Date:
April 25th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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
116/04:28:01
560 -5
5 8
1 8
1
N/A 0
4 -0
2 189
7
000/00:12:03
119 -6
0 -0
1 179
3
Coasting Arc #1 (Orbit 2006)
---------------------------------------
Vector Time (GMT): 2008/115/13:43:34
986
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3647453
61 A = 6710915
21 meter
Y = -2141348
14 meter E =
0018102
Z = -5225869
29 I = 51
31638
XDOT = 3282
391567 Wp = 90
43573
YDOT = -6935
609228 meter/sec RA = 292
02177 deg
ZDOT = 552
460603 TA = 184
83401
MA = 184
85151
Ha = 186
274 n
mi
Hp = 177
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11966711
31 X = -3597850
95
Y = -7025420
39 feet Y = -2181858
37 meter
Z = -17145240
45 Z = -5243468
52
XDOT = 10769
001204 XDOT = 3357
018886
YDOT = -22754
623452 feet/sec YDOT = -6898
486422 meter/sec
ZDOT = 1812
534788 ZDOT = 568
587518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12235860
31 X = -3729490
22
Y = 6365185
99 feet Y = 1940108
69 meter
Z = -17212963
46 Z = -5246511
26
XDOT = -13170
684660 XDOT = -4014
424684
YDOT = -20264
539125 feet/sec YDOT = -6176
631525 meter/sec
ZDOT = 1873
714237 ZDOT = 571
108099
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 08115
58684051
00020000 00000-0 20000-3 0 9001
2 25544 51
6385 292
5997 0003375 73
4991 286
6545 15
77267677 20074
Satellite: ISS
Catalog Number: 25544
Epoch time: 08115
58684051 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 292
5997 deg
Eccentricity:
0003375
Arg of perigee: 73
4991 deg
Mean anomaly: 286
6545 deg
Mean motion: 15
77267677 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2007
Checksum: 327
Coasting Arc #2 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2008/116/04:34:03
119
Vector Time (MET): N/A
Weight (LBS) : 614690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2769625
43 A = 6727160
45 meter
Y = 6065997
17 meter E =
0017217
Z = -829128
02 I = 51
35111
XDOT = -4109
051745 Wp = 139
00422
YDOT = -2677
314517 meter/sec RA = 288
83418 deg
ZDOT = -5944
020511 TA = 50
08596
MA = 49
93476
Ha = 189
720 n
mi
Hp = 179
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9086697
61 X = -2833222
71
Y = 19901565
52 feet Y = 6034670
10 meter
Z = -2720236
28 Z = -842737
09
XDOT = -13481
140896 XDOT = -4049
932880
YDOT = -8783
840278 feet/sec YDOT = -2722
933331 meter/sec
ZDOT = -19501
379629 ZDOT = -5963
839103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21296014
93 X = -6491025
35
Y = -4983643
31 feet Y = -1519014
48 meter
Z = -2771843
48 Z = -844857
89
XDOT = 5622
005169 XDOT = 1713
587175
YDOT = -13282
511767 feet/sec YDOT = -4048
509587 meter/sec
ZDOT = -19577
672390 ZDOT = -5967
274544
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 08116
22045828
00020000 00000-0 20000-3 0 9017
2 25544 51
6401 289
3343 0006951 136
4753 223
6960 15
75655940 20176
Satellite: ISS
Catalog Number: 25544
Epoch time: 08116
22045828 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 289
3343 deg
Eccentricity:
0006951
Arg of perigee: 136
4753 deg
Mean anomaly: 223
6960 deg
Mean motion: 15
75655940 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2017
Checksum: 285
Coasting Arc #3 (Orbit 2032)
---------------------------------------
Vector Time (GMT): 2008/117/04:34:03
119
Vector Time (MET): N/A
Weight (LBS) : 614690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3517036
46 A = 6716041
97 meter
Y = 2669233
40 meter E =
0008678
Z = 5052980
81 I = 51
30564
XDOT = -2986
383809 Wp = 105
26897
YDOT = 6930
452888 meter/sec RA = 283
64258 deg
ZDOT = -1582
391665 TA = 359
97558
MA = 359
97562
Ha = 189
435 n
mi
Hp = 179
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11538833
54 X = 3462380
61
Y = 8757327
43 feet Y = 2708256
98 meter
Z = 16578021
01 Z = 5069934
13
XDOT = -9797
847143 XDOT = -3055
972224
YDOT = 22737
706327 feet/sec YDOT = 6896
668456 meter/sec
ZDOT = -5191
573703 ZDOT = -1597
068207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6114251
19 X = -1863623
76
Y = 13049208
51 feet Y = 3977398
75 meter
Z = 16643327
00 Z = 5072886
07
XDOT = -23346
588563 XDOT = -7116
040194
YDOT = -4246
726526 feet/sec YDOT = -1294
402245 meter/sec
ZDOT = -5247
189625 ZDOT = -1599
343398
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 08117
23520351
00020000 00000-0 20000-3 0 9029
2 25544 51
6397 284
1106 0006767 140
0514 220
1149 15
75718604 20337
Satellite: ISS
Catalog Number: 25544
Epoch time: 08117
23520351 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 284
1106 deg
Eccentricity:
0006767
Arg of perigee: 140
0514 deg
Mean anomaly: 220
1149 deg
Mean motion: 15
75718604 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2033
Checksum: 258
Coasting Arc #4 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2008/118/04:34:03
119
Vector Time (MET): N/A
Weight (LBS) : 614690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2447905
96 A = 6725662
18 meter
Y = -5956477
74 meter E =
0017117
Z = 1924970
48 I = 51
33267
XDOT = 4006
115035 Wp = 89
94604
YDOT = 3467
345879 meter/sec RA = 278
50186 deg
ZDOT = 5591
881405 TA = 291
57245
MA = 291
75477
Ha = 189
485 n
mi
Hp = 179
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8031187
52 X = 2504979
08
Y = -19542249
82 feet Y = -5928784
86 meter
Z = 6315519
96 Z = 1937000
75
XDOT = 13143
422030 XDOT = 3939
880389
YDOT = 11375
806688 feet/sec YDOT = 3511
773874 meter/sec
ZDOT = 18346
067602 ZDOT = 5611
182544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20857581
86 X = 6357390
95
Y = 3283787
34 feet Y = 1000898
38 meter
Z = 6361077
98 Z = 1938856
57
XDOT = -7830
730238 XDOT = -2386
806576
YDOT = 13785
743752 feet/sec YDOT = 4201
894695 meter/sec
ZDOT = 18420
467972 ZDOT = 5614
558638
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 08118
24993174
00020000 00000-0 20000-3 0 9039
2 25544 51
6399 278
8858 0006741 143
3062 216
8565 15
75719087 20496
Satellite: ISS
Catalog Number: 25544
Epoch time: 08118
24993174 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 278
8858 deg
Eccentricity:
0006741
Arg of perigee: 143
3062 deg
Mean anomaly: 216
8565 deg
Mean motion: 15
75719087 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2049
Checksum: 327
Coasting Arc #5 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2008/119/04:34:03
119
Vector Time (MET): N/A
Weight (LBS) : 614690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3518128
84 A = 6717805
83 meter
Y = -3389178
91 meter E =
0016573
Z = -4627546
86 I = 51
30398
XDOT = 2657
851463 Wp = 123
62073
YDOT = -6635
194102 meter/sec RA = 273
29004 deg
ZDOT = 2837
163961 TA = 174
59805
MA = 174
58015
Ha = 189
335 n
mi
Hp = 179
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11542417
44 X = -3457489
16
Y = -11119353
37 feet Y = -3428181
36 meter
Z = -15182240
35 Z = -4644490
86
XDOT = 8719
985116 XDOT = 2718
067224
YDOT = -21769
009521 feet/sec YDOT = -6605
135939 meter/sec
ZDOT = 9308
280713 ZDOT = 2850
221799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7947881
98 X = 2422514
43
Y = -13845930
79 feet Y = -4220239
71 meter
Z = -15247597
00 Z = -4647467
57
XDOT = 22224
992075 XDOT = 6774
177585
YDOT = 2446
350787 feet/sec YDOT = 745
647720 meter/sec
ZDOT = 9357
708235 ZDOT = 2852
229470
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 08119
20122091
00020000 00000-0 20000-3 0 9049
2 25544 51
6404 273
9877 0006637 147
0130 213
1449 15
75754768 20644
Satellite: ISS
Catalog Number: 25544
Epoch time: 08119
20122091 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 273
9877 deg
Eccentricity:
0006637
Arg of perigee: 147
0130 deg
Mean anomaly: 213
1449 deg
Mean motion: 15
75754768 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2064
Checksum: 285
Coasting Arc #6 (Orbit 2079)
---------------------------------------
Vector Time (GMT): 2008/120/04:34:03
119
Vector Time (MET): N/A
Weight (LBS) : 614690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2231587
79 A = 6723146
83 meter
Y = 5581034
09 meter E =
0010322
Z = -3009629
09 I = 51
32207
XDOT = -4084
686185 Wp = 134
13305
YDOT = -4281
593120 meter/sec RA = 268
16387 deg
ZDOT = -4928
556541 TA = 80
86257
MA = 80
74580
Ha = 189
154 n
mi
Hp = 179
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7321482
25 X = -2279209
65
Y = 18310479
31 feet Y = 5555813
03 meter
Z = -9874111
19 Z = -3020585
67
XDOT = -13401
201394 XDOT = -4012
563041
YDOT = -14047
221522 feet/sec YDOT = -4326
866996 meter/sec
ZDOT = -16169
804923 ZDOT = -4948
224963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19577639
32 X = -5967264
46
Y = -2184758
52 feet Y = -665914
40 meter
Z = -9915578
44 Z = -3022268
31
XDOT = 9885
458179 XDOT = 3013
087653
YDOT = -15111
980204 feet/sec YDOT = -4606
131566 meter/sec
ZDOT = -16245
714661 ZDOT = -4951
693829
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 08120
21591144
00020000 00000-0 20000-3 0 9052
2 25544 51
6406 268
7629 0006556 151
6992 208
4530 15
75774913 20800
Satellite: ISS
Catalog Number: 25544
Epoch time: 08120
21591144 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 268
7629 deg
Eccentricity:
0006556
Arg of perigee: 151
6992 deg
Mean anomaly: 208
4530 deg
Mean motion: 15
75774913 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2080
Checksum: 294
Coasting Arc #7 (Orbit 2095)
---------------------------------------
Vector Time (GMT): 2008/121/04:34:03
119
Vector Time (MET): N/A
Weight (LBS) : 614690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3659127
21 A = 6720235
16 meter
Y = 4041232
96 meter E =
0014198
Z = 3914826
37 I = 51
31437
XDOT = -2468
065146 Wp = 105
33917
YDOT = 6115
093530 meter/sec RA = 262
94095 deg
ZDOT = -3997
374231 TA = 26
30901
MA = 26
23697
Ha = 188
944 n
mi
Hp = 179
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12005010
53 X = 3594647
94
Y = 13258638
32 feet Y = 4081790
83 meter
Z = 12843918
54 Z = 3932445
94
XDOT = -8097
326595 XDOT = -2516
843029
YDOT = 20062
642816 feet/sec YDOT = 6087
221548 meter/sec
ZDOT = -13114
744853 ZDOT = -4009
482533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9387377
11 X = -2861272
54
Y = 15166961
42 feet Y = 4622889
84 meter
Z = 12911949
65 Z = 3935562
25
XDOT = -20400
482461 XDOT = -6218
067054
YDOT = -1399
639649 feet/sec YDOT = -426
610165 meter/sec
ZDOT = -13160
570396 ZDOT = -4011
341857
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 08121
23058334
00020000 00000-0 20000-3 0 9065
2 25544 51
6400 263
5382 0006447 154
2702 205
8784 15
75821385 20965
Satellite: ISS
Catalog Number: 25544
Epoch time: 08121
23058334 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 263
5382 deg
Eccentricity:
0006447
Arg of perigee: 154
2702 deg
Mean anomaly: 205
8784 deg
Mean motion: 15
75821385 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2096
Checksum: 282
Coasting Arc #8 (Orbit 2111)
---------------------------------------
Vector Time (GMT): 2008/122/04:34:03
119
Vector Time (MET): N/A
Weight (LBS) : 614690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2121012
25 A = 6720249
25 meter
Y = -5029199
37 meter E =
0015492
Z = 3915096
11 I = 51
31976
XDOT = 4341
530740 Wp = 120
81246
YDOT = 4956
000741 meter/sec RA = 257
81973 deg
ZDOT = 3994
752173 TA = 287
48693
MA = 287
65619
Ha = 188
899 n
mi
Hp = 179
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6958701
60 X = 2158072
91
Y = -16499997
94 feet Y = -5005273
80 meter
Z = 12844803
52 Z = 3925490
08
XDOT = 14243
867256 XDOT = 4266
383343
YDOT = 16259
844950 feet/sec YDOT = 5004
130038 meter/sec
ZDOT = 13106
142300 ZDOT = 4015
660988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17799559
69 X = 5425305
79
Y = 1684204
33 feet Y = 513345
48 meter
Z = 12884159
58 Z = 3927091
84
XDOT = -11205
250964 XDOT = -3415
360494
YDOT = 17054
745208 feet/sec YDOT = 5198
286339 meter/sec
ZDOT = 13186
897670 ZDOT = 4019
366410
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 08122
24523627
00020000 00000-0 20000-3 0 9070
2 25544 51
6405 258
3126 0006357 158
1875 201
9561 15
75832889 21122
Satellite: ISS
Catalog Number: 25544
Epoch time: 08122
24523627 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 258
3126 deg
Eccentricity:
0006357
Arg of perigee: 158
1875 deg
Mean anomaly: 201
9561 deg
Mean motion: 15
75832889 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2112
Checksum: 294
Coasting Arc #9 (Orbit 2126)
---------------------------------------
Vector Time (GMT): 2008/123/04:34:03
119
Vector Time (MET): N/A
Weight (LBS) : 614690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3935764
21 A = 6722910
64 meter
Y = -4566132
61 meter E =
0007526
Z = -2986976
23 I = 51
33683
XDOT = 2465
860839 Wp = 126
26319
YDOT = -5356
292161 meter/sec RA = 252
59651 deg
ZDOT = 4943
206334 TA = 199
08405
MA = 199
11226
Ha = 188
703 n
mi
Hp = 179
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12912612
25 X = -3869902
10
Y = -14980750
02 feet Y = -4609776
33 meter
Z = -9799790
77 Z = -3005936
44
XDOT = 8090
094615 XDOT = 2501
558939
YDOT = -17573
137010 feet/sec YDOT = -5328
517885 meter/sec
ZDOT = 16217
868549 ZDOT = 4955
272370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10206418
27 X = 3110916
29
Y = -16898123
61 feet Y = -5150548
08 meter
Z = -9873032
46 Z = -3009300
30
XDOT = 17960
891053 XDOT = 5474
479593
YDOT = 1354
143274 feet/sec YDOT = 412
742870 meter/sec
ZDOT = 16263
603641 ZDOT = 4957
146390
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 08123
19645530
00020000 00000-0 20000-3 0 9084
2 25544 51
6406 253
4136 0006189 163
0862 197
0510 15
75871271 21277
Satellite: ISS
Catalog Number: 25544
Epoch time: 08123
19645530 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 253
4136 deg
Eccentricity:
0006189
Arg of perigee: 163
0862 deg
Mean anomaly: 197
0510 deg
Mean motion: 15
75871271 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2127
Checksum: 283
Coasting Arc #10 (Orbit 2142)
---------------------------------------
Vector Time (GMT): 2008/124/04:34:03
119
Vector Time (MET): N/A
Weight (LBS) : 614690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2256286
81 A = 6717258
17 meter
Y = 4291169
60 meter E =
0011881
Z = -4658346
17 I = 51
32786
XDOT = -4666
353883 Wp = 101
30956
YDOT = -5455
489141 meter/sec RA = 247
46998 deg
ZDOT = -2773
585013 TA = 141
24259
MA = 141
15730
Ha = 188
477 n
mi
Hp = 179
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7402515
77 X = -2281473
80
Y = 14078640
43 feet Y = 4265797
71 meter
Z = -15283287
94 Z = -4669368
57
XDOT = -15309
559984 XDOT = -4591
529098
YDOT = -17898
586420 feet/sec YDOT = -5507
252597 meter/sec
ZDOT = -9099
688363 ZDOT = -2796
072875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15702034
73 X = -4785980
19
Y = -2273918
80 feet Y = -693090
45 meter
Z = -15325131
16 Z = -4671099
98
XDOT = 11713
423084 XDOT = 3570
251356
YDOT = -19153
685184 feet/sec YDOT = -5838
043244 meter/sec
ZDOT = -9186
564474 ZDOT = -2800
064852
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 08124
21107132
00020000 00000-0 20000-3 0 9090
2 25544 51
6405 248
1879 0006077 167
7553 192
3760 15
75906817 21433
Satellite: ISS
Catalog Number: 25544
Epoch time: 08124
21107132 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 248
1879 deg
Eccentricity:
0006077
Arg of perigee: 167
7553 deg
Mean anomaly: 192
3760 deg
Mean motion: 15
75906817 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2143
Checksum: 295
Coasting Arc #11 (Orbit 2158)
---------------------------------------
Vector Time (GMT): 2008/125/04:34:03
119
Vector Time (MET): N/A
Weight (LBS) : 614690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4219003
77 A = 6725263
92 meter
Y = 4895890
10 meter E =
0018259
Z = 1820941
44 I = 51
36775
XDOT = -2745
447079 Wp = 130
11877
YDOT = 4475
686673 meter/sec RA = 242
26045 deg
ZDOT = -5646
993724 TA = 29
56740
MA = 29
46428
Ha = 188
407 n
mi
Hp = 180
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13841875
88 X = 4155097
57
Y = 16062631
55 feet Y = 4942712
04 meter
Z = 5974217
31 Z = 1841282
76
XDOT = -9007
372307 XDOT = -2767
858121
YDOT = 14684
011395 feet/sec YDOT = 4444
860368 meter/sec
ZDOT = -18526
882297 ZDOT = -5660
385739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10306026
88 X = -3141276
99
Y = 18505306
68 feet Y = 5640417
48 meter
Z = 6052798
31 Z = 1844892
93
XDOT = -15505
364867 XDOT = -4726
035212
YDOT = -2531
690071 feet/sec YDOT = -771
659134 meter/sec
ZDOT = -18577
802502 ZDOT = -5662
514203
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 08125
22567054
00020000 00000-0 20000-3 0 9107
2 25544 51
6408 242
9627 0006132 170
2295 189
8989 15
75912573 21590
Satellite: ISS
Catalog Number: 25544
Epoch time: 08125
22567054 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 242
9627 deg
Eccentricity:
0006132
Arg of perigee: 170
2295 deg
Mean anomaly: 189
8989 deg
Mean motion: 15
75912573 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2159
Checksum: 309
Coasting Arc #12 (Orbit 2174)
---------------------------------------
Vector Time (GMT): 2008/126/04:34:03
119
Vector Time (MET): N/A
Weight (LBS) : 614690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2592709
02 A = 6715219
90 meter
Y = -3507833
96 meter E =
0009541
Z = 5103737
61 I = 51
34860
XDOT = 4995
666084 Wp = 154
04979
YDOT = 5704
372970 meter/sec RA = 237
11840 deg
ZDOT = 1373
413003 TA = 282
70496
MA = 282
81160
Ha = 188
217 n
mi
Hp = 180
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8506263
18 X = 2606947
78
Y = -11508641
60 feet Y = -3478761
51 meter
Z = 16744545
97 Z = 5116367
69
XDOT = 16389
980592 XDOT = 4924
835633
YDOT = 18715
134415 feet/sec YDOT = 5759
841245 meter/sec
ZDOT = 4505
948174 ZDOT = 1397
510895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13770609
25 X = 4197281
70
Y = 3682715
43 feet Y = 1122491
66 meter
Z = 16792649
95 Z = 5118399
71
XDOT = -11266
851037 XDOT = -3434
136196
YDOT = 21017
973662 feet/sec YDOT = 6406
278372 meter/sec
ZDOT = 4599
033376 ZDOT = 1401
785373
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 08126
24024972
00020000 00000-0 20000-3 0 9118
2 25544 51
6405 237
7369 0005979 174
8266 185
2961 15
75943168 21750
Satellite: ISS
Catalog Number: 25544
Epoch time: 08126
24024972 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 237
7369 deg
Eccentricity:
0005979
Arg of perigee: 174
8266 deg
Mean anomaly: 185
2961 deg
Mean motion: 15
75943168 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2175
Checksum: 320
Coasting Arc #13 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2008/127/04:34:03
119
Vector Time (MET): N/A
Weight (LBS) : 614690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4463849
26 A = 6726388
79 meter
Y = -5001222
25 meter E =
0007617
Z = -539271
66 I = 51
40284
XDOT = 3278
121407 Wp = 71
31189
YDOT = -3563
673324 meter/sec RA = 231
93105 deg
ZDOT = 5986
105036 TA = 282
79928
MA = 282
88439
Ha = 188
044 n
mi
Hp = 180
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14645174
72 X = -4404973
29
Y = -16408209
49 feet Y = -5050810
32 meter
Z = -1769263
97 Z = -560815
06
XDOT = 10754
991492 XDOT = 3288
647196
YDOT = -11691
841615 feet/sec YDOT = -3526
957241 meter/sec
ZDOT = 19639
452219 ZDOT = 6002
055753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9671210
62 X = 2947785
00
Y = -19745298
07 feet Y = -6018366
85 meter
Z = -1852475
58 Z = -564634
56
XDOT = 13404
195772 XDOT = 4085
598871
YDOT = 4738
059068 feet/sec YDOT = 1444
160404 meter/sec
ZDOT = 19700
302931 ZDOT = 6004
652333
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 08127
19140092
00020000 00000-0 20000-3 0 9126
2 25544 51
6396 232
8373 0005875 179
8438 180
2729 15
75984286 21901
Satellite: ISS
Catalog Number: 25544
Epoch time: 08127
19140092 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 232
8373 deg
Eccentricity:
0005875
Arg of perigee: 179
8438 deg
Mean anomaly: 180
2729 deg
Mean motion: 15
75984286 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2190
Checksum: 319
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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