Date:
July 30th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 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 3503)
---------------------------------------
Vector Time (GMT): 2008/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6519519
69 A = 6734844
87 meter
Y = -716939
68 meter E =
0006665
Z = -1544590
76 I = 51
75102
XDOT = -814
186034 Wp = 57
76543
YDOT = 5009
519863 meter/sec RA = 163
02576 deg
ZDOT = -5776
415013 TA = 139
20557
MA = 139
15566
Ha = 194
525 n
mi
Hp = 184
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21389500
30 X = 6534555
37
Y = -2352164
32 feet Y = -643950
35 meter
Z = -5067554
97 Z = -1512882
73
XDOT = -2671
214023 XDOT = -842
082177
YDOT = 16435
432621 feet/sec YDOT = 5000
260149 meter/sec
ZDOT = -18951
492824 ZDOT = -5780
437233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14428641
38 X = -4397849
89
Y = -16002577
27 feet Y = -4877585
55 meter
Z = -4945234
26 Z = -1507307
40
XDOT = 13666
036007 XDOT = 4165
407775
YDOT = -6475
916424 feet/sec YDOT = -1973
859326 meter/sec
ZDOT = -18966
531207 ZDOT = -5780
998712
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 08210
52887852
00020000 00000-0 20000-3 0 9005
2 25544 51
6393 163
8615 0010230 3
3519 356
7710 15
72714866 35044
Satellite: ISS
Catalog Number: 25544
Epoch time: 08210
52887852 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 163
8615 deg
Eccentricity:
0010230
Arg of perigee: 3
3519 deg
Mean anomaly: 356
7710 deg
Mean motion: 15
72714866 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3504
Checksum: 281
Coasting Arc #2 (Orbit 3519)
---------------------------------------
Vector Time (GMT): 2008/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -166565
75 A = 6724285
68 meter
Y = -4316817
09 meter E =
0013394
Z = 5151313
61 I = 51
74369
XDOT = 7353
713728 Wp = 20
78989
YDOT = -1869
113338 meter/sec RA = 157
88313 deg
ZDOT = -1315
220658 TA = 81
84838
MA = 81
69647
Ha = 194
611 n
mi
Hp = 184
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -546475
57 X = -143305
86
Y = -14162785
73 feet Y = -4318550
55 meter
Z = 16900635
22 Z = 5150560
21
XDOT = 24126
357374 XDOT = 7380
456929
YDOT = -6132
261608 feet/sec YDOT = -1786
730138 meter/sec
ZDOT = -4315
028404 ZDOT = -1279
432126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10961970
41 X = -3341208
58
Y = 8990593
52 feet Y = 2740332
90 meter
Z = 16897308
63 Z = 5150299
67
XDOT = -18709
903204 XDOT = -5702
778497
YDOT = -14879
754333 feet/sec YDOT = -4535
349121 meter/sec
ZDOT = -4177
047516 ZDOT = -1273
164083
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 08211
54554180
00020000 00000-0 20000-3 0 9014
2 25544 51
6397 158
6508 0010223 7
0927 353
0379 15
72722426 35207
Satellite: ISS
Catalog Number: 25544
Epoch time: 08211
54554180 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 158
6508 deg
Eccentricity:
0010223
Arg of perigee: 7
0927 deg
Mean anomaly: 353
0379 deg
Mean motion: 15
72722426 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3520
Checksum: 273
Coasting Arc #3 (Orbit 3535)
---------------------------------------
Vector Time (GMT): 2008/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6184999
36 A = 6735563
87 meter
Y = 2527838
54 meter E =
0022085
Z = 738057
02 I = 51
80855
XDOT = -1193
587529 Wp = 34
74521
YDOT = -4691
918189 meter/sec RA = 152
78480 deg
ZDOT = 5997
818429 TA = 333
28497
MA = 333
39857
Ha = 194
704 n
mi
Hp = 184
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20291992
66 X = -6216391
65
Y = 8293433
54 feet Y = 2458498
69 meter
Z = 2421446
92 Z = 707935
02
XDOT = -3915
969583 XDOT = -1170
168795
YDOT = -15393
432378 feet/sec YDOT = -4705
135578 meter/sec
ZDOT = 19677
881986 ZDOT = 5992
076232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18987618
82 X = 5787426
22
Y = 10980206
24 feet Y = 3346766
86 meter
Z = 2305388
00 Z = 702682
26
XDOT = -8905
912791 XDOT = -2714
522219
YDOT = 11223
509630 feet/sec YDOT = 3420
925735 meter/sec
ZDOT = 19655
256037 ZDOT = 5990
922040
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 08212
56219406
00020000 00000-0 20000-3 0 9027
2 25544 51
6399 153
4395 0010227 10
6854 349
4523 15
72741256 35368
Satellite: ISS
Catalog Number: 25544
Epoch time: 08212
56219406 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 153
4395 deg
Eccentricity:
0010227
Arg of perigee: 10
6854 deg
Mean anomaly: 349
4523 deg
Mean motion: 15
72741256 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3536
Checksum: 287
Coasting Arc #4 (Orbit 3550)
---------------------------------------
Vector Time (GMT): 2008/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1855008
15 A = 6723709
73 meter
Y = 3745315
78 meter E =
0019731
Z = -5281320
11 I = 51
79524
XDOT = -6647
561929 Wp = 62
43998
YDOT = 3838
663667 meter/sec RA = 147
66027 deg
ZDOT = 397
408863 TA = 211
27370
MA = 211
39123
Ha = 194
797 n
mi
Hp = 183
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6085984
76 X = 1838644
65
Y = 12287781
44 feet Y = 3765968
76 meter
Z = -17327165
71 Z = -5272347
94
XDOT = -21809
586381 XDOT = -6691
922913
YDOT = 12594
040901 feet/sec YDOT = 3764
078724 meter/sec
ZDOT = 1303
834854 ZDOT = 365
008544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5716319
19 X = 1742334
09
Y = -12512576
16 feet Y = -3813833
21 meter
Z = -17292153
93 Z = -5270648
52
XDOT = 22561
667722 XDOT = 6876
796322
YDOT = 8723
417766 feet/sec YDOT = 2658
897735 meter/sec
ZDOT = 1179
090577 ZDOT = 359
386808
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 08213
51529621
00020000 00000-0 20000-3 0 9037
2 25544 51
6409 148
5541 0010260 14
0191 346
1255 15
72750901 35517
Satellite: ISS
Catalog Number: 25544
Epoch time: 08213
51529621 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 148
5541 deg
Eccentricity:
0010260
Arg of perigee: 14
0191 deg
Mean anomaly: 346
1255 deg
Mean motion: 15
72750901 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3551
Checksum: 256
Coasting Arc #5 (Orbit 3566)
---------------------------------------
Vector Time (GMT): 2008/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5335579
49 A = 6735686
53 meter
Y = -4112103
12 meter E =
0012087
Z = 25721
05 I = 51
86071
XDOT = 2925
449040 Wp = 84
95164
YDOT = 3742
840350 meter/sec RA = 142
55053 deg
ZDOT = -6049
678020 TA = 94
77021
MA = 94
63218
Ha = 194
857 n
mi
Hp = 183
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17505182
06 X = 5381040
19
Y = -13491151
96 feet Y = -4052183
42 meter
Z = 84386
65 Z = 51750
62
XDOT = 9597
929922 XDOT = 2912
766053
YDOT = 12279
659942 feet/sec YDOT = 3775
484107 meter/sec
ZDOT = -19848
025000 ZDOT = -6035
496980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21562563
39 X = -6572269
32
Y = -4844741
11 feet Y = -1476677
09 meter
Z = 184511
77 Z = 56239
19
XDOT = 2887
530589 XDOT = 880
119324
YDOT = -13744
062935 feet/sec YDOT = -4189
190383 meter/sec
ZDOT = -19792
890117 ZDOT = -6032
872908
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 08214
53192861
00020000 00000-0 20000-3 0 9043
2 25544 51
6419 143
3431 0010242 18
1064 342
0461 15
72765357 35675
Satellite: ISS
Catalog Number: 25544
Epoch time: 08214
53192861 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 143
3431 deg
Eccentricity:
0010242
Arg of perigee: 18
1064 deg
Mean anomaly: 342
0461 deg
Mean motion: 15
72765357 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3567
Checksum: 270
Coasting Arc #6 (Orbit 3582)
---------------------------------------
Vector Time (GMT): 2008/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3188228
48 A = 6723518
66 meter
Y = -2690650
86 meter E =
0010506
Z = 5266804
46 I = 51
84276
XDOT = 5401
726917 Wp = 36
26147
YDOT = -5473
150334 meter/sec RA = 137
44453 deg
ZDOT = 481
650912 TA = 49
22428
MA = 49
13316
Ha = 194
896 n
mi
Hp = 183
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10460067
18 X = -3183488
78
Y = -8827594
68 feet Y = -2726277
34 meter
Z = 17279542
19 Z = 5251327
75
XDOT = 17722
201170 XDOT = 5460
187376
YDOT = -17956
529967 feet/sec YDOT = -5412
418285 meter/sec
ZDOT = 1580
219529 ZDOT = 508
033453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 192860
82 X = 58783
98
Y = 13761309
58 feet Y = 4194447
16 meter
Z = 17219499
84 Z = 5248503
55
XDOT = -24160
507094 XDOT = -7364
122562
YDOT = -1733
362118 feet/sec YDOT = -528
328773 meter/sec
ZDOT = 1681
580293 ZDOT = 512
545673
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 08215
54854846
00020000 00000-0 20000-3 0 9054
2 25544 51
6419 138
1324 0010200 21
0192 339
1387 15
72828285 35839
Satellite: ISS
Catalog Number: 25544
Epoch time: 08215
54854846 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 138
1324 deg
Eccentricity:
0010200
Arg of perigee: 21
0192 deg
Mean anomaly: 339
1387 deg
Mean motion: 15
72828285 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3583
Checksum: 285
Coasting Arc #7 (Orbit 3597)
---------------------------------------
Vector Time (GMT): 2008/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3998187
00 A = 6735315
29 meter
Y = 5344853
38 meter E =
0020449
Z = -819590
27 I = 51
90290
XDOT = -4269
635510 Wp = 32
22922
YDOT = -2288
149919 meter/sec RA = 132
32246 deg
ZDOT = 5991
499029 TA = 318
86182
MA = 319
01580
Ha = 194
992 n
mi
Hp = 183
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13117411
40 X = -4053675
51
Y = 17535608
20 feet Y = 5299833
14 meter
Z = -2688944
46 Z = -839147
57
XDOT = -14007
990518 XDOT = -4272
836727
YDOT = -7507
053539 feet/sec YDOT = -2335
913628 meter/sec
ZDOT = 19657
149046 ZDOT = 5970
749692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21808948
55 X = 6647367
52
Y = -1877432
13 feet Y = -572241
31 meter
Z = -2763959
33 Z = -842454
80
XDOT = 3647
356976 XDOT = 1111
714406
YDOT = 13947
117181 feet/sec YDOT = 4251
081317 meter/sec
ZDOT = 19576
775699 ZDOT = 5967
001233
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 08216
50162292
00020000 00000-0 20000-3 0 9069
2 25544 51
6419 133
2468 0010333 24
8793 335
2866 15
72790051 35983
Satellite: ISS
Catalog Number: 25544
Epoch time: 08216
50162292 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 133
2468 deg
Eccentricity:
0010333
Arg of perigee: 24
8793 deg
Mean anomaly: 335
2866 deg
Mean motion: 15
72790051 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3598
Checksum: 294
Coasting Arc #8 (Orbit 3613)
---------------------------------------
Vector Time (GMT): 2008/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4137964
44 A = 6724051
01 meter
Y = 1255366
24 meter E =
0022112
Z = -5167591
48 I = 51
88471
XDOT = -3691
878184 Wp = 58
65393
YDOT = 6602
411905 meter/sec RA = 127
23314 deg
ZDOT = -1345
330074 TA = 198
44673
MA = 198
52704
Ha = 195
033 n
mi
Hp = 183
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13575998
82 X = 4148722
00
Y = 4118655
63 feet Y = 1301699
66 meter
Z = -16954040
28 Z = -5147463
40
XDOT = -12112
461233 XDOT = -3758
897757
YDOT = 21661
456382 feet/sec YDOT = 6560
752522 meter/sec
ZDOT = -4413
812578 ZDOT = -1363
427481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6239023
38 X = -1901654
33
Y = -12844461
03 feet Y = -3914991
72 meter
Z = -16876165
38 Z = -5143855
21
XDOT = 23182
519431 XDOT = 7066
031923
YDOT = -5339
932408 feet/sec YDOT = -1627
611398 meter/sec
ZDOT = -4483
068369 ZDOT = -1366
439239
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 08217
51822366
00020000 00000-0 20000-3 0 9077
2 25544 51
6426 128
0352 0010328 29
0957 331
0779 15
72836765 36147
Satellite: ISS
Catalog Number: 25544
Epoch time: 08217
51822366 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 128
0352 deg
Eccentricity:
0010328
Arg of perigee: 29
0957 deg
Mean anomaly: 331
0779 deg
Mean motion: 15
72836765 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3614
Checksum: 296
Coasting Arc #9 (Orbit 3629)
---------------------------------------
Vector Time (GMT): 2008/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2419075
46 A = 6734507
86 meter
Y = -6096068
78 meter E =
0018114
Z = 1519855
70 I = 51
93622
XDOT = 5028
202799 Wp = 83
63441
YDOT = 533
731435 meter/sec RA = 122
09980 deg
ZDOT = -5801
621867 TA = 79
70285
MA = 79
49867
Ha = 195
093 n
mi
Hp = 182
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7936599
28 X = 2479679
79
Y = -20000225
66 feet Y = -6068678
48 meter
Z = 4986403
20 Z = 1531754
44
XDOT = 16496
728342 XDOT = 5050
043720
YDOT = 1751
087386 feet/sec YDOT = 590
081989 meter/sec
ZDOT = -19034
192476 ZDOT = -5777
142078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19929054
05 X = -6074375
67
Y = 8085601
20 feet Y = 2464491
25 meter
Z = 5031770
03 Z = 1533683
51
XDOT = -9606
809186 XDOT = -2928
155440
YDOT = -11769
243575 feet/sec YDOT = -3587
265442 meter/sec
ZDOT = -18939
575485 ZDOT = -5772
782608
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 08218
53481421
00020000 00000-0 20000-3 0 9084
2 25544 51
6422 122
8235 0010261 32
8852 327
2947 15
72824331 36305
Satellite: ISS
Catalog Number: 25544
Epoch time: 08218
53481421 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 122
8235 deg
Eccentricity:
0010261
Arg of perigee: 32
8852 deg
Mean anomaly: 327
2947 deg
Mean motion: 15
72824331 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3630
Checksum: 271
Coasting Arc #10 (Orbit 3645)
---------------------------------------
Vector Time (GMT): 2008/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4533581
49 A = 6724881
63 meter
Y = 365249
70 meter E =
0012351
Z = 4942236
29 I = 51
91869
XDOT = 1769
839425 Wp = 67
06760
YDOT = -7186
261077 meter/sec RA = 117
02465 deg
ZDOT = 2155
070027 TA = 2
13054
MA = 2
12528
Ha = 195
247 n
mi
Hp = 182
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14873955
03 X = -4561337
13
Y = 1198325
80 feet Y = 314397
22 meter
Z = 16214686
00 Z = 4920144
92
XDOT = 5806
559794 XDOT = 1839
596949
YDOT = -23576
972036 feet/sec YDOT = -7166
079760 meter/sec
ZDOT = 7070
439720 ZDOT = 2163
837013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11369272
96 X = 3465354
40
Y = 9806594
76 feet Y = 2989050
08 meter
Z = 16129379
92 Z = 4916235
00
XDOT = -20111
694910 XDOT = -6130
044608
YDOT = 11635
443589 feet/sec YDOT = 3546
483206 meter/sec
ZDOT = 7103
610089 ZDOT = 2165
180355
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 08219
55139290
00020000 00000-0 20000-3 0 9092
2 25544 51
6423 117
6118 0010280 36
3305 323
8554 15
72862852 36464
Satellite: ISS
Catalog Number: 25544
Epoch time: 08219
55139290 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 117
6118 deg
Eccentricity:
0010280
Arg of perigee: 36
3305 deg
Mean anomaly: 323
8554 deg
Mean motion: 15
72862852 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3646
Checksum: 288
Coasting Arc #11 (Orbit 3660)
---------------------------------------
Vector Time (GMT): 2008/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -652869
17 A = 6733181
82 meter
Y = 6313650
38 meter E =
0016311
Z = -2233088
50 I = 51
95953
XDOT = -5200
684624 Wp = 40
95107
YDOT = 1396
340860 meter/sec RA = 111
88181 deg
ZDOT = 5502
891416 TA = 294
12658
MA = 294
29708
Ha = 195
143 n
mi
Hp = 182
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2141959
22 X = -712573
01
Y = 20714076
05 feet Y = 6306015
91 meter
Z = -7326405
84 Z = -2236404
83
XDOT = -17062
613595 XDOT = -5242
644108
YDOT = 4581
170799 feet/sec YDOT = 1337
948934 meter/sec
ZDOT = 18054
105694 ZDOT = 5477
524777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15986736
14 X = 4872757
18
Y = -13338147
83 feet Y = -4065467
46 meter
Z = -7338612
83 Z = -2236809
19
XDOT = 14501
298410 XDOT = 4419
995755
YDOT = 7563
576037 feet/sec YDOT = 2305
377976 meter/sec
ZDOT = 17956
240736 ZDOT = 5473
062176
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 08220
50442652
00020000 00000-0 20000-3 0 9100
2 25544 51
6427 112
7258 0010291 39
3947 320
7962 15
72881394 36614
Satellite: ISS
Catalog Number: 25544
Epoch time: 08220
50442652 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 112
7258 deg
Eccentricity:
0010291
Arg of perigee: 39
3947 deg
Mean anomaly: 320
7962 deg
Mean motion: 15
72881394 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3661
Checksum: 286
Coasting Arc #12 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2008/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4424977
14 A = 6726021
31 meter
Y = -2031756
13 meter E =
0020328
Z = -4659871
34 I = 51
94532
XDOT = 216
600078 Wp = 56
70967
YDOT = 7113
417863 meter/sec RA = 106
81807 deg
ZDOT = -2893
993341 TA = 184
70065
MA = 184
71976
Ha = 195
154 n
mi
Hp = 182
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14517641
55 X = 4470004
40
Y = -6665866
56 feet Y = -1982021
42 meter
Z = -15288291
79 Z = -4638265
66
XDOT = 710
630177 XDOT = 151
099039
YDOT = 23337
985115 feet/sec YDOT = 7115
473965 meter/sec
ZDOT = -9494
728810 ZDOT = -2893
099737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15192807
83 X = -4630767
83
Y = -5187852
70 feet Y = -1581257
50 meter
Z = -15205010
15 Z = -4634487
09
XDOT = 15096
958860 XDOT = 4601
553061
YDOT = -16378
148187 feet/sec YDOT = -4992
059567 meter/sec
ZDOT = -9490
604556 ZDOT = -2892
736269
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 08221
52098501
00020000 00000-0 20000-3 0 9114
2 25544 51
6429 107
5139 0010286 42
4947 317
7010 15
72900771 36773
Satellite: ISS
Catalog Number: 25544
Epoch time: 08221
52098501 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 107
5139 deg
Eccentricity:
0010286
Arg of perigee: 42
4947 deg
Mean anomaly: 317
7010 deg
Mean motion: 15
72900771 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3677
Checksum: 279
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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