Date:
June 19th 2008
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) : 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
171/06:51:03
282 8
8 11
2 11
2
N/A -3
7 0
1 187
1
000/00:20:06
565 -5
7 0
1 186
9
Coasting Arc #1 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2008/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -256470
12 A = 6711560
48 meter
Y = 4166488
22 meter E =
0005350
Z = 5254770
91 I = 51
67011
XDOT = -7641
687049 Wp = 4
86988
YDOT = -931
026291 meter/sec RA = 9
12674 deg
ZDOT = 370
448017 TA = 81
64756
MA = 81
58691
Ha = 186
102 n
mi
Hp = 179
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -841437
41 X = -328568
15
Y = 13669580
78 feet Y = 4163215
96 meter
Z = 17240062
05 Z = 5253350
76
XDOT = -25071
151737 XDOT = -7632
507790
YDOT = -3054
548200 feet/sec YDOT = -1016
428767 meter/sec
ZDOT = 1215
380633 ZDOT = 333
346730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13582047
98 X = 4139808
22
Y = 1808620
56 feet Y = 551267
55 meter
Z = 17234908
16 Z = 5253200
01
XDOT = -4514
024387 XDOT = -1375
874633
YDOT = 23841
726096 feet/sec YDOT = 7266
958114 meter/sec
ZDOT = 1072
457631 ZDOT = 326
885086
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 08170
54809449
00020000 00000-0 20000-3 0 9008
2 25544 51
6390 9
3694 0006297 342
2051 17
8893 15
77011640 28747
Satellite: ISS
Catalog Number: 25544
Epoch time: 08170
54809449 = yrday
fracday
Element set: 900
Inclination: 51
6390 deg
RA of node: 9
3694 deg
Eccentricity:
0006297
Arg of perigee: 342
2051 deg
Mean anomaly: 17
8893 deg
Mean motion: 15
77011640 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2874
Checksum: 297
Coasting Arc #2 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2008/171/07:01:06
565
Vector Time (MET): N/A
Weight (LBS) : 661039
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 178940
64 A = 6718401
93 meter
Y = -4169987
16 meter E =
0006265
Z = -5269980
01 I = 51
64914
XDOT = 7676
720099 Wp = 88
60090
YDOT = 542
951168 meter/sec RA = 5
04105 deg
ZDOT = -168
983218 TA = 179
79518
MA = 179
79492
Ha = 187
056 n
mi
Hp = 186
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 587075
58 X = 251157
35
Y = -13681060
23 feet Y = -4167581
21 meter
Z = -17289960
67 Z = -5268936
22
XDOT = 25186
089565 XDOT = 7670
899071
YDOT = 1781
335854 feet/sec YDOT = 628
764137 meter/sec
ZDOT = -554
406884 ZDOT = -131
703792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2269574
48 X = -691766
30
Y = -13509004
74 feet Y = -4117544
65 meter
Z = -17286255
50 Z = -5268850
68
XDOT = 23998
288520 XDOT = 7314
678341
YDOT = -3506
222492 feet/sec YDOT = -1068
696616 meter/sec
ZDOT = -410
822065 ZDOT = -125
218565
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 08171
30851600
00020000 00000-0 20000-3 0 9010
2 25544 51
6412 5
4486 0008790 269
0804 90
9352 15
74596586 28869
Satellite: ISS
Catalog Number: 25544
Epoch time: 08171
30851600 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 5
4486 deg
Eccentricity:
0008790
Arg of perigee: 269
0804 deg
Mean anomaly: 90
9352 deg
Mean motion: 15
74596586 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2886
Checksum: 301
Coasting Arc #3 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2008/172/07:01:06
565
Vector Time (MET): N/A
Weight (LBS) : 661039
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6724446
96 A = 6730508
29 meter
Y = -44125
87 meter E =
0008248
Z = -70387
50 I = 51
66073
XDOT = 94
790729 Wp = 182
68419
YDOT = -4777
417415 meter/sec RA = 359
90166 deg
ZDOT = -6040
528089 TA = 358
08041
MA = 358
08357
Ha = 187
061 n
mi
Hp = 186
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22061833
85 X = -6723111
83
Y = -144769
93 feet Y = -119315
01 meter
Z = -230930
12 Z = -103051
45
XDOT = 310
993206 XDOT = 177
549139
YDOT = -15673
941649 feet/sec YDOT = -4775
893402 meter/sec
ZDOT = -19818
005540 ZDOT = -6039
867593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21493878
03 X = -6551334
02
Y = 4968376
46 feet Y = 1514361
14 meter
Z = -356711
03 Z = -108725
52
XDOT = -2855
414649 XDOT = -870
330385
YDOT = -13778
715814 feet/sec YDOT = -4199
752580 meter/sec
ZDOT = -19815
822706 ZDOT = -6039
862761
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 08172
32396406
00020000 00000-0 20000-3 0 9022
2 25544 51
6414
2291 0008868 272
5771 87
4378 15
74585648 29021
Satellite: ISS
Catalog Number: 25544
Epoch time: 08172
32396406 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node:
2291 deg
Eccentricity:
0008868
Arg of perigee: 272
5771 deg
Mean anomaly: 87
4378 deg
Mean motion: 15
74585648 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2902
Checksum: 305
Coasting Arc #4 (Orbit 2917)
---------------------------------------
Vector Time (GMT): 2008/173/07:01:06
565
Vector Time (MET): N/A
Weight (LBS) : 661039
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1354
06 A = 6718238
88 meter
Y = 4187273
52 meter E =
0006759
Z = 5259369
06 I = 51
59098
XDOT = -7677
831052 Wp = 286
14185
YDOT = 432
963466 meter/sec RA = 354
75620 deg
ZDOT = -341
244889 TA = 167
11000
MA = 167
09271
Ha = 187
381 n
mi
Hp = 186
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4442
44 X = -71017
64
Y = 13737774
03 feet Y = 4186882
97 meter
Z = 17255147
85 Z = 5259200
68
XDOT = -25189
734423 XDOT = -7680
444194
YDOT = 1420
483812 feet/sec YDOT = 347
091020 meter/sec
ZDOT = -1119
569846 ZDOT = -378
549738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3320149
80 X = 1011981
66
Y = 13330958
49 feet Y = 4063276
15 meter
Z = 17254817
68 Z = 5259268
43
XDOT = -23069
455067 XDOT = -7031
569904
YDOT = 7386
880738 feet/sec YDOT = 2251
521249 meter/sec
ZDOT = -1263
190127 ZDOT = -385
020351
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 08173
33939255
00020000 00000-0 20000-3 0 9030
2 25544 51
6415 355
0092 0009022 277
4748 82
5390 15
74671260 29186
Satellite: ISS
Catalog Number: 25544
Epoch time: 08173
33939255 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 355
0092 deg
Eccentricity:
0009022
Arg of perigee: 277
4748 deg
Mean anomaly: 82
5390 deg
Mean motion: 15
74671260 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2918
Checksum: 298
Coasting Arc #5 (Orbit 2933)
---------------------------------------
Vector Time (GMT): 2008/174/07:01:06
565
Vector Time (MET): N/A
Weight (LBS) : 661039
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6655402
77 A = 6730158
95 meter
Y = -789327
48 meter E =
0010301
Z = 533288
75 I = 51
60251
XDOT = 90
442946 Wp = 7
65172
YDOT = 4822
955340 meter/sec RA = 349
62078 deg
ZDOT = 6006
582730 TA = 358
15713
MA = 358
16093
Ha = 187
654 n
mi
Hp = 186
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21835310
92 X = 6661143
92
Y = -2589657
08 feet Y = -714870
95 meter
Z = 1749635
00 Z = 565634
18
XDOT = 296
728826 XDOT = 7
326584
YDOT = 15823
344292 feet/sec YDOT = 4823
500928 meter/sec
ZDOT = 19706
636253 ZDOT = 6006
821069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20359055
67 X = 6205440
17
Y = -8279180
38 feet Y = -2523494
18 meter
Z = 1874132
84 Z = 571235
69
XDOT = 3766
123294 XDOT = 1147
914380
YDOT = 13724
599021 feet/sec YDOT = 4183
257782 meter/sec
ZDOT = 19707
924280 ZDOT = 6006
975321
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 08174
35480660
00020000 00000-0 20000-3 0 9045
2 25544 51
6419 349
7891 0009028 282
1727 77
8425 15
74662781 29345
Satellite: ISS
Catalog Number: 25544
Epoch time: 08174
35480660 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 349
7891 deg
Eccentricity:
0009028
Arg of perigee: 282
1727 deg
Mean anomaly: 77
8425 deg
Mean motion: 15
74662781 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2934
Checksum: 322
Coasting Arc #6 (Orbit 2948)
---------------------------------------
Vector Time (GMT): 2008/175/07:01:06
565
Vector Time (MET): N/A
Weight (LBS) : 661039
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -155946
16 A = 6718362
74 meter
Y = -4249526
84 meter E =
0005786
Z = -5206142
40 I = 51
53480
XDOT = 7524
975303 Wp = 82
85922
YDOT = -1360
877240 meter/sec RA = 344
46191 deg
ZDOT = 886
961165 TA = 195
59356
MA = 195
61139
Ha = 187
814 n
mi
Hp = 186
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -511634
39 X = -83125
44
Y = -13942017
21 feet Y = -4250862
75 meter
Z = -17080519
68 Z = -5206723
76
XDOT = 24688
239183 XDOT = 7535
324922
YDOT = -4464
820341 feet/sec YDOT = -1276
670926 meter/sec
ZDOT = 2909
977574 ZDOT = 923
542068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4321846
31 X = -1317298
75
Y = -13261805
95 feet Y = -4042198
45 meter
Z = -17083088
53 Z = -5206925
38
XDOT = 21449
936412 XDOT = 6537
940618
YDOT = -10913
501887 feet/sec YDOT = -3326
435375 meter/sec
ZDOT = 3050
741966 ZDOT = 929
866151
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 08175
30673995
00020000 00000-0 20000-3 0 9057
2 25544 51
6421 344
8956 0009104 285
9876 74
0285 15
74708362 29492
Satellite: ISS
Catalog Number: 25544
Epoch time: 08175
30673995 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 344
8956 deg
Eccentricity:
0009104
Arg of perigee: 285
9876 deg
Mean anomaly: 74
0285 deg
Mean motion: 15
74708362 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2949
Checksum: 331
Coasting Arc #7 (Orbit 2964)
---------------------------------------
Vector Time (GMT): 2008/176/07:01:06
565
Vector Time (MET): N/A
Weight (LBS) : 661039
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6460474
28 A = 6729745
84 meter
Y = 1566005
30 meter E =
0005389
Z = -1026245
82 I = 51
54526
XDOT = -252
807925 Wp = 210
03431
YDOT = -4924
369668 meter/sec RA = 339
33226 deg
ZDOT = -5914
119368 TA = 341
20052
MA = 341
22041
Ha = 188
053 n
mi
Hp = 185
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21195781
76 X = -6472520
16
Y = 5137812
67 feet Y = 1493693
36 meter
Z = -3366948
24 Z = -1057659
62
XDOT = -829
422325 XDOT = -168
994552
YDOT = -16156
068466 feet/sec YDOT = -4926
727275 meter/sec
ZDOT = -19403
278766 ZDOT = -5915
144594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18683747
17 X = -5694806
14
Y = 11213718
80 feet Y = 3417941
49 meter
Z = -3487796
72 Z = -1063080
44
XDOT = -4681
970127 XDOT = -1427
064495
YDOT = -13845
836773 feet/sec YDOT = -4220
211048 meter/sec
ZDOT = -19407
613496 ZDOT = -5915
440594
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 08176
32211995
00020000 00000-0 20000-3 0 9069
2 25544 51
6423 339
6762 0009164 289
0102 71
0069 15
74681889 29653
Satellite: ISS
Catalog Number: 25544
Epoch time: 08176
32211995 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 339
6762 deg
Eccentricity:
0009164
Arg of perigee: 289
0102 deg
Mean anomaly: 71
0069 deg
Mean motion: 15
74681889 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2965
Checksum: 314
Coasting Arc #8 (Orbit 2980)
---------------------------------------
Vector Time (GMT): 2008/177/07:01:06
565
Vector Time (MET): N/A
Weight (LBS) : 661039
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 288874
50 A = 6718649
50 meter
Y = 4370546
31 meter E =
0008042
Z = 5100067
83 I = 51
48167
XDOT = -7228
501351 Wp = 324
22088
YDOT = 2200
082762 meter/sec RA = 334
15919 deg
ZDOT = -1470
693031 TA = 139
94274
MA = 139
88341
Ha = 188
210 n
mi
Hp = 185
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 947750
99 X = 215205
78
Y = 14339062
71 feet Y = 4373364
13 meter
Z = 16732505
99 Z = 5101292
78
XDOT = -23715
555613 XDOT = -7245
421452
YDOT = 7218
119299 feet/sec YDOT = 2119
155097 meter/sec
ZDOT = -4825
108371 ZDOT = -1505
849791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5316142
64 X = 1620360
28
Y = 13344515
94 feet Y = 4067408
46 meter
Z = 16737569
41 Z = 5101611
16
XDOT = -19245
254871 XDOT = -5865
953685
YDOT = 13910
032042 feet/sec YDOT = 4239
777766 meter/sec
ZDOT = -4960
317294 ZDOT = -1511
904711
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 08177
33747987
00020000 00000-0 20000-3 0 9077
2 25544 51
6422 334
4558 0009318 294
1971 65
8218 15
74776656 29812
Satellite: ISS
Catalog Number: 25544
Epoch time: 08177
33747987 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 334
4558 deg
Eccentricity:
0009318
Arg of perigee: 294
1971 deg
Mean anomaly: 65
8218 deg
Mean motion: 15
74776656 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2981
Checksum: 341
Coasting Arc #9 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2008/178/07:01:06
565
Vector Time (MET): N/A
Weight (LBS) : 661039
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6141389
29 A = 6728860
71 meter
Y = -2251077
19 meter E =
0011655
Z = 1545418
89 I = 51
48977
XDOT = 417
581820 Wp = 21
00776
YDOT = 5097
670752 meter/sec RA = 329
03360 deg
ZDOT = 5763
225179 TA = 356
08090
MA = 356
09002
Ha = 188
346 n
mi
Hp = 185
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20148914
98 X = 6158597
37
Y = -7385423
84 feet Y = -2182304
63 meter
Z = 5070271
94 Z = 1575295
31
XDOT = 1370
019095 XDOT = 332
551091
YDOT = 16724
641574 feet/sec YDOT = 5101
864246 meter/sec
ZDOT = 18908
219092 ZDOT = 5765
047886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16546753
22 X = 5043450
38
Y = -13621681
20 feet Y = -4151888
43 meter
Z = 5185140
01 Z = 1580430
68
XDOT = 5727
070361 XDOT = 1745
611046
YDOT = 14160
442810 feet/sec YDOT = 4316
102969 meter/sec
ZDOT = 18915
643873 ZDOT = 5765
488253
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 08178
35282419
00020000 00000-0 20000-3 0 9085
2 25544 51
6415 329
2350 0009398 298
2991 61
7224 15
74786797 29977
Satellite: ISS
Catalog Number: 25544
Epoch time: 08178
35282419 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 329
2350 deg
Eccentricity:
0009398
Arg of perigee: 298
2991 deg
Mean anomaly: 61
7224 deg
Mean motion: 15
74786797 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2997
Checksum: 344
Coasting Arc #10 (Orbit 3011)
---------------------------------------
Vector Time (GMT): 2008/179/07:01:06
565
Vector Time (MET): N/A
Weight (LBS) : 661039
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -455801
37 A = 6719252
05 meter
Y = -4540518
68 meter E =
0004562
Z = -4935114
78 I = 51
43220
XDOT = 6811
616489 Wp = 69
08090
YDOT = -2931
495204 meter/sec RA = 323
84694 deg
ZDOT = 2071
130565 TA = 221
02535
MA = 221
05967
Ha = 188
556 n
mi
Hp = 184
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1495411
33 X = -381020
68
Y = -14896714
83 feet Y = -4545196
93 meter
Z = -16191321
45 Z = -4937148
04
XDOT = 22347
823126 XDOT = 6833
829445
YDOT = -9617
766417 feet/sec YDOT = -2855
199883 meter/sec
ZDOT = 6795
047786 ZDOT = 2104
275145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6481957
33 X = -1975700
59
Y = -13485817
26 feet Y = -4110477
10 meter
Z = -16199512
95 Z = -4937611
55
XDOT = 16605
646519 XDOT = 5061
401059
YDOT = -16284
549333 feet/sec YDOT = -4963
530637 meter/sec
ZDOT = 6922
444646 ZDOT = 2109
961128
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 08179
30469354
00020000 00000-0 20000-3 0 9097
2 25544 51
6406 324
3404 0009445 302
1386 57
8861 15
74811861 30122
Satellite: ISS
Catalog Number: 25544
Epoch time: 08179
30469354 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 324
3404 deg
Eccentricity:
0009445
Arg of perigee: 302
1386 deg
Mean anomaly: 57
8861 deg
Mean motion: 15
74811861 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3012
Checksum: 291
Coasting Arc #11 (Orbit 3027)
---------------------------------------
Vector Time (GMT): 2008/180/07:01:06
565
Vector Time (MET): N/A
Weight (LBS) : 661039
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5738037
90 A = 6727940
83 meter
Y = 2829040
86 meter E =
0003602
Z = -2080801
82 I = 51
43818
XDOT = -616
312348 Wp = 281
10350
YDOT = -5321
941911 meter/sec RA = 318
72731 deg
ZDOT = -5527
358213 TA = 282
19730
MA = 282
23764
Ha = 188
791 n
mi
Hp = 184
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18825583
65 X = -5759137
97
Y = 9281630
12 feet Y = 2764757
18 meter
Z = -6826777
62 Z = -2108728
26
XDOT = -2022
022140 XDOT = -529
904617
YDOT = -17460
439340 feet/sec YDOT = -5328
349881 meter/sec
ZDOT = -18134
377338 ZDOT = -5530
143223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14137889
27 X = -4309228
65
Y = 15465918
48 feet Y = 4714011
95 meter
Z = -6934089
91 Z = -2113510
60
XDOT = -6995
855386 XDOT = -2132
336722
YDOT = -14543
304355 feet/sec YDOT = -4432
799167 meter/sec
ZDOT = -18145
524671 ZDOT = -5530
755920
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 08180
32000387
00020000 00000-0 20000-3 0 9100
2 25544 51
6401 319
1205 0009512 305
6667 54
3611 15
74805987 30287
Satellite: ISS
Catalog Number: 25544
Epoch time: 08180
32000387 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 319
1205 deg
Eccentricity:
0009512
Arg of perigee: 305
6667 deg
Mean anomaly: 54
3611 deg
Mean motion: 15
74805987 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3028
Checksum: 269
Coasting Arc #12 (Orbit 3043)
---------------------------------------
Vector Time (GMT): 2008/181/07:01:06
565
Vector Time (MET): N/A
Weight (LBS) : 661039
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 639413
52 A = 6720102
04 meter
Y = 4770227
81 meter E =
0009794
Z = 4694662
66 I = 51
39106
XDOT = -6300
169657 Wp = 356
79867
YDOT = 3506
785412 meter/sec RA = 313
52804 deg
ZDOT = -2695
779673 TA = 119
87541
MA = 119
77806
Ha = 188
919 n
mi
Hp = 184
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2097813
37 X = 563218
53
Y = 15650353
70 feet Y = 4776951
20 meter
Z = 15402436
55 Z = 4697584
76
XDOT = -20669
847956 XDOT = -6325
819117
YDOT = 11505
201482 feet/sec YDOT = 3436
190388 meter/sec
ZDOT = -8844
421500 ZDOT = -2726
447835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7789158
97 X = 2374135
65
Y = 13722426
97 feet Y = 4182595
74 meter
Z = 15414066
44 Z = 4698207
45
XDOT = -13722
843269 XDOT = -4182
722628
YDOT = 17890
956798 feet/sec YDOT = 5453
163632 meter/sec
ZDOT = -8962
241908 ZDOT = -2731
691334
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 08181
33529523
00020000 00000-0 20000-3 0 9111
2 25544 51
6401 313
8987 0009617 309
8804 50
1513 15
74870962 30448
Satellite: ISS
Catalog Number: 25544
Epoch time: 08181
33529523 = yrday
fracday
Element set: 911
Inclination: 51
6401 deg
RA of node: 313
8987 deg
Eccentricity:
0009617
Arg of perigee: 309
8804 deg
Mean anomaly: 50
1513 deg
Mean motion: 15
74870962 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3044
Checksum: 291
Coasting Arc #13 (Orbit 3059)
---------------------------------------
Vector Time (GMT): 2008/182/07:01:06
565
Vector Time (MET): N/A
Weight (LBS) : 661039
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5257346
81 A = 6726554
40 meter
Y = -3259342
14 meter E =
0011403
Z = 2623094
77 I = 51
39288
XDOT = 871
527635 Wp = 33
81046
YDOT = 5605
323620 meter/sec RA = 308
41075 deg
ZDOT = 5216
661487 TA = 356
16278
MA = 356
17152
Ha = 188
941 n
mi
Hp = 184
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17248513
16 X = 5280659
95
Y = -10693379
72 feet Y = -3200421
68 meter
Z = 8605953
96 Z = 2648691
06
XDOT = 2859
342636 XDOT = 783
441490
YDOT = 18390
169357 feet/sec YDOT = 5614
575913 meter/sec
ZDOT = 17115
031124 ZDOT = 5220
682630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11581981
36 X = 3530187
92
Y = -16613711
84 feet Y = -5063859
37 meter
Z = 8704269
43 Z = 2653061
32
XDOT = 8584
690497 XDOT = 2616
613664
YDOT = 14962
501453 feet/sec YDOT = 4560
570443 meter/sec
ZDOT = 17130
958381 ZDOT = 5221
516115
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 08182
35056993
00020000 00000-0 20000-3 0 9121
2 25544 51
6390 308
6768 0009622 313
4128 46
6234 15
74900975 30606
Satellite: ISS
Catalog Number: 25544
Epoch time: 08182
35056993 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 308
6768 deg
Eccentricity:
0009622
Arg of perigee: 313
4128 deg
Mean anomaly: 46
6234 deg
Mean motion: 15
74900975 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3060
Checksum: 299
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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