[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 8th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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
228/16:14:35
095 -4
9 9
3 9
3
N/A -5
2 0
2 224
6
000/00:29:10
190 5
9 -0
0 217
3
Coasting Arc #1 (Orbit 2584)
---------------------------------------
Vector Time (GMT): 2012/219/13:07:40
463
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5002963
06 A = 6777957
03 meter
Y = -254908
67 meter E =
0010161
Z = -4575401
21 I = 51
35818
XDOT = -2422
015562 Wp = 101
12466
YDOT = -6611
070716 meter/sec RA = 229
82100 deg
ZDOT = 3020
463859 TA = 199
17153
MA = 199
20979
Ha = 219
907 n
mi
Hp = 213
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16413920
81 X = -4977514
80
Y = -836314
52 feet Y = -310712
65 meter
Z = -15011158
82 Z = -4599643
26
XDOT = -7946
245283 XDOT = -2362
581745
YDOT = -21689
864555 feet/sec YDOT = -6637
822867 meter/sec
ZDOT = 9909
658331 ZDOT = 3008
842371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13957327
76 X = 4254193
50
Y = 8502753
54 feet Y = 2591639
28 meter
Z = -15111164
46 Z = -4605882
93
XDOT = -2658
039926 XDOT = -810
170569
YDOT = 21868
543622 feet/sec YDOT = 6665
532096 meter/sec
ZDOT = 9862
282173 ZDOT = 3006
023606
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 12219
55771654
00016717 00000-0 10270-3 0 9002
2 25544 51
6386 230
7689 0001626 14
0298 346
0900 15
54948513 25852
Satellite: ISS
Catalog Number: 25544
Epoch time: 12219
55771654 = yrday
fracday
Element set: 900
Inclination: 51
6386 deg
RA of node: 230
7689 deg
Eccentricity:
0001626
Arg of perigee: 14
0298 deg
Mean anomaly: 346
0900 deg
Mean motion: 15
54948513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2585
Checksum: 318
Coasting Arc #2 (Orbit 2600)
---------------------------------------
Vector Time (GMT): 2012/220/13:07:40
463
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5625369
36 A = 6782185
34 meter
Y = 1929979
06 meter E =
0013145
Z = 3249987
71 I = 51
39293
XDOT = 683
462961 Wp = 85
18508
YDOT = 6001
755991 meter/sec RA = 224
80767 deg
ZDOT = -4729
477500 TA = 56
96045
MA = 56
83425
Ha = 219
785 n
mi
Hp = 213
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18455936
21 X = 5587582
29
Y = 6331952
30 feet Y = 1992674
16 meter
Z = 10662689
32 Z = 3277223
45
XDOT = 2242
332548 XDOT = 639
273802
YDOT = 19690
800495 feet/sec YDOT = 6009
151826 meter/sec
ZDOT = -15516
658463 ZDOT = -4726
264629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13406264
97 X = -4086229
56
Y = -14091895
51 feet Y = -4295209
75 meter
Z = 10774910
00 Z = 3284192
57
XDOT = 5967
573832 XDOT = 1818
916504
YDOT = -17575
524618 feet/sec YDOT = -5357
019903 meter/sec
ZDOT = -15503
919099 ZDOT = -4725
594541
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 12220
58598264
00016717 00000-0 10270-3 0 9012
2 25544 51
6382 225
6350 0001709 14
6505 345
4697 15
55011540 26012
Satellite: ISS
Catalog Number: 25544
Epoch time: 12220
58598264 = yrday
fracday
Element set: 901
Inclination: 51
6382 deg
RA of node: 225
6350 deg
Eccentricity:
0001709
Arg of perigee: 14
6505 deg
Mean anomaly: 345
4697 deg
Mean motion: 15
55011540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2601
Checksum: 288
Coasting Arc #3 (Orbit 2615)
---------------------------------------
Vector Time (GMT): 2012/221/13:07:40
463
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5759874
44 A = 6785732
46 meter
Y = -3255734
30 meter E =
0009854
Z = -1488138
67 I = 51
42706
XDOT = 1289
992691 Wp = 35
90801
YDOT = -4900
703147 meter/sec RA = 219
81048 deg
ZDOT = 5755
959755 TA = 307
79143
MA = 307
88063
Ha = 219
872 n
mi
Hp = 212
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18897225
86 X = -5715811
08
Y = -10681542
99 feet Y = -3319898
41 meter
Z = -4882344
70 Z = -1516012
66
XDOT = 4232
259486 XDOT = 1316
736563
YDOT = -16078
422399 feet/sec YDOT = -4886
128186 meter/sec
ZDOT = 18884
382399 ZDOT = 5762
291329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12136778
34 X = 3699290
04
Y = 17965674
16 feet Y = 5475937
48 meter
Z = -4997095
08 Z = -1523114
58
XDOT = -9534
992603 XDOT = -2906
265745
YDOT = 11677
165357 feet/sec YDOT = 3559
200001 meter/sec
ZDOT = 18910
931729 ZDOT = 5764
051991
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 12221
54997064
00016717 00000-0 10270-3 0 9021
2 25544 51
6380 220
8232 0001667 25
3335 334
7900 15
55026151 26167
Satellite: ISS
Catalog Number: 25544
Epoch time: 12221
54997064 = yrday
fracday
Element set: 902
Inclination: 51
6380 deg
RA of node: 220
8232 deg
Eccentricity:
0001667
Arg of perigee: 25
3335 deg
Mean anomaly: 334
7900 deg
Mean motion: 15
55026151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 282
Coasting Arc #4 (Orbit 2631)
---------------------------------------
Vector Time (GMT): 2012/222/13:07:40
463
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5299176
38 A = 6786572
39 meter
Y = 4200221
26 meter E =
0010388
Z = -529884
70 I = 51
45428
XDOT = -3338
568613 Wp = 129
80255
YDOT = 3469
833390 meter/sec RA = 214
82136 deg
ZDOT = -5967
949508 TA = 55
93020
MA = 55
83164
Ha = 219
921 n
mi
Hp = 212
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17385749
28 X = 5254388
83
Y = 13780253
49 feet Y = 4259229
54 meter
Z = -1738466
88 Z = -504250
43
XDOT = -10953
309097 XDOT = -3348
130148
YDOT = 11383
967814 feet/sec YDOT = 3432
446129 meter/sec
ZDOT = -19579
886837 ZDOT = -5984
191136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9784145
95 X = -2982207
68
Y = -19919478
80 feet Y = -6071457
14 meter
Z = -1633029
02 Z = -497747
25
XDOT = 13221
606636 XDOT = 4029
945703
YDOT = -4907
714708 feet/sec YDOT = -1495
871443 meter/sec
ZDOT = -19647
214281 ZDOT = -5988
470913
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 12222
57821025
00016717 00000-0 10270-3 0 9039
2 25544 51
6383 215
6891 0001810 22
8820 337
2413 15
55040316 26328
Satellite: ISS
Catalog Number: 25544
Epoch time: 12222
57821025 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 215
6891 deg
Eccentricity:
0001810
Arg of perigee: 22
8820 deg
Mean anomaly: 337
2413 deg
Mean motion: 15
55040316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2632
Checksum: 271
Coasting Arc #5 (Orbit 2647)
---------------------------------------
Vector Time (GMT): 2012/223/13:07:40
463
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4249749
00 A = 6784048
53 meter
Y = -4679212
50 meter E =
0014857
Z = 2442777
61 I = 51
47168
XDOT = 5182
505906 Wp = 70
00302
YDOT = -1915
771555 meter/sec RA = 209
83238 deg
ZDOT = 5325
022383 TA = 317
43469
MA = 317
54975
Ha = 219
820 n
mi
Hp = 212
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13942746
07 X = -4208975
59
Y = -15351747
06 feet Y = -4726507
95 meter
Z = 8014362
24 Z = 2422231
57
XDOT = 17002
972131 XDOT = 5177
675747
YDOT = -6285
339748 feet/sec YDOT = -1857
844750 meter/sec
ZDOT = 17470
545875 ZDOT = 5350
186748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6375803
77 X = 1943344
99
Y = 19767935
05 feet Y = 6025266
60 meter
Z = 7929954
49 Z = 2417050
13
XDOT = -16539
740861 XDOT = -5041
313015
YDOT = -1743
901872 feet/sec YDOT = -531
541291 meter/sec
ZDOT = 17574
575944 ZDOT = 5356
730748
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 12223
60643386
00016717 00000-0 10270-3 0 9047
2 25544 51
6381 210
5563 0001571 25
7962 334
3269 15
55093531 26480
Satellite: ISS
Catalog Number: 25544
Epoch time: 12223
60643386 = yrday
fracday
Element set: 904
Inclination: 51
6381 deg
RA of node: 210
5563 deg
Eccentricity:
0001571
Arg of perigee: 25
7962 deg
Mean anomaly: 334
3269 deg
Mean motion: 15
55093531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2648
Checksum: 301
Coasting Arc #6 (Orbit 2662)
---------------------------------------
Vector Time (GMT): 2012/224/13:07:40
463
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2643775
01 A = 6779700
79 meter
Y = 4766912
59 meter E =
0008459
Z = -4040633
15 I = 51
48419
XDOT = -6590
892585 Wp = 63
88597
YDOT = 360
903916 meter/sec RA = 204
83220 deg
ZDOT = -3889
323604 TA = 165
67412
MA = 165
65012
Ha = 219
905 n
mi
Hp = 212
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8673802
51 X = 2609902
19
Y = 15639476
99 feet Y = 4796287
70 meter
Z = -13256670
45 Z = -4027872
02
XDOT = -21623
663335 XDOT = -6575
545175
YDOT = 1184
067966 feet/sec YDOT = 287
286438 meter/sec
ZDOT = -12760
248046 ZDOT = -3921
304241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1797368
71 X = -547837
98
Y = -17832016
97 feet Y = -5435198
77 meter
Z = -13204394
67 Z = -4024699
50
XDOT = 18931
733173 XDOT = 5770
392271
YDOT = 7631
802606 feet/sec YDOT = 2326
173434 meter/sec
ZDOT = -12892
295656 ZDOT = -3929
571716
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 12224
57038321
00016717 00000-0 10270-3 0 9052
2 25544 51
6383 205
7430 0001827 28
5218 331
6035 15
55079412 26630
Satellite: ISS
Catalog Number: 25544
Epoch time: 12224
57038321 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 205
7430 deg
Eccentricity:
0001827
Arg of perigee: 28
5218 deg
Mean anomaly: 331
6035 deg
Mean motion: 15
55079412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2663
Checksum: 286
Coasting Arc #7 (Orbit 2678)
---------------------------------------
Vector Time (GMT): 2012/225/13:07:40
463
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -660962
55 A = 6775702
58 meter
Y = -4489262
33 meter E =
0005798
Z = 5027581
25 I = 51
49956
XDOT = 7360
685106 Wp = 107
25971
YDOT = 1047
171882 meter/sec RA = 199
82100 deg
ZDOT = 1899
240320 TA = 324
28412
MA = 324
32289
Ha = 219
796 n
mi
Hp = 212
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2168512
30 X = -635136
11
Y = -14728550
94 feet Y = -4496509
45 meter
Z = 16494689
15 Z = 5024432
89
XDOT = 24149
229349 XDOT = 7339
202388
YDOT = 3435
603288 feet/sec YDOT = 1129
363434 meter/sec
ZDOT = 6231
103413 ZDOT = 1934
945608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3539219
16 X = -1078754
00
Y = 14474902
32 feet Y = 4411950
23 meter
Z = 16482067
81 Z = 5023734
27
XDOT = -19905
068737 XDOT = -6067
064951
YDOT = -12142
900710 feet/sec YDOT = -3701
156136 meter/sec
ZDOT = 6378
426380 ZDOT = 1944
144360
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 12225
59857868
00016717 00000-0 10270-3 0 9061
2 25544 51
6384 200
6101 0001726 26
6494 333
4748 15
55123564 26799
Satellite: ISS
Catalog Number: 25544
Epoch time: 12225
59857868 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 200
6101 deg
Eccentricity:
0001726
Arg of perigee: 26
6494 deg
Mean anomaly: 333
4748 deg
Mean motion: 15
55123564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2679
Checksum: 324
Coasting Arc #8 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2012/226/13:07:40
463
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1497331
52 A = 6774534
80 meter
Y = 3961798
25 meter E =
0015769
Z = -5300983
71 I = 51
52475
XDOT = -7310
752055 Wp = 87
28618
YDOT = -2248
985560 meter/sec RA = 194
80129 deg
ZDOT = 385
915667 TA = 186
39414
MA = 186
41429
Ha = 219
868 n
mi
Hp = 212
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4912504
98 X = -1515771
30
Y = 12998025
76 feet Y = 3944951
29 meter
Z = -17391678
83 Z = -5308302
18
XDOT = -23985
407005 XDOT = -7286
934745
YDOT = -7378
561550 feet/sec YDOT = -2330
605782 meter/sec
ZDOT = 1266
127516 ZDOT = 350
458675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9237508
73 X = 2815592
66
Y = -10328906
06 feet Y = -3148250
57 meter
Z = -17422227
28 Z = -5310294
87
XDOT = 18862
051663 XDOT = 5749
153347
YDOT = 14989
527515 feet/sec YDOT = 4568
807987 meter/sec
ZDOT = 1119
910206 ZDOT = 341
348631
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 12226
56249987
00016717 00000-0 10270-3 0 9077
2 25544 51
6385 195
7966 0001811 31
2579 328
8681 15
55112005 26943
Satellite: ISS
Catalog Number: 25544
Epoch time: 12226
56249987 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 195
7966 deg
Eccentricity:
0001811
Arg of perigee: 31
2579 deg
Mean anomaly: 328
8681 deg
Mean motion: 15
55112005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2694
Checksum: 334
Coasting Arc #9 (Orbit 2709)
---------------------------------------
Vector Time (GMT): 2012/227/13:07:40
463
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3567945
26 A = 6776625
56 meter
Y = -3225619
82 meter E =
0009061
Z = 4769237
15 I = 51
56244
XDOT = 6444
808937 Wp = 56
39753
YDOT = 3229
011356 meter/sec RA = 189
78637 deg
ZDOT = -2629
051081 TA = 59
58777
MA = 59
49826
Ha = 219
762 n
mi
Hp = 212
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11705857
14 X = 3580582
18
Y = -10582742
18 feet Y = -3185650
33 meter
Z = 15647103
50 Z = 4786600
33
XDOT = 21144
386277 XDOT = 6420
993572
YDOT = 10593
869277 feet/sec YDOT = 3300
948143 meter/sec
ZDOT = -8625
495674 ZDOT = -2597
800813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14583390
50 X = -4445017
43
Y = 5838565
53 feet Y = 1779594
77 meter
Z = 15719072
67 Z = 4791173
35
XDOT = -15710
259803 XDOT = -4788
487188
YDOT = -16290
214680 feet/sec YDOT = -4965
257434 meter/sec
ZDOT = -8496
710734 ZDOT = -2589
797432
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 12227
59066693
00016717 00000-0 10270-3 0 9083
2 25544 51
6390 190
6632 0001821 34
8743 325
2529 15
55141529 27100
Satellite: ISS
Catalog Number: 25544
Epoch time: 12227
59066693 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 190
6632 deg
Eccentricity:
0001821
Arg of perigee: 34
8743 deg
Mean anomaly: 325
2529 deg
Mean motion: 15
55141529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2710
Checksum: 307
Coasting Arc #10 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2012/228/13:07:40
463
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5267545
45 A = 6780905
81 meter
Y = 2381266
02 meter E =
0006380
Z = -3549164
12 I = 51
60725
XDOT = -4799
802983 Wp = 82
78089
YDOT = -3959
754749 meter/sec RA = 184
78424 deg
ZDOT = 4474
642886 TA = 235
33998
MA = 235
40013
Ha = 219
803 n
mi
Hp = 212
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17281973
25 X = -5276541
08
Y = 7812552
55 feet Y = 2322310
80 meter
Z = -11644239
23 Z = -3574774
90
XDOT = -15747
385115 XDOT = -4776
903812
YDOT = -12991
321354 feet/sec YDOT = -4013
301158 meter/sec
ZDOT = 14680
586895 ZDOT = 4451
381705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18832103
52 X = 5740025
15
Y = -1604790
09 feet Y = -489140
02 meter
Z = -11750208
93 Z = -3581463
68
XDOT = 10462
172514 XDOT = 3188
870182
YDOT = 16166
333655 feet/sec YDOT = 4927
498498 meter/sec
ZDOT = 14584
838714 ZDOT = 4445
458840
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 12228
55455896
00016717 00000-0 10270-3 0 9098
2 25544 51
6391 185
8501 0001828 35
3532 324
7742 15
55153906 27250
Satellite: ISS
Catalog Number: 25544
Epoch time: 12228
55455896 = yrday
fracday
Element set: 909
Inclination: 51
6391 deg
RA of node: 185
8501 deg
Eccentricity:
0001828
Arg of perigee: 35
3532 deg
Mean anomaly: 324
7742 deg
Mean motion: 15
55153906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2725
Checksum: 322
Coasting Arc #11 (Orbit 2727)
---------------------------------------
Vector Time (GMT): 2012/228/16:29:10
190
Vector Time (MET): N/A
Weight (LBS) : 953457
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6156360
40 A = 6791848
80 meter
Y = -2026470
72 meter E =
0016659
Z = 1992701
42 I = 51
62599
XDOT = 3189
045981 Wp = 32
54488
YDOT = -4196
951685 meter/sec RA = 184
12913 deg
ZDOT = 5576
401092 TA = 349
47050
MA = 349
50534
Ha = 224
606 n
mi
Hp = 217
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20198032
81 X = -6142922
33
Y = -6648525
97 feet Y = -2095239
85 meter
Z = 6537734
33 Z = 1962827
34
XDOT = 10462
749280 XDOT = 3208
651811
YDOT = -13769
526527 feet/sec YDOT = -4161
180230 meter/sec
ZDOT = 18295
279172 ZDOT = 5591
940584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20773606
06 X = 6331795
13
Y = -4713459
08 feet Y = -1436662
33 meter
Z = 6414514
17 Z = 1955143
92
XDOT = -2133
931342 XDOT = -650
422273
YDOT = 15616
977472 feet/sec YDOT = 4760
054733 meter/sec
ZDOT = 18359
801904 ZDOT = 5596
067620
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 12228
74743703
00016717 00000-0 10270-3 0 9108
2 25544 51
6411 184
8889 0009705 335
6336 24
4355 15
52707477 27283
Satellite: ISS
Catalog Number: 25544
Epoch time: 12228
74743703 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 184
8889 deg
Eccentricity:
0009705
Arg of perigee: 335
6336 deg
Mean anomaly: 24
4355 deg
Mean motion: 15
52707477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 325
Coasting Arc #12 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2012/229/16:29:10
190
Vector Time (MET): N/A
Weight (LBS) : 953457
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5562364
87 A = 6789442
08 meter
Y = 2370107
34 meter E =
0007612
Z = -3098346
01 I = 51
64905
XDOT = -4398
109875 Wp = 5
16356
YDOT = 3928
968647 meter/sec RA = 179
15995 deg
ZDOT = -4883
820871 TA = 210
39449
MA = 210
43864
Ha = 224
608 n
mi
Hp = 217
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18249228
57 X = 5550499
18
Y = 7775942
71 feet Y = 2432242
78 meter
Z = -10165177
21 Z = -3071353
72
XDOT = -14429
494342 XDOT = -4417
993542
YDOT = 12890
317082 feet/sec YDOT = 3879
675011 meter/sec
ZDOT = -16023
034355 ZDOT = -4905
234580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19651382
03 X = -5989741
24
Y = 3094071
45 feet Y = 943072
98 meter
Z = -10053872
99 Z = -3064420
49
XDOT = 5563
502954 XDOT = 1695
755700
YDOT = -17087
934143 feet/sec YDOT = -5208
402327 meter/sec
ZDOT = -16111
803067 ZDOT = -4910
877575
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
71283540
00016717 00000-0 10270-3 0 9115
2 25544 51
6417 180
0863 0009666 337
7412 22
3319 15
52725216 27438
Satellite: ISS
Catalog Number: 25544
Epoch time: 12229
71283540 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 180
0863 deg
Eccentricity:
0009666
Arg of perigee: 337
7412 deg
Mean anomaly: 22
3319 deg
Mean motion: 15
52725216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 297
Coasting Arc #13 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2012/230/16:29:10
190
Vector Time (MET): N/A
Weight (LBS) : 953457
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4727275
29 A = 6786564
02 meter
Y = -2719133
50 meter E =
0010582
Z = 4027312
31 I = 51
67034
XDOT = 5465
000903 Wp = 47
57108
YDOT = -3679
979668 meter/sec RA = 174
18665 deg
ZDOT = 3930
610158 TA = 1
65395
MA = 1
65045
Ha = 224
870 n
mi
Hp = 216
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15509433
37 X = -4716081
42
Y = -8921041
67 feet Y = -2771934
11 meter
Z = 13212966
90 Z = 4004375
16
XDOT = 17929
792988 XDOT = 5486
651387
YDOT = -12073
424107 feet/sec YDOT = -3618
745436 meter/sec
ZDOT = 12895
702618 ZDOT = 3957
211071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17934169
05 X = 5466334
73
Y = -991149
90 feet Y = -302102
49 meter
Z = 13118429
96 Z = 3998497
45
XDOT = -8488
442665 XDOT = -2587
277324
YDOT = 18530
548030 feet/sec YDOT = 5648
111040 meter/sec
ZDOT = 13005
885521 ZDOT = 3964
193907
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
74258136
00016717 00000-0 10270-3 0 9124
2 25544 51
6420 174
9625 0009740 342
8052 17
2769 15
52747711 27593
Satellite: ISS
Catalog Number: 25544
Epoch time: 12230
74258136 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 174
9625 deg
Eccentricity:
0009740
Arg of perigee: 342
8052 deg
Mean anomaly: 17
2769 deg
Mean motion: 15
52747711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 311
Coasting Arc #14 (Orbit 2773)
---------------------------------------
Vector Time (GMT): 2012/231/16:29:10
190
Vector Time (MET): N/A
Weight (LBS) : 953457
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3749298
50 A = 6783817
20 meter
Y = 3098527
59 meter E =
0015139
Z = -4741358
28 I = 51
69157
XDOT = -6287
171116 Wp = 30
99770
YDOT = 3401
624715 meter/sec RA = 169
21035 deg
ZDOT = -2739
909483 TA = 211
82029
MA = 211
91184
Ha = 224
837 n
mi
Hp = 216
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12300848
08 X = 3737403
52
Y = 10165772
92 feet Y = 3140387
82 meter
Z = -15555637
41 Z = -4723173
72
XDOT = -20627
201823 XDOT = -6311
431872
YDOT = 11160
186074 feet/sec YDOT = 3331
181863 meter/sec
ZDOT = -8989
204340 ZDOT = -2770
510863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15958687
32 X = -4864207
90
Y = -1515963
37 feet Y = -462065
64 meter
Z = -15480756
18 Z = -4718534
48
XDOT = 10730
669959 XDOT = 3270
708204
YDOT = -19577
667841 feet/sec YDOT = -5967
273158 meter/sec
ZDOT = -9115
899924 ZDOT = -2778
526297
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
70795312
00016717 00000-0 10270-3 0 9134
2 25544 51
6418 170
1596 0009809 345
0532 15
0329 15
52792858 27746
Satellite: ISS
Catalog Number: 25544
Epoch time: 12231
70795312 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 170
1596 deg
Eccentricity:
0009809
Arg of perigee: 345
0532 deg
Mean anomaly: 15
0329 deg
Mean motion: 15
52792858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2774
Checksum: 314
Coasting Arc #15 (Orbit 2789)
---------------------------------------
Vector Time (GMT): 2012/232/16:29:10
190
Vector Time (MET): N/A
Weight (LBS) : 953457
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2607732
97 A = 6781891
62 meter
Y = -3511872
29 meter E =
0007226
Z = 5179619
27 I = 51
71522
XDOT = 6885
581389 Wp = 15
56266
YDOT = -3080
072954 meter/sec RA = 164
23087 deg
ZDOT = 1384
626916 TA = 61
17581
MA = 61
10328
Ha = 224
991 n
mi
Hp = 216
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8555554
37 X = -2593429
78
Y = -11521890
71 feet Y = -3540953
29 meter
Z = 16993501
56 Z = 5166986
15
XDOT = 22590
490120 XDOT = 6912
785529
YDOT = -10105
226228 feet/sec YDOT = -3002
921905 meter/sec
ZDOT = 4542
739226 ZDOT = 1418
142596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13694473
07 X = 4174075
39
Y = 4491626
20 feet Y = 1369047
66 meter
Z = 16941584
12 Z = 5163794
84
XDOT = -12391
140118 XDOT = -3776
819508
YDOT = 20200
476985 feet/sec YDOT = 6157
105385 meter/sec
ZDOT = 4681
459204 ZDOT = 1426
908765
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
73767104
00016717 00000-0 10270-3 0 9147
2 25544 51
6421 165
0361 0009743 349
4386 10
6560 15
52797501 27901
Satellite: ISS
Catalog Number: 25544
Epoch time: 12232
73767104 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 165
0361 deg
Eccentricity:
0009743
Arg of perigee: 349
4386 deg
Mean anomaly: 10
6560 deg
Mean motion: 15
52797501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2790
Checksum: 302
Coasting Arc #16 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2012/233/16:29:10
190
Vector Time (MET): N/A
Weight (LBS) : 953457
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1447047
48 A = 6781091
11 meter
Y = 3947974
84 meter E =
0016661
Z = -5331725
35 I = 51
74090
XDOT = -7172
577166 Wp = 54
76318
YDOT = 2678
490187 meter/sec RA = 159
25026 deg
ZDOT = 46
151879 TA = 215
62099
MA = 215
73230
Ha = 225
007 n
mi
Hp = 216
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4747531
09 X = 1428692
96
Y = 12952673
36 feet Y = 3964053
67 meter
Z = -17492537
24 Z = -5324740
54
XDOT = -23532
077317 XDOT = -7202
219707
YDOT = 8787
697463 feet/sec YDOT = 2598
116226 meter/sec
ZDOT = 151
416926 ZDOT = 11
235951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11526375
49 X = -3513239
25
Y = -7645347
90 feet Y = -2330302
04 meter
Z = -17463990
99 Z = -5323024
45
XDOT = 13352
965230 XDOT = 4069
983802
YDOT = -20076
077677 feet/sec YDOT = -6119
188476 meter/sec
ZDOT = 6
932398 ZDOT = 2
112995
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
70301662
00016717 00000-0 10270-3 0 9159
2 25544 51
6409 160
2323 0009799 352
2685 7
8315 15
52846825 28054
Satellite: ISS
Catalog Number: 25544
Epoch time: 12233
70301662 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 160
2323 deg
Eccentricity:
0009799
Arg of perigee: 352
2685 deg
Mean anomaly: 7
8315 deg
Mean motion: 15
52846825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 307
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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