[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 17th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 ET - UTC (sec) : 67 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
235/13:28:37
051 -5
3 7
9 8
1
N/A -0
2 -1
5 231
6
000/00:41:10
102 6
2 -1
1 219
2
Coasting Arc #1 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2012/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2093376
31 A = 6780625
78 meter
Y = 4010856
79 meter E =
0012452
Z = -5060445
74 I = 51
62016
XDOT = -7286
902701 Wp = 43
25147
YDOT = 1457
550606 meter/sec RA = 180
07914 deg
ZDOT = -1853
007521 TA = 208
73700
MA = 208
80567
Ha = 222
387 n
mi
Hp = 216
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6868032
50 X = 2072952
47
Y = 13158978
98 feet Y = 4034152
00 meter
Z = -16602512
28 Z = -5050326
07
XDOT = -23907
161091 XDOT = -7293
658454
YDOT = 4781
990178 feet/sec YDOT = 1376
026139 meter/sec
ZDOT = -6079
421001 ZDOT = -1888
422631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1972537
36 X = 601229
39
Y = -14758495
31 feet Y = -4498389
37 meter
Z = -16561036
34 Z = -5047803
88
XDOT = 21129
238075 XDOT = 6440
191765
YDOT = 9832
958717 feet/sec YDOT = 2997
085817 meter/sec
ZDOT = -6225
822605 ZDOT = -1897
630730
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 12229
51938366
00016717 00000-0 10270-3 0 9004
2 25544 51
6411 181
0472 0007250 325
3059 34
7620 15
53417064 35549
Satellite: ISS
Catalog Number: 25544
Epoch time: 12229
51938366 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 181
0472 deg
Eccentricity:
0007250
Arg of perigee: 325
3059 deg
Mean anomaly: 34
7620 deg
Mean motion: 15
53417064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 287
Coasting Arc #2 (Orbit 3569)
---------------------------------------
Vector Time (GMT): 2012/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -576652
51 A = 6779340
95 meter
Y = -4170819
73 meter E =
0005932
Z = 5314299
66 I = 51
64758
XDOT = 7621
462888 Wp = 346
94015
YDOT = -810
941475 meter/sec RA = 175
08729 deg
ZDOT = 196
243671 TA = 101
22278
MA = 101
15609
Ha = 222
449 n
mi
Hp = 216
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1891904
57 X = -555785
83
Y = -13683791
76 feet Y = -4177151
38 meter
Z = 17435366
35 Z = 5311549
18
XDOT = 25004
799502 XDOT = 7629
011272
YDOT = -2660
569144 feet/sec YDOT = -725
671323 meter/sec
ZDOT = 643
844066 ZDOT = 233
286001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6110781
14 X = -1862566
09
Y = 12404364
88 feet Y = 3780850
42 meter
Z = 17424337
73 Z = 5310938
14
XDOT = -21198
304747 XDOT = -6461
243287
YDOT = -11536
143176 feet/sec YDOT = -3516
216440 meter/sec
ZDOT = 796
929294 ZDOT = 242
904049
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 12230
54868060
00016717 00000-0 10270-3 0 9013
2 25544 51
6420 175
9218 0007333 328
6870 31
3845 15
53450605 35706
Satellite: ISS
Catalog Number: 25544
Epoch time: 12230
54868060 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 175
9218 deg
Eccentricity:
0007333
Arg of perigee: 328
6870 deg
Mean anomaly: 31
3845 deg
Mean motion: 15
53450605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3570
Checksum: 293
Coasting Arc #3 (Orbit 3584)
---------------------------------------
Vector Time (GMT): 2012/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -929242
38 A = 6779999
35 meter
Y = 4304494
63 meter E =
0010906
Z = -5163196
51 I = 51
68040
XDOT = -7517
083981 Wp = 69
36313
YDOT = 133
084762 meter/sec RA = 170
09592 deg
ZDOT = 1470
098475 TA = 214
75929
MA = 214
83058
Ha = 222
610 n
mi
Hp = 216
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3048695
48 X = -952225
86
Y = 14122357
72 feet Y = 4293974
50 meter
Z = -16939621
10 Z = -5167766
69
XDOT = -24662
349020 XDOT = -7525
154758
YDOT = 436
629798 feet/sec YDOT = 48
978997 meter/sec
ZDOT = 4823
157727 ZDOT = 1433
561854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10258841
80 X = 3126894
98
Y = -10141009
60 feet Y = -3090979
73 meter
Z = -16958843
83 Z = -5169055
60
XDOT = 20079
736361 XDOT = 6120
303643
YDOT = 12534
048730 feet/sec YDOT = 3820
378053 meter/sec
ZDOT = 4672
202972 ZDOT = 1424
087466
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 12231
51363687
00016717 00000-0 10270-3 0 9027
2 25544 51
6423 171
1158 0007352 332
4768 27
5994 15
53448842 35858
Satellite: ISS
Catalog Number: 25544
Epoch time: 12231
51363687 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 171
1158 deg
Eccentricity:
0007352
Arg of perigee: 332
4768 deg
Mean anomaly: 27
5994 deg
Mean motion: 15
53448842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3585
Checksum: 319
Coasting Arc #4 (Orbit 3600)
---------------------------------------
Vector Time (GMT): 2012/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2394408
77 A = 6782278
40 meter
Y = -4383936
77 meter E =
0011241
Z = 4588698
32 I = 51
71862
XDOT = 7006
374463 Wp = 25
45191
YDOT = 624
903447 meter/sec RA = 165
11107 deg
ZDOT = -3046
258070 TA = 95
02704
MA = 94
89871
Ha = 222
676 n
mi
Hp = 216
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7855671
82 X = 2420962
34
Y = -14382994
66 feet Y = -4357012
26 meter
Z = 15054784
52 Z = 4600394
85
XDOT = 22986
792857 XDOT = 7013
663767
YDOT = 2050
208160 feet/sec YDOT = 703
293661 meter/sec
ZDOT = -9994
285007 ZDOT = -3012
204217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14284108
00 X = -4353796
12
Y = 7942195
98 feet Y = 2420781
34 meter
Z = 15103457
67 Z = 4603533
90
XDOT = -17741
641099 XDOT = -5407
652207
YDOT = -13091
186338 feet/sec YDOT = -3990
193596 meter/sec
ZDOT = -9853
637001 ZDOT = -3003
388558
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 12232
54291227
00016717 00000-0 10270-3 0 9032
2 25544 51
6428 165
9904 0007329 336
3691 23
7124 15
53466468 36011
Satellite: ISS
Catalog Number: 25544
Epoch time: 12232
54291227 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 165
9904 deg
Eccentricity:
0007329
Arg of perigee: 336
3691 deg
Mean anomaly: 23
7124 deg
Mean motion: 15
53466468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3601
Checksum: 307
Coasting Arc #5 (Orbit 3615)
---------------------------------------
Vector Time (GMT): 2012/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3645933
61 A = 6785423
35 meter
Y = 4390653
99 meter E =
0006604
Z = -3667598
15 I = 51
75845
XDOT = -6129
982571 Wp = 27
31433
YDOT = -1447
155996 meter/sec RA = 160
13429 deg
ZDOT = 4370
156687 TA = 289
18673
MA = 289
25819
Ha = 222
773 n
mi
Hp = 216
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11961724
43 X = -3676943
63
Y = 14405032
78 feet Y = 4349709
28 meter
Z = -12032802
31 Z = -3685385
36
XDOT = -20111
491374 XDOT = -6134
573620
YDOT = -4747
887126 feet/sec YDOT = -1515
730675 meter/sec
ZDOT = 14337
784406 ZDOT = 4340
366722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17670708
20 X = 5386031
86
Y = -6045769
34 feet Y = -1842750
49 meter
Z = -12106646
81 Z = -3690105
95
XDOT = 14280
912532 XDOT = 4352
822140
YDOT = 13333
163050 feet/sec YDOT = 4063
948098 meter/sec
ZDOT = 14214
810269 ZDOT = 4332
674170
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 12233
50784686
00016717 00000-0 10270-3 0 9046
2 25544 51
6428 161
1845 0007390 339
6396 20
4461 15
53486018 36166
Satellite: ISS
Catalog Number: 25544
Epoch time: 12233
50784686 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 161
1845 deg
Eccentricity:
0007390
Arg of perigee: 339
6396 deg
Mean anomaly: 20
4461 deg
Mean motion: 15
53486018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3616
Checksum: 316
Coasting Arc #6 (Orbit 3631)
---------------------------------------
Vector Time (GMT): 2012/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4687408
33 A = 6788597
24 meter
Y = -4269400
66 meter E =
0011664
Z = 2422035
17 I = 51
79777
XDOT = 4938
181277 Wp = 73
22577
YDOT = 2365
328578 meter/sec RA = 155
16763 deg
ZDOT = -5362
861367 TA = 79
76657
MA = 79
63505
Ha = 222
909 n
mi
Hp = 215
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15378636
24 X = 4723035
63
Y = -14007220
01 feet Y = -4216783
81 meter
Z = 7946309
63 Z = 2444893
05
XDOT = 16201
382143 XDOT = 4937
416104
YDOT = 7760
264362 feet/sec YDOT = 2420
545823 meter/sec
ZDOT = -17594
689524 ZDOT = -5338
874018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20324490
87 X = -6194904
82
Y = 4254901
56 feet Y = 1296893
99 meter
Z = 8041105
98 Z = 2450929
10
XDOT = -9779
202250 XDOT = -2980
700846
YDOT = -13497
250633 feet/sec YDOT = -4113
961993 meter/sec
ZDOT = -17495
759039 ZDOT = -5332
707355
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 12234
53709932
00016717 00000-0 10270-3 0 9052
2 25544 51
6431 156
0584 0007394 343
6284 16
4629 15
53506016 36328
Satellite: ISS
Catalog Number: 25544
Epoch time: 12234
53709932 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 156
0584 deg
Eccentricity:
0007394
Arg of perigee: 343
6284 deg
Mean anomaly: 16
4629 deg
Mean motion: 15
53506016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3632
Checksum: 304
Coasting Arc #7 (Orbit 3646)
---------------------------------------
Vector Time (GMT): 2012/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 956127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5387064
54 A = 6790672
76 meter
Y = 3994507
98 meter E =
0015436
Z = -1005171
70 I = 51
83157
XDOT = -3564
271206 Wp = 16
56733
YDOT = -3325
299933 meter/sec RA = 150
20887 deg
ZDOT = 5924
332575 TA = 332
56539
MA = 332
64680
Ha = 223
022 n
mi
Hp = 215
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17674096
27 X = -5426448
69
Y = 13105341
13 feet Y = 3934046
22 meter
Z = -3297807
42 Z = -1031437
57
XDOT = -11693
803169 XDOT = -3555
601108
YDOT = -10909
776684 feet/sec YDOT = -3365
109125 meter/sec
ZDOT = 19436
786662 ZDOT = 5907
038739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21823261
78 X = 6651730
19
Y = -2671885
52 feet Y = -814390
71 meter
Z = -3406677
53 Z = -1038355
31
XDOT = 4685
674336 XDOT = 1428
193538
YDOT = 13728
918267 feet/sec YDOT = 4184
574288 meter/sec
ZDOT = 19365
590267 ZDOT = 5902
631913
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 12235
50201261
00016717 00000-0 10270-3 0 9063
2 25544 51
6428 151
2525 0007478 346
8983 13
1974 15
53509803 36470
Satellite: ISS
Catalog Number: 25544
Epoch time: 12235
50201261 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 151
2525 deg
Eccentricity:
0007478
Arg of perigee: 346
8983 deg
Mean anomaly: 13
1974 deg
Mean motion: 15
53509803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3647
Checksum: 307
Coasting Arc #8 (Orbit 3648)
---------------------------------------
Vector Time (GMT): 2012/235/13:49:12
102
Vector Time (MET): N/A
Weight (LBS) : 954317
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5179971
95 A = 6793521
18 meter
Y = -896080
85 meter E =
0014090
Z = 4291704
02 I = 51
81370
XDOT = 3916
946406 Wp = 12
54138
YDOT = -5532
987746 meter/sec RA = 149
86418 deg
ZDOT = 3583
599099 TA = 41
02881
MA = 40
92291
Ha = 231
553 n
mi
Hp = 219
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16994658
64 X = -5190414
88
Y = -2939897
81 feet Y = -954064
75 meter
Z = 14080393
75 Z = 4266514
68
XDOT = 12850
874036 XDOT = 3961
118027
YDOT = -18152
846937 feet/sec YDOT = -5488
938902 meter/sec
ZDOT = 11757
214891 ZDOT = 3602
734899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16952979
23 X = 5167268
07
Y = 3602287
40 feet Y = 1097977
20 meter
Z = 13976370
43 Z = 4259997
71
XDOT = -13213
596318 XDOT = -4027
504158
YDOT = 16404
184616 feet/sec YDOT = 4999
995471 meter/sec
ZDOT = 11836
746165 ZDOT = 3607
840231
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 12235
63081169
00016717 00000-0 10270-3 0 9071
2 25544 51
6471 150
6105 0017858 338
5753 21
4648 15
50054120 36497
Satellite: ISS
Catalog Number: 25544
Epoch time: 12235
63081169 = yrday
fracday
Element set: 907
Inclination: 51
6471 deg
RA of node: 150
6105 deg
Eccentricity:
0017858
Arg of perigee: 338
5753 deg
Mean anomaly: 21
4648 deg
Mean motion: 15
50054120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3649
Checksum: 302
Coasting Arc #9 (Orbit 3663)
---------------------------------------
Vector Time (GMT): 2012/236/13:49:12
102
Vector Time (MET): N/A
Weight (LBS) : 954317
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5044729
16 A = 6792717
33 meter
Y = 775106
76 meter E =
0020511
Z = -4496245
72 I = 51
83683
XDOT = -3801
134525 Wp = 8
72288
YDOT = 5789
385388 meter/sec RA = 144
92148 deg
ZDOT = -3248
992475 TA = 228
49401
MA = 228
67020
Ha = 231
613 n
mi
Hp = 219
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16550948
69 X = 5057528
52
Y = 2543001
17 feet Y = 831591
55 meter
Z = -14751462
33 Z = -4471707
63
XDOT = -12470
913796 XDOT = -3849
807279
YDOT = 18994
046547 feet/sec YDOT = 5746
606537 meter/sec
ZDOT = -10659
424129 ZDOT = -3267
576497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16581586
50 X = -5054067
57
Y = -2903723
37 feet Y = -885054
88 meter
Z = -14650111
87 Z = -4465354
10
XDOT = 12604
264895 XDOT = 3841
779940
YDOT = -17509
660213 feet/sec YDOT = -5336
944433 meter/sec
ZDOT = -10736
711235 ZDOT = -3272
549584
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 12236
59786984
00016717 00000-0 10270-3 0 9085
2 25544 51
6470 145
8195 0017976 341
5453 18
5043 15
50088433 36640
Satellite: ISS
Catalog Number: 25544
Epoch time: 12236
59786984 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 145
8195 deg
Eccentricity:
0017976
Arg of perigee: 341
5453 deg
Mean anomaly: 18
5043 deg
Mean motion: 15
50088433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3664
Checksum: 339
Coasting Arc #10 (Orbit 3679)
---------------------------------------
Vector Time (GMT): 2012/237/13:49:12
102
Vector Time (MET): N/A
Weight (LBS) : 954317
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4848285
66 A = 6791929
56 meter
Y = -737826
12 meter E =
0014147
Z = 4689886
60 I = 51
85845
XDOT = 3700
965358 Wp = 12
09498
YDOT = -6064
871162 meter/sec RA = 139
97859 deg
ZDOT = 2883
727783 TA = 49
40002
MA = 49
27702
Ha = 231
889 n
mi
Hp = 218
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15906449
03 X = -4862457
12
Y = -2420689
38 feet Y = -792121
92 meter
Z = 15386767
07 Z = 4666299
52
XDOT = 12142
274795 XDOT = 3754
500493
YDOT = -19897
871268 feet/sec YDOT = -6023
185340 meter/sec
ZDOT = 9461
049158 ZDOT = 2901
836855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15989049
89 X = 4873462
41
Y = 2492788
52 feet Y = 759801
94 meter
Z = 15289334
44 Z = 4660189
14
XDOT = -11993
173151 XDOT = -3655
519176
YDOT = 18675
909619 feet/sec YDOT = 5692
417252 meter/sec
ZDOT = 9536
412558 ZDOT = 2906
698548
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 12237
62939062
00016717 00000-0 10270-3 0 9098
2 25544 51
6470 140
7078 0017948 345
7333 14
3309 15
50081532 36806
Satellite: ISS
Catalog Number: 25544
Epoch time: 12237
62939062 = yrday
fracday
Element set: 909
Inclination: 51
6470 deg
RA of node: 140
7078 deg
Eccentricity:
0017948
Arg of perigee: 345
7333 deg
Mean anomaly: 14
3309 deg
Mean motion: 15
50081532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3680
Checksum: 308
Coasting Arc #11 (Orbit 3694)
---------------------------------------
Vector Time (GMT): 2012/238/13:49:12
102
Vector Time (MET): N/A
Weight (LBS) : 954317
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4711314
97 A = 6791208
04 meter
Y = 682703
93 meter E =
0022474
Z = -4858202
78 I = 51
87846
XDOT = -3523
750968 Wp = 19
34288
YDOT = 6306
768547 meter/sec RA = 135
03778 deg
ZDOT = -2513
641737 TA = 225
87442
MA = 226
05949
Ha = 231
924 n
mi
Hp = 218
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15457070
11 X = 4726930
54
Y = 2239842
29 feet Y = 735476
16 meter
Z = -15938985
49 Z = -4835277
66
XDOT = -11560
862755 XDOT = -3581
802055
YDOT = 20691
497856 feet/sec YDOT = 6267
039220 meter/sec
ZDOT = -8246
856092 ZDOT = -2530
900751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15581327
35 X = -4749188
58
Y = -2042151
86 feet Y = -622447
89 meter
Z = -15844274
11 Z = -4829334
75
XDOT = 11098
968089 XDOT = 3382
965474
YDOT = -19698
519815 feet/sec YDOT = -6004
108840 meter/sec
ZDOT = -8318
742194 ZDOT = -2535
552621
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 12238
59643013
00016717 00000-0 10270-3 0 9105
2 25544 51
6466 135
9163 0018052 348
6126 11
4613 15
50118913 36957
Satellite: ISS
Catalog Number: 25544
Epoch time: 12238
59643013 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 135
9163 deg
Eccentricity:
0018052
Arg of perigee: 348
6126 deg
Mean anomaly: 11
4613 deg
Mean motion: 15
50118913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3695
Checksum: 296
Coasting Arc #12 (Orbit 3710)
---------------------------------------
Vector Time (GMT): 2012/239/13:49:12
102
Vector Time (MET): N/A
Weight (LBS) : 954317
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4523991
48 A = 6790560
50 meter
Y = -721019
49 meter E =
0014786
Z = 5005320
01 I = 51
89735
XDOT = 3363
092457 Wp = 11
49590
YDOT = -6560
360367 meter/sec RA = 130
09702 deg
ZDOT = 2107
703833 TA = 58
12991
MA = 57
98611
Ha = 232
184 n
mi
Hp = 218
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14842491
73 X = -4539907
07
Y = -2365549
50 feet Y = -771698
62 meter
Z = 16421653
59 Z = 4983304
27
XDOT = 11033
767903 XDOT = 3425
963188
YDOT = -21523
492018 feet/sec YDOT = -6522
400666 meter/sec
ZDOT = 6915
038821 ZDOT = 2124
194024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15006563
43 X = 4574000
53
Y = 1917695
77 feet Y = 584513
67 meter
Z = 16330694
67 Z = 4977595
74
XDOT = -10204
462561 XDOT = -3110
320188
YDOT = 20747
056591 feet/sec YDOT = 6323
702849 meter/sec
ZDOT = 6983
782582 ZDOT = 2128
656931
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 12239
62793144
00016717 00000-0 10270-3 0 9112
2 25544 51
6469 130
8048 0018022 352
7769 7
3119 15
50107039 37113
Satellite: ISS
Catalog Number: 25544
Epoch time: 12239
62793144 = yrday
fracday
Element set: 911
Inclination: 51
6469 deg
RA of node: 130
8048 deg
Eccentricity:
0018022
Arg of perigee: 352
7769 deg
Mean anomaly: 7
3119 deg
Mean motion: 15
50107039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3711
Checksum: 299
Coasting Arc #13 (Orbit 3725)
---------------------------------------
Vector Time (GMT): 2012/240/13:49:12
102
Vector Time (MET): N/A
Weight (LBS) : 954317
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4405144
81 A = 6789977
97 meter
Y = 728722
39 meter E =
0023997
Z = -5130846
24 I = 51
91360
XDOT = -3128
880804 Wp = 29
07658
YDOT = 6767
254426 meter/sec RA = 125
15781 deg
ZDOT = -1708
161491 TA = 224
34369
MA = 224
53614
Ha = 232
194 n
mi
Hp = 218
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14452574
83 X = 4421592
76
Y = 2390821
48 feet Y = 778075
40 meter
Z = -16833485
03 Z = -5109406
65
XDOT = -10265
356967 XDOT = -3196
023371
YDOT = 22202
278299 feet/sec YDOT = 6731
889911 meter/sec
ZDOT = -5604
204367 ZDOT = -1723
524314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14651562
03 X = -4465796
11
Y = -1702713
67 feet Y = -518987
13 meter
Z = -16744899
55 Z = -5103845
38
XDOT = 9051
449176 XDOT = 2758
881709
YDOT = -21590
014283 feet/sec YDOT = -6580
636353 meter/sec
ZDOT = -5668
316528 ZDOT = -1727
702878
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 12240
59495273
00016717 00000-0 10270-3 0 9123
2 25544 51
6460 126
0129 0018081 355
7492 4
3502 15
50147869 37266
Satellite: ISS
Catalog Number: 25544
Epoch time: 12240
59495273 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 126
0129 deg
Eccentricity:
0018081
Arg of perigee: 355
7492 deg
Mean anomaly: 4
3502 deg
Mean motion: 15
50147869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3726
Checksum: 303
Coasting Arc #14 (Orbit 3741)
---------------------------------------
Vector Time (GMT): 2012/241/13:49:12
102
Vector Time (MET): N/A
Weight (LBS) : 954317
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4248158
38 A = 6789540
02 meter
Y = -836497
50 meter E =
0016025
Z = 5224021
32 I = 51
92901
XDOT = 2914
854720 Wp = 12
21904
YDOT = -6977
272578 meter/sec RA = 120
21880 deg
ZDOT = 1267
653056 TA = 65
74129
MA = 65
57396
Ha = 232
434 n
mi
Hp = 217
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13937527
51 X = -4263865
40
Y = -2744414
36 feet Y = -884090
74 meter
Z = 17139177
57 Z = 5203346
23
XDOT = 9563
171653 XDOT = 2986
501531
YDOT = -22891
314233 feet/sec YDOT = -6944
276226 meter/sec
ZDOT = 4158
966720 ZDOT = 1281
987224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14189278
03 X = 4324891
94
Y = 1836225
30 feet Y = 559681
47 meter
Z = 17053754
91 Z = 5197984
50
XDOT = -7914
460142 XDOT = -2412
327451
YDOT = 22421
403269 feet/sec YDOT = 6834
043716 meter/sec
ZDOT = 4218
852706 ZDOT = 1285
906305
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 12241
62643464
00016717 00000-0 10270-3 0 9136
2 25544 51
6464 120
9015 0018052 359
7850
3290 15
50131912 37427
Satellite: ISS
Catalog Number: 25544
Epoch time: 12241
62643464 = yrday
fracday
Element set: 913
Inclination: 51
6464 deg
RA of node: 120
9015 deg
Eccentricity:
0018052
Arg of perigee: 359
7850 deg
Mean anomaly:
3290 deg
Mean motion: 15
50131912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3742
Checksum: 277
Coasting Arc #15 (Orbit 3756)
---------------------------------------
Vector Time (GMT): 2012/242/13:49:12
102
Vector Time (MET): N/A
Weight (LBS) : 954317
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4165729
86 A = 6789150
83 meter
Y = 897967
75 meter E =
0024948
Z = -5300807
00 I = 51
94099
XDOT = -2635
086141 Wp = 37
94480
YDOT = 7130
337712 meter/sec RA = 115
28069 deg
ZDOT = -845
932220 TA = 223
88113
MA = 224
07955
Ha = 232
426 n
mi
Hp = 217
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13667092
73 X = 4181128
62
Y = 2946088
43 feet Y = 944637
38 meter
Z = -17391099
07 Z = -5280533
10
XDOT = -8645
295737 XDOT = -2710
513938
YDOT = 23393
496431 feet/sec YDOT = 7100
448756 meter/sec
ZDOT = -2775
368176 ZDOT = -858
916661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13967176
92 X = -4257195
52
Y = -1814746
78 feet Y = -553134
82 meter
Z = -17307335
17 Z = -5275275
76
XDOT = 6564
118820 XDOT = 2000
743416
YDOT = -22999
195994 feet/sec YDOT = -7010
154939 meter/sec
ZDOT = -2829
693024 ZDOT = -862
490434
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 12242
59343790
00016717 00000-0 10270-3 0 9143
2 25544 51
6449 116
1092 0018061 3
0066 357
1190 15
50174657 37571
Satellite: ISS
Catalog Number: 25544
Epoch time: 12242
59343790 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 116
1092 deg
Eccentricity:
0018061
Arg of perigee: 3
0066 deg
Mean anomaly: 357
1190 deg
Mean motion: 15
50174657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3757
Checksum: 298
Coasting Arc #16 (Orbit 3772)
---------------------------------------
Vector Time (GMT): 2012/243/13:49:12
102
Vector Time (MET): N/A
Weight (LBS) : 954317
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4057637
66 A = 6788976
91 meter
Y = -1062592
85 meter E =
0017745
Z = 5333288
05 I = 51
95243
XDOT = 2382
079004 Wp = 15
21053
YDOT = -7277
526036 meter/sec RA = 110
34273 deg
ZDOT = 378
743552 TA = 71
28915
MA = 71
09663
Ha = 232
641 n
mi
Hp = 217
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13312459
51 X = -4071361
41
Y = -3486197
03 feet Y = -1108044
25 meter
Z = 17497664
20 Z = 5313543
31
XDOT = 7815
219828 XDOT = 2461
440946
YDOT = -23876
397756 feet/sec YDOT = -7250
444381 meter/sec
ZDOT = 1242
596956 ZDOT = 390
508658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13697267
46 X = 4174927
12
Y = 2146564
63 feet Y = 654272
90 meter
Z = 17416099
59 Z = 5308427
15
XDOT = -5261
534828 XDOT = -1603
715816
YDOT = 23530
338672 feet/sec YDOT = 7172
047227 meter/sec
ZDOT = 1291
898378 ZDOT = 393
770625
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 12243
62490016
00016717 00000-0 10270-3 0 9153
2 25544 51
6450 110
9974 0018033 6
8776 353
2619 15
50157404 37734
Satellite: ISS
Catalog Number: 25544
Epoch time: 12243
62490016 = yrday
fracday
Element set: 915
Inclination: 51
6450 deg
RA of node: 110
9974 deg
Eccentricity:
0018033
Arg of perigee: 6
8776 deg
Mean anomaly: 353
2619 deg
Mean motion: 15
50157404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3773
Checksum: 301
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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