Date:
January 28th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9526 06 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
035/08:30:34
844 -2
4 4
6 4
6
N/A -2
8 -0
0 196
5
000/00:01:05
688 -2
8 0
0 191
3
Coasting Arc #1 (Orbit 2366)
---------------------------------------
Vector Time (GMT): 2009/026/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2801608
73 A = 6729875
40 meter
Y = -3159251
26 meter E =
0009890
Z = -5247532
76 I = 51
37570
XDOT = 5361
610020 Wp = 61
41093
YDOT = -5493
693010 meter/sec RA = 311
61690 deg
ZDOT = 450
237400 TA = 212
85638
MA = 212
91790
Ha = 195
263 n
mi
Hp = 190
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9191629
71 X = -2740582
42
Y = -10364997
57 feet Y = -3190238
94 meter
Z = -17216314
83 Z = -5260994
54
XDOT = 17590
584055 XDOT = 5420
455810
YDOT = -18023
927197 feet/sec YDOT = -5433
407378 meter/sec
ZDOT = 1477
156823 ZDOT = 476
425955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1457801
98 X = 444338
04
Y = -13710562
62 feet Y = -4178979
49 meter
Z = -17268932
03 Z = -5263570
48
XDOT = 24169
173786 XDOT = 7366
764170
YDOT = 603
146063 feet/sec YDOT = 183
838920 meter/sec
ZDOT = 1578
775564 ZDOT = 481
210792
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
53593283
00010596 00000-0 82463-4 0 9005
2 25544 51
6428 312
1259 0008371 312
5562 47
4892 15
70602462 23679
Satellite: ISS
Catalog Number: 25544
Epoch time: 09026
53593283 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 312
1259 deg
Eccentricity:
0008371
Arg of perigee: 312
5562 deg
Mean anomaly: 47
4892 deg
Mean motion: 15
70602462 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2367
Checksum: 304
Coasting Arc #2 (Orbit 2382)
---------------------------------------
Vector Time (GMT): 2009/027/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3525409
34 A = 6741659
16 meter
Y = 5701835
60 meter E =
0005213
Z = 696547
84 I = 51
39673
XDOT = -4430
988635 Wp = 114
71896
YDOT = -2007
857313 meter/sec RA = 306
48675 deg
ZDOT = -5957
587168 TA = 57
68160
MA = 57
63113
Ha = 195
473 n
mi
Hp = 190
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11566303
62 X = -3592289
80
Y = 18706809
72 feet Y = 5662038
46 meter
Z = 2285261
96 Z = 679259
65
XDOT = -14537
364288 XDOT = -4379
267067
YDOT = -6587
458377 feet/sec YDOT = -2057
117792 meter/sec
ZDOT = -19545
889660 ZDOT = -5978
986744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21527561
63 X = -6561600
78
Y = 4537585
05 feet Y = 1383055
92 meter
Z = 2218320
10 Z = 676143
97
XDOT = -4861
436223 XDOT = -1481
765761
YDOT = -13413
508656 feet/sec YDOT = -4088
437438 meter/sec
ZDOT = -19629
345031 ZDOT = -5983
024365
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
55396232
00010596 00000-0 82463-4 0 9014
2 25544 51
6428 306
9245 0008335 316
0278 44
0220 15
70603118 23833
Satellite: ISS
Catalog Number: 25544
Epoch time: 09027
55396232 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 306
9245 deg
Eccentricity:
0008335
Arg of perigee: 316
0278 deg
Mean anomaly: 44
0220 deg
Mean motion: 15
70603118 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2383
Checksum: 287
Coasting Arc #3 (Orbit 2398)
---------------------------------------
Vector Time (GMT): 2009/028/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4552935
03 A = 6730970
78 meter
Y = 146536
74 meter E =
0003146
Z = 4954866
43 I = 51
34458
XDOT = -2406
799200 Wp = 349
72730
YDOT = 7028
826027 meter/sec RA = 301
38055 deg
ZDOT = 2006
937222 TA = 80
78200
MA = 80
74641
Ha = 195
469 n
mi
Hp = 190
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14937450
90 X = 4526888
84
Y = 480763
59 feet Y = 197304
60 meter
Z = 16256123
46 Z = 4976920
74
XDOT = -7896
322835 XDOT = -2494
966898
YDOT = 23060
452845 feet/sec YDOT = 7001
418800 meter/sec
ZDOT = 6584
439705 ZDOT = 1995
031251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10088530
05 X = 3074983
96
Y = 10898646
38 feet Y = 3321907
42 meter
Z = 16342006
96 Z = 4981043
72
XDOT = -21187
628890 XDOT = -6457
989286
YDOT = 9824
349210 feet/sec YDOT = 2994
461639 meter/sec
ZDOT = 6538
553030 ZDOT = 1992
950964
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 09028
57197632
00010596 00000-0 82463-4 0 9021
2 25544 51
6425 301
7227 0008397 319
9198 40
1343 15
70650144 23995
Satellite: ISS
Catalog Number: 25544
Epoch time: 09028
57197632 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 301
7227 deg
Eccentricity:
0008397
Arg of perigee: 319
9198 deg
Mean anomaly: 40
1343 deg
Mean motion: 15
70650144 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2399
Checksum: 316
Coasting Arc #4 (Orbit 2413)
---------------------------------------
Vector Time (GMT): 2009/029/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 570942
07 A = 6738409
52 meter
Y = -6122674
03 meter E =
0009412
Z = -2741509
85 I = 51
35574
XDOT = 5452
537179 Wp = 354
00372
YDOT = -1785
925330 meter/sec RA = 296
21071 deg
ZDOT = 5131
714828 TA = 334
57343
MA = 334
61970
Ha = 195
694 n
mi
Hp = 190
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1873169
53 X = 652681
85
Y = -20087513
23 feet Y = -6115832
40 meter
Z = -8994454
89 Z = -2738537
73
XDOT = 17888
901506 XDOT = 5447
174075
YDOT = -5859
335072 feet/sec YDOT = -1724
981870 meter/sec
ZDOT = 16836
334736 ZDOT = 5158
189623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15422939
77 X = 4700912
04
Y = -13013468
96 feet Y = -3966505
34 meter
Z = -8983302
56 Z = -2738110
62
XDOT = 15866
459900 XDOT = 4836
096977
YDOT = 7128
142242 feet/sec YDOT = 2172
657755 meter/sec
ZDOT = 16939
297539 ZDOT = 5163
097890
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 09029
52635247
00010596 00000-0 82463-4 0 9037
2 25544 51
6428 296
8460 0008468 323
6504 36
4081 15
70672750 24145
Satellite: ISS
Catalog Number: 25544
Epoch time: 09029
52635247 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 296
8460 deg
Eccentricity:
0008468
Arg of perigee: 323
6504 deg
Mean anomaly: 36
4081 deg
Mean motion: 15
70672750 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2414
Checksum: 312
Coasting Arc #5 (Orbit 2429)
---------------------------------------
Vector Time (GMT): 2009/030/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4527552
07 A = 6735164
72 meter
Y = 3190812
94 meter E =
0009085
Z = -3840314
41 I = 51
33308
XDOT = -1038
222089 Wp = 9
58912
YDOT = -6418
453876 meter/sec RA = 291
12835 deg
ZDOT = -4101
473997 TA = 217
27573
MA = 217
33882
Ha = 195
860 n
mi
Hp = 189
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14854173
45 X = -4544240
56
Y = 10468546
38 feet Y = 3140089
87 meter
Z = -12599456
73 Z = -3862349
42
XDOT = -3406
240449 XDOT = -946
448862
YDOT = -21057
919541 feet/sec YDOT = -6429
550787 meter/sec
ZDOT = -13456
279518 ZDOT = -4106
294612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17933133
70 X = -5466019
15
Y = -2544785
89 feet Y = -775650
74 meter
Z = -12685031
43 Z = -3866397
58
XDOT = 11859
666871 XDOT = 3614
826462
YDOT = -16283
007705 feet/sec YDOT = -4963
060749 meter/sec
ZDOT = -13475
497856 ZDOT = -4107
331747
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 09030
54433952
00010596 00000-0 82463-4 0 9041
2 25544 51
6427 291
6441 0008585 326
9576 33
1048 15
70684812 24308
Satellite: ISS
Catalog Number: 25544
Epoch time: 09030
54433952 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 291
6441 deg
Eccentricity:
0008585
Arg of perigee: 326
9576 deg
Mean anomaly: 33
1048 deg
Mean motion: 15
70684812 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2430
Checksum: 309
Coasting Arc #6 (Orbit 2445)
---------------------------------------
Vector Time (GMT): 2009/031/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2230266
66 A = 6733474
77 meter
Y = 4690287
16 meter E =
0011795
Z = 4287781
83 I = 51
31800
XDOT = -4395
499508 Wp = 25
45285
YDOT = 5274
293289 meter/sec RA = 285
94502 deg
ZDOT = -3469
068245 TA = 99
90316
MA = 99
76999
Ha = 195
962 n
mi
Hp = 189
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7317147
85 X = 2156824
36
Y = 15388081
23 feet Y = 4714816
69 meter
Z = 14067525
68 Z = 4298437
89
XDOT = -14420
930145 XDOT = -4437
298973
YDOT = 17304
111839 feet/sec YDOT = 5224
906521 meter/sec
ZDOT = -11381
457496 ZDOT = -3490
522853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5032365
61 X = -1533865
04
Y = 16242861
40 feet Y = 4950824
16 meter
Z = 14109348
85 Z = 4300529
53
XDOT = -21084
125600 XDOT = -6426
441483
YDOT = 3466
345866 feet/sec YDOT = 1056
542220 meter/sec
ZDOT = -11464
621849 ZDOT = -3494
416740
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 09031
56231246
00010596 00000-0 82463-4 0 9057
2 25544 51
6423 286
4417 0008669 331
2498 28
8185 15
70736976 24463
Satellite: ISS
Catalog Number: 25544
Epoch time: 09031
56231246 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 286
4417 deg
Eccentricity:
0008669
Arg of perigee: 331
2498 deg
Mean anomaly: 28
8185 deg
Mean motion: 15
70736976 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2446
Checksum: 330
Coasting Arc #7 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2009/032/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2816533
48 A = 6739592
47 meter
Y = -5736874
37 meter E =
0015827
Z = 2106566
79 I = 51
33138
XDOT = 3747
150352 Wp = 36
82198
YDOT = 3865
580966 meter/sec RA = 280
85463 deg
ZDOT = 5508
344631 TA = 346
81541
MA = 346
85673
Ha = 196
093 n
mi
Hp = 189
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9240595
41 X = 2870241
61
Y = -18821766
30 feet Y = -5705077
97 meter
Z = 6911308
38 Z = 2120379
80
XDOT = 12293
800368 XDOT = 3676
888023
YDOT = 12682
352250 feet/sec YDOT = 3907
090896 meter/sec
ZDOT = 18071
996821 ZDOT = 5526
377451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19350197
87 X = 5897940
31
Y = -8029738
61 feet Y = -2447464
33 meter
Z = 6964683
31 Z = 2122835
47
XDOT = 166
925484 XDOT = 50
878887
YDOT = 16163
391840 feet/sec YDOT = 4926
601833 meter/sec
ZDOT = 18142
487289 ZDOT = 5529
830126
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 09032
58027296
00010596 00000-0 82463-4 0 9069
2 25544 51
6422 281
2386 0008707 335
0589 25
0151 15
70715050 24626
Satellite: ISS
Catalog Number: 25544
Epoch time: 09032
58027296 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 281
2386 deg
Eccentricity:
0008707
Arg of perigee: 335
0589 deg
Mean anomaly: 25
0151 deg
Mean motion: 15
70715050 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2462
Checksum: 295
Coasting Arc #8 (Orbit 2476)
---------------------------------------
Vector Time (GMT): 2009/033/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3959462
06 A = 6729868
57 meter
Y = -1808585
14 meter E =
0012122
Z = -5140698
98 I = 51
29453
XDOT = 1748
479347 Wp = 61
95722
YDOT = -7381
013724 meter/sec RA = 275
69059 deg
ZDOT = 1257
928503 TA = 220
09975
MA = 220
18929
Ha = 196
135 n
mi
Hp = 189
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12990361
10 X = -3913971
52
Y = -5933678
28 feet Y = -1852607
67 meter
Z = -16865810
30 Z = -5159823
43
XDOT = 5736
480796 XDOT = 1824
774374
YDOT = -24215
924292 feet/sec YDOT = -7361
034655 meter/sec
ZDOT = 4127
062018 ZDOT = 1266
607686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5966542
36 X = -1818602
11
Y = -12877753
80 feet Y = -3925139
36 meter
Z = -16940407
48 Z = -5163436
20
XDOT = 19112
961561 XDOT = 5825
630684
YDOT = -14294
438156 feet/sec YDOT = -4356
944750 meter/sec
ZDOT = 4160
328419 ZDOT = 1268
068102
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 09033
53459662
00010596 00000-0 82463-4 0 9072
2 25544 51
6419 276
3611 0008722 337
8925 22
1860 15
70763265 24771
Satellite: ISS
Catalog Number: 25544
Epoch time: 09033
53459662 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 276
3611 deg
Eccentricity:
0008722
Arg of perigee: 337
8925 deg
Mean anomaly: 22
1860 deg
Mean motion: 15
70763265 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2477
Checksum: 323
Coasting Arc #9 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2009/034/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -124808
74 A = 6741485
21 meter
Y = 6739674
90 meter E =
0005775
Z = -72454
09 I = 51
33166
XDOT = -4802
939976 Wp = 94
66464
YDOT = -149
050795 meter/sec RA = 270
56808 deg
ZDOT = -6003
393937 TA = 86
12410
MA = 86
05808
Ha = 196
344 n
mi
Hp = 188
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -409477
50 X = -199811
66
Y = 22111794
30 feet Y = 6737859
86 meter
Z = -237710
26 Z = -73242
26
XDOT = -15757
677086 XDOT = -4771
753166
YDOT = -489
011796 feet/sec YDOT = -202
585400 meter/sec
ZDOT = -19696
174333 ZDOT = -6026
650661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14362460
53 X = -4377677
97
Y = 16817182
02 feet Y = 5125877
08 meter
Z = -240294
62 Z = -73241
80
XDOT = -10544
227709 XDOT = -3213
880606
YDOT = -9268
748738 feet/sec YDOT = -2825
114615 meter/sec
ZDOT = -19786
747910 ZDOT = -6031
000763
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 09034
55253074
00010596 00000-0 82463-4 0 9085
2 25544 51
6419 271
1590 0008575 341
4137 18
6710 15
70731517 24939
Satellite: ISS
Catalog Number: 25544
Epoch time: 09034
55253074 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 271
1590 deg
Eccentricity:
0008575
Arg of perigee: 341
4137 deg
Mean anomaly: 18
6710 deg
Mean motion: 15
70731517 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2493
Checksum: 304
Coasting Arc #10 (Orbit 2505)
---------------------------------------
Vector Time (GMT): 2009/035/08:31:07
688
Vector Time (MET): N/A
Weight (LBS) : 640039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2410887
35 A = 6738731
76 meter
Y = 5280348
84 meter E =
0005716
Z = -3429026
31 I = 51
31435
XDOT = -3958
872696 Wp = 5
00366
YDOT = -4765
978321 meter/sec RA = 266
30960 deg
ZDOT = -4550
666720 TA = 215
65740
MA = 215
69560
Ha = 196
451 n
mi
Hp = 191
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7909735
39 X = -2453096
50
Y = 17323979
12 feet Y = 5253153
12 meter
Z = -11250086
31 Z = -3440840
44
XDOT = -12988
427480 XDOT = -3883
178449
YDOT = -15636
411813 feet/sec YDOT = -4809
825206 meter/sec
ZDOT = -14930
008925 ZDOT = -4569
715154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16003347
81 X = -4877820
41
Y = -10273672
35 feet Y = -3131415
33 meter
Z = -11295712
63 Z = -3442933
21
XDOT = 16592
894809 XDOT = 5057
514338
YDOT = -9331
522780 feet/sec YDOT = -2844
248143 meter/sec
ZDOT = -15004
533716 ZDOT = -4573
381877
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 09035
37960132
00010596 00000-0 82463-4 0 9097
2 25544 51
6411 266
9314 0007095 320
7969 39
2677 15
69905305 25068
Satellite: ISS
Catalog Number: 25544
Epoch time: 09035
37960132 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 266
9314 deg
Eccentricity:
0007095
Arg of perigee: 320
7969 deg
Mean anomaly: 39
2677 deg
Mean motion: 15
69905305 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2506
Checksum: 325
Coasting Arc #11 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2009/036/08:31:07
688
Vector Time (MET): N/A
Weight (LBS) : 640039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4190652
40 A = 6734108
42 meter
Y = 2362159
54 meter E =
0009753
Z = 4714251
45 I = 51
30152
XDOT = -1034
622565 Wp = 14
91462
YDOT = 7146
488498 meter/sec RA = 261
13606 deg
ZDOT = -2650
653582 TA = 101
34194
MA = 101
23234
Ha = 196
529 n
mi
Hp = 191
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13748859
59 X = 4141026
29
Y = 7749867
26 feet Y = 2408744
00 meter
Z = 15466704
23 Z = 4734488
95
XDOT = -3394
430989 XDOT = -1101
582707
YDOT = 23446
484575 feet/sec YDOT = 7134
544567 meter/sec
ZDOT = -8696
370020 ZDOT = -2655
841765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9434099
06 X = -2875513
39
Y = 12555463
12 feet Y = 3826905
16 meter
Z = 15545695
32 Z = 4738327
93
XDOT = -21910
204196 XDOT = -6678
230239
YDOT = -5628
824097 feet/sec YDOT = -1715
665585 meter/sec
ZDOT = -8716
055192 ZDOT = -2656
653622
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 09036
39808827
00010596 00000-0 82463-4 0 9104
2 25544 51
6406 261
7331 0007151 324
4146 35
6537 15
69917194 25227
Satellite: ISS
Catalog Number: 25544
Epoch time: 09036
39808827 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 261
7331 deg
Eccentricity:
0007151
Arg of perigee: 324
4146 deg
Mean anomaly: 35
6537 deg
Mean motion: 15
69917194 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2522
Checksum: 311
Coasting Arc #12 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2009/037/08:31:07
688
Vector Time (MET): N/A
Weight (LBS) : 640039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -764653
24 A = 6743341
09 meter
Y = -6604487
71 meter E =
0015738
Z = 1064106
89 I = 51
33837
XDOT = 4947
949770 Wp = 29
24401
YDOT = 379
434701 meter/sec RA = 256
03901 deg
ZDOT = 5887
423357 TA = 342
43291
MA = 342
48728
Ha = 196
715 n
mi
Hp = 191
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2508704
87 X = -695913
06
Y = -21668266
77 feet Y = -6612654
25 meter
Z = 3491164
35 Z = 1060558
73
XDOT = 16233
431004 XDOT = 4914
739754
YDOT = 1244
864504 feet/sec YDOT = 434
579384 meter/sec
ZDOT = 19315
693430 ZDOT = 5911
379308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21815013
85 X = 6649216
22
Y = -110747
90 feet Y = -33755
96 meter
Z = 3476854
77 Z = 1059745
33
XDOT = -3032
961610 XDOT = -924
446699
YDOT = 14293
476900 feet/sec YDOT = 4356
651759 meter/sec
ZDOT = 19409
032969 ZDOT = 5915
873249
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 09037
41656292
00010596 00000-0 82463-4 0 9116
2 25544 51
6406 256
5339 0007227 328
5681 31
5047 15
69917293 25388
Satellite: ISS
Catalog Number: 25544
Epoch time: 09037
41656292 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 256
5339 deg
Eccentricity:
0007227
Arg of perigee: 328
5681 deg
Mean anomaly: 31
5047 deg
Mean motion: 15
69917293 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2538
Checksum: 324
Coasting Arc #13 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2009/038/08:31:07
688
Vector Time (MET): N/A
Weight (LBS) : 640039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3872181
89 A = 6731652
08 meter
Y = 1679107
67 meter E =
0013513
Z = -5254502
50 I = 51
30814
XDOT = -2724
271581 Wp = 58
97430
YDOT = -7181
340081 meter/sec RA = 250
90422 deg
ZDOT = -280
928366 TA = 208
30483
MA = 208
37831
Ha = 196
771 n
mi
Hp = 190
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12704008
82 X = -3865145
49
Y = 5508883
42 feet Y = 1635846
37 meter
Z = -17239181
42 Z = -5273295
80
XDOT = -8937
898887 XDOT = -2642
401516
YDOT = -23560
827036 feet/sec YDOT = -7211
346690 meter/sec
ZDOT = -921
680992 ZDOT = -293
964106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4302613
96 X = -1311436
73
Y = -13065297
70 feet Y = -3982302
74 meter
Z = -17312265
06 Z = -5276778
39
XDOT = 23341
839126 XDOT = 7114
592566
YDOT = -6370
181064 feet/sec YDOT = -1941
631188 meter/sec
ZDOT = -973
005757 ZDOT = -296
572155
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 09038
37136970
00010596 00000-0 82463-4 0 9129
2 25544 51
6409 251
6601 0007233 332
0360 28
0411 15
69967192 25536
Satellite: ISS
Catalog Number: 25544
Epoch time: 09038
37136970 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 251
6601 deg
Eccentricity:
0007233
Arg of perigee: 332
0360 deg
Mean anomaly: 28
0411 deg
Mean motion: 15
69967192 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2553
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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