Date:
December 6th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12109 4 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 1010)
---------------------------------------
Vector Time (GMT): 2010/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4146096
96 A = 6724826
08 meter
Y = -1741518
33 meter E =
0007252
Z = 5003859
86 I = 51
96988
XDOT = 696
613291 Wp = 343
43298
YDOT = -7400
542385 meter/sec RA = 83
27630 deg
ZDOT = -1992
359091 TA = 125
78924
MA = 125
72181
Ha = 191
168 n
mi
Hp = 188
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13602680
30 X = -4150623
23
Y = -5713642
81 feet Y = -1787908
30 meter
Z = 16416863
05 Z = 4983706
48
XDOT = 2285
476676 XDOT = 788
994504
YDOT = -24279
994700 feet/sec YDOT = -7392
235702 meter/sec
ZDOT = -6536
611192 ZDOT = -1988
751219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9779052
74 X = 2980655
27
Y = -11166993
25 feet Y = -3403699
54 meter
Z = 16335862
61 Z = 4979170
92
XDOT = 21461
122723 XDOT = 6541
350206
YDOT = 9223
613354 feet/sec YDOT = 2811
357350 meter/sec
ZDOT = -6521
936893 ZDOT = -1987
886365
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
54426835
00016717 00000-0 10270-3 0 9008
2 25544 51
6468 83
8163 0007838 297
8548 62
1820 15
72802254 10118
Satellite: ISS
Catalog Number: 25544
Epoch time: 10337
54426835 = yrday
fracday
Element set: 900
Inclination: 51
6468 deg
RA of node: 83
8163 deg
Eccentricity:
0007838
Arg of perigee: 297
8548 deg
Mean anomaly: 62
1820 deg
Mean motion: 15
72802254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1011
Checksum: 310
Coasting Arc #2 (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 = 273058
15 A = 6734671
32 meter
Y = 6577928
90 meter E =
0012389
Z = 1379093
50 I = 51
99928
XDOT = -4892
035920 Wp = 26
25851
YDOT = -1027
447350 meter/sec RA = 78
20334 deg
ZDOT = 5860
268170 TA = 348
82236
MA = 348
84986
Ha = 191
330 n
mi
Hp = 187
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 895860
06 X = 192782
70
Y = 21581131
57 feet Y = 6580533
39 meter
Z = 4524584
97 Z = 1380225
87
XDOT = -16049
986613 XDOT = -4908
651923
YDOT = -3370
890256 feet/sec YDOT = -1082
246672 meter/sec
ZDOT = 19226
601606 ZDOT = 5836
461681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20835127
48 X = -6350546
86
Y = -5692584
54 feet Y = -1735099
77 meter
Z = 4528975
42 Z = 1380431
71
XDOT = 7681
553352 XDOT = 2341
337462
YDOT = -12870
960303 feet/sec YDOT = -3923
068700 meter/sec
ZDOT = 19130
891673 ZDOT = 5831
095782
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
56086410
00016717 00000-0 10270-3 0 9013
2 25544 51
6474 78
6055 0007860 302
2974 57
7427 15
72835151 10278
Satellite: ISS
Catalog Number: 25544
Epoch time: 10338
56086410 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 78
6055 deg
Eccentricity:
0007860
Arg of perigee: 302
2974 deg
Mean anomaly: 57
7427 deg
Mean motion: 15
72835151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1027
Checksum: 305
Coasting Arc #3 (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 = 4269813
55 A = 6723712
14 meter
Y = 54624
78 meter E =
0008157
Z = -5199875
19 I = 51
95573
XDOT = 1322
505855 Wp = 72
37278
YDOT = 7488
897635 meter/sec RA = 73
07899 deg
ZDOT = 1168
536223 TA = 208
72387
MA = 208
76881
Ha = 191
508 n
mi
Hp = 187
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14008574
65 X = 4294145
84
Y = 179215
16 feet Y = 102509
18 meter
Z = -17059957
97 Z = -5179072
99
XDOT = 4338
929970 XDOT = 1232
988683
YDOT = 24569
874130 feet/sec YDOT = 7503
186010 meter/sec
ZDOT = 3833
780258 ZDOT = 1174
744666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4202452
41 X = -1280907
49
Y = 13470675
50 feet Y = 4105861
89 meter
Z = -16976299
46 Z = -5174376
08
XDOT = -23796
685601 XDOT = -7253
229771
YDOT = -2577
390674 feet/sec YDOT = -785
588677 meter/sec
ZDOT = 3858
547451 ZDOT = 1176
085263
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
51390154
00016717 00000-0 10270-3 0 9023
2 25544 51
6476 73
7216 0007920 306
4284 53
6148 15
72891440 10427
Satellite: ISS
Catalog Number: 25544
Epoch time: 10339
51390154 = yrday
fracday
Element set: 902
Inclination: 51
6476 deg
RA of node: 73
7216 deg
Eccentricity:
0007920
Arg of perigee: 306
4284 deg
Mean anomaly: 53
6148 deg
Mean motion: 15
72891440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1042
Checksum: 294
Coasting Arc #4 (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 = -2010505
34 A = 6735098
41 meter
Y = -6389991
19 meter E =
0003198
Z = -678651
45 I = 51
98377
XDOT = 4726
613636 Wp = 165
18199
YDOT = -849
525641 meter/sec RA = 67
99223 deg
ZDOT = -6012
910668 TA = 22
16840
MA = 22
15457
Ha = 191
568 n
mi
Hp = 187
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6596146
13 X = -1935605
04
Y = -20964538
03 feet Y = -6412054
98 meter
Z = -2226546
75 Z = -688237
59
XDOT = 15507
262585 XDOT = 4764
971842
YDOT = -2787
157614 feet/sec YDOT = -796
454451 meter/sec
ZDOT = -19727
397204 ZDOT = -5989
855476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21962778
89 X = 6694255
01
Y = -696412
80 feet Y = -212266
62 meter
Z = -2264919
76 Z = -690347
54
XDOT = -1571
610376 XDOT = -479
026843
YDOT = 14196
595468 feet/sec YDOT = 4327
122299 meter/sec
ZDOT = -19634
645142 ZDOT = -5984
639839
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
53045332
00016717 00000-0 10270-3 0 9033
2 25544 51
6471 68
5108 0007901 310
2230 49
8241 15
72899869 10588
Satellite: ISS
Catalog Number: 25544
Epoch time: 10340
53045332 = yrday
fracday
Element set: 903
Inclination: 51
6471 deg
RA of node: 68
5108 deg
Eccentricity:
0007901
Arg of perigee: 310
2230 deg
Mean anomaly: 49
8241 deg
Mean motion: 15
72899869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1058
Checksum: 295
Coasting Arc #5 (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 = -3881502
64 A = 6723069
56 meter
Y = 1499455
26 meter E =
0007237
Z = 5283816
80 I = 51
93213
XDOT = -3231
282428 Wp = 332
89544
YDOT = -6975
149878 meter/sec RA = 62
87716 deg
ZDOT = -388
188534 TA = 120
81309
MA = 120
74184
Ha = 191
756 n
mi
Hp = 187
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12734588
71 X = -3923649
32
Y = 4919472
65 feet Y = 1455813
55 meter
Z = 17335356
97 Z = 5264858
19
XDOT = -10601
320302 XDOT = -3151
159082
YDOT = -22884
349992 feet/sec YDOT = -7010
835972 meter/sec
ZDOT = -1273
584430 ZDOT = -403
692585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1518134
60 X = -462727
42
Y = -13664033
98 feet Y = -4164797
56 meter
Z = 17259055
73 Z = 5260560
19
XDOT = 23821
721259 XDOT = 7260
860640
YDOT = -4359
227602 feet/sec YDOT = -1328
692573 meter/sec
ZDOT = -1335
737957 ZDOT = -407
132929
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
54698016
00016717 00000-0 10270-3 0 9049
2 25544 51
6478 63
2992 0008051 314
5029 45
5475 15
72976560 10742
Satellite: ISS
Catalog Number: 25544
Epoch time: 10341
54698016 = yrday
fracday
Element set: 904
Inclination: 51
6478 deg
RA of node: 63
2992 deg
Eccentricity:
0008051
Arg of perigee: 314
5029 deg
Mean anomaly: 45
5475 deg
Mean motion: 15
72976560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1074
Checksum: 315
Coasting Arc #6 (Orbit 1089)
---------------------------------------
Vector Time (GMT): 2010/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3583830
55 A = 6735185
22 meter
Y = 5690715
33 meter E =
0015254
Z = 3469
49 I = 51
95727
XDOT = -4020
621751 Wp = 13
28016
YDOT = 2525
182871 meter/sec RA = 57
77546 deg
ZDOT = 6067
612329 TA = 346
75737
MA = 346
79737
Ha = 192
006 n
mi
Hp = 186
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11757974
25 X = 3519912
70
Y = 18670325
88 feet Y = 5730434
49 meter
Z = 11382
83 Z = 20725
28
XDOT = -13191
016243 XDOT = -4078
035413
YDOT = 8284
720704 feet/sec YDOT = 2479
900032 meter/sec
ZDOT = 19906
864596 ZDOT = 6047
940986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20917034
63 X = -6375512
15
Y = 7021561
03 feet Y = 2140171
80 meter
Z = 80619
27 Z = 24572
75
XDOT = -4400
020497 XDOT = -1341
126248
YDOT = -13362
907414 feet/sec YDOT = -4073
014180 meter/sec
ZDOT = 19827
659241 ZDOT = 6043
470537
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
56348809
00016717 00000-0 10270-3 0 9055
2 25544 51
6474 58
0883 0008119 320
2166 39
8401 15
72946173 10900
Satellite: ISS
Catalog Number: 25544
Epoch time: 10342
56348809 = yrday
fracday
Element set: 905
Inclination: 51
6474 deg
RA of node: 58
0883 deg
Eccentricity:
0008119
Arg of perigee: 320
2166 deg
Mean anomaly: 39
8401 deg
Mean motion: 15
72946173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1090
Checksum: 309
Coasting Arc #7 (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 = 3051792
91 A = 6723016
17 meter
Y = -2834298
98 meter E =
0012410
Z = -5286505
29 I = 51
89849
XDOT = 4879
650750 Wp = 54
31261
YDOT = 5935
074217 meter/sec RA = 52
67128 deg
ZDOT = -358
605954 TA = 212
25290
MA = 212
32885
Ha = 192
080 n
mi
Hp = 186
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10012443
93 X = 3108940
63
Y = -9298881
16 feet Y = -2799851
85 meter
Z = -17344177
47 Z = -5271541
20
XDOT = 16009
352854 XDOT = 4814
663015
YDOT = 19472
028271 feet/sec YDOT = 5989
278084 meter/sec
ZDOT = -1176
528721 ZDOT = -335
057780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6856724
12 X = 2089929
51
Y = 11907605
86 feet Y = 3629438
27 meter
Z = -17283893
47 Z = -5268130
73
XDOT = -21640
226236 XDOT = -6595
940957
YDOT = 10859
502185 feet/sec YDOT = 3309
976266 meter/sec
ZDOT = -1081
989044 ZDOT = -329
790261
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
51644028
00016717 00000-0 10270-3 0 9064
2 25544 51
6464 53
2028 0008133 323
3115 36
7490 15
72989793 11057
Satellite: ISS
Catalog Number: 25544
Epoch time: 10343
51644028 = yrday
fracday
Element set: 906
Inclination: 51
6464 deg
RA of node: 53
2028 deg
Eccentricity:
0008133
Arg of perigee: 323
3115 deg
Mean anomaly: 36
7490 deg
Mean motion: 15
72989793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1105
Checksum: 295
Coasting Arc #8 (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 = -4866923
78 A = 6734712
10 meter
Y = -4612894
88 meter E =
0006222
Z = 610164
68 I = 51
91914
XDOT = 2877
652974 Wp = 102
27595
YDOT = -3838
520453 meter/sec RA = 47
55358 deg
ZDOT = -6016
207825 TA = 71
11331
MA = 71
04586
Ha = 192
162 n
mi
Hp = 186
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15967597
69 X = -4817943
87
Y = -15134169
54 feet Y = -4667045
94 meter
Z = 2001852
63 Z = 586639
71
XDOT = 9441
118682 XDOT = 2949
587770
YDOT = -12593
571040 feet/sec YDOT = -3805
938011 meter/sec
ZDOT = -19738
214649 ZDOT = -6002
053844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18054188
97 X = 5502916
80
Y = -12586615
72 feet Y = -3836400
47 meter
Z = 1907365
45 Z = 581364
99
XDOT = 9482
054411 XDOT = 2890
130185
YDOT = 10592
473225 feet/sec YDOT = 3228
585839 meter/sec
ZDOT = -19681
154775 ZDOT = -5998
815975
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
53290207
00016717 00000-0 10270-3 0 9074
2 25544 51
6464 47
9908 0008136 328
8651 31
2029 15
73056594 11213
Satellite: ISS
Catalog Number: 25544
Epoch time: 10344
53290207 = yrday
fracday
Element set: 907
Inclination: 51
6464 deg
RA of node: 47
9908 deg
Eccentricity:
0008136
Arg of perigee: 328
8651 deg
Mean anomaly: 31
2029 deg
Mean motion: 15
73056594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1121
Checksum: 301
Coasting Arc #9 (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 = -1918846
36 A = 6723001
09 meter
Y = 3790244
49 meter E =
0005339
Z = 5210585
18 I = 51
85880
XDOT = -6145
129375 Wp = 350
91933
YDOT = -4523
373150 meter/sec RA = 42
45696 deg
ZDOT = 1032
660864 TA = 89
29325
MA = 89
23207
Ha = 192
315 n
mi
Hp = 185
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6295427
69 X = -1986399
04
Y = 12435185
34 feet Y = 3768408
67 meter
Z = 17095095
75 Z = 5201099
65
XDOT = -20161
185613 XDOT = -6099
107928
YDOT = -14840
463091 feet/sec YDOT = -4591
834449 meter/sec
ZDOT = 3387
994959 ZDOT = 1002
919248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11033750
95 X = -3363087
29
Y = -8592434
55 feet Y = -2618974
05 meter
Z = 17056815
40 Z = 5198917
33
XDOT = 17699
022746 XDOT = 5394
662133
YDOT = -16274
071663 feet/sec YDOT = -4960
337043 meter/sec
ZDOT = 3268
499274 ZDOT = 996
238579
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
54934037
00016717 00000-0 10270-3 0 9083
2 25544 51
6465 42
7784 0008167 332
2225 27
8501 15
73094155 11377
Satellite: ISS
Catalog Number: 25544
Epoch time: 10345
54934037 = yrday
fracday
Element set: 908
Inclination: 51
6465 deg
RA of node: 42
7784 deg
Eccentricity:
0008167
Arg of perigee: 332
2225 deg
Mean anomaly: 27
8501 deg
Mean motion: 15
73094155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1137
Checksum: 304
Coasting Arc #10 (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 = 5776587
73 A = 6734229
31 meter
Y = 3230727
96 meter E =
0015348
Z = -1189257
91 I = 51
87264
XDOT = -1436
807701 Wp = 9
07960
YDOT = 4733
949721 meter/sec RA = 37
32473 deg
ZDOT = 5906
284352 TA = 337
92825
MA = 337
99427
Ha = 192
578 n
mi
Hp = 185
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18952059
49 X = 5745809
01
Y = 10599501
17 feet Y = 3295153
23 meter
Z = -3901764
81 Z = -1161269
73
XDOT = -4713
936027 XDOT = -1518
328545
YDOT = 15531
331107 feet/sec YDOT = 4717
426260 meter/sec
ZDOT = 19377
573334 ZDOT = 5899
106635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13645530
94 X = -4159157
83
Y = 16917285
92 feet Y = 5156388
75 meter
Z = -3789284
24 Z = -1154973
84
XDOT = -13262
471029 XDOT = -4042
401170
YDOT = -6382
672441 feet/sec YDOT = -1945
438560 meter/sec
ZDOT = 19348
543734 ZDOT = 5897
436130
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
50223257
00016717 00000-0 10270-3 0 9096
2 25544 51
6461 37
8920 0008362 337
2948 22
7844 15
73075734 11527
Satellite: ISS
Catalog Number: 25544
Epoch time: 10346
50223257 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 37
8920 deg
Eccentricity:
0008362
Arg of perigee: 337
2948 deg
Mean anomaly: 22
7844 deg
Mean motion: 15
73075734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1152
Checksum: 307
Coasting Arc #11 (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 = 572325
80 A = 6723447
66 meter
Y = -4370839
69 meter E =
0015156
Z = -5088470
37 I = 51
81252
XDOT = 6949
959038 Wp = 44
82339
YDOT = 2844
440541 meter/sec RA = 32
23485 deg
ZDOT = -1654
046004 TA = 209
25123
MA = 209
33617
Ha = 192
537 n
mi
Hp = 185
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1877709
31 X = 645877
80
Y = -14340025
23 feet Y = -4364028
02 meter
Z = -16694456
60 Z = -5085511
62
XDOT = 22801
702882 XDOT = 6925
670529
YDOT = 9332
154006 feet/sec YDOT = 2922
023469 meter/sec
ZDOT = -5426
660119 ZDOT = -1620
341748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13875441
56 X = 4229234
59
Y = 4127516
33 feet Y = 1258066
98 meter
Z = -16682407
72 Z = -5084797
87
XDOT = -12383
524757 XDOT = -3774
498346
YDOT = 20143
849959 feet/sec YDOT = 6139
845468 meter/sec
ZDOT = -5291
178212 ZDOT = -1612
751119
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
51862897
00016717 00000-0 10270-3 0 9109
2 25544 51
6466 32
6794 0008210 341
4747 18
6116 15
73130537 11686
Satellite: ISS
Catalog Number: 25544
Epoch time: 10347
51862897 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 32
6794 deg
Eccentricity:
0008210
Arg of perigee: 341
4747 deg
Mean anomaly: 18
6116 deg
Mean motion: 15
73130537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1168
Checksum: 309
Coasting Arc #12 (Orbit 1183)
---------------------------------------
Vector Time (GMT): 2010/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6285146
28 A = 6733255
01 meter
Y = -1727748
12 meter E =
0010796
Z = 1683610
43 I = 51
81990
XDOT = -133
721185 Wp = 79
61234
YDOT = -5131
821723 meter/sec RA = 27
08942 deg
ZDOT = -5732
679552 TA = 81
83704
MA = 81
71460
Ha = 192
638 n
mi
Hp = 185
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20620558
66 X = -6273537
89
Y = -5668464
97 feet Y = -1797967
62 meter
Z = 5523656
27 Z = 1653105
03
XDOT = -438
717797 XDOT = -48
477709
YDOT = -16836
685442 feet/sec YDOT = -5132
840080 meter/sec
ZDOT = -18808
003780 ZDOT = -5733
122449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8395005
12 X = 2558797
56
Y = -19702860
18 feet Y = -6005431
78 meter
Z = 5401009
43 Z = 1646227
68
XDOT = 15291
595047 XDOT = 4660
878170
YDOT = 1329
062279 feet/sec YDOT = 405
098183 meter/sec
ZDOT = -18809
608086 ZDOT = -5733
168545
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 10348
53500172
00016717 00000-0 10270-3 0 9118
2 25544 51
6468 27
4668 0008369 346
2806 13
8128 15
73207732 11844
Satellite: ISS
Catalog Number: 25544
Epoch time: 10348
53500172 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 27
4668 deg
Eccentricity:
0008369
Arg of perigee: 346
2806 deg
Mean anomaly: 13
8128 deg
Mean motion: 15
73207732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1184
Checksum: 306
Coasting Arc #13 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2010/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 810621
23 A = 6723841
47 meter
Y = 4507578
00 meter E =
0006172
Z = 4917920
40 I = 51
76040
XDOT = -7303
346025 Wp = 39
55613
YDOT = -1082
290157 meter/sec RA = 22
00378 deg
ZDOT = 2198
960204 TA = 29
15035
MA = 29
11591
Ha = 192
752 n
mi
Hp = 184
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2659518
46 X = 736265
77
Y = 14788641
73 feet Y = 4516226
75 meter
Z = 16134909
46 Z = 4921678
16
XDOT = -23961
109007 XDOT = -7301
383117
YDOT = -3550
820725 feet/sec YDOT = -1163
949754 meter/sec
ZDOT = 7214
436365 ZDOT = 2163
484846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14988007
85 X = -4568344
79
Y = 808561
16 feet Y = 246449
44 meter
Z = 16149864
25 Z = 4922478
62
XDOT = 6404
299582 XDOT = 1952
030513
YDOT = -22327
513215 feet/sec YDOT = -6805
426028 meter/sec
ZDOT = 7071
780974 ZDOT = 2155
478841
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 10349
55135363
00016717 00000-0 10270-3 0 9128
2 25544 51
6463 22
2542 0008282 351
1024 8
9991 15
73221870 12005
Satellite: ISS
Catalog Number: 25544
Epoch time: 10349
55135363 = yrday
fracday
Element set: 912
Inclination: 51
6463 deg
RA of node: 22
2542 deg
Eccentricity:
0008282
Arg of perigee: 351
1024 deg
Mean anomaly: 8
9991 deg
Mean motion: 15
73221870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 277
Coasting Arc #14 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2010/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6370318
95 A = 6732286
84 meter
Y = 158961
88 meter E =
0013516
Z = -2149809
07 I = 51
76150
XDOT = 1732
166001 Wp = 14
57621
YDOT = 5076
313030 meter/sec RA = 16
84687 deg
ZDOT = 5528
406180 TA = 321
40795
MA = 321
50448
Ha = 192
853 n
mi
Hp = 184
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20899996
57 X = 6378511
47
Y = 521528
47 feet Y = 230244
61 meter
Z = -7053179
36 Z = -2118841
74
XDOT = 5682
959320 XDOT = 1648
416635
YDOT = 16654
570309 feet/sec YDOT = 5095
214406 meter/sec
ZDOT = 18137
815552 ZDOT = 5536
618163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2620248
15 X = -798651
64
Y = 20783590
06 feet Y = 6334838
25 meter
Z = -6928626
96 Z = -2111845
50
XDOT = -15615
131467 XDOT = -4759
492071
YDOT = 4066
313931 feet/sec YDOT = 1239
412486 meter/sec
ZDOT = 18170
659982 ZDOT = 5538
417162
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 10350
50416319
00016717 00000-0 10270-3 0 9139
2 25544 51
6474 17
3677 0008270 354
9992 5
1087 15
73278934 12157
Satellite: ISS
Catalog Number: 25544
Epoch time: 10350
50416319 = yrday
fracday
Element set: 913
Inclination: 51
6474 deg
RA of node: 17
3677 deg
Eccentricity:
0008270
Arg of perigee: 354
9992 deg
Mean anomaly: 5
1087 deg
Mean motion: 15
73278934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1215
Checksum: 310
Coasting Arc #15 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2010/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2168010
18 A = 6724458
44 meter
Y = -4270164
60 meter E =
0016007
Z = -4734724
81 I = 51
70579
XDOT = 7175
275245 Wp = 41
15488
YDOT = -665
885654 meter/sec RA = 11
76349 deg
ZDOT = -2678
281076 TA = 202
45755
MA = 202
52770
Ha = 192
896 n
mi
Hp = 184
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7112894
28 X = -2097098
52
Y = -14009726
39 feet Y = -4294011
60 meter
Z = -15533874
06 Z = -4745085
36
XDOT = 23540
929280 XDOT = 7195
198796
YDOT = -2184
664220 feet/sec YDOT = -585
535722 meter/sec
ZDOT = -8787
011404 ZDOT = -2643
374786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14546029
83 X = 4433629
89
Y = -5829866
87 feet Y = -1776943
42 meter
Z = -15575384
75 Z = -4747377
27
XDOT = -211
253900 XDOT = -64
390189
YDOT = 22632
122990 feet/sec YDOT = 6898
271088 meter/sec
ZDOT = -8646
586072 ZDOT = -2635
479435
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 10351
52047135
00016717 00000-0 10270-3 0 9149
2 25544 51
6473 12
1548 0008337 358
8100 1
3041 15
73282107 12317
Satellite: ISS
Catalog Number: 25544
Epoch time: 10351
52047135 = yrday
fracday
Element set: 914
Inclination: 51
6473 deg
RA of node: 12
1548 deg
Eccentricity:
0008337
Arg of perigee: 358
8100 deg
Mean anomaly: 1
3041 deg
Mean motion: 15
73282107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 260
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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