Date:
May 29th 2010
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) : 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
156/03:21:57
281 -1
7 13
1 13
1
N/A -11
0 -0
0 191
1
000/00:03:54
562 -7
0 0
1 187
2
158/23:59:56
236 -0
7 2
6 2
6
N/A -2
2 0
0 191
3
000/00:09:52
473 -1
3 0
2 188
3
159/01:30:56
147 -0
8 2
7 2
7
N/A -2
2 -0
0 191
3
000/00:09:52
294 -1
3 0
2 189
6
Coasting Arc #1 (Orbit 2007)
---------------------------------------
Vector Time (GMT): 2010/146/14:12:41
884
Vector Time (MET): N/A
Weight (LBS) : 816195
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4872490
23 A = 6721869
78 meter
Y = 1866051
61 meter E =
0009424
Z = 4227895
31 I = 51
52828
XDOT = -4921
882656 Wp = 53
20445
YDOT = 4724
140101 meter/sec RA = 340
87238 deg
ZDOT = 3587
271921 TA =
32233
MA =
32172
Ha = 190
185 n
mi
Hp = 182
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15985860
35 X = 4830722
84
Y = 6122216
56 feet Y = 1920304
58 meter
Z = 13871047
61 Z = 4251465
11
XDOT = -16147
908976 XDOT = -4991
769671
YDOT = 15499
147312 feet/sec YDOT = 4668
709428 meter/sec
ZDOT = 11769
264832 ZDOT = 3563
191860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4299992
07 X = 1310637
58
Y = -16490199
07 feet Y = -5026212
68 meter
Z = 13964907
13 Z = 4256503
69
XDOT = 16018
347440 XDOT = 4882
392300
YDOT = 14062
469218 feet/sec YDOT = 4286
240618 meter/sec
ZDOT = 11673
339437 ZDOT = 3558
033860
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 10146
64612078
00016717 00000-0 10270-3 0 9003
2 25544 51
6443 341
0903 0008781 347
9131 12
1821 15
74844372 20087
Satellite: ISS
Catalog Number: 25544
Epoch time: 10146
64612078 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 341
0903 deg
Eccentricity:
0008781
Arg of perigee: 347
9131 deg
Mean anomaly: 12
1821 deg
Mean motion: 15
74844372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2008
Checksum: 284
Coasting Arc #2 (Orbit 2022)
---------------------------------------
Vector Time (GMT): 2010/147/14:12:41
884
Vector Time (MET): N/A
Weight (LBS) : 816195
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4168506
99 A = 6726170
90 meter
Y = -4408110
09 meter E =
0011113
Z = -2892573
64 I = 51
51542
XDOT = 5505
042471 Wp = 15
26977
YDOT = 1908
446005 meter/sec RA = 335
67367 deg
ZDOT = 5039
911457 TA = 311
37747
MA = 311
47297
Ha = 190
466 n
mi
Hp = 182
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13676204
04 X = 4231541
28
Y = -14462303
44 feet Y = -4361142
47 meter
Z = -9490071
01 Z = -2872170
30
XDOT = 18061
162961 XDOT = 5458
809374
YDOT = 6261
305791 feet/sec YDOT = 1969
747372 meter/sec
ZDOT = 16535
142575 ZDOT = 5066
543373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16116154
86 X = -4912204
00
Y = -11747447
68 feet Y = -3580622
05 meter
Z = -9408785
86 Z = -2867797
93
XDOT = 3030
874689 XDOT = 923
810605
YDOT = -17446
775330 feet/sec YDOT = -5317
777121 meter/sec
ZDOT = 16641
197763 ZDOT = 5072
237078
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 10147
59795867
00016717 00000-0 10270-3 0 9017
2 25544 51
6454 336
1967 0008748 352
4715 7
6316 15
74849896 20237
Satellite: ISS
Catalog Number: 25544
Epoch time: 10147
59795867 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 336
1967 deg
Eccentricity:
0008748
Arg of perigee: 352
4715 deg
Mean anomaly: 7
6316 deg
Mean motion: 15
74849896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2023
Checksum: 348
Coasting Arc #3 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2010/148/14:12:41
884
Vector Time (MET): N/A
Weight (LBS) : 816195
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4709778
35 A = 6720503
74 meter
Y = -1514328
93 meter E =
0015488
Z = -4562683
92 I = 51
47006
XDOT = 4633
581009 Wp = 36
33116
YDOT = -5355
645864 meter/sec RA = 330
56820 deg
ZDOT = -2998
369799 TA = 203
73956
MA = 203
81108
Ha = 190
517 n
mi
Hp = 181
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15452028
69 X = -4670329
86
Y = -4968270
76 feet Y = -1566775
13 meter
Z = -14969435
43 Z = -4585468
73
XDOT = 15202
037432 XDOT = 4707
690131
YDOT = -17571
016613 feet/sec YDOT = -5303
415525 meter/sec
ZDOT = -9837
171257 ZDOT = -2975
680499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2667776
49 X = -813138
27
Y = 15925044
39 feet Y = 4853953
53 meter
Z = -15060173
70 Z = -4590340
94
XDOT = -18453
360773 XDOT = -5624
584364
YDOT = -12330
601305 feet/sec YDOT = -3758
367278 meter/sec
ZDOT = -9746
772080 ZDOT = -2970
816130
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 10148
61323404
00016717 00000-0 10270-3 0 9026
2 25544 51
6457 330
9771 0008861 356
5270 3
5830 15
74888389 20395
Satellite: ISS
Catalog Number: 25544
Epoch time: 10148
61323404 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 330
9771 deg
Eccentricity:
0008861
Arg of perigee: 356
5270 deg
Mean anomaly: 3
5830 deg
Mean motion: 15
74888389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 315
Coasting Arc #4 (Orbit 2054)
---------------------------------------
Vector Time (GMT): 2010/149/14:12:41
884
Vector Time (MET): N/A
Weight (LBS) : 816195
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3908741
81 A = 6727320
11 meter
Y = 4953701
21 meter E =
0014099
Z = 2329045
95 I = 51
46660
XDOT = -5254
338397 Wp = 70
38039
YDOT = -1594
131102 meter/sec RA = 325
36967 deg
ZDOT = -5396
415229 TA = 83
34624
MA = 83
18579
Ha = 190
613 n
mi
Hp = 181
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12823956
06 X = -3975158
64
Y = 16252300
57 feet Y = 4909619
57 meter
Z = 7641226
87 Z = 2309896
69
XDOT = -17238
643036 XDOT = -5209
907033
YDOT = -5230
088917 feet/sec YDOT = -1652
638864 meter/sec
ZDOT = -17704
774374 ZDOT = -5421
833342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18135685
86 X = 5527757
05
Y = 10042322
72 feet Y = 3060899
96 meter
Z = 7564927
21 Z = 2305789
82
XDOT = -1630
459047 XDOT = -496
963917
YDOT = 16435
544844 feet/sec YDOT = 5009
554069 meter/sec
ZDOT = -17806
004258 ZDOT = -5427
270098
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 10149
62849197
00016717 00000-0 10270-3 0 9031
2 25544 51
6452 325
7557 0008806 359
7879
3279 15
74894962 20557
Satellite: ISS
Catalog Number: 25544
Epoch time: 10149
62849197 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 325
7557 deg
Eccentricity:
0008806
Arg of perigee: 359
7879 deg
Mean anomaly:
3279 deg
Mean motion: 15
74894962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 352
Coasting Arc #5 (Orbit 2070)
---------------------------------------
Vector Time (GMT): 2010/150/14:12:41
884
Vector Time (MET): N/A
Weight (LBS) : 816195
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4469286
82 A = 6719108
28 meter
Y = 1303173
30 meter E =
0008075
Z = 4837819
84 I = 51
41680
XDOT = -4269
940049 Wp = 48
71132
YDOT = 5976
456860 meter/sec RA = 320
25246 deg
ZDOT = 2337
511842 TA = 18
47687
MA = 18
44756
Ha = 190
485 n
mi
Hp = 181
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14663014
51 X = 4430881
02
Y = 4275502
96 feet Y = 1352935
96 meter
Z = 15872112
33 Z = 4859438
63
XDOT = -14008
989661 XDOT = -4347
807753
YDOT = 19607
798098 feet/sec YDOT = 5928
272065 meter/sec
ZDOT = 7669
002106 ZDOT = 2316
580302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1580186
25 X = 481640
77
Y = -15101199
79 feet Y = -4602845
70 meter
Z = 15958215
63 Z = 4864064
12
XDOT = 20718
702844 XDOT = 6315
060627
YDOT = 10174
659876 feet/sec YDOT = 3101
236330 meter/sec
ZDOT = 7585
597795 ZDOT = 2312
090208
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 10150
64373081
00016717 00000-0 10270-3 0 9040
2 25544 51
6465 320
5354 0008852 2
9057 357
2156 15
74962959 20713
Satellite: ISS
Catalog Number: 25544
Epoch time: 10150
64373081 = yrday
fracday
Element set: 904
Inclination: 51
6465 deg
RA of node: 320
5354 deg
Eccentricity:
0008852
Arg of perigee: 2
9057 deg
Mean anomaly: 357
2156 deg
Mean motion: 15
74962959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2071
Checksum: 307
Coasting Arc #6 (Orbit 2085)
---------------------------------------
Vector Time (GMT): 2010/151/14:12:41
884
Vector Time (MET): N/A
Weight (LBS) : 816195
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3509140
83 A = 6728177
75 meter
Y = -5460812
76 meter E =
0016030
Z = -1738691
52 I = 51
42547
XDOT = 5004
099873 Wp = 20
93274
YDOT = 1414
631455 meter/sec RA = 315
06029 deg
ZDOT = 5687
400814 TA = 319
74080
MA = 319
85940
Ha = 190
781 n
mi
Hp = 181
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11512929
25 X = 3578390
06
Y = -17916052
35 feet Y = -5421183
98 meter
Z = -5704368
51 Z = -1721476
79
XDOT = 16417
650502 XDOT = 4960
280946
YDOT = 4641
179313 feet/sec YDOT = 1470
344362 meter/sec
ZDOT = 18659
451491 ZDOT = 5711
604513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19840751
83 X = -6047461
16
Y = -7788126
18 feet Y = -2373820
86 meter
Z = -5635774
07 Z = -1717783
94
XDOT = 768
229286 XDOT = 234
156286
YDOT = -15455
483550 feet/sec YDOT = -4710
831386 meter/sec
ZDOT = 18755
854757 ZDOT = 5716
784530
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 10151
59550313
00016717 00000-0 10270-3 0 9051
2 25544 51
6474 315
6421 0008960 7
1847 352
9443 15
74953001 20862
Satellite: ISS
Catalog Number: 25544
Epoch time: 10151
59550313 = yrday
fracday
Element set: 905
Inclination: 51
6474 deg
RA of node: 315
6421 deg
Eccentricity:
0008960
Arg of perigee: 7
1847 deg
Mean anomaly: 352
9443 deg
Mean motion: 15
74953001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2086
Checksum: 297
Coasting Arc #7 (Orbit 2101)
---------------------------------------
Vector Time (GMT): 2010/152/14:12:41
884
Vector Time (MET): N/A
Weight (LBS) : 816195
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4259117
72 A = 6718116
65 meter
Y = -1219009
83 meter E =
0019115
Z = -5066199
32 I = 51
37153
XDOT = 3775
435492 Wp = 51
86517
YDOT = -6504
210452 meter/sec RA = 309
93071 deg
ZDOT = -1601
436863 TA = 202
63048
MA = 202
71488
Ha = 190
809 n
mi
Hp = 180
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13973483
33 X = -4220559
36
Y = -3999376
08 feet Y = -1266421
50 meter
Z = -16621388
85 Z = -5086796
59
XDOT = 12386
599383 XDOT = 3855
665621
YDOT = -21339
273137 feet/sec YDOT = -6461
542464 meter/sec
ZDOT = -5254
057948 ZDOT = -1582
901889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -938572
04 X = -286076
76
Y = 14409659
19 feet Y = 4392064
12 meter
Z = -16703431
31 Z = -5091205
86
XDOT = -22451
305326 XDOT = -6843
157863
YDOT = -7495
652494 feet/sec YDOT = -2284
674880 meter/sec
ZDOT = -5180
205652 ZDOT = -1578
926683
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 10152
61070836
00016717 00000-0 10270-3 0 9063
2 25544 51
6476 310
4225 0009021 10
5546 349
5805 15
74989203 21028
Satellite: ISS
Catalog Number: 25544
Epoch time: 10152
61070836 = yrday
fracday
Element set: 906
Inclination: 51
6476 deg
RA of node: 310
4225 deg
Eccentricity:
0009021
Arg of perigee: 10
5546 deg
Mean anomaly: 349
5805 deg
Mean motion: 15
74989203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2102
Checksum: 285
Coasting Arc #8 (Orbit 2117)
---------------------------------------
Vector Time (GMT): 2010/153/14:12:41
884
Vector Time (MET): N/A
Weight (LBS) : 816195
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3075406
08 A = 6728838
34 meter
Y = 5892425
02 meter E =
0013678
Z = 1040891
41 I = 51
38937
XDOT = -4742
431896 Wp = 85
46578
YDOT = -1422
013440 meter/sec RA = 304
74551 deg
ZDOT = -5894
448890 TA = 83
11430
MA = 82
95871
Ha = 190
885 n
mi
Hp = 180
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10089914
97 X = -3146124
12
Y = 19332103
08 feet Y = 5857638
46 meter
Z = 3414998
05 Z = 1025780
08
XDOT = -15559
159764 XDOT = -4697
544111
YDOT = -4665
398425 feet/sec YDOT = -1474
794415 meter/sec
ZDOT = -19338
743079 ZDOT = -5917
378726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21143234
21 X = 6444457
79
Y = 5376599
67 feet Y = 1638787
58 meter
Z = 3354791
85 Z = 1022540
56
XDOT = -584
478541 XDOT = -178
149059
YDOT = 14562
829683 feet/sec YDOT = 4438
750487 meter/sec
ZDOT = -19430
079610 ZDOT = -5922
288265
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 10153
62589586
00016717 00000-0 10270-3 0 9073
2 25544 51
6476 305
2016 0008995 14
4978 345
6442 15
75013043 21181
Satellite: ISS
Catalog Number: 25544
Epoch time: 10153
62589586 = yrday
fracday
Element set: 907
Inclination: 51
6476 deg
RA of node: 305
2016 deg
Eccentricity:
0008995
Arg of perigee: 14
4978 deg
Mean anomaly: 345
6442 deg
Mean motion: 15
75013043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2118
Checksum: 318
Coasting Arc #9 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2010/154/14:12:41
884
Vector Time (MET): N/A
Weight (LBS) : 816195
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4049373
52 A = 6717203
16 meter
Y = 1289573
15 meter E =
0009007
Z = 5196453
96 I = 51
33529
XDOT = -3223
383855 Wp = 37
24662
YDOT = 6956
907944 meter/sec RA = 299
59941 deg
ZDOT = 791
753373 TA = 45
23082
MA = 45
15758
Ha = 190
776 n
mi
Hp = 180
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13285346
20 X = 4009408
90
Y = 4230883
04 feet Y = 1334631
63 meter
Z = 17048733
45 Z = 5216028
87
XDOT = -10575
406350 XDOT = -3304
783880
YDOT = 22824
501129 feet/sec YDOT = 6920
406926 meter/sec
ZDOT = 2597
616053 ZDOT = 775
897234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 837568
48 X = 255290
87
Y = -13821520
93 feet Y = -4212799
58 meter
Z = 17126708
55 Z = 5220220
76
XDOT = 23727
417790 XDOT = 7232
116942
YDOT = 4552
623858 feet/sec YDOT = 1387
639752 meter/sec
ZDOT = 2534
449184 ZDOT = 772
500111
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 10154
64106381
00016717 00000-0 10270-3 0 9085
2 25544 51
6483 299
9812 0009098 17
6170 342
5308 15
75080213 21344
Satellite: ISS
Catalog Number: 25544
Epoch time: 10154
64106381 = yrday
fracday
Element set: 908
Inclination: 51
6483 deg
RA of node: 299
9812 deg
Eccentricity:
0009098
Arg of perigee: 17
6170 deg
Mean anomaly: 342
5308 deg
Mean motion: 15
75080213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 303
Coasting Arc #10 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2010/155/14:12:41
884
Vector Time (MET): N/A
Weight (LBS) : 816195
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2527402
99 A = 6729137
21 meter
Y = -6215404
91 meter E =
0020531
Z = -336476
02 I = 51
36138
XDOT = 4574
619133 Wp = 33
04616
YDOT = 1545
075944 meter/sec RA = 294
42590 deg
ZDOT = 6009
666338 TA = 323
27742
MA = 323
41793
Ha = 191
062 n
mi
Hp = 180
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8292004
57 X = 2598351
47
Y = -20391748
40 feet Y = -6186745
26 meter
Z = -1103923
94 Z = -324026
16
XDOT = 15008
592955 XDOT = 4527
807879
YDOT = 5069
146799 feet/sec YDOT = 1595
969713 meter/sec
ZDOT = 19716
753079 ZDOT = 6031
776344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21859275
55 X = -6662707
19
Y = -2619130
41 feet Y = -798310
95 meter
Z = -1054333
45 Z = -321360
83
XDOT = 766
418220 XDOT = 233
604273
YDOT = -14108
117545 feet/sec YDOT = -4300
154228 meter/sec
ZDOT = 19804
828365 ZDOT = 6036
511686
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 10155
59276972
00016717 00000-0 10270-3 0 9095
2 25544 51
6484 295
0875 0009286 21
5345 338
6208 15
75054065 21495
Satellite: ISS
Catalog Number: 25544
Epoch time: 10155
59276972 = yrday
fracday
Element set: 909
Inclination: 51
6484 deg
RA of node: 295
0875 deg
Eccentricity:
0009286
Arg of perigee: 21
5345 deg
Mean anomaly: 338
6208 deg
Mean motion: 15
75054065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 334
Coasting Arc #11 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2010/156/03:23:54
562
Vector Time (MET): N/A
Weight (LBS) : 815047
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4622558
76 A = 6728103
37 meter
Y = 2411476
41 meter E =
0006484
Z = -4259259
56 I = 51
32804
XDOT = -321
020737 Wp = 41
00816
YDOT = -6832
820039 meter/sec RA = 291
61937 deg
ZDOT = -3518
362793 TA = 193
12021
MA = 193
13708
Ha = 191
087 n
mi
Hp = 187
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15165875
20 X = -4628489
97
Y = 7911668
00 feet Y = 2359751
46 meter
Z = -13973948
69 Z = -4281730
21
XDOT = -1053
217642 XDOT = -227
499409
YDOT = -22417
388578 feet/sec YDOT = -6835
886628 meter/sec
ZDOT = -11543
185015 ZDOT = -3519
695833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14944251
12 X = -4555007
74
Y = -8170558
62 feet Y = -2490386
27 meter
Z = -14063457
37 Z = -4286541
81
XDOT = 17518
434664 XDOT = 5339
618886
YDOT = -12154
116633 feet/sec YDOT = -3704
574750 meter/sec
ZDOT = -11548
502391 ZDOT = -3519
983529
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 10156
16380696
00016717 00000-0 10270-3 0 9100
2 25544 51
6483 292
1546 0004230 296
0086 64
0641 15
72632503 21589
Satellite: ISS
Catalog Number: 25544
Epoch time: 10156
16380696 = yrday
fracday
Element set: 910
Inclination: 51
6483 deg
RA of node: 292
1546 deg
Eccentricity:
0004230
Arg of perigee: 296
0086 deg
Mean anomaly: 64
0641 deg
Mean motion: 15
72632503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 293
Coasting Arc #12 (Orbit 2173)
---------------------------------------
Vector Time (GMT): 2010/157/03:23:54
562
Vector Time (MET): N/A
Weight (LBS) : 815047
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1172400
76 A = 6731008
45 meter
Y = 5679701
10 meter E =
0009106
Z = 3411233
76 I = 51
32703
XDOT = -4921
228832 Wp = 75
66519
YDOT = 3766
483775 meter/sec RA = 286
42191 deg
ZDOT = -4567
418851 TA = 63
83894
MA = 63
74531
Ha = 191
190 n
mi
Hp = 187
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3846459
19 X = 1092230
90
Y = 18634189
95 feet Y = 5692362
99 meter
Z = 11191711
79 Z = 3416735
16
XDOT = -16145
763884 XDOT = -4940
792709
YDOT = 12357
230233 feet/sec YDOT = 3711
342730 meter/sec
ZDOT = -14984
969985 ZDOT = -4591
373515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13182270
01 X = -4017955
90
Y = 13702729
32 feet Y = 4176591
90 meter
Z = 11213637
37 Z = 3417916
67
XDOT = -18294
426733 XDOT = -5576
141268
YDOT = -5225
280760 feet/sec YDOT = -1592
665576 meter/sec
ZDOT = -15080
385715 ZDOT = -4596
501566
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 10157
18052817
00016717 00000-0 10270-3 0 9115
2 25544 51
6477 286
9446 0004209 300
1233 59
9512 15
72629752 21749
Satellite: ISS
Catalog Number: 25544
Epoch time: 10157
18052817 = yrday
fracday
Element set: 911
Inclination: 51
6477 deg
RA of node: 286
9446 deg
Eccentricity:
0004209
Arg of perigee: 300
1233 deg
Mean anomaly: 59
9512 deg
Mean motion: 15
72629752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2174
Checksum: 308
Coasting Arc #13 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2010/158/03:23:54
562
Vector Time (MET): N/A
Weight (LBS) : 815047
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3841285
40 A = 6729996
01 meter
Y = -4098146
32 meter E =
0008194
Z = 3699073
85 I = 51
31706
XDOT = 2281
413619 Wp = 81
61533
YDOT = 5993
300261 meter/sec RA = 281
32516 deg
ZDOT = 4263
889621 TA = 323
17967
MA = 323
23592
Ha = 191
188 n
mi
Hp = 187
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12602642
38 X = 3868856
48
Y = -13445361
95 feet Y = -4055037
02 meter
Z = 12136069
05 Z = 3717801
55
XDOT = 7484
952817 XDOT = 2193
512453
YDOT = 19663
058599 feet/sec YDOT = 6018
320448 meter/sec
ZDOT = 13989
139177 ZDOT = 4274
759985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18227690
67 X = 5555800
12
Y = 2353630
56 feet Y = 717386
60 meter
Z = 12210660
96 Z = 3721809
46
XDOT = -11499
570798 XDOT = -3505
069179
YDOT = 16141
638908 feet/sec YDOT = 4919
971539 meter/sec
ZDOT = 14032
456379 ZDOT = 4277
092704
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 10158
19723303
00016717 00000-0 10270-3 0 9123
2 25544 51
6482 281
7338 0004319 305
0780 54
9977 15
72652794 21901
Satellite: ISS
Catalog Number: 25544
Epoch time: 10158
19723303 = yrday
fracday
Element set: 912
Inclination: 51
6482 deg
RA of node: 281
7338 deg
Eccentricity:
0004319
Arg of perigee: 305
0780 deg
Mean anomaly: 54
9977 deg
Mean motion: 15
72652794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 318
Coasting Arc #14 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2010/159/00:04:52
473
Vector Time (MET): N/A
Weight (LBS) : 814792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4165577
07 A = 6727080
54 meter
Y = 2123736
46 meter E =
0008239
Z = -4843938
48 I = 51
29673
XDOT = -998
831138 Wp = 53
32297
YDOT = -7263
727748 meter/sec RA = 276
87996 deg
ZDOT = -2323
581213 TA = 193
89085
MA = 193
91353
Ha = 191
286 n
mi
Hp = 188
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13666591
45 X = -4165484
18
Y = 6967639
32 feet Y = 2077155
60 meter
Z = -15892186
61 Z = -4864174
65
XDOT = -3277
005045 XDOT = -906
244893
YDOT = -23831
127783 feet/sec YDOT = -7274
379317 meter/sec
ZDOT = -7623
297943 ZDOT = -2328
209579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3662434
12 X = -1116309
92
Y = -14810191
39 feet Y = -4514146
34 meter
Z = -15972793
18 Z = -4868507
36
XDOT = 22856
431480 XDOT = 6966
640315
YDOT = 2596
884187 feet/sec YDOT = 791
530300 meter/sec
ZDOT = -7641
755866 ZDOT = -2329
207188
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 10159
02329867
00016717 00000-0 10270-3 0 9134
2 25544 51
6465 277
4997 0005242 285
1503 74
9079 15
72182968 22033
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
02329867 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 277
4997 deg
Eccentricity:
0005242
Arg of perigee: 285
1503 deg
Mean anomaly: 74
9079 deg
Mean motion: 15
72182968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 331
Coasting Arc #15 (Orbit 2203)
---------------------------------------
Vector Time (GMT): 2010/159/01:35:52
294
Vector Time (MET): N/A
Weight (LBS) : 814537
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4117367
11 A = 6728870
44 meter
Y = 2378144
90 meter E =
0005734
Z = -4766543
60 I = 51
29880
XDOT = -1212
974494 Wp = 51
72069
YDOT = -7164
066401 meter/sec RA = 276
55670 deg
ZDOT = -2525
108944 TA = 193
39749
MA = 193
41272
Ha = 191
280 n
mi
Hp = 189
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13508422
28 X = -4120498
62
Y = 7802312
66 feet Y = 2332085
12 meter
Z = -15638266
41 Z = -4786553
37
XDOT = -3979
575113 XDOT = -1120
507765
YDOT = -23504
154858 feet/sec YDOT = -7177
113289 meter/sec
ZDOT = -8284
478164 ZDOT = -2530
777920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9915134
34 X = -3022132
95
Y = -11939197
94 feet Y = -3639067
53 meter
Z = -15717970
46 Z = -4790837
40
XDOT = 21658
774898 XDOT = 6601
594589
YDOT = -7044
451144 feet/sec YDOT = -2147
148709 meter/sec
ZDOT = -8307
081323 ZDOT = -2531
998387
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 10159
08686648
00016717 00000-0 10270-3 0 9144
2 25544 51
6477 277
1749 0006609 269
4422 90
5983 15
71669703 22046
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
08686648 = yrday
fracday
Element set: 914
Inclination: 51
6477 deg
RA of node: 277
1749 deg
Eccentricity:
0006609
Arg of perigee: 269
4422 deg
Mean anomaly: 90
5983 deg
Mean motion: 15
71669703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2204
Checksum: 344
Coasting Arc #16 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2010/160/01:35:52
294
Vector Time (MET): N/A
Weight (LBS) : 814537
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2156957
55 A = 6735261
14 meter
Y = 5697822
73 meter E =
0006845
Z = 2863673
11 I = 51
31767
XDOT = -4131
637071 Wp = 104
03394
YDOT = 4099
497491 meter/sec RA = 271
37220 deg
ZDOT = -5036
291260 TA = 42
94579
MA = 42
89236
Ha = 191
325 n
mi
Hp = 189
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7076632
39 X = 2079171
74
Y = 18693644
12 feet Y = 5721507
78 meter
Z = 9395252
97 Z = 2873963
63
XDOT = -13555
239735 XDOT = -4152
705553
YDOT = 13449
794918 feet/sec YDOT = 4053
177980 meter/sec
ZDOT = -16523
265289 ZDOT = -5056
413657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17098787
99 X = -5211710
58
Y = 10314561
92 feet Y = 3143878
47 meter
Z = 9436264
99 Z = 2876173
57
XDOT = -14927
096467 XDOT = -4549
779003
YDOT = -9530
318190 feet/sec YDOT = -2904
840984 meter/sec
ZDOT = -16603
415342 ZDOT = -5060
720996
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 10160
10421245
00016717 00000-0 10270-3 0 9150
2 25544 51
6474 271
9692 0006637 273
1395 86
9008 15
71658825 22202
Satellite: ISS
Catalog Number: 25544
Epoch time: 10160
10421245 = yrday
fracday
Element set: 915
Inclination: 51
6474 deg
RA of node: 271
9692 deg
Eccentricity:
0006637
Arg of perigee: 273
1395 deg
Mean anomaly: 86
9008 deg
Mean motion: 15
71658825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 306
Coasting Arc #17 (Orbit 2235)
---------------------------------------
Vector Time (GMT): 2010/161/01:35:52
294
Vector Time (MET): N/A
Weight (LBS) : 814537
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2873346
56 A = 6731925
78 meter
Y = -4626220
17 meter E =
0004336
Z = 3954701
09 I = 51
30775
XDOT = 3535
038620 Wp = 106
32436
YDOT = 5578
476412 meter/sec RA = 266
28012 deg
ZDOT = 3952
494466 TA = 302
51138
MA = 302
55327
Ha = 191
401 n
mi
Hp = 189
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9426990
03 X = 2905652
73
Y = -15177887
71 feet Y = -4593908
73 meter
Z = 12974741
12 Z = 3968737
72
XDOT = 11597
895736 XDOT = 3453
195567
YDOT = 18302
087967 feet/sec YDOT = 5617
549051 meter/sec
ZDOT = 12967
501530 ZDOT = 3969
470075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16736944
43 X = 5101420
66
Y = 6136547
67 feet Y = 1870419
73 meter
Z = 13030648
38 Z = 3971741
63
XDOT = -15190
574715 XDOT = -4630
087173
YDOT = 13718
388199 feet/sec YDOT = 4181
364723 meter/sec
ZDOT = 13035
149405 ZDOT = 3973
113539
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 10161
12154348
00016717 00000-0 10270-3 0 9161
2 25544 51
6480 266
7629 0006667 278
1364 81
9042 15
71687200 22364
Satellite: ISS
Catalog Number: 25544
Epoch time: 10161
12154348 = yrday
fracday
Element set: 916
Inclination: 51
6480 deg
RA of node: 266
7629 deg
Eccentricity:
0006667
Arg of perigee: 278
1364 deg
Mean anomaly: 81
9042 deg
Mean motion: 15
71687200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2236
Checksum: 309
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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