Date:
February 3rd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
040/21:39:00
434 0
5 1
9 1
9
N/A 1
7 0
1 191
5
000/00:05:00
869 -0
8 -0
0 188
5
Coasting Arc #1 (Orbit 1940)
---------------------------------------
Vector Time (GMT): 2011/031/13:58:03
031
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5572277
26 A = 6736861
59 meter
Y = 3657549
63 meter E =
0009845
Z = 940481
56 I = 51
87945
XDOT = -1926
884802 Wp = 45
61789
YDOT = -4476
044684 meter/sec RA = 140
36312 deg
ZDOT = 5959
391219 TA = 324
61168
MA = 324
67697
Ha = 191
412 n
mi
Hp = 188
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18281749
53 X = -5617331
07
Y = 11999834
73 feet Y = 3594985
09 meter
Z = 3085569
42 Z = 913303
05
XDOT = -6321
800530 XDOT = -1905
638371
YDOT = -14685
185971 feet/sec YDOT = -4497
473824 meter/sec
ZDOT = 19551
808462 ZDOT = 5950
082046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21370747
77 X = -6513803
92
Y = 4708978
55 feet Y = 1435296
66 meter
Z = 2975869
46 Z = 907045
01
XDOT = -453
035391 XDOT = -138
085187
YDOT = -14455
687658 feet/sec YDOT = -4406
093598 meter/sec
ZDOT = 19514
313490 ZDOT = 5947
962752
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 11031
64379615
00016717 00000-0 10270-3 0 9004
2 25544 51
6443 141
0293 0004226 257
3204 102
7486 15
72231114 19412
Satellite: ISS
Catalog Number: 25544
Epoch time: 11031
64379615 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 141
0293 deg
Eccentricity:
0004226
Arg of perigee: 257
3204 deg
Mean anomaly: 102
7486 deg
Mean motion: 15
72231114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1941
Checksum: 270
Coasting Arc #2 (Orbit 1955)
---------------------------------------
Vector Time (GMT): 2011/032/13:58:03
031
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2568505
66 A = 6725136
59 meter
Y = 3292307
36 meter E =
0010774
Z = -5280933
89 I = 51
86244
XDOT = -5691
658442 Wp = 97
86052
YDOT = 5152
795452 meter/sec RA = 135
24530 deg
ZDOT = 443
476954 TA = 176
34793
MA = 176
34006
Ha = 191
274 n
mi
Hp = 188
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8426855
84 X = 2557152
53
Y = 10801533
33 feet Y = 3320966
67 meter
Z = -17325898
60 Z = -5268483
95
XDOT = -18673
420084 XDOT = -5751
009216
YDOT = 16905
496890 feet/sec YDOT = 5088
816025 meter/sec
ZDOT = 1454
976884 ZDOT = 415
683842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4357529
76 X = 1328175
07
Y = 13055019
65 feet Y = 3979169
99 meter
Z = -17275710
70 Z = -5265636
62
XDOT = -22358
985502 XDOT = -6815
018781
YDOT = 9242
837260 feet/sec YDOT = 2817
216797 meter/sec
ZDOT = 1342
763297 ZDOT = 409
274253
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 11032
59719439
00016717 00000-0 10270-3 0 9012
2 25544 51
6437 136
1467 0004293 262
2011 97
8664 15
72253933 19569
Satellite: ISS
Catalog Number: 25544
Epoch time: 11032
59719439 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 136
1467 deg
Eccentricity:
0004293
Arg of perigee: 262
2011 deg
Mean anomaly: 97
8664 deg
Mean motion: 15
72253933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1956
Checksum: 315
Coasting Arc #3 (Orbit 1971)
---------------------------------------
Vector Time (GMT): 2011/033/13:58:03
031
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4241271
96 A = 6736998
50 meter
Y = -5224133
92 meter E =
0010176
Z = 160600
32 I = 51
92396
XDOT = 3780
591094 Wp = 150
06000
YDOT = 2878
326357 meter/sec RA = 130
14318 deg
ZDOT = -6057
600441 TA = 28
20309
MA = 28
14801
Ha = 191
247 n
mi
Hp = 187
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13914934
26 X = 4298593
85
Y = -17139546
98 feet Y = -5176384
95 meter
Z = 526903
95 Z = 181342
85
XDOT = 12403
514087 XDOT = 3777
549848
YDOT = 9443
327944 feet/sec YDOT = 2920
586319 meter/sec
ZDOT = -19874
017196 ZDOT = -6039
242291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18704478
32 X = 5701124
99
Y = -11723338
10 feet Y = -3573273
45 meter
Z = 610678
68 Z = 186134
86
XDOT = 7943
144099 XDOT = 2421
070321
YDOT = 11618
953533 feet/sec YDOT = 3541
457037 meter/sec
ZDOT = -19799
977508 ZDOT = -6035
033145
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 11033
61413699
00016717 00000-0 10270-3 0 9026
2 25544 51
6439 130
9382 0004109 267
1305 92
9387 15
72302222 19727
Satellite: ISS
Catalog Number: 25544
Epoch time: 11033
61413699 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 130
9382 deg
Eccentricity:
0004109
Arg of perigee: 267
1305 deg
Mean anomaly: 92
9387 deg
Mean motion: 15
72302222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1972
Checksum: 297
Coasting Arc #4 (Orbit 1987)
---------------------------------------
Vector Time (GMT): 2011/034/13:58:03
031
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3884200
10 A = 6725065
61 meter
Y = -1624178
17 meter E =
0002074
Z = 5245552
63 I = 51
90312
XDOT = 3860
454705 Wp = 221
86470
YDOT = -6609
993330 meter/sec RA = 125
04865 deg
ZDOT = 810
592304 TA = 220
43770
MA = 220
45312
Ha = 191
258 n
mi
Hp = 187
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12743438
65 X = -3891230
65
Y = -5328668
53 feet Y = -1667652
94 meter
Z = 17209818
35 Z = 5226666
75
XDOT = 12665
533808 XDOT = 3930
144402
YDOT = -21686
329822 feet/sec YDOT = -6566
433735 meter/sec
ZDOT = 2659
423569 ZDOT = 829
515050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10591094
78 X = -3228165
69
Y = -9013066
08 feet Y = -2747182
54 meter
Z = 17133625
88 Z = 5222329
17
XDOT = 18036
885221 XDOT = 5497
642615
YDOT = -15985
659405 feet/sec YDOT = -4872
428987 meter/sec
ZDOT = 2735
881093 ZDOT = 833
896557
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 11034
63106112
00016717 00000-0 10270-3 0 9039
2 25544 51
6441 125
7293 0004210 271
5080 88
5600 15
72338440 19882
Satellite: ISS
Catalog Number: 25544
Epoch time: 11034
63106112 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 125
7293 deg
Eccentricity:
0004210
Arg of perigee: 271
5080 deg
Mean anomaly: 88
5600 deg
Mean motion: 15
72338440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1988
Checksum: 275
Coasting Arc #5 (Orbit 2002)
---------------------------------------
Vector Time (GMT): 2011/035/13:58:03
031
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2422816
82 A = 6736284
73 meter
Y = 6156267
02 meter E =
0007976
Z = -1241711
35 I = 51
95673
XDOT = -4895
629896 Wp = 10
63999
YDOT = -740
565779 meter/sec RA = 119
92758 deg
ZDOT = 5894
296587 TA = 335
81383
MA = 335
85126
Ha = 191
242 n
mi
Hp = 187
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7948874
08 X = -2485445
47
Y = 20197726
43 feet Y = 6128823
41 meter
Z = -4073856
15 Z = -1253633
28
XDOT = -16061
777874 XDOT = -4915
617424
YDOT = -2429
677753 feet/sec YDOT = -795
423304 meter/sec
ZDOT = 19338
243396 ZDOT = 5870
465835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13449393
69 X = -4099375
20
Y = 17025025
43 feet Y = 5189227
75 meter
Z = -4122059
54 Z = -1256403
75
XDOT = -13532
534443 XDOT = -4124
716498
YDOT = -6042
254295 feet/sec YDOT = -1841
679109 meter/sec
ZDOT = 19242
077400 ZDOT = 5864
985192
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 11035
58441377
00016717 00000-0 10270-3 0 9040
2 25544 51
6435 120
8458 0004131 278
8348 81
2347 15
72316098 20035
Satellite: ISS
Catalog Number: 25544
Epoch time: 11035
58441377 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 120
8458 deg
Eccentricity:
0004131
Arg of perigee: 278
8348 deg
Mean anomaly: 81
2347 deg
Mean motion: 15
72316098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2003
Checksum: 299
Coasting Arc #6 (Orbit 2018)
---------------------------------------
Vector Time (GMT): 2011/036/13:58:03
031
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4487739
24 A = 6726108
94 meter
Y = -363000
88 meter E =
0009513
Z = -5005453
12 I = 51
93725
XDOT = -1637
099626 Wp = 64
45038
YDOT = 7245
754038 meter/sec RA = 114
85392 deg
ZDOT = -1992
157307 TA = 186
33591
MA = 186
34795
Ha = 191
249 n
mi
Hp = 187
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14723553
93 X = 4515779
74
Y = -1190947
76 feet Y = -312659
66 meter
Z = -16422090
30 Z = -4983584
19
XDOT = -5371
061764 XDOT = -1708
324076
YDOT = 23772
158917 feet/sec YDOT = 7227
048694 meter/sec
ZDOT = -6535
949169 ZDOT = -2000
283361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14580763
69 X = 4444216
77
Y = 2914453
74 feet Y = 888325
50 meter
Z = -16333821
86 Z = -4978548
90
XDOT = -11427
965631 XDOT = -3483
243924
YDOT = 20338
426792 feet/sec YDOT = 6199
152486 meter/sec
ZDOT = -6568
854111 ZDOT = -2002
186733
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 11036
60130633
00016717 00000-0 10270-3 0 9055
2 25544 51
6437 115
6364 0004022 281
6500 78
4211 15
72359154 20191
Satellite: ISS
Catalog Number: 25544
Epoch time: 11036
60130633 = yrday
fracday
Element set: 905
Inclination: 51
6437 deg
RA of node: 115
6364 deg
Eccentricity:
0004022
Arg of perigee: 281
6500 deg
Mean anomaly: 78
4211 deg
Mean motion: 15
72359154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2019
Checksum: 270
Coasting Arc #7 (Orbit 2034)
---------------------------------------
Vector Time (GMT): 2011/037/13:58:03
031
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 426452
88 A = 6734514
33 meter
Y = -6338341
85 meter E =
0009994
Z = 2221473
38 I = 51
97778
XDOT = 5141
981307 Wp = 108
61567
YDOT = -1589
317457 meter/sec RA = 109
71745 deg
ZDOT = -5504
835919 TA = 46
61171
MA = 46
52853
Ha = 191
268 n
mi
Hp = 187
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1399123
61 X = 486506
47
Y = -20795084
82 feet Y = -6333237
13 meter
Z = 7288298
50 Z = 2223691
17
XDOT = 16870
017411 XDOT = 5186
112032
YDOT = -5214
296118 feet/sec YDOT = -1531
570196 meter/sec
ZDOT = -18060
485300 ZDOT = -5479
749535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6661993
44 X = 2030575
60
Y = -19745351
99 feet Y = -6018383
29 meter
Z = 7297349
69 Z = 2224232
19
XDOT = 16307
987024 XDOT = 4970
674445
YDOT = -1155
496269 feet/sec YDOT = -352
195263 meter/sec
ZDOT = -17959
208054 ZDOT = -5473
966615
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 11037
61818034
00016717 00000-0 10270-3 0 9066
2 25544 51
6434 110
4270 0004021 288
5714 71
5011 15
72426004 20358
Satellite: ISS
Catalog Number: 25544
Epoch time: 11037
61818034 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 110
4270 deg
Eccentricity:
0004021
Arg of perigee: 288
5714 deg
Mean anomaly: 71
5011 deg
Mean motion: 15
72426004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2035
Checksum: 258
Coasting Arc #8 (Orbit 2050)
---------------------------------------
Vector Time (GMT): 2011/038/13:58:03
031
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4319482
38 A = 6727685
35 meter
Y = 2387546
98 meter E =
0004803
Z = 4569323
55 I = 51
96329
XDOT = -639
520504 Wp = 114
96284
YDOT = -7033
509872 meter/sec RA = 104
65915 deg
ZDOT = 3066
095540 TA = 304
64262
MA = 304
68789
Ha = 191
531 n
mi
Hp = 187
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14171530
12 X = -4368055
83
Y = 7833159
38 feet Y = 2338972
52 meter
Z = 14991218
98 Z = 4548221
86
XDOT = -2098
164382 XDOT = -575
717164
YDOT = -23075
819790 feet/sec YDOT = -7040
304503 meter/sec
ZDOT = 10059
368571 ZDOT = 3063
144089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15727186
96 X = -4793646
58
Y = 4170593
03 feet Y = 1271196
76 meter
Z = 14906006
92 Z = 4543350
91
XDOT = 3764
015513 XDOT = 1147
271928
YDOT = -21769
569840 feet/sec YDOT = -6635
364887 meter/sec
ZDOT = 10047
574465 ZDOT = 3062
500697
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 11038
63503893
00016717 00000-0 10270-3 0 9074
2 25544 51
6427 105
2172 0003841 293
1309 66
9448 15
72428757 20511
Satellite: ISS
Catalog Number: 25544
Epoch time: 11038
63503893 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 105
2172 deg
Eccentricity:
0003841
Arg of perigee: 293
1309 deg
Mean anomaly: 66
9448 deg
Mean motion: 15
72428757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2051
Checksum: 309
Coasting Arc #9 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2011/039/13:58:03
031
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1493382
52 A = 6732332
01 meter
Y = 5781597
91 meter E =
0003072
Z = -3106650
77 I = 51
98715
XDOT = -4533
778474 Wp = 19
20450
YDOT = 3809
841119 meter/sec RA = 99
51222 deg
ZDOT = 4915
050690 TA = 304
93617
MA = 304
96502
Ha = 191
455 n
mi
Hp = 187
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4899548
96 X = 1443711
89
Y = 18968497
08 feet Y = 5798019
98 meter
Z = -10192423
79 Z = -3099516
91
XDOT = -14874
601294 XDOT = -4599
919882
YDOT = 12499
478737 feet/sec YDOT = 3758
772031 meter/sec
ZDOT = 16125
494389 ZDOT = 4892
865192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 585729
84 X = 178530
46
Y = 19597203
48 feet Y = 5973227
62 meter
Z = -10163734
58 Z = -3097906
30
XDOT = -15961
065888 XDOT = -4864
932883
YDOT = 8786
604464 feet/sec YDOT = 2678
157041 meter/sec
ZDOT = 16035
875959 ZDOT = 4887
734992
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 11039
58832784
00016717 00000-0 10270-3 0 9084
2 25544 51
6438 100
3333 0003812 297
6696 62
4079 15
72481705 20663
Satellite: ISS
Catalog Number: 25544
Epoch time: 11039
58832784 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 100
3333 deg
Eccentricity:
0003812
Arg of perigee: 297
6696 deg
Mean anomaly: 62
4079 deg
Mean motion: 15
72481705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2066
Checksum: 321
Coasting Arc #10 (Orbit 2081)
---------------------------------------
Vector Time (GMT): 2011/040/13:58:03
031
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3458220
00 A = 6729640
06 meter
Y = -4173693
22 meter E =
0005409
Z = -3994654
28 I = 51
98186
XDOT = 2656
578612 Wp = 38
53001
YDOT = 6018
030029 meter/sec RA = 94
46240 deg
ZDOT = -3986
666334 TA = 190
32644
MA = 190
33756
Ha = 191
513 n
mi
Hp = 187
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11345866
15 X = 3524039
02
Y = -13693219
24 feet Y = -4134653
41 meter
Z = -13105821
12 Z = -3977694
52
XDOT = 8715
809095 XDOT = 2608
452627
YDOT = 19744
193007 feet/sec YDOT = 6047
468304 meter/sec
ZDOT = -13079
613956 ZDOT = -3973
877931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14013226
61 X = 4271231
47
Y = -11029699
85 feet Y = -3361852
51 meter
Z = -13037280
40 Z = -3973763
07
XDOT = 3708
007684 XDOT = 1130
200742
YDOT = 20115
361205 feet/sec YDOT = 6131
162095 meter/sec
ZDOT = -13028
113222 ZDOT = -3970
968910
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 11040
60515262
00016717 00000-0 10270-3 0 9099
2 25544 51
6436 95
1233 0003898 302
5779 57
5006 15
72486588 20820
Satellite: ISS
Catalog Number: 25544
Epoch time: 11040
60515262 = yrday
fracday
Element set: 909
Inclination: 51
6436 deg
RA of node: 95
1233 deg
Eccentricity:
0003898
Arg of perigee: 302
5779 deg
Mean anomaly: 57
5006 deg
Mean motion: 15
72486588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2082
Checksum: 313
Coasting Arc #11 (Orbit 2086)
---------------------------------------
Vector Time (GMT): 2011/040/21:41:30
869
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4042427
94 A = 6726557
48 meter
Y = -1883010
66 meter E =
0009463
Z = -5044115
60 I = 51
96958
XDOT = 1101
583511 Wp = 59
04253
YDOT = 7378
375070 meter/sec RA = 92
81124 deg
ZDOT = -1869
401793 TA = 192
97115
MA = 192
99551
Ha = 191
538 n
mi
Hp = 188
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13262558
86 X = 4087686
72
Y = -6177856
49 feet Y = -1837552
85 meter
Z = -16548935
68 Z = -5024367
80
XDOT = 3614
119131 XDOT = 1028
076336
YDOT = 24207
267290 feet/sec YDOT = 7390
282600 meter/sec
ZDOT = -6133
207983 ZDOT = -1864
229094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9272432
78 X = -2826237
51
Y = -11433135
91 feet Y = -3484819
83 meter
Z = -16469184
69 Z = -5019807
49
XDOT = 21733
891061 XDOT = 6624
489995
YDOT = -8811
231861 feet/sec YDOT = -2685
663471 meter/sec
ZDOT = -6112
478731 ZDOT = -1863
083517
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 11040
92290982
00016717 00000-0 10270-3 0 9105
2 25544 51
6444 93
4959 0005011 289
6916 70
3705 15
72139908 20877
Satellite: ISS
Catalog Number: 25544
Epoch time: 11040
92290982 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 93
4959 deg
Eccentricity:
0005011
Arg of perigee: 289
6916 deg
Mean anomaly: 70
3705 deg
Mean motion: 15
72139908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2087
Checksum: 316
Coasting Arc #12 (Orbit 2102)
---------------------------------------
Vector Time (GMT): 2011/041/21:41:30
869
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1962913
71 A = 6735449
08 meter
Y = -6052552
53 meter E =
0009073
Z = 2196677
65 I = 51
99952
XDOT = 4179
475863 Wp = 106
93105
YDOT = -3364
434960 meter/sec RA = 87
67971 deg
ZDOT = -5519
346303 TA = 48
60473
MA = 48
52677
Ha = 191
674 n
mi
Hp = 188
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6440005
62 X = -1905757
95
Y = -19857455
80 feet Y = -6074183
42 meter
Z = 7206947
66 Z = 2187280
84
XDOT = 13712
191150 XDOT = 4243
598580
YDOT = -11038
172440 feet/sec YDOT = -3317
339056 meter/sec
ZDOT = -18108
091546 ZDOT = -5498
886922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17460495
20 X = -5321958
94
Y = 11465893
83 feet Y = 3494804
44 meter
Z = 7169149
46 Z = 2185156
76
XDOT = -13442
133306 XDOT = -4097
162232
YDOT = -9166
310653 feet/sec YDOT = -2793
891487 meter/sec
ZDOT = -18025
428925 ZDOT = -5494
150736
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 11041
93995129
00016717 00000-0 10270-3 0 9113
2 25544 51
6442 88
2877 0004974 292
9328 67
1309 15
72124552 21039
Satellite: ISS
Catalog Number: 25544
Epoch time: 11041
93995129 = yrday
fracday
Element set: 911
Inclination: 51
6442 deg
RA of node: 88
2877 deg
Eccentricity:
0004974
Arg of perigee: 292
9328 deg
Mean anomaly: 67
1309 deg
Mean motion: 15
72124552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2103
Checksum: 316
Coasting Arc #13 (Orbit 2118)
---------------------------------------
Vector Time (GMT): 2011/042/21:41:30
869
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3078108
24 A = 6728516
12 meter
Y = 3891232
17 meter E =
0003736
Z = 4542466
69 I = 51
97491
XDOT = -3268
068141 Wp = 107
35936
YDOT = -6232
690694 meter/sec RA = 82
62442 deg
ZDOT = 3121
414857 TA = 311
64751
MA = 311
67950
Ha = 191
902 n
mi
Hp = 188
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10098780
30 X = -3143458
09
Y = 12766509
74 feet Y = 3856445
49 meter
Z = 14903105
94 Z = 4527354
76
XDOT = -10722
008337 XDOT = -3213
293157
YDOT = -20448
460281 feet/sec YDOT = -6268
929957 meter/sec
ZDOT = 10240
862393 ZDOT = 3105
671852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15102080
63 X = 4603114
17
Y = 6222029
29 feet Y = 1896474
53 meter
Z = 14842008
41 Z = 4523844
16
XDOT = -16174
948591 XDOT = -4930
124331
YDOT = 14957
476960 feet/sec YDOT = 4559
038978 meter/sec
ZDOT = 10177
457811 ZDOT = 3102
089141
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 11042
95697465
00016717 00000-0 10270-3 0 9129
2 25544 51
6449 83
0791 0005043 298
2375 61
8278 15
72165452 21190
Satellite: ISS
Catalog Number: 25544
Epoch time: 11042
95697465 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 83
0791 deg
Eccentricity:
0005043
Arg of perigee: 298
2375 deg
Mean anomaly: 61
8278 deg
Mean motion: 15
72165452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2119
Checksum: 323
Coasting Arc #14 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2011/043/21:41:30
869
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3616879
74 A = 6732860
57 meter
Y = 4674879
21 meter E =
0003483
Z = -3220357
20 I = 51
98513
XDOT = -2663
985567 Wp = 2
03076
YDOT = 5377
816259 meter/sec RA = 77
47910 deg
ZDOT = 4818
341926 TA = 320
57733
MA = 320
60267
Ha = 191
957 n
mi
Hp = 188
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11866403
33 X = 3579979
16
Y = 15337530
22 feet Y = 4715119
07 meter
Z = -10565476
37 Z = -3202876
28
XDOT = -8740
110128 XDOT = -2747
329530
YDOT = 17643
754132 feet/sec YDOT = 5347
559886 meter/sec
ZDOT = 15808
208417 ZDOT = 4805
198170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11128497
83 X = 3391966
14
Y = -15927702
25 feet Y = -4854763
65 meter
Z = -10495022
13 Z = -3198882
74
XDOT = 18305
244706 XDOT = 5579
438586
YDOT = 2416
168424 feet/sec YDOT = 736
448136 meter/sec
ZDOT = 15755
009852 ZDOT = 4802
127003
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 11043
91041861
00016717 00000-0 10270-3 0 9130
2 25544 51
6452 78
1962 0005190 301
9932 58
0726 15
72199843 21347
Satellite: ISS
Catalog Number: 25544
Epoch time: 11043
91041861 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 78
1962 deg
Eccentricity:
0005190
Arg of perigee: 301
9932 deg
Mean anomaly: 58
0726 deg
Mean motion: 15
72199843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 301
Coasting Arc #15 (Orbit 2149)
---------------------------------------
Vector Time (GMT): 2011/044/21:41:30
869
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1461176
06 A = 6730901
84 meter
Y = -5335165
25 meter E =
0005010
Z = -3840171
33 I = 51
97097
XDOT = 4796
958053 Wp = 20
65270
YDOT = 4323
640277 meter/sec RA = 72
43168 deg
ZDOT = -4178
684320 TA = 205
73063
MA = 205
75556
Ha = 191
961 n
mi
Hp = 188
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4793884
72 X = 1539380
72
Y = -17503822
99 feet Y = -5318388
15 meter
Z = -12598987
31 Z = -3832883
26
XDOT = 15738
051355 XDOT = 4768
552602
YDOT = 14185
171513 feet/sec YDOT = 4377
124025 meter/sec
ZDOT = -13709
594225 ZDOT = -4155
450132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18149867
04 X = -5532079
47
Y = 831620
90 feet Y = 253478
05 meter
Z = -12569421
79 Z = -3831159
76
XDOT = 8605
451860 XDOT = 2622
941727
YDOT = -18130
326355 feet/sec YDOT = -5526
123473 meter/sec
ZDOT = -13615
904101 ZDOT = -4150
127570
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 11044
92740947
00016717 00000-0 10270-3 0 9144
2 25544 51
6452 72
9879 0005292 304
9529 55
1136 15
72213907 21503
Satellite: ISS
Catalog Number: 25544
Epoch time: 11044
92740947 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 72
9879 deg
Eccentricity:
0005292
Arg of perigee: 304
9529 deg
Mean anomaly: 55
1136 deg
Mean motion: 15
72213907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2150
Checksum: 311
Coasting Arc #16 (Orbit 2165)
---------------------------------------
Vector Time (GMT): 2011/045/21:41:30
869
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4598270
51 A = 6730058
58 meter
Y = -2791788
80 meter E =
0008699
Z = 4042777
75 I = 51
95843
XDOT = 556
769315 Wp = 48
59877
YDOT = -6603
069628 meter/sec RA = 67
28128 deg
ZDOT = -3915
531585 TA = 81
68653
MA = 81
58791
Ha = 192
111 n
mi
Hp = 187
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15086189
35 X = -4586349
00
Y = -9159412
07 feet Y = -2843142
85 meter
Z = 13263706
53 Z = 4020468
88
XDOT = 1826
670982 XDOT = 649
585131
YDOT = -21663
614266 feet/sec YDOT = -6596
324474 meter/sec
ZDOT = -12846
232233 ZDOT = -3912
601535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3676133
65 X = -1120485
54
Y = 17330703
51 feet Y = 5282398
43 meter
Z = 13173708
92 Z = 4015346
48
XDOT = -19825
576627 XDOT = -6042
835756
YDOT = 5578
114358 feet/sec YDOT = 1700
209256 meter/sec
ZDOT = -12834
221954 ZDOT = -3911
870852
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 11045
94438272
00016717 00000-0 10270-3 0 9153
2 25544 51
6453 67
7791 0005323 310
6718 49
3981 15
72287843 21668
Satellite: ISS
Catalog Number: 25544
Epoch time: 11045
94438272 = yrday
fracday
Element set: 915
Inclination: 51
6453 deg
RA of node: 67
7791 deg
Eccentricity:
0005323
Arg of perigee: 310
6718 deg
Mean anomaly: 49
3981 deg
Mean motion: 15
72287843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2166
Checksum: 325
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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