Date:
February 23rd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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
There are no maneuvers
Coasting Arc #1 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2010/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2457049
23 A = 6727092
44 meter
Y = 4803615
99 meter E =
0005168
Z = -4017285
71 I = 51
97472
XDOT = -3924
109813 Wp = 36
59839
YDOT = 5310
657534 meter/sec RA = 98
51858 deg
ZDOT = 3956
731842 TA = 274
10268
MA = 274
16176
Ha = 191
644 n
mi
Hp = 185
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8061185
13 X = 2422666
73
Y = 15759894
98 feet Y = 4830899
93 meter
Z = -13180071
21 Z = -4005433
03
XDOT = -12874
376028 XDOT = -4002
423727
YDOT = 17423
417107 feet/sec YDOT = 5266
337938 meter/sec
ZDOT = 12981
403681 ZDOT = 3937
478530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -363410
10 X = -110767
40
Y = 17733233
35 feet Y = 5405089
52 meter
Z = -13132845
88 Z = -4002891
42
XDOT = -18399
679292 XDOT = -5608
222248
YDOT = 9163
971516 feet/sec YDOT = 2793
178518 meter/sec
ZDOT = 12905
108750 ZDOT = 3933
477147
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 10053
50870820
00016717 00000-0 10270-3 0 9006
2 25544 51
6449 99
3105 0007399 329
8827 30
1910 15
73338468 5417
Satellite: ISS
Catalog Number: 25544
Epoch time: 10053
50870820 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 99
3105 deg
Eccentricity:
0007399
Arg of perigee: 329
8827 deg
Mean anomaly: 30
1910 deg
Mean motion: 15
73338468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 307
Coasting Arc #2 (Orbit 556)
---------------------------------------
Vector Time (GMT): 2010/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2897184
06 A = 6729330
55 meter
Y = -5100659
62 meter E =
0006474
Z = -3305496
99 I = 51
98640
XDOT = 3407
802594 Wp = 12
80452
YDOT = 5009
486670 meter/sec RA = 93
46293 deg
ZDOT = -4738
798958 TA = 205
73860
MA = 205
77083
Ha = 191
722 n
mi
Hp = 185
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9505197
04 X = 2970062
45
Y = -16734447
56 feet Y = -5067854
07 meter
Z = -10844806
41 Z = -3291245
73
XDOT = 11180
454704 XDOT = 3374
552189
YDOT = 16435
323722 feet/sec YDOT = 5047
408865 meter/sec
ZDOT = -15547
240677 ZDOT = -4722
324858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16214999
09 X = 4942331
72
Y = -10425231
19 feet Y = -3177610
47 meter
Z = -10788359
06 Z = -3288291
84
XDOT = 1648
696200 XDOT = 502
522602
YDOT = 18600
267624 feet/sec YDOT = 5669
361572 meter/sec
ZDOT = -15481
655659 ZDOT = -4718
808645
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 10054
52497465
00016717 00000-0 10270-3 0 9010
2 25544 51
6457 94
0971 0007443 334
2137 25
8654 15
73351352 5573
Satellite: ISS
Catalog Number: 25544
Epoch time: 10054
52497465 = yrday
fracday
Element set: 901
Inclination: 51
6457 deg
RA of node: 94
0971 deg
Eccentricity:
0007443
Arg of perigee: 334
2137 deg
Mean anomaly: 25
8654 deg
Mean motion: 15
73351352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 557
Checksum: 307
Coasting Arc #3 (Orbit 572)
---------------------------------------
Vector Time (GMT): 2010/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3447382
59 A = 6726124
73 meter
Y = -3901224
97 meter E =
0011992
Z = 4259225
41 I = 51
97547
XDOT = 2632
003592 Wp = 34
19021
YDOT = -6273
623249 meter/sec RA = 88
30686 deg
ZDOT = -3601
416495 TA = 92
31340
MA = 92
17608
Ha = 191
874 n
mi
Hp = 185
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11310310
34 X = -3424192
28
Y = -12799294
52 feet Y = -3939646
01 meter
Z = 13973836
65 Z = 4242534
70
XDOT = 8635
182389 XDOT = 2719
455392
YDOT = -20582
753440 feet/sec YDOT = -6243
701632 meter/sec
ZDOT = -11815
670916 ZDOT = -3588
418125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4480016
29 X = -1365508
97
Y = -16538627
87 feet Y = -5040973
77 meter
Z = 13907422
95 Z = 4238982
52
XDOT = 15771
915448 XDOT = 4807
279828
YDOT = -14205
312482 feet/sec YDOT = -4329
779244 meter/sec
ZDOT = -11764
225762 ZDOT = -3585
736012
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 10055
54122887
00016717 00000-0 10270-3 0 9027
2 25544 51
6447 88
8838 0007550 338
1143 21
9697 15
73384526 5735
Satellite: ISS
Catalog Number: 25544
Epoch time: 10055
54122887 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 88
8838 deg
Eccentricity:
0007550
Arg of perigee: 338
1143 deg
Mean anomaly: 21
9697 deg
Mean motion: 15
73384526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 573
Checksum: 326
Coasting Arc #4 (Orbit 588)
---------------------------------------
Vector Time (GMT): 2010/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1660864
88 A = 6730179
18 meter
Y = 5790377
95 meter E =
0014149
Z = 2980901
72 I = 51
98657
XDOT = -4404
479189 Wp = 51
14030
YDOT = -3849
630771 meter/sec RA = 83
24873 deg
ZDOT = 5016
710090 TA = 343
11860
MA = 343
16563
Ha = 192
139 n
mi
Hp = 184
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5449031
75 X = -1739970
77
Y = 18997302
99 feet Y = 5771362
90 meter
Z = 9779861
29 Z = 2972641
26
XDOT = -14450
391041 XDOT = -4385
474204
YDOT = -12630
022214 feet/sec YDOT = -3898
777959 meter/sec
ZDOT = 16459
022606 ZDOT = 4995
359903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13156327
54 X = -4010048
63
Y = 14769494
65 feet Y = 4501741
97 meter
Z = 9747216
44 Z = 2970951
57
XDOT = -6606
435017 XDOT = -2013
641393
YDOT = -16706
533538 feet/sec YDOT = -5092
151422 meter/sec
ZDOT = 16374
097644 ZDOT = 4990
824962
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 10056
55747430
00016717 00000-0 10270-3 0 9037
2 25544 51
6445 83
6700 0007566 343
5677 16
5240 15
73353625 5890
Satellite: ISS
Catalog Number: 25544
Epoch time: 10056
55747430 = yrday
fracday
Element set: 903
Inclination: 51
6445 deg
RA of node: 83
6700 deg
Eccentricity:
0007566
Arg of perigee: 343
5677 deg
Mean anomaly: 16
5240 deg
Mean motion: 15
73353625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 589
Checksum: 311
Coasting Arc #5 (Orbit 603)
---------------------------------------
Vector Time (GMT): 2010/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4172819
24 A = 6725300
45 meter
Y = 2778317
43 meter E =
0008225
Z = -4487068
65 I = 51
96648
XDOT = -1127
473952 Wp = 60
75346
YDOT = 6894
042482 meter/sec RA = 78
09474 deg
ZDOT = 3228
497762 TA = 241
38840
MA = 241
47116
Ha = 192
227 n
mi
Hp = 184
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13690351
83 X = 4163238
19
Y = 9115214
67 feet Y = 2824926
64 meter
Z = -14721353
84 Z = -4466821
07
XDOT = -3699
061521 XDOT = -1220
163560
YDOT = 22618
249613 feet/sec YDOT = 6880
916264 meter/sec
ZDOT = 10592
184257 ZDOT = 3222
795263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8745556
38 X = 2665645
58
Y = 14014003
12 feet Y = 4271468
15 meter
Z = -14640836
41 Z = -4462526
94
XDOT = -11795
062089 XDOT = -3595
134925
YDOT = 18374
588117 feet/sec YDOT = 5600
574458 meter/sec
ZDOT = 10569
730834 ZDOT = 3221
653958
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 10057
51019114
00016717 00000-0 10270-3 0 9046
2 25544 51
6455 78
7826 0007637 345
9134 14
1815 15
73375662 6043
Satellite: ISS
Catalog Number: 25544
Epoch time: 10057
51019114 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 78
7826 deg
Eccentricity:
0007637
Arg of perigee: 345
9134 deg
Mean anomaly: 14
1815 deg
Mean motion: 15
73375662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 604
Checksum: 303
Coasting Arc #6 (Orbit 619)
---------------------------------------
Vector Time (GMT): 2010/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 304223
66 A = 6730774
91 meter
Y = -6172505
23 meter E =
0005391
Z = -2675782
86 I = 51
97656
XDOT = 5044
995916 Wp = 30
09173
YDOT = 2516
638908 meter/sec RA = 73
03234 deg
ZDOT = -5231
763416 TA = 180
19852
MA = 180
19874
Ha = 192
214 n
mi
Hp = 184
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 998109
12 X = 386221
19
Y = -20251001
41 feet Y = -6168644
93 meter
Z = -8778815
17 Z = -2674105
40
XDOT = 16551
823872 XDOT = 5041
893679
YDOT = 8256
689330 feet/sec YDOT = 2573
037340 meter/sec
ZDOT = -17164
578138 ZDOT = -5207
263256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9056313
04 X = 2760364
21
Y = -18143767
26 feet Y = -5530220
26 meter
Z = -8772330
33 Z = -2673806
29
XDOT = 10641
516725 XDOT = 3243
534298
YDOT = 13563
490713 feet/sec YDOT = 4134
151969 meter/sec
ZDOT = -17067
171941 ZDOT = -5202
074008
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 10058
52641232
00016717 00000-0 10270-3 0 9051
2 25544 51
6442 73
5682 0007573 350
0060 10
0951 15
73401321 6202
Satellite: ISS
Catalog Number: 25544
Epoch time: 10058
52641232 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 73
5682 deg
Eccentricity:
0007573
Arg of perigee: 350
0060 deg
Mean anomaly: 10
0951 deg
Mean motion: 15
73401321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 620
Checksum: 257
Coasting Arc #7 (Orbit 635)
---------------------------------------
Vector Time (GMT): 2010/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4582663
73 A = 6724461
85 meter
Y = -1599700
67 meter E =
0013002
Z = 4653514
96 I = 51
94479
XDOT = -457
654888 Wp = 30
04276
YDOT = -7123
720501 meter/sec RA = 67
87907 deg
ZDOT = -2885
090365 TA = 88
44843
MA = 88
29950
Ha = 192
383 n
mi
Hp = 184
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15034986
00 X = -4587040
36
Y = -5248361
77 feet Y = -1650970
76 meter
Z = 15267437
52 Z = 4631242
47
XDOT = -1501
492414 XDOT = -363
947273
YDOT = -23371
786419 feet/sec YDOT = -7128
314599 meter/sec
ZDOT = -9465
519571 ZDOT = -2887
085302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11951326
40 X = -3642764
29
Y = -10651632
80 feet Y = -3246617
68 meter
Z = 15178908
71 Z = 4626531
38
XDOT = 6859
748040 XDOT = 2090
851203
YDOT = -21265
006235 feet/sec YDOT = -6481
573901 meter/sec
ZDOT = -9473
650155 ZDOT = -2887
568567
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 10059
54262116
00016717 00000-0 10270-3 0 9065
2 25544 51
6434 68
3536 0007685 353
9554 6
1514 15
73442060 6360
Satellite: ISS
Catalog Number: 25544
Epoch time: 10059
54262116 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 68
3536 deg
Eccentricity:
0007685
Arg of perigee: 353
9554 deg
Mean anomaly: 6
1514 deg
Mean motion: 15
73442060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 636
Checksum: 299
Coasting Arc #8 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2010/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1107206
18 A = 6731280
21 meter
Y = 6194789
95 meter E =
0017412
Z = 2358424
79 I = 51
95549
XDOT = -5352
655046 Wp = 48
05436
YDOT = -1116
803765 meter/sec RA = 62
81240 deg
ZDOT = 5432
321125 TA = 338
40834
MA = 338
48168
Ha = 192
389 n
mi
Hp = 184
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3632566
19 X = 1026396
06
Y = 20324114
00 feet Y = 6206719
81 meter
Z = 7737614
14 Z = 2363606
53
XDOT = -17561
204219 XDOT = -5366
157647
YDOT = -3664
054347 feet/sec YDOT = -1176
735235 meter/sec
ZDOT = 17822
575871 ZDOT = 5406
285767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4142254
70 X = -1262559
23
Y = 20218436
61 feet Y = 6162579
48 meter
Z = 7758373
96 Z = 2364752
38
XDOT = -13604
296469 XDOT = -4146
589564
YDOT = -9604
138355 feet/sec YDOT = -2927
341371 meter/sec
ZDOT = 17719
115179 ZDOT = 5400
786307
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 10060
55881844
00016717 00000-0 10270-3 0 9074
2 25544 51
6433 63
1399 0007672 357
3395 2
7725 15
73462360 6525
Satellite: ISS
Catalog Number: 25544
Epoch time: 10060
55881844 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 63
1399 deg
Eccentricity:
0007672
Arg of perigee: 357
3395 deg
Mean anomaly: 2
7725 deg
Mean motion: 15
73462360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 652
Checksum: 313
Coasting Arc #9 (Orbit 666)
---------------------------------------
Vector Time (GMT): 2010/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4688201
21 A = 6723827
33 meter
Y = 350892
38 meter E =
0012002
Z = -4814968
80 I = 51
91515
XDOT = 2065
529276 Wp = 69
42169
YDOT = 6965
968906 meter/sec RA = 57
66126 deg
ZDOT = 2527
960799 TA = 225
20579
MA = 225
30345
Ha = 192
626 n
mi
Hp = 184
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15381237
56 X = 4707318
96
Y = 1151221
73 feet Y = 403425
01 meter
Z = -15797141
72 Z = -4792147
43
XDOT = 6776
670853 XDOT = 1975
200845
YDOT = 22854
228693 feet/sec YDOT = 6988
562099 meter/sec
ZDOT = 8293
834642 ZDOT = 2537
774851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14079322
17 X = 4291377
40
Y = 6522026
37 feet Y = 1987913
64 meter
Z = -15706474
02 Z = -4787333
28
XDOT = -1268
611706 XDOT = -386
672848
YDOT = 22733
484261 feet/sec YDOT = 6929
166003 meter/sec
ZDOT = 8333
009882 ZDOT = 2539
901412
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 10061
51149347
00016717 00000-0 10270-3 0 9087
2 25544 51
6433 58
2513 0007802 1
0655 359
0523 15
73437560 6679
Satellite: ISS
Catalog Number: 25544
Epoch time: 10061
51149347 = yrday
fracday
Element set: 908
Inclination: 51
6433 deg
RA of node: 58
2513 deg
Eccentricity:
0007802
Arg of perigee: 1
0655 deg
Mean anomaly: 359
0523 deg
Mean motion: 15
73437560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 667
Checksum: 290
Coasting Arc #10 (Orbit 682)
---------------------------------------
Vector Time (GMT): 2010/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2470388
95 A = 6731748
73 meter
Y = -5910447
79 meter E =
0005775
Z = -2079057
04 I = 51
92507
XDOT = 5297
158443 Wp = 59
26504
YDOT = -257
558722 meter/sec RA = 52
58733 deg
ZDOT = -5570
516715 TA = 143
82308
MA = 143
78400
Ha = 192
632 n
mi
Hp = 183
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8104950
62 X = -2394014
07
Y = -19391232
90 feet Y = -5937646
30 meter
Z = -6821053
29 Z = -2090872
02
XDOT = 17379
128750 XDOT = 5326
705134
YDOT = -845
008929 feet/sec YDOT = -198
158059 meter/sec
ZDOT = -18275
973475 ZDOT = -5544
711565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1086675
51 X = -331218
70
Y = -20973428
71 feet Y = -6392701
07 meter
Z = -6868138
77 Z = -2093408
70
XDOT = 15225
840521 XDOT = 4640
836191
YDOT = 5153
292040 feet/sec YDOT = 1570
723414 meter/sec
ZDOT = -18173
471599 ZDOT = -5539
274143
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 10062
52766816
00016717 00000-0 10270-3 0 9096
2 25544 51
6431 53
0364 0007852 5
5531 354
5717 15
73479873 6837
Satellite: ISS
Catalog Number: 25544
Epoch time: 10062
52766816 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 53
0364 deg
Eccentricity:
0007852
Arg of perigee: 5
5531 deg
Mean anomaly: 354
5717 deg
Mean motion: 15
73479873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 683
Checksum: 317
Coasting Arc #11 (Orbit 698)
---------------------------------------
Vector Time (GMT): 2010/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4511545
23 A = 6723181
86 meter
Y = 794497
35 meter E =
0013103
Z = 4919192
06 I = 51
87692
XDOT = -3567
583955 Wp = 29
92717
YDOT = -6455
503019 meter/sec RA = 47
43782 deg
ZDOT = -2215
678063 TA = 81
59852
MA = 81
45000
Ha = 192
781 n
mi
Hp = 183
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14801657
58 X = -4543990
51
Y = 2606618
60 feet Y = 743865
51 meter
Z = 16139081
55 Z = 4897196
26
XDOT = -11704
671769 XDOT = -3484
368931
YDOT = -21179
471848 feet/sec YDOT = -6494
932739 meter/sec
ZDOT = -7269
284985 ZDOT = -2232
806677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14948534
30 X = -4556313
26
Y = -2288426
47 feet Y = -697512
39 meter
Z = 16051725
99 Z = 4892566
08
XDOT = -4451
415565 XDOT = -1356
791464
YDOT = -22705
228484 feet/sec YDOT = -6920
553642 meter/sec
ZDOT = -7337
480658 ZDOT = -2236
464105
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 10063
54382999
00016717 00000-0 10270-3 0 9107
2 25544 51
6430 47
8222 0007898 8
0650 352
0639 15
73501811 6991
Satellite: ISS
Catalog Number: 25544
Epoch time: 10063
54382999 = yrday
fracday
Element set: 910
Inclination: 51
6430 deg
RA of node: 47
8222 deg
Eccentricity:
0007898
Arg of perigee: 8
0650 deg
Mean anomaly: 352
0639 deg
Mean motion: 15
73501811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 699
Checksum: 312
Coasting Arc #12 (Orbit 714)
---------------------------------------
Vector Time (GMT): 2010/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3730638
15 A = 6732013
63 meter
Y = 5296848
03 meter E =
0019700
Z = 1785268
24 I = 51
88651
XDOT = -4944
411879 Wp = 47
06343
YDOT = 1550
152641 meter/sec RA = 42
35833 deg
ZDOT = 5706
771827 TA = 332
67005
MA = 332
77356
Ha = 192
629 n
mi
Hp = 183
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12239626
47 X = 3662458
13
Y = 17378110
33 feet Y = 5338185
11 meter
Z = 5857179
25 Z = 1803225
67
XDOT = -16221
823751 XDOT = -4989
100747
YDOT = 5085
802628 feet/sec YDOT = 1494
611705 meter/sec
ZDOT = 18723
004682 ZDOT = 5682
643427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6363166
70 X = 1939493
21
Y = 20260186
81 feet Y = 6175304
94 meter
Z = 5928630
86 Z = 1807046
69
XDOT = -15627
597852 XDOT = -4763
291825
YDOT = -567
426879 feet/sec YDOT = -172
951713 meter/sec
ZDOT = 18627
193656 ZDOT = 5677
568626
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 10064
55997850
00016717 00000-0 10270-3 0 9118
2 25544 51
6435 42
6086 0007727 12
2872 347
8478 15
73561399 7150
Satellite: ISS
Catalog Number: 25544
Epoch time: 10064
55997850 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 42
6086 deg
Eccentricity:
0007727
Arg of perigee: 12
2872 deg
Mean anomaly: 347
8478 deg
Mean motion: 15
73561399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 715
Checksum: 332
Coasting Arc #13 (Orbit 729)
---------------------------------------
Vector Time (GMT): 2010/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4064616
89 A = 6722695
70 meter
Y = -1875166
18 meter E =
0015518
Z = -5027118
83 I = 51
83170
XDOT = 4916
017354 Wp = 73
02565
YDOT = 5602
334409 meter/sec RA = 37
20983 deg
ZDOT = 1894
278197 TA = 215
18145
MA = 215
28400
Ha = 192
913 n
mi
Hp = 183
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13335357
23 X = 4109703
84
Y = -6152120
00 feet Y = -1829461
29 meter
Z = -16493172
00 Z = -5007263
53
XDOT = 16128
665860 XDOT = 4843
803709
YDOT = 18380
362234 feet/sec YDOT = 5656
904528 meter/sec
ZDOT = 6214
823481 ZDOT = 1917
984393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14632099
54 X = 4459863
94
Y = -2043571
11 feet Y = -622880
47 meter
Z = -16414339
34 Z = -5003090
63
XDOT = 9998
104431 XDOT = 3047
422230
YDOT = 21155
220126 feet/sec YDOT = 6448
111094 meter/sec
ZDOT = 6309
110967 ZDOT = 1923
017023
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 10065
51260948
00016717 00000-0 10270-3 0 9127
2 25544 51
6437 37
7200 0007986 15
6704 344
4705 15
73516349 7301
Satellite: ISS
Catalog Number: 25544
Epoch time: 10065
51260948 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 37
7200 deg
Eccentricity:
0007986
Arg of perigee: 15
6704 deg
Mean anomaly: 344
4705 deg
Mean motion: 15
73516349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 730
Checksum: 302
Coasting Arc #14 (Orbit 745)
---------------------------------------
Vector Time (GMT): 2010/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4808365
11 A = 6732332
15 meter
Y = -4454301
03 meter E =
0007649
Z = -1547188
55 I = 51
84070
XDOT = 4316
347363 Wp = 80
70336
YDOT = -2657
853232 meter/sec RA = 32
12170 deg
ZDOT = -5785
485083 TA = 116
28492
MA = 116
20631
Ha = 192
909 n
mi
Hp = 182
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15775476
10 X = -4750683
09
Y = -14613848
51 feet Y = -4507748
54 meter
Z = -5076077
92 Z = -1570407
07
XDOT = 14161
244629 XDOT = 4373
851636
YDOT = -8719
990920 feet/sec YDOT = -2609
263890 meter/sec
ZDOT = -18981
250272 ZDOT = -5764
376795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11211824
09 X = -3417363
98
Y = -18324284
86 feet Y = -5585242
03 meter
Z = -5168400
75 Z = -1575328
55
XDOT = 14761
553361 XDOT = 4499
321464
YDOT = -3722
758404 feet/sec YDOT = -1134
696761 meter/sec
ZDOT = -18897
452869 ZDOT = -5759
943634
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 10066
52873472
00016717 00000-0 10270-3 0 9132
2 25544 51
6443 32
5054 0008076 19
1823 340
9643 15
73564025 7463
Satellite: ISS
Catalog Number: 25544
Epoch time: 10066
52873472 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 32
5054 deg
Eccentricity:
0008076
Arg of perigee: 19
1823 deg
Mean anomaly: 340
9643 deg
Mean motion: 15
73564025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 746
Checksum: 299
Coasting Arc #15 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2010/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3432939
87 A = 6722235
03 meter
Y = 2744070
41 meter E =
0012664
Z = 5082949
81 I = 51
78052
XDOT = -6031
200983 Wp = 34
50132
YDOT = -4507
770808 meter/sec RA = 26
97406 deg
ZDOT = -1627
616434 TA = 71
16776
MA = 71
03045
Ha = 193
066 n
mi
Hp = 182
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11262926
09 X = -3488061
06
Y = 9002855
67 feet Y = 2705373
16 meter
Z = 16676344
51 Z = 5066138
91
XDOT = -19787
404799 XDOT = -5972
439498
YDOT = -14789
274304 feet/sec YDOT = -4574
886765 meter/sec
ZDOT = -5339
948930 ZDOT = -1656
772687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13272348
69 X = -4045411
88
Y = 5828443
76 feet Y = 1776509
66 meter
Z = 16609617
22 Z = 5062611
33
XDOT = -14935
121566 XDOT = -4552
225053
YDOT = -18347
413743 feet/sec YDOT = -5592
291709 meter/sec
ZDOT = -5455
858693 ZDOT = -1662
945730
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 10067
54484752
00016717 00000-0 10270-3 0 9145
2 25544 51
6444 27
2914 0008045 22
7389 337
4128 15
73571895 7623
Satellite: ISS
Catalog Number: 25544
Epoch time: 10067
54484752 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 27
2914 deg
Eccentricity:
0008045
Arg of perigee: 22
7389 deg
Mean anomaly: 337
4128 deg
Mean motion: 15
73571895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 322
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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