2361648
53 Z = -719830
47
XDOT = -1707
103505 XDOT = -520
325148
YDOT = 14201
466957 feet/sec YDOT = 4328
607128 meter/sec
ZDOT = -19619
705086 ZDOT = -5980
086110
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 10340
53039559
00016717 00000-0 10270-3 0 9059
2 25544 51
6472 68
5093 0007938 310
6653 49
3819 15
72936194 10584
Satellite: ISS
Catalog Number: 25544
Epoch time: 10340
53039559 = yrday
fracday
Element set: 905
Inclination: 51
6472 deg
RA of node: 68
5093 deg
Eccentricity:
0007938
Arg of perigee: 310
6653 deg
Mean anomaly: 49
3819 deg
Mean motion: 15
72936194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1058
Checksum: 327
Coasting Arc #7 (Orbit 1073)
---------------------------------------
Vector Time (GMT): 2010/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3904323
40 A = 6722958
55 meter
Y = 1449687
63 meter E =
0007370
Z = 5280762
67 I = 51
93217
XDOT = -3195
243582 Wp = 333
84377
YDOT = -6988
873731 meter/sec RA = 62
87468 deg
ZDOT = -437
557463 TA = 120
33344
MA = 120
26052
Ha = 191
718 n
mi
Hp = 186
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12809459
96 X = -3945897
03
Y = 4756193
02 feet Y = 1405793
93 meter
Z = 17325336
84 Z = 5261694
58
XDOT = -10483
082617 XDOT = -3114
729625
YDOT = -22929
375757 feet/sec YDOT = -7024
154626 meter/sec
ZDOT = -1435
555980 ZDOT = -452
885489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1341253
15 X = -408813
96
Y = -13695177
40 feet Y = -4174290
07 meter
Z = 17248596
73 Z = 5257372
28
XDOT = 23832
914980 XDOT = 7264
272486
YDOT = -4245
417043 feet/sec YDOT = -1294
003115 meter/sec
ZDOT = -1497
001076 ZDOT = -456
285928
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 10341
54689642
00016717 00000-0 10270-3 0 9066
2 25544 51
6478 63
2975 0008089 314
9867 45
0639 15
73020446 10749
Satellite: ISS
Catalog Number: 25544
Epoch time: 10341
54689642 = yrday
fracday
Element set: 906
Inclination: 51
6478 deg
RA of node: 63
2975 deg
Eccentricity:
0008089
Arg of perigee: 314
9867 deg
Mean anomaly: 45
0639 deg
Mean motion: 15
73020446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1074
Checksum: 329
Coasting Arc #8 (Orbit 1089)
---------------------------------------
Vector Time (GMT): 2010/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3544560
88 A = 6735034
32 meter
Y = 5714654
02 meter E =
0015366
Z = 62515
19 I = 51
95726
XDOT = -4066
152059 Wp = 13
93571
YDOT = 2452
500459 meter/sec RA = 57
77361 deg
ZDOT = 6067
299790 TA = 346
74061
MA = 346
78095
Ha = 191
954 n
mi
Hp = 186
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11629136
75 X = 3480091
42
Y = 18748864
88 feet Y = 5753930
95 meter
Z = 205102
34 Z = 79578
87
XDOT = -13340
393895 XDOT = -4122
748071
YDOT = 8046
261350 feet/sec YDOT = 2406
713046 meter/sec
ZDOT = 19905
839207 ZDOT = 6047
409237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20962700
55 X = -6389431
13
Y = 6876712
20 feet Y = 2096021
88 meter
Z = 273565
29 Z = 83382
70
XDOT = -4143
617561 XDOT = -1262
974633
YDOT = -13448
478481 feet/sec YDOT = -4099
096241 meter/sec
ZDOT = 19825
754313 ZDOT = 6042
889915
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 10342
56337336
00016717 00000-0 10270-3 0 9070
2 25544 51
6474 58
0864 0008153 320
7249 39
3322 15
72998214 10904
Satellite: ISS
Catalog Number: 25544
Epoch time: 10342
56337336 = yrday
fracday
Element set: 907
Inclination: 51
6474 deg
RA of node: 58
0864 deg
Eccentricity:
0008153
Arg of perigee: 320
7249 deg
Mean anomaly: 39
3322 deg
Mean motion: 15
72998214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1090
Checksum: 308
Coasting Arc #9 (Orbit 1104)
---------------------------------------
Vector Time (GMT): 2010/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3113498
07 A = 6722831
00 meter
Y = -2758412
52 meter E =
0012416
Z = -5290405
53 I = 51
89842
XDOT = 4828
655709 Wp = 54
88249
YDOT = 5981
436561 meter/sec RA = 52
66770 deg
ZDOT = -270
427712 TA = 212
51858
MA = 212
59512
Ha = 192
024 n
mi
Hp = 186
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10214888
67 X = 3169811
57
Y = -9049909
85 feet Y = -2723280
03 meter
Z = -17356973
51 Z = -5275143
69
XDOT = 15842
046291 XDOT = 4762
724979
YDOT = 19624
135699 feet/sec YDOT = 6035
064888 meter/sec
ZDOT = -887
230025 ZDOT = -247
129557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6569424
09 X = 2002360
46
Y = 12050638
86 feet Y = 3673034
72 meter
Z = -17295494
17 Z = -5271666
62
XDOT = -21741
175707 XDOT = -6626
710355
YDOT = 10682
198842 feet/sec YDOT = 3255
934207 meter/sec
ZDOT = -793
697545 ZDOT = -241
919012
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 10343
51629208
00016717 00000-0 10270-3 0 9089
2 25544 51
6464 53
2007 0008173 323
8804 36
1806 15
73048723 11053
Satellite: ISS
Catalog Number: 25544
Epoch time: 10343
51629208 = yrday
fracday
Element set: 908
Inclination: 51
6464 deg
RA of node: 53
2007 deg
Eccentricity:
0008173
Arg of perigee: 323
8804 deg
Mean anomaly: 36
1806 deg
Mean motion: 15
73048723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1105
Checksum: 286
Coasting Arc #10 (Orbit 1120)
---------------------------------------
Vector Time (GMT): 2010/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4819564
40 A = 6734570
40 meter
Y = -4673986
98 meter E =
0006028
Z = 512592
89 I = 51
91927
XDOT = 2980
080104 Wp = 102
89826
YDOT = -3740
341425 meter/sec RA = 47
55121 deg
ZDOT = -6028
170009 TA = 71
55172
MA = 71
48620
Ha = 192
093 n
mi
Hp = 186
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15812219
16 X = -4769430
88
Y = -15334602
95 feet Y = -4727601
99 meter
Z = 1681735
20 Z = 489300
79
XDOT = 9777
165696 XDOT = 3050
967541
YDOT = -12271
461369 feet/sec YDOT = -3706
619436 meter/sec
ZDOT = -19777
460661 ZDOT = -6013
520972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18218666
20 X = 5553049
46
Y = -12392030
53 feet Y = -3777090
90 meter
Z = 1588186
74 Z = 484079
32
XDOT = 9112
758550 XDOT = 2777
568806
YDOT = 10844
625952 feet/sec YDOT = 3305
441990 meter/sec
ZDOT = -19718
412447 ZDOT = -6010
172114
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 10344
53271344
00016717 00000-0 10270-3 0 9097
2 25544 51
6464 47
9884 0008171 329
4436 30
6250 15
73122036 11217
Satellite: ISS
Catalog Number: 25544
Epoch time: 10344
53271344 = yrday
fracday
Element set: 909
Inclination: 51
6464 deg
RA of node: 47
9884 deg
Eccentricity:
0008171
Arg of perigee: 329
4436 deg
Mean anomaly: 30
6250 deg
Mean motion: 15
73122036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1121
Checksum: 288
Coasting Arc #11 (Orbit 1136)
---------------------------------------
Vector Time (GMT): 2010/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2041232
95 A = 6722705
81 meter
Y = 3698561
66 meter E =
0005670
Z = 5229704
27 I = 51
85849
XDOT = -6093
593321 Wp = 350
35198
YDOT = -4621
317923 meter/sec RA = 42
45200 deg
ZDOT = 895
486312 TA = 91
17709
MA = 91
11214
Ha = 192
235 n
mi
Hp = 185
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6696958
49 X = -2107844
20
Y = 12134388
65 feet Y = 3675362
50 meter
Z = 17157822
42 Z = 5219626
46
XDOT = -19992
104072 XDOT = -6045
814099
YDOT = -15161
804208 feet/sec YDOT = -4689
193075 meter/sec
ZDOT = 2937
947218 ZDOT = 865
999320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10663640
15 X = -3250277
52
Y = -8931575
37 feet Y = -2722344
17 meter
Z = 17117162
48 Z = 5217311
12
XDOT = 17958
222804 XDOT = 5473
666311
YDOT = -16072
684007 feet/sec YDOT = -4898
954085 meter/sec
ZDOT = 2819
478993 ZDOT = 859
377197
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 10345
54910636
00016717 00000-0 10270-3 0 9105
2 25544 51
6465 42
7757 0008204 332
8185 27
2548 15
73168297 11374
Satellite: ISS
Catalog Number: 25544
Epoch time: 10345
54910636 = yrday
fracday
Element set: 910
Inclination: 51
6465 deg
RA of node: 42
7757 deg
Eccentricity:
0008204
Arg of perigee: 332
8185 deg
Mean anomaly: 27
2548 deg
Mean motion: 15
73168297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1137
Checksum: 313
Coasting Arc #12 (Orbit 1151)
---------------------------------------
Vector Time (GMT): 2010/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5739448
06 A = 6734143
07 meter
Y = 3343889
00 meter E =
0015769
Z = -1045474
78 I = 51
87307
XDOT = -1620
033386 Wp = 10
31492
YDOT = 4629
414091 meter/sec RA = 37
32161 deg
ZDOT = 5942
115918 TA = 338
28571
MA = 338
35249
Ha = 192
492 n
mi
Hp = 185
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18830210
16 X = 5706708
23
Y = 10970764
42 feet Y = 3407887
97 meter
Z = -3430035
37 Z = -1017671
78
XDOT = -5315
070165 XDOT = -1700
545739
YDOT = 15188
366440 feet/sec YDOT = 4610
847326 meter/sec
ZDOT = 19495
130965 ZDOT = 5934
050531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13990494
83 X = -4264302
83
Y = 16731842
27 feet Y = 5099865
52 meter
Z = -3318303
46 Z = -1011418
89
XDOT = -12836
515812 XDOT = -3912
570019
YDOT = -6892
934994 feet/sec YDOT = -2100
966586 meter/sec
ZDOT = 19462
534011 ZDOT = 5932
180366
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 10346
50195164
00016717 00000-0 10270-3 0 9114
2 25544 51
6461 37
8890 0008409 338
0057 22
0744 15
73153643 11523
Satellite: ISS
Catalog Number: 25544
Epoch time: 10346
50195164 = yrday
fracday
Element set: 911
Inclination: 51
6461 deg
RA of node: 37
8890 deg
Eccentricity:
0008409
Arg of perigee: 338
0057 deg
Mean anomaly: 22
0744 deg
Mean motion: 15
73153643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1152
Checksum: 291
Coasting Arc #13 (Orbit 1167)
---------------------------------------
Vector Time (GMT): 2010/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 772725
86 A = 6723002
17 meter
Y = -4286128
28 meter E =
0015339
Z = -5133375
25 I = 51
81181
XDOT = 6924
851420 Wp = 46
53036
YDOT = 3007
203028 meter/sec RA = 32
22830 deg
ZDOT = -1460
864778 TA = 209
43910
MA = 209
52558
Ha = 192
437 n
mi
Hp = 185
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2535189
84 X = 845533
85
Y = -14062100
65 feet Y = -4277079
77 meter
Z = -16841782
32 Z = -5129444
75
XDOT = 22719
328805 XDOT = 6897
806292
YDOT = 9866
151667 feet/sec YDOT = 3084
489762 meter/sec
ZDOT = -4792
863446 ZDOT = -1427
289181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13500962
75 X = 4115093
45
Y = 4736141
02 feet Y = 1443575
78 meter
Z = -16825827
38 Z = -5128512
19
XDOT = -12853
943116 XDOT = -3917
881862
YDOT = 20005
077003 feet/sec YDOT = 6097
547471 meter/sec
ZDOT = -4657
904568 ZDOT = -1419
729312
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 10347
51829308
00016717 00000-0 10270-3 0 9121
2 25544 51
6466 32
6760 0008249 342
1335 17
9527 15
73218506 11683
Satellite: ISS
Catalog Number: 25544
Epoch time: 10347
51829308 = yrday
fracday
Element set: 912
Inclination: 51
6466 deg
RA of node: 32
6760 deg
Eccentricity:
0008249
Arg of perigee: 342
1335 deg
Mean anomaly: 17
9527 deg
Mean motion: 15
73218506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1168
Checksum: 308
Coasting Arc #14 (Orbit 1183)
---------------------------------------
Vector Time (GMT): 2010/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6284827
89 A = 6733246
47 meter
Y = -1900450
41 meter E =
0010484
Z = 1487353
07 I = 51
82078
XDOT = 145
435725 Wp = 81
85272
YDOT = -5051
239546 meter/sec RA = 27
08530 deg
ZDOT = -5803
489355 TA = 81
82425
MA = 81
70534
Ha = 192
523 n
mi
Hp = 184
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20619514
06 X = -6270334
94
Y = -6235073
53 feet Y = -1970650
20 meter
Z = 4879767
29 Z = 1456856
21
XDOT = 477
151330 XDOT = 230
101352
YDOT = -16572
308221 feet/sec YDOT = -5049
139429 meter/sec
ZDOT = -19040
319406 ZDOT = -5802
577495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8955832
93 X = 2729737
88
Y = -19621801
87 feet Y = -5980725
21 meter
Z = 4757160
79 Z = 1449982
61
XDOT = 14912
153014 XDOT = 4545
224239
YDOT = 2161
502053 feet/sec YDOT = 658
825826 meter/sec
ZDOT = -19036
477047 ZDOT = -5802
318204
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 10348
53460640
00016717 00000-0 10270-3 0 9135
2 25544 51
6468 27
4630 0008400 347
0137 13
0808 15
73303069 11842
Satellite: ISS
Catalog Number: 25544
Epoch time: 10348
53460640 = yrday
fracday
Element set: 913
Inclination: 51
6468 deg
RA of node: 27
4630 deg
Eccentricity:
0008400
Arg of perigee: 347
0137 deg
Mean anomaly: 13
0808 deg
Mean motion: 15
73303069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1184
Checksum: 281
Coasting Arc #15 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2010/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 521957
04 A = 6723199
97 meter
Y = 4460002
84 meter E =
0006068
Z = 4999367
63 I = 51
75918
XDOT = -7338
129959 Wp = 34
06764
YDOT = -1313
653854 meter/sec RA = 21
99547 deg
ZDOT = 1941
862751 TA = 37
23343
MA = 37
19137
Ha = 192
631 n
mi
Hp = 184
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1712457
49 X = 447759
37
Y = 14632555
24 feet Y = 4465424
45 meter
Z = 16402124
76 Z = 5001723
42
XDOT = -24075
229523 XDOT = -7332
328366
YDOT = -4309
887972 feet/sec YDOT = -1395
680944 meter/sec
ZDOT = 6370
940783 ZDOT = 1906
227718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14721589
05 X = -4487140
34
Y = -115175
58 feet Y = -35105
52 meter
Z = 16411442
06 Z = 5002207
54
XDOT = 7103
600390 XDOT = 2165
177399
YDOT = -22366
120530 feet/sec YDOT = -6817
193537 meter/sec
ZDOT = 6227
651363 ZDOT = 1898
188135
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 10349
55089372
00016717 00000-0 10270-3 0 9148
2 25544 51
6463 22
2500 0008315 351
7946 8
3079 15
73325755 12003
Satellite: ISS
Catalog Number: 25544
Epoch time: 10349
55089372 = yrday
fracday
Element set: 914
Inclination: 51
6463 deg
RA of node: 22
2500 deg
Eccentricity:
0008315
Arg of perigee: 351
7946 deg
Mean anomaly: 8
3079 deg
Mean motion: 15
73325755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 295
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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