Date:
January 8th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13723 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 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
012/00:42:49
251 -0
7 8
2 8
2
N/A 7
9 0
0 183
6
000/00:01:38
502 -1
9 -0
0 180
5
Coasting Arc #1 (Orbit 302)
---------------------------------------
Vector Time (GMT): 2008/007/14:13:36
877
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5300345
98 A = 6714282
85 meter
Y = -2258123
40 meter E =
0006294
Z = -3454938
79 I = 51
89409
XDOT = -356
215465 Wp = 73
44550
YDOT = 6175
026018 meter/sec RA = 128
87010 deg
ZDOT = -4587
521215 TA = 147
36749
MA = 147
32858
Ha = 183
670 n
mi
Hp = 176
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17389586
54 X = 5341985
98
Y = -7408541
34 feet Y = -2198618
54 meter
Z = -11335101
02 Z = -3429089
26
XDOT = -1168
685910 XDOT = -402
954017
YDOT = 20259
271714 feet/sec YDOT = 6170
782029 meter/sec
ZDOT = -15050
922623 ZDOT = -4589
364215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18051809
91 X = 5502191
66
Y = 5800020
83 feet Y = 1767846
35 meter
Z = -11236575
86 Z = -3424908
32
XDOT = -13638
231277 XDOT = -4156
932893
YDOT = 13308
787011 feet/sec YDOT = 4056
518281 meter/sec
ZDOT = -15057
311986 ZDOT = -4589
468693
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 08007
61734392
00020000 00000-0 20000-3 0 9009
2 25544 51
6389 129
6211 0001943 32
7115 327
4171 15
78497908 3031
Satellite: ISS
Catalog Number: 25544
Epoch time: 08007
61734392 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 129
6211 deg
Eccentricity:
0001943
Arg of perigee: 32
7115 deg
Mean anomaly: 327
4171 deg
Mean motion: 15
78497908 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 303
Checksum: 282
Coasting Arc #2 (Orbit 318)
---------------------------------------
Vector Time (GMT): 2008/008/14:13:36
877
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1279303
71 A = 6715651
93 meter
Y = -5941182
99 meter E =
0014605
Z = 2844643
18 I = 51
91718
XDOT = 5638
969570 Wp = 91
38278
YDOT = -1242
815945 meter/sec RA = 123
66957 deg
ZDOT = -5109
651184 TA = 56
02989
MA = 55
89117
Ha = 183
638 n
mi
Hp = 176
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4197190
66 X = 1331825
33
Y = -19492070
16 feet Y = -5926583
85 meter
Z = 9332818
82 Z = 2850984
61
XDOT = 18500
556332 XDOT = 5677
269158
YDOT = -4077
480135 feet/sec YDOT = -1179
542873 meter/sec
ZDOT = -16763
947454 ZDOT = -5082
164699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15666803
82 X = 4775241
80
Y = -12315327
89 feet Y = -3753711
94 meter
Z = 9356424
16 Z = 2851838
08
XDOT = 15994
209179 XDOT = 4875
034958
YDOT = 7635
608007 feet/sec YDOT = 2327
333321 meter/sec
ZDOT = -16659
047490 ZDOT = -5077
677675
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 08008
63025534
00020000 00000-0 20000-3 0 9014
2 25544 51
6392 124
3846 0002194 35
5535 324
5776 15
78569912 3198
Satellite: ISS
Catalog Number: 25544
Epoch time: 08008
63025534 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 124
3846 deg
Eccentricity:
0002194
Arg of perigee: 35
5535 deg
Mean anomaly: 324
5776 deg
Mean motion: 15
78569912 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 319
Checksum: 294
Coasting Arc #3 (Orbit 334)
---------------------------------------
Vector Time (GMT): 2008/009/14:13:36
877
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4374854
71 A = 6707830
14 meter
Y = -280198
23 meter E =
0005589
Z = 5072782
91 I = 51
90683
XDOT = 2395
498159 Wp = 103
00794
YDOT = -7138
474630 meter/sec RA = 118
55603 deg
ZDOT = 1668
861450 TA = 331
01764
MA = 331
04867
Ha = 183
663 n
mi
Hp = 176
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14353197
88 X = -4396038
50
Y = -919285
53 feet Y = -329239
45 meter
Z = 16642988
55 Z = 5051478
81
XDOT = 7859
245930 XDOT = 2467
036777
YDOT = -23420
192355 feet/sec YDOT = -7111
287036 meter/sec
ZDOT = 5475
267226 ZDOT = 1680
671369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10676163
55 X = -3254094
65
Y = -9776669
46 feet Y = -2979928
85 meter
Z = 16561543
08 Z = 5047958
33
XDOT = 20072
569322 XDOT = 6118
119129
YDOT = -12553
713088 feet/sec YDOT = -3826
371749 meter/sec
ZDOT = 5519
646967 ZDOT = 1682
388396
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 08009
64312841
00020000 00000-0 20000-3 0 9027
2 25544 51
6396 119
1473 0002166 36
0667 324
0645 15
78643183 3352
Satellite: ISS
Catalog Number: 25544
Epoch time: 08009
64312841 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 119
1473 deg
Eccentricity:
0002166
Arg of perigee: 36
0667 deg
Mean anomaly: 324
0645 deg
Mean motion: 15
78643183 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 335
Checksum: 281
Coasting Arc #4 (Orbit 350)
---------------------------------------
Vector Time (GMT): 2008/010/14:13:36
877
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2722735
06 A = 6719013
96 meter
Y = 6134156
56 meter E =
0014936
Z = 81068
60 I = 51
95692
XDOT = -4310
379764 Wp = 44
65687
YDOT = -2002
175694 meter/sec RA = 113
39316 deg
ZDOT = 6071
607003 TA = 316
22190
MA = 316
34022
Ha = 183
661 n
mi
Hp = 176
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8932857
80 X = -2791519
58
Y = 20125185
56 feet Y = 6103324
79 meter
Z = 265973
09 Z = 67675
42
XDOT = -14141
665894 XDOT = -4317
164891
YDOT = -6568
817895 feet/sec YDOT = -2050
415395 meter/sec
ZDOT = 19919
970483 ZDOT = 6050
650943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19404351
34 X = -5914446
29
Y = 10407426
28 feet Y = 3172183
53 meter
Z = 215433
24 Z = 65664
05
XDOT = -6464
507714 XDOT = -1970
381951
YDOT = -12518
821775 feet/sec YDOT = -3815
736877 meter/sec
ZDOT = 19839
665628 ZDOT = 6047
130083
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 08010
65596802
00020000 00000-0 20000-3 0 9032
2 25544 51
6391 113
9104 0002527 37
8876 322
2467 15
78640346 3510
Satellite: ISS
Catalog Number: 25544
Epoch time: 08010
65596802 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 113
9104 deg
Eccentricity:
0002527
Arg of perigee: 37
8876 deg
Mean anomaly: 322
2467 deg
Mean motion: 15
78640346 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 351
Checksum: 284
Coasting Arc #5 (Orbit 365)
---------------------------------------
Vector Time (GMT): 2008/011/14:13:36
877
Vector Time (MET): N/A
Weight (LBS) : 540573
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3086794
27 A = 6707816
23 meter
Y = 3213783
20 meter E =
0014632
Z = -5026578
12 I = 51
92969
XDOT = -3690
455572 Wp = 95
11297
YDOT = 6487
110894 meter/sec RA = 108
22720 deg
ZDOT = 1884
685670 TA = 192
98785
MA = 193
02557
Ha = 183
575 n
mi
Hp = 175
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10127277
79 X = 3075045
52
Y = 10543908
13 feet Y = 3248236
21 meter
Z = -16491398
04 Z = -5011611
07
XDOT = -12107
793871 XDOT = -3771
876423
YDOT = 21283
172225 feet/sec YDOT = 6445
386723 meter/sec
ZDOT = 6183
351936 ZDOT = 1866
560580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1850015
54 X = 563884
74
Y = 14567359
65 feet Y = 4440131
22 meter
Z = -16433850
40 Z = -5009037
60
XDOT = -21421
671371 XDOT = -6529
325434
YDOT = 9606
146065 feet/sec YDOT = 2927
953321 meter/sec
ZDOT = 6114
760351 ZDOT = 1863
778955
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 08011
60546776
00020000 00000-0 20000-3 0 9044
2 25544 51
6385 109
0002 0002566 41
3491 318
7868 15
78724614 3664
Satellite: ISS
Catalog Number: 25544
Epoch time: 08011
60546776 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 109
0002 deg
Eccentricity:
0002566
Arg of perigee: 41
3491 deg
Mean anomaly: 318
7868 deg
Mean motion: 15
78724614 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 366
Checksum: 290
Coasting Arc #6 (Orbit 372)
---------------------------------------
Vector Time (GMT): 2008/012/00:43:38
502
Vector Time (MET): N/A
Weight (LBS) : 540063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4304865
86 A = 6711534
44 meter
Y = -402968
35 meter E =
0009920
Z = -5141952
90 I = 51
93335
XDOT = -994
460023 Wp = 72
88464
YDOT = 7501
206976 meter/sec RA = 106
00198 deg
ZDOT = -1419
805404 TA = 183
56491
MA = 183
57199
Ha = 183
567 n
mi
Hp = 180
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14123575
64 X = 4334030
13
Y = -1322074
64 feet Y = -354665
46 meter
Z = -16869924
23 Z = -5120969
48
XDOT = -3262
664117 XDOT = -1071
368740
YDOT = 24610
259108 feet/sec YDOT = 7489
656442 meter/sec
ZDOT = -4658
154213 ZDOT = -1424
822666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8470152
46 X = -2581702
47
Y = -11496870
81 feet Y = -3504246
22 meter
Z = -16789761
54 Z = -5117519
32
XDOT = 21911
732474 XDOT = 6678
696058
YDOT = -9310
654196 feet/sec YDOT = -2837
887399 meter/sec
ZDOT = -4676
537643 ZDOT = -1425
408674
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 08012
04856374
00020000 00000-0 20000-3 0 9052
2 25544 51
6400 106
7096 0004301 273
9744 86
0929 15
77246677 3730
Satellite: ISS
Catalog Number: 25544
Epoch time: 08012
04856374 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 106
7096 deg
Eccentricity:
0004301
Arg of perigee: 273
9744 deg
Mean anomaly: 86
0929 deg
Mean motion: 15
77246677 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 373
Checksum: 294
Coasting Arc #7 (Orbit 388)
---------------------------------------
Vector Time (GMT): 2008/013/00:43:38
502
Vector Time (MET): N/A
Weight (LBS) : 540063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1151129
83 A = 6722941
65 meter
Y = -6616389
91 meter E =
0009462
Z = 147022
12 I = 51
97848
XDOT = 4701
025662 Wp = 149
16092
YDOT = 679
431107 meter/sec RA = 100
85041 deg
ZDOT = -6068
471520 TA = 29
24704
MA = 29
19410
Ha = 183
588 n
mi
Hp = 180
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3776672
68 X = 1224315
57
Y = -21707315
97 feet Y = -6603108
12 meter
Z = 482356
05 Z = 152791
63
XDOT = 15423
312539 XDOT = 4722
557808
YDOT = 2229
104682 feet/sec YDOT = 732
121361 meter/sec
ZDOT = -19909
683466 ZDOT = -6045
581987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20400887
98 X = -6218190
66
Y = 8321870
93 feet Y = 2536506
26 meter
Z = 503710
52 Z = 153530
97
XDOT = -5748
925119 XDOT = -1752
272376
YDOT = -12862
636562 feet/sec YDOT = -3920
531624 meter/sec
ZDOT = -19822
116790 ZDOT = -6041
781198
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 08013
06230092
00020000 00000-0 20000-3 0 9069
2 25544 51
6398 101
4781 0004322 276
8716 83
1957 15
77248370 3891
Satellite: ISS
Catalog Number: 25544
Epoch time: 08013
06230092 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 101
4781 deg
Eccentricity:
0004322
Arg of perigee: 276
8716 deg
Mean anomaly: 83
1957 deg
Mean motion: 15
77248370 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 389
Checksum: 292
Coasting Arc #8 (Orbit 404)
---------------------------------------
Vector Time (GMT): 2008/014/00:43:38
502
Vector Time (MET): N/A
Weight (LBS) : 540063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3927129
02 A = 6710907
71 meter
Y = -1619041
42 meter E =
0003376
Z = 5196956
75 I = 51
94325
XDOT = 1611
385382 Wp = 339
35083
YDOT = -7454
185166 meter/sec RA = 95
70421 deg
ZDOT = -1101
715110 TA = 121
12760
MA = 121
09448
Ha = 183
568 n
mi
Hp = 180
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12884281
55 X = -3933978
34
Y = -5311815
68 feet Y = -1662995
34 meter
Z = 17050383
05 Z = 5177862
28
XDOT = 5286
697447 XDOT = 1699
971327
YDOT = -24455
988079 feet/sec YDOT = -7435
670380 meter/sec
ZDOT = -3614
550887 ZDOT = -1093
672259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2624329
56 X = 799895
65
Y = 13777607
64 feet Y = 4199414
81 meter
Z = 16977222
42 Z = 5174657
39
XDOT = -22390
154912 XDOT = -6824
519217
YDOT = 8693
559691 feet/sec YDOT = 2649
796994 meter/sec
ZDOT = -3584
590114 ZDOT = -1092
583067
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 08014
07600152
00020000 00000-0 20000-3 0 9070
2 25544 51
6398 96
2463 0004466 283
7440 76
3228 15
77369460 4057
Satellite: ISS
Catalog Number: 25544
Epoch time: 08014
07600152 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 96
2463 deg
Eccentricity:
0004466
Arg of perigee: 283
7440 deg
Mean anomaly: 76
3228 deg
Mean motion: 15
77369460 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 405
Checksum: 289
Coasting Arc #9 (Orbit 420)
---------------------------------------
Vector Time (GMT): 2008/015/00:43:38
502
Vector Time (MET): N/A
Weight (LBS) : 540063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1659127
59 A = 6720807
61 meter
Y = 6178063
42 meter E =
0011174
Z = 2040046
02 I = 51
97828
XDOT = -4348
702939 Wp = 53
93043
YDOT = -3022
342146 meter/sec RA = 90
59294 deg
ZDOT = 5601
441325 TA = 328
75571
MA = 328
82208
Ha = 183
655 n
mi
Hp = 180
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5443331
99 X = -1737998
43
Y = 20269236
94 feet Y = 6159069
02 meter
Z = 6693064
36 Z = 2031794
77
XDOT = -14267
398095 XDOT = -4341
794026
YDOT = -9915
820689 feet/sec YDOT = -3070
933467 meter/sec
ZDOT = 18377
432170 ZDOT = 5580
332114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19865980
82 X = 6055150
95
Y = -6799065
53 feet Y = -2072355
17 meter
Z = 6662165
87 Z = 2030628
16
XDOT = -672
505661 XDOT = -204
979726
YDOT = 16010
497286 feet/sec YDOT = 4879
999573 meter/sec
ZDOT = 18296
423264 ZDOT = 5576
749811
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 08015
08967222
00020000 00000-0 20000-3 0 9087
2 25544 51
6398 91
0138 0004403 289
9594 70
1097 15
77371785 4215
Satellite: ISS
Catalog Number: 25544
Epoch time: 08015
08967222 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 91
0138 deg
Eccentricity:
0004403
Arg of perigee: 289
9594 deg
Mean anomaly: 70
1097 deg
Mean motion: 15
77371785 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 421
Checksum: 304
Coasting Arc #10 (Orbit 435)
---------------------------------------
Vector Time (GMT): 2008/016/00:43:38
502
Vector Time (MET): N/A
Weight (LBS) : 540063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3682612
22 A = 6714325
01 meter
Y = 3585664
80 meter E =
0004298
Z = -4324411
54 I = 51
95612
XDOT = -2221
777235 Wp = 107
85830
YDOT = 6493
992561 meter/sec RA = 85
41115 deg
ZDOT = 3494
106379 TA = 197
30889
MA = 197
32355
Ha = 183
637 n
mi
Hp = 180
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12082061
08 X = 3663250
19
Y = 11763992
13 feet Y = 3626737
90 meter
Z = -14187701
91 Z = -4306568
27
XDOT = -7289
295389 XDOT = -2311
202591
YDOT = 21305
749872 feet/sec YDOT = 6468
647143 meter/sec
ZDOT = 11463
603607 ZDOT = 3483
096262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2657465
46 X = 809995
47
Y = -16710681
45 feet Y = -5093415
71 meter
Z = -14119121
76 Z = -4303508
31
XDOT = 20451
029542 XDOT = 6233
473804
YDOT = -6394
235659 feet/sec YDOT = -1948
963029 meter/sec
ZDOT = 11422
181326 ZDOT = 3481
480868
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 08016
03995597
00020000 00000-0 20000-3 0 9090
2 25544 51
6399 86
1087 0004504 293
3511 66
7180 15
77437967 4369
Satellite: ISS
Catalog Number: 25544
Epoch time: 08016
03995597 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 86
1087 deg
Eccentricity:
0004504
Arg of perigee: 293
3511 deg
Mean anomaly: 66
7180 deg
Mean motion: 15
77437967 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 436
Checksum: 321
Coasting Arc #11 (Orbit 451)
---------------------------------------
Vector Time (GMT): 2008/017/00:43:38
502
Vector Time (MET): N/A
Weight (LBS) : 540063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2268628
39 A = 6715646
91 meter
Y = -4959782
90 meter E =
0004691
Z = -3923534
87 I = 51
95716
XDOT = 4098
246137 Wp = 30
25368
YDOT = 5094
440918 meter/sec RA = 80
32209 deg
ZDOT = -4068
417921 TA = 197
60657
MA = 197
62283
Ha = 183
628 n
mi
Hp = 180
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7443006
53 X = 2342980
59
Y = -16272253
61 feet Y = -4933997
71 meter
Z = -12872489
74 Z = -3912333
78
XDOT = 13445
689427 XDOT = 4060
738300
YDOT = 16714
045008 feet/sec YDOT = 5140
060505 meter/sec
ZDOT = -13347
827825 ZDOT = -4048
599328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17582383
70 X = -5359110
55
Y = 3483117
07 feet Y = 1061654
08 meter
Z = -12830169
71 Z = -3910635
73
XDOT = 5829
834895 XDOT = 1776
933676
YDOT = -19480
493345 feet/sec YDOT = -5937
654372 meter/sec
ZDOT = -13271
545776 ZDOT = -4045
167152
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 08017
05356072
00020000 00000-0 20000-3 0 9104
2 25544 51
6398 80
8764 0004579 297
0990 62
9707 15
77470391 4524
Satellite: ISS
Catalog Number: 25544
Epoch time: 08017
05356072 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 80
8764 deg
Eccentricity:
0004579
Arg of perigee: 297
0990 deg
Mean anomaly: 62
9707 deg
Mean motion: 15
77470391 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 452
Checksum: 310
Coasting Arc #12 (Orbit 467)
---------------------------------------
Vector Time (GMT): 2008/018/00:43:38
502
Vector Time (MET): N/A
Weight (LBS) : 540063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3457010
76 A = 6719226
27 meter
Y = -5145143
27 meter E =
0009744
Z = 2583815
98 I = 51
96419
XDOT = 3035
486852 Wp = 94
15283
YDOT = -4706
167582 meter/sec RA = 75
13434 deg
ZDOT = -5293
765381 TA = 56
60579
MA = 56
51260
Ha = 183
739 n
mi
Hp = 179
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11341898
82 X = -3411771
69
Y = -16880391
30 feet Y = -5183548
90 meter
Z = 8477086
54 Z = 2567131
16
XDOT = 9958
946364 XDOT = 3113
602349
YDOT = -15440
182357 feet/sec YDOT = -4671
785630 meter/sec
ZDOT = -17367
996658 ZDOT = -5278
829898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6632870
99 X = -2021699
08
Y = 19252983
31 feet Y = 5868309
31 meter
Z = 8412783
81 Z = 2564216
50
XDOT = -16980
019215 XDOT = -5175
509857
YDOT = 1738
090310 feet/sec YDOT = 529
769927 meter/sec
ZDOT = -17311
362873 ZDOT = -5276
503404
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 08018
06713281
00020000 00000-0 20000-3 0 9116
2 25544 51
6402 75
6440 0004468 303
8144 56
2595 15
77550101 4683
Satellite: ISS
Catalog Number: 25544
Epoch time: 08018
06713281 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 75
6440 deg
Eccentricity:
0004468
Arg of perigee: 303
8144 deg
Mean anomaly: 56
2595 deg
Mean motion: 15
77550101 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 468
Checksum: 271
Coasting Arc #13 (Orbit 483)
---------------------------------------
Vector Time (GMT): 2008/019/00:43:38
502
Vector Time (MET): N/A
Weight (LBS) : 540063
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3090245
01 A = 6710892
40 meter
Y = 3125755
85 meter E =
0000716
Z = 5070611
23 I = 51
92706
XDOT = -3779
571825 Wp = 112
66447
YDOT = -6497
833412 meter/sec RA = 70
02894 deg
ZDOT = 1701
670583 TA = 321
04521
MA = 321
05037
Ha = 183
936 n
mi
Hp = 179
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10138599
11 X = -3149599
87
Y = 10255104
48 feet Y = 3090866
38 meter
Z = 16635863
63 Z = 5055455
25
XDOT = -12400
170029 XDOT = -3714
897474
YDOT = -21318
351089 feet/sec YDOT = -6539
737361 meter/sec
ZDOT = 5582
908736 ZDOT = 1683
465772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14379947
79 X = 4383008
08
Y = 1757848
52 feet Y = 535792
23 meter
Z = 16578220
31 Z = 5053041
55
XDOT = -9030
255476 XDOT = -2752
421869
YDOT = 21867
302781 feet/sec YDOT = 6665
153888 meter/sec
ZDOT = 5512
662880 ZDOT = 1680
259646
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 08019
08067253
00020000 00000-0 20000-3 0 9121
2 25544 51
6398 70
4108 0004441 307
8171 52
2591 15
77564015 4845
Satellite: ISS
Catalog Number: 25544
Epoch time: 08019
08067253 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 70
4108 deg
Eccentricity:
0004441
Arg of perigee: 307
8171 deg
Mean anomaly: 52
2591 deg
Mean motion: 15
77564015 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 484
Checksum: 278
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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