Date:
November 30th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 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
There are no maneuvers
Coasting Arc #1 (Orbit 947)
---------------------------------------
Vector Time (GMT): 2010/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2269502
20 A = 6728367
51 meter
Y = -4705314
62 meter E =
0004468
Z = 4241240
04 I = 51
96943
XDOT = 4217
469895 Wp = 25
69131
YDOT = -5314
263453 meter/sec RA = 103
67068 deg
ZDOT = -3633
611645 TA = 101
16016
MA = 101
10992
Ha = 190
182 n
mi
Hp = 189
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7445873
34 X = -2237321
25
Y = -15437383
92 feet Y = -4730513
77 meter
Z = 13914829
53 Z = 4230292
67
XDOT = 13836
843487 XDOT = 4294
233174
YDOT = -17435
247549 feet/sec YDOT = -5266
671837 meter/sec
ZDOT = -11921
298049 ZDOT = -3612
936640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17143105
29 X = 5225218
49
Y = -1043498
79 feet Y = -318058
43 meter
Z = 13870882
61 Z = 4227845
02
XDOT = 10705
068950 XDOT = 3262
905016
YDOT = 18273
978520 feet/sec YDOT = 5569
908653 meter/sec
ZDOT = -11838
096982 ZDOT = -3608
251960
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 10333
54118303
00016717 00000-0 10270-3 0 9002
2 25544 51
6445 104
3301 0007787 278
5933 81
4347 15
72613535 9481
Satellite: ISS
Catalog Number: 25544
Epoch time: 10333
54118303 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 104
3301 deg
Eccentricity:
0007787
Arg of perigee: 278
5933 deg
Mean anomaly: 81
4347 deg
Mean motion: 15
72613535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 948
Checksum: 297
Coasting Arc #2 (Orbit 963)
---------------------------------------
Vector Time (GMT): 2010/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3033952
63 A = 6732445
96 meter
Y = 5300905
59 meter E =
0006914
Z = 2821967
63 I = 51
99116
XDOT = -3353
282053 Wp = 54
73679
YDOT = -4655
315058 meter/sec RA = 98
61714 deg
ZDOT = 5134
696456 TA = 337
42588
MA = 337
45628
Ha = 190
543 n
mi
Hp = 189
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9953912
84 X = -3106711
70
Y = 17391422
55 feet Y = 5266571
19 meter
Z = 9258423
97 Z = 2807051
89
XDOT = -11001
581539 XDOT = -3325
920075
YDOT = -15273
343366 feet/sec YDOT = -4692
660672 meter/sec
ZDOT = 16846
116981 ZDOT = 5118
472231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12505292
85 X = -3811613
26
Y = -15692929
66 feet Y = -4783204
96 meter
Z = 9198368
51 Z = 2803662
72
XDOT = 17136
823790 XDOT = 5223
303891
YDOT = -3810
357292 feet/sec YDOT = -1161
396903 meter/sec
ZDOT = 16780
958459 ZDOT = 5114
836138
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 10334
55788017
00016717 00000-0 10270-3 0 9010
2 25544 51
6455 99
1195 0007874 282
7747 77
2536 15
72707441 9642
Satellite: ISS
Catalog Number: 25544
Epoch time: 10334
55788017 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 99
1195 deg
Eccentricity:
0007874
Arg of perigee: 282
7747 deg
Mean anomaly: 77
2536 deg
Mean motion: 15
72707441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 964
Checksum: 336
Coasting Arc #3 (Orbit 978)
---------------------------------------
Vector Time (GMT): 2010/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3476812
30 A = 6726338
83 meter
Y = 3336027
28 meter E =
0003094
Z = -4696197
36 I = 51
97419
XDOT = -2606
817728 Wp = 113
73350
YDOT = 6672
964227 meter/sec RA = 93
47231 deg
ZDOT = 2810
542231 TA = 183
88646
MA = 183
88887
Ha = 190
869 n
mi
Hp = 188
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11406864
51 X = 3462063
57
Y = 10944971
40 feet Y = 3374824
87 meter
Z = -15407471
65 Z = -4679342
30
XDOT = -8552
551600 XDOT = -2694
895703
YDOT = 21892
927253 feet/sec YDOT = 6643
320607 meter/sec
ZDOT = 9220
939077 ZDOT = 2797
664442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14283401
05 X = -4353580
64
Y = 6926423
70 feet Y = 2111173
94 meter
Z = -15339760
38 Z = -4675558
96
XDOT = -16975
366728 XDOT = -5174
091779
YDOT = -14701
204206 feet/sec YDOT = -4480
927042 meter/sec
ZDOT = 9169
041127 ZDOT = 2794
723735
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 10335
51101712
00016717 00000-0 10270-3 0 9029
2 25544 51
6456 94
2356 0007890 287
6127 72
4174 15
72716824 9798
Satellite: ISS
Catalog Number: 25544
Epoch time: 10335
51101712 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 94
2356 deg
Eccentricity:
0007890
Arg of perigee: 287
6127 deg
Mean anomaly: 72
4174 deg
Mean motion: 15
72716824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 979
Checksum: 311
Coasting Arc #4 (Orbit 994)
---------------------------------------
Vector Time (GMT): 2010/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1461970
73 A = 6733858
13 meter
Y = -6229338
61 meter E =
0003638
Z = -2091767
08 I = 52
00109
XDOT = 4436
313778 Wp = 237
25812
YDOT = 2914
159510 meter/sec RA = 88
41047 deg
ZDOT = -5572
790937 TA = 325
96505
MA = 325
98837
Ha = 190
930 n
mi
Hp = 188
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4796491
90 X = 1541681
36
Y = -20437462
64 feet Y = -6212544
13 meter
Z = -6862752
88 Z = -2084471
51
XDOT = 14554
835231 XDOT = 4430
469620
YDOT = 9560
890781 feet/sec YDOT = 2963
736784 meter/sec
ZDOT = -18283
434834 ZDOT = -5551
252800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17639162
83 X = 5376416
83
Y = 11399984
10 feet Y = 3474715
15 meter
Z = -6833292
62 Z = -2082787
59
XDOT = -13086
055835 XDOT = -3988
629818
YDOT = 9330
617763 feet/sec YDOT = 2843
972294 meter/sec
ZDOT = -18196
889659 ZDOT = -5546
411968
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 10336
52767411
00016717 00000-0 10270-3 0 9036
2 25544 51
6461 89
0245 0007874 292
1143 67
9183 15
72747745 9957
Satellite: ISS
Catalog Number: 25544
Epoch time: 10336
52767411 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 89
0245 deg
Eccentricity:
0007874
Arg of perigee: 292
1143 deg
Mean anomaly: 67
9183 deg
Mean motion: 15
72747745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 995
Checksum: 327
Coasting Arc #5 (Orbit 1010)
---------------------------------------
Vector Time (GMT): 2010/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4148631
28 A = 6724868
47 meter
Y = -1715283
61 meter E =
0007227
Z = 5010937
97 I = 51
96996
XDOT = 677
267477 Wp = 342
35386
YDOT = -7408
436078 meter/sec RA = 83
27464 deg
ZDOT = -1969
252096 TA = 126
63697
MA = 126
57050
Ha = 191
191 n
mi
Hp = 188
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13610995
02 X = -4153485
11
Y = -5627570
90 feet Y = -1761703
75 meter
Z = 16440085
20 Z = 4990771
49
XDOT = 2222
006159 XDOT = 769
626145
YDOT = -24305
892645 feet/sec YDOT = -7400
345860 meter/sec
ZDOT = -6460
800841 ZDOT = -1965
738264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9700154
80 X = 2956607
18
Y = -11202420
59 feet Y = -3414497
80 meter
Z = 16359031
47 Z = 4986232
79
XDOT = 21503
444810 XDOT = 6554
249978
YDOT = 9177
022897 feet/sec YDOT = 2797
156579 meter/sec
ZDOT = -6446
504509 ZDOT = -1964
894574
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 10337
54430963
00016717 00000-0 10270-3 0 9049
2 25544 51
6470 83
8141 0007879 297
3496 62
6864 15
72776796 10113
Satellite: ISS
Catalog Number: 25544
Epoch time: 10337
54430963 = yrday
fracday
Element set: 904
Inclination: 51
6470 deg
RA of node: 83
8141 deg
Eccentricity:
0007879
Arg of perigee: 297
3496 deg
Mean anomaly: 62
6864 deg
Mean motion: 15
72776796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1011
Checksum: 336
Coasting Arc #6 (Orbit 1026)
---------------------------------------
Vector Time (GMT): 2010/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 297725
96 A = 6734787
33 meter
Y = 6583061
74 meter E =
0012358
Z = 1349814
27 I = 51
99957
XDOT = -4890
122097 Wp = 25
66673
YDOT = -984
117554 meter/sec RA = 78
20149 deg
ZDOT = 5869
188615 TA = 349
08627
MA = 349
11306
Ha = 191
358 n
mi
Hp = 187
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 976791
22 X = 217533
52
Y = 21597971
59 feet Y = 6585942
54 meter
Z = 4428524
50 Z = 1351066
68
XDOT = -16043
707666 XDOT = -4907
266099
YDOT = -3228
732133 feet/sec YDOT = -1038
898428 meter/sec
ZDOT = 19255
868160 ZDOT = 5845
390147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20875802
74 X = -6362944
68
Y = -5619979
81 feet Y = -1712969
85 meter
Z = 4433397
56 Z = 1351299
58
XDOT = 7549
488596 XDOT = 2301
084124
YDOT = -12905
128942 feet/sec YDOT = -3933
483302 meter/sec
ZDOT = 19160
189405 ZDOT = 5840
025731
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 10338
56092303
00016717 00000-0 10270-3 0 9055
2 25544 51
6477 78
6035 0007899 301
7805 58
2588 15
72806584 10270
Satellite: ISS
Catalog Number: 25544
Epoch time: 10338
56092303 = yrday
fracday
Element set: 905
Inclination: 51
6477 deg
RA of node: 78
6035 deg
Eccentricity:
0007899
Arg of perigee: 301
7805 deg
Mean anomaly: 58
2588 deg
Mean motion: 15
72806584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1027
Checksum: 329
Coasting Arc #7 (Orbit 1041)
---------------------------------------
Vector Time (GMT): 2010/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4260947
92 A = 6723767
34 meter
Y = 4914
64 meter E =
0008159
Z = -5207508
64 I = 51
95579
XDOT = 1359
609611 Wp = 72
09924
YDOT = 7489
114467 meter/sec RA = 73
07800 deg
ZDOT = 1123
424209 TA = 208
56316
MA = 208
60789
Ha = 191
541 n
mi
Hp = 187
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13979487
92 X = 4285873
82
Y = 16124
13 feet Y = 52703
21 meter
Z = -17085002
12 Z = -5186748
08
XDOT = 4460
661455 XDOT = 1270
306407
YDOT = 24570
585521 feet/sec YDOT = 7503
818961 meter/sec
ZDOT = 3685
774964 ZDOT = 1129
813425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4037891
08 X = -1230749
20
Y = 13489541
99 feet Y = 4111612
40 meter
Z = -17001509
71 Z = -5182060
16
XDOT = -23831
017149 XDOT = -7263
694027
YDOT = -2472
093102 feet/sec YDOT = -753
493977 meter/sec
ZDOT = 3711
269161 ZDOT = 1131
194840
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 10339
51397841
00016717 00000-0 10270-3 0 9067
2 25544 51
6479 73
7197 0007960 305
8858 54
1565 15
72860088 10425
Satellite: ISS
Catalog Number: 25544
Epoch time: 10339
51397841 = yrday
fracday
Element set: 906
Inclination: 51
6479 deg
RA of node: 73
7197 deg
Eccentricity:
0007960
Arg of perigee: 305
8858 deg
Mean anomaly: 54
1565 deg
Mean motion: 15
72860088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1042
Checksum: 336
Coasting Arc #8 (Orbit 1057)
---------------------------------------
Vector Time (GMT): 2010/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2050300
52 A = 6735222
24 meter
Y = -6382567
31 meter E =
0003303
Z = -628136
14 I = 51
98403
XDOT = 4704
281833 Wp = 164
71837
YDOT = -919
721006 meter/sec RA = 67
99066 deg
ZDOT = -6020
099560 TA = 22
08212
MA = 22
06789
Ha = 191
603 n
mi
Hp = 187
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6726707
76 X = -1975725
68
Y = -20940181
48 feet Y = -6405077
94 meter
Z = -2060814
10 Z = -637916
40
XDOT = 15433
995516 XDOT = 4743
461560
YDOT = -3017
457368 feet/sec YDOT = -866
894949 meter/sec
ZDOT = -19750
982810 ZDOT = -5997
150873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21974725
23 X = 6697896
25
Y = -829661
11 feet Y = -252880
71 meter
Z = -2099968
06 Z = -640070
26
XDOT = -1339
842753 XDOT = -408
384071
YDOT = 14187
291827 feet/sec YDOT = 4324
286549 meter/sec
ZDOT = -19658
657102 ZDOT = -5991
958685
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 10340
53055086
00016717 00000-0 10270-3 0 9074
2 25544 51
6474 68
5092 0007937 309
6701 50
3761 15
72866617 10586
Satellite: ISS
Catalog Number: 25544
Epoch time: 10340
53055086 = yrday
fracday
Element set: 907
Inclination: 51
6474 deg
RA of node: 68
5092 deg
Eccentricity:
0007937
Arg of perigee: 309
6701 deg
Mean anomaly: 50
3761 deg
Mean motion: 15
72866617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1058
Checksum: 314
Coasting Arc #9 (Orbit 1073)
---------------------------------------
Vector Time (GMT): 2010/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3848066
42 A = 6723153
79 meter
Y = 1571152
52 meter E =
0007136
Z = 5287574
23 I = 51
93224
XDOT = -3283
267680 Wp = 331
42923
YDOT = -6954
358345 meter/sec RA = 62
87695 deg
ZDOT = -317
045356 TA = 121
60471
MA = 121
53505
Ha = 191
795 n
mi
Hp = 187
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12624889
83 X = -3891035
57
Y = 5154699
87 feet Y = 1527880
11 meter
Z = 17347684
48 Z = 5268776
06
XDOT = -10771
875591 XDOT = -3203
718568
YDOT = -22816
136302 feet/sec YDOT = -6990
628990 meter/sec
ZDOT = -1040
175053 ZDOT = -332
803345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1773424
02 X = -540539
64
Y = -13617378
60 feet Y = -4150577
00 meter
Z = 17272026
46 Z = 5264513
67
XDOT = 23802
541361 XDOT = 7255
014607
YDOT = -4524
209860 feet/sec YDOT = -1378
979165 meter/sec
ZDOT = -1103
350603 ZDOT = -336
301264
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 10341
54709994
00016717 00000-0 10270-3 0 9081
2 25544 51
6481 63
2977 0008085 313
9349 46
1146 15
72940825 10741
Satellite: ISS
Catalog Number: 25544
Epoch time: 10341
54709994 = yrday
fracday
Element set: 908
Inclination: 51
6481 deg
RA of node: 63
2977 deg
Eccentricity:
0008085
Arg of perigee: 313
9349 deg
Mean anomaly: 46
1146 deg
Mean motion: 15
72940825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1074
Checksum: 326
Coasting Arc #10 (Orbit 1088)
---------------------------------------
Vector Time (GMT): 2010/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3633002
62 A = 6735294
97 meter
Y = 5659193
66 meter E =
0015165
Z = -70987
97 I = 51
95743
XDOT = -3962
361364 Wp = 12
22223
YDOT = 2616
683413 meter/sec RA = 57
77423 deg
ZDOT = 6067
017894 TA = 347
00984
MA = 347
04886
Ha = 192
054 n
mi
Hp = 186
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11919299
93 X = 3569795
29
Y = 18566908
34 feet Y = 5699466
68 meter
Z = -232900
15 Z = -53491
58
XDOT = -12999
873241 XDOT = -4020
799645
YDOT = 8584
919335 feet/sec YDOT = 2572
046349 meter/sec
ZDOT = 19904
914351 ZDOT = 6047
627104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20854925
12 X = -6356581
18
Y = 7204142
37 feet Y = 2195822
59 meter
Z = -162694
93 Z = -49589
42
XDOT = -4723
525075 XDOT = -1439
730443
YDOT = -13252
496496 feet/sec YDOT = -4039
360932 meter/sec
ZDOT = 19826
834707 ZDOT = 6043
219219
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 10342
50009787
00016717 00000-0 10270-3 0 9092
2 25544 51
6476 58
4128 0008160 319
4014 40
6539 15
72905516 10892
Satellite: ISS
Catalog Number: 25544
Epoch time: 10342
50009787 = yrday
fracday
Element set: 909
Inclination: 51
6476 deg
RA of node: 58
4128 deg
Eccentricity:
0008160
Arg of perigee: 319
4014 deg
Mean anomaly: 40
6539 deg
Mean motion: 15
72905516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1089
Checksum: 308
Coasting Arc #11 (Orbit 1104)
---------------------------------------
Vector Time (GMT): 2010/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2980927
86 A = 6723156
67 meter
Y = -2919622
12 meter E =
0012399
Z = -5280666
09 I = 51
89874
XDOT = 4936
508648 Wp = 53
28839
YDOT = 5880
859888 meter/sec RA = 52
67194 deg
ZDOT = -458
303631 TA = 212
33115
MA = 212
40720
Ha = 192
125 n
mi
Hp = 186
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9779947
05 X = 3039006
58
Y = -9578812
73 feet Y = -2885962
24 meter
Z = -17325019
99 Z = -5266044
02
XDOT = 16195
894515 XDOT = 4872
607236
YDOT = 19294
159736 feet/sec YDOT = 5935
705659 meter/sec
ZDOT = -1503
620836 ZDOT = -434
476609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7180825
62 X = 2188715
65
Y = 11741999
62 feet Y = 3578961
48 meter
Z = -17266109
10 Z = -5262710
06
XDOT = -21520
051019 XDOT = -6559
311551
YDOT = 11058
754451 feet/sec YDOT = 3370
708357 meter/sec
ZDOT = -1407
957754 ZDOT = -429
145523
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 10343
51660759
00016717 00000-0 10270-3 0 9108
2 25544 51
6466 53
2017 0008166 322
7090 37
3505 15
72949412 11056
Satellite: ISS
Catalog Number: 25544
Epoch time: 10343
51660759 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 53
2017 deg
Eccentricity:
0008166
Arg of perigee: 322
7090 deg
Mean anomaly: 37
3505 deg
Mean motion: 15
72949412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1105
Checksum: 288
Coasting Arc #12 (Orbit 1120)
---------------------------------------
Vector Time (GMT): 2010/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4914309
97 A = 6734776
47 meter
Y = -4547867
63 meter E =
0006365
Z = 710678
26 I = 51
91914
XDOT = 2770
660445 Wp = 101
06363
YDOT = -3938
631432 meter/sec RA = 47
55277 deg
ZDOT = -6001
694902 TA = 71
23054
MA = 71
16150
Ha = 192
213 n
mi
Hp = 186
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16123064
19 X = -4866541
96
Y = -14920825
55 feet Y = -4602555
38 meter
Z = 2331621
57 Z = 686920
15
XDOT = 9090
093322 XDOT = 2843
652151
YDOT = -12922
019133 feet/sec YDOT = -3907
239536 meter/sec
ZDOT = -19690
600073 ZDOT = -5988
058133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17877097
24 X = 5448939
24
Y = -12783955
64 feet Y = -3896549
68 meter
Z = 2236194
47 Z = 681592
07
XDOT = 9860
397024 XDOT = 3005
449013
YDOT = 10327
805686 feet/sec YDOT = 3147
915173 meter/sec
ZDOT = -19635
617602 ZDOT = -5984
936245
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 10344
53309615
00016717 00000-0 10270-3 0 9113
2 25544 51
6467 47
9899 0008174 328
2620 31
8049 15
73014789 11215
Satellite: ISS
Catalog Number: 25544
Epoch time: 10344
53309615 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 47
9899 deg
Eccentricity:
0008174
Arg of perigee: 328
2620 deg
Mean anomaly: 31
8049 deg
Mean motion: 15
73014789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1121
Checksum: 312
Coasting Arc #13 (Orbit 1136)
---------------------------------------
Vector Time (GMT): 2010/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1800950
66 A = 6723221
64 meter
Y = 3875900
97 meter E =
0005095
Z = 5189761
40 I = 51
85928
XDOT = -6191
556107 Wp = 351
48411
YDOT = -4427
397795 meter/sec RA = 42
45851 deg
ZDOT = 1163
023940 TA = 87
47293
MA = 87
41461
Ha = 192
370 n
mi
Hp = 186
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5908630
78 X = -1869368
78
Y = 12716210
52 feet Y = 3855378
69 meter
Z = 17026776
26 Z = 5180846
51
XDOT = -20313
504287 XDOT = -6147
237704
YDOT = -14525
583318 feet/sec YDOT = -4496
387799 meter/sec
ZDOT = 3815
695340 ZDOT = 1133
052654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11381706
72 X = -3469144
21
Y = -8264072
25 feet Y = -2518889
22 meter
Z = 16990788
66 Z = 5178792
39
XDOT = 17442
253429 XDOT = 5316
398845
YDOT = -16459
273907 feet/sec YDOT = -5016
786687 meter/sec
ZDOT = 3695
272647 ZDOT = 1126
319103
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 10345
54956285
00016717 00000-0 10270-3 0 9127
2 25544 51
6467 42
7777 0008201 331
6307 28
4408 15
73048767 11375
Satellite: ISS
Catalog Number: 25544
Epoch time: 10345
54956285 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 42
7777 deg
Eccentricity:
0008201
Arg of perigee: 331
6307 deg
Mean anomaly: 28
4408 deg
Mean motion: 15
73048767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1137
Checksum: 316
Coasting Arc #14 (Orbit 1151)
---------------------------------------
Vector Time (GMT): 2010/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5806015
28 A = 6734220
14 meter
Y = 3127366
62 meter E =
0015006
Z = -1316661
63 I = 51
87235
XDOT = -1272
281418 Wp = 7
86123
YDOT = 4824
187134 meter/sec RA = 37
32446 deg
ZDOT = 5870
561191 TA = 337
72664
MA = 337
79175
Ha = 192
631 n
mi
Hp = 185
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19048606
57 X = 5777009
08
Y = 10260389
18 feet Y = 3192130
89 meter
Z = -4319756
01 Z = -1288526
19
XDOT = -4174
151635 XDOT = -1354
650005
YDOT = 15827
385611 feet/sec YDOT = 4809
498767 meter/sec
ZDOT = 19260
371360 ZDOT = 5864
180691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13327942
64 X = -4062356
92
Y = 17072055
58 feet Y = 5203562
54 meter
Z = -4206679
66 Z = -1282195
96
XDOT = -13634
084583 XDOT = -4155
668981
YDOT = -5922
981306 feet/sec YDOT = -1805
324702 meter/sec
ZDOT = 19234
545724 ZDOT = 5862
689537
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 10346
50248302
00016717 00000-0 10270-3 0 9139
2 25544 51
6463 37
8915 0008385 336
6157 23
4624 15
73031493 11521
Satellite: ISS
Catalog Number: 25544
Epoch time: 10346
50248302 = yrday
fracday
Element set: 913
Inclination: 51
6463 deg
RA of node: 37
8915 deg
Eccentricity:
0008385
Arg of perigee: 336
6157 deg
Mean anomaly: 23
4624 deg
Mean motion: 15
73031493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1152
Checksum: 294
Coasting Arc #15 (Orbit 1167)
---------------------------------------
Vector Time (GMT): 2010/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 403126
98 A = 6723768
95 meter
Y = -4438348
49 meter E =
0014993
Z = -5046365
89 I = 51
81333
XDOT = 6965
401224 Wp = 43
12967
YDOT = 2704
906148 meter/sec RA = 32
23731 deg
ZDOT = -1815
024704 TA = 209
35217
MA = 209
43647
Ha = 192
598 n
mi
Hp = 185
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1322595
06 X = 477241
91
Y = -14561510
79 feet Y = -4433425
76 meter
Z = -16556318
54 Z = -5044227
74
XDOT = 22852
366221 XDOT = 6943
453876
YDOT = 8874
364002 feet/sec YDOT = 2782
674860 meter/sec
ZDOT = -5954
805460 ZDOT = -1781
239752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14178612
30 X = 4321641
03
Y = 3611574
81 feet Y = 1100808
00 meter
Z = -16547568
34 Z = -5043698
83
XDOT = -11976
778586 XDOT = -3650
522113
YDOT = 20244
307457 feet/sec YDOT = 6170
464913 meter/sec
ZDOT = -5818
994246 ZDOT = -1773
629446
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 10347
51891075
00016717 00000-0 10270-3 0 9143
2 25544 51
6468 32
6792 0008240 340
8542 19
2310 15
73081339 11683
Satellite: ISS
Catalog Number: 25544
Epoch time: 10347
51891075 = yrday
fracday
Element set: 914
Inclination: 51
6468 deg
RA of node: 32
6792 deg
Eccentricity:
0008240
Arg of perigee: 340
8542 deg
Mean anomaly: 19
2310 deg
Mean motion: 15
73081339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1168
Checksum: 300
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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