Date:
April 26th 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
There are no maneuvers
Coasting Arc #1 (Orbit 2021)
---------------------------------------
Vector Time (GMT): 2008/116/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4172485
01 A = 6715360
79 meter
Y = -692346
68 meter E =
0020440
Z = -5232827
73 I = 51
30555
XDOT = 1865
276442 Wp = 103
24436
YDOT = -7442
319548 meter/sec RA = 287
11578 deg
ZDOT = -508
910734 TA = 161
92766
MA = 161
85490
Ha = 189
866 n
mi
Hp = 178
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13689255
29 X = -4139012
57
Y = -2271478
60 feet Y = -738818
28 meter
Z = -17168069
97 Z = -5253016
62
XDOT = 6119
673365 XDOT = 1950
831213
YDOT = -24417
058886 feet/sec YDOT = -7420
982565 meter/sec
ZDOT = -1669
654640 ZDOT = -499
641816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11792245
11 X = -3594276
31
Y = 7129556
56 feet Y = 2173088
84 meter
Z = -17245588
72 Z = -5256455
44
XDOT = -10734
153113 XDOT = -3271
769869
YDOT = -21659
079505 feet/sec YDOT = -6601
687433 meter/sec
ZDOT = -1634
833793 ZDOT = -498
297340
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
53756166
00020000 00000-0 20000-3 0 9004
2 25544 51
6370 287
6963 0007595 139
0624 221
1111 15
75695371 20220
Satellite: ISS
Catalog Number: 25544
Epoch time: 08116
53756166 = yrday
fracday
Element set: 900
Inclination: 51
6370 deg
RA of node: 287
6963 deg
Eccentricity:
0007595
Arg of perigee: 139
0624 deg
Mean anomaly: 221
1111 deg
Mean motion: 15
75695371 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2022
Checksum: 286
Coasting Arc #2 (Orbit 2037)
---------------------------------------
Vector Time (GMT): 2008/117/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1507221
44 A = 6727196
57 meter
Y = 6544755
84 meter E =
0019218
Z = -150621
19 I = 51
33822
XDOT = -4665
906749 Wp = 138
48285
YDOT = -1202
616349 meter/sec RA = 281
94069 deg
ZDOT = -6016
784763 TA = 43
16258
MA = 43
01209
Ha = 189
607 n
mi
Hp = 179
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4944952
24 X = -1579562
21
Y = 21472296
08 feet Y = 6527496
77 meter
Z = -494164
00 Z = -158118
61
XDOT = -15308
093009 XDOT = -4622
883454
YDOT = -3945
591697 feet/sec YDOT = -1254
552235 meter/sec
ZDOT = -19740
107491 ZDOT = -6039
347483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10570674
08 X = 3221941
46
Y = 19332468
24 feet Y = 5892536
32 meter
Z = -522274
90 Z = -159189
39
XDOT = -12569
312801 XDOT = -3831
126542
YDOT = 6374
912865 feet/sec YDOT = 1943
073441 meter/sec
ZDOT = -19826
789668 ZDOT = -6043
205491
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
55229402
00020000 00000-0 20000-3 0 9016
2 25544 51
6366 282
4706 0007295 142
7063 217
4609 15
75750334 20386
Satellite: ISS
Catalog Number: 25544
Epoch time: 08117
55229402 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 282
4706 deg
Eccentricity:
0007295
Arg of perigee: 142
7063 deg
Mean anomaly: 217
4609 deg
Mean motion: 15
75750334 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2038
Checksum: 284
Coasting Arc #3 (Orbit 2053)
---------------------------------------
Vector Time (GMT): 2008/118/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4017844
70 A = 6715475
89 meter
Y = 1410255
40 meter E =
0008385
Z = 5186248
45 I = 51
29362
XDOT = -1562
269618 Wp = 122
91341
YDOT = 7504
003577 meter/sec RA = 276
76011 deg
ZDOT = -833
724777 TA = 335
03138
MA = 335
07192
Ha = 189
606 n
mi
Hp = 179
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13181905
20 X = 3976582
42
Y = 4626822
17 feet Y = 1454954
23 meter
Z = 17015250
83 Z = 5205667
09
XDOT = -5125
556488 XDOT = -1642
014344
YDOT = 24619
434309 feet/sec YDOT = 7486
087557 meter/sec
ZDOT = -2735
317509 ZDOT = -841
507596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12762066
27 X = 3889877
80
Y = -5454717
08 feet Y = -1662597
77 meter
Z = 17089897
45 Z = 5209000
74
XDOT = 12511
234865 XDOT = 3813
424387
YDOT = 20646
806935 feet/sec YDOT = 6293
146754 meter/sec
ZDOT = -2764
421905 ZDOT = -842
595797
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
56701152
00020000 00000-0 20000-3 0 9026
2 25544 51
6367 277
2460 0007508 146
1217 214
0428 15
75702844 20545
Satellite: ISS
Catalog Number: 25544
Epoch time: 08118
56701152 = yrday
fracday
Element set: 902
Inclination: 51
6367 deg
RA of node: 277
2460 deg
Eccentricity:
0007508
Arg of perigee: 146
1217 deg
Mean anomaly: 214
0428 deg
Mean motion: 15
75702844 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2054
Checksum: 273
Coasting Arc #4 (Orbit 2069)
---------------------------------------
Vector Time (GMT): 2008/119/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1229435
03 A = 6726314
79 meter
Y = -6479146
23 meter E =
0015707
Z = 1308488
79 I = 51
33002
XDOT = 4602
420446 Wp = 88
03595
YDOT = 2060
915168 meter/sec RA = 271
60770 deg
ZDOT = 5820
918137 TA = 286
39837
MA = 286
57098
Ha = 189
493 n
mi
Hp = 179
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4033579
49 X = 1295438
06
Y = -21257041
44 feet Y = -6465029
00 meter
Z = 4292942
22 Z = 1314621
45
XDOT = 15099
804612 XDOT = 4550
755845
YDOT = 6761
532705 feet/sec YDOT = 2112
092944 meter/sec
ZDOT = 19097
500450 ZDOT = 5843
151366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11756555
43 X = -3583398
09
Y = -18158141
35 feet Y = -5534601
48 meter
Z = 4315812
15 Z = 1315459
54
XDOT = 14194
673343 XDOT = 4326
536435
YDOT = -4584
759239 feet/sec YDOT = -1397
434616 meter/sec
ZDOT = 19183
018666 ZDOT = 5846
984090
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
58170492
00020000 00000-0 20000-3 0 9037
2 25544 51
6377 272
0214 0007504 151
1996 208
9583 15
75799755 20701
Satellite: ISS
Catalog Number: 25544
Epoch time: 08119
58170492 = yrday
fracday
Element set: 903
Inclination: 51
6377 deg
RA of node: 272
0214 deg
Eccentricity:
0007504
Arg of perigee: 151
1996 deg
Mean anomaly: 208
9583 deg
Mean motion: 15
75799755 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2070
Checksum: 310
Coasting Arc #5 (Orbit 2084)
---------------------------------------
Vector Time (GMT): 2008/120/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4064659
34 A = 6716561
24 meter
Y = -2197402
39 meter E =
0018300
Z = -4891182
24 I = 51
29776
XDOT = 1294
956899 Wp = 123
54567
YDOT = -7259
461459 meter/sec RA = 266
40533 deg
ZDOT = 2181
136438 TA = 167
78871
MA = 167
74429
Ha = 189
368 n
mi
Hp = 179
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13335496
52 X = -4016024
98
Y = -7209325
42 feet Y = -2242583
67 meter
Z = -16047185
84 Z = -4910810
36
XDOT = 4248
546255 XDOT = 1365
441483
YDOT = -23817
130770 feet/sec YDOT = -7244
586469 meter/sec
ZDOT = 7155
959443 ZDOT = 2187
598374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14493086
03 X = -4417492
62
Y = 4162943
09 feet Y = 1268865
05 meter
Z = -16122728
56 Z = -4914207
66
XDOT = -13419
265957 XDOT = -4090
192264
YDOT = -18859
096234 feet/sec YDOT = -5748
252532 meter/sec
ZDOT = 7180
004919 ZDOT = 2188
465499
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
53296601
00020000 00000-0 20000-3 0 9046
2 25544 51
6378 267
1237 0007362 154
2789 205
8743 15
75803812 20858
Satellite: ISS
Catalog Number: 25544
Epoch time: 08120
53296601 = yrday
fracday
Element set: 904
Inclination: 51
6378 deg
RA of node: 267
1237 deg
Eccentricity:
0007362
Arg of perigee: 154
2789 deg
Mean anomaly: 205
8743 deg
Mean motion: 15
75803812 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2085
Checksum: 296
Coasting Arc #6 (Orbit 2100)
---------------------------------------
Vector Time (GMT): 2008/121/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1067013
80 A = 6724259
77 meter
Y = 6152464
76 meter E =
0012239
Z = -2484292
12 I = 51
32705
XDOT = -4745
803307 Wp = 146
59679
YDOT = -2954
319299 meter/sec RA = 261
27091 deg
ZDOT = -5300
602852 TA = 61
66443
MA = 61
54104
Ha = 189
183 n
mi
Hp = 179
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3500701
44 X = -1123664
01
Y = 20185251
85 feet Y = 6140216
09 meter
Z = -8150564
70 Z = -2489613
24
XDOT = -15570
220823 XDOT = -4686
665405
YDOT = -9692
648620 feet/sec YDOT = -3007
058869 meter/sec
ZDOT = -17390
429304 ZDOT = -5323
514486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11997142
67 X = 3656729
09
Y = 16596539
26 feet Y = 5058625
17 meter
Z = -8170340
26 Z = -2490319
71
XDOT = -16541
476329 XDOT = -5041
841985
YDOT = 3388
889918 feet/sec YDOT = 1032
933647 meter/sec
ZDOT = -17478
656053 ZDOT = -5327
494365
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
54762496
00020000 00000-0 20000-3 0 9059
2 25544 51
6377 261
8976 0007262 158
0740 202
0736 15
75832867 21018
Satellite: ISS
Catalog Number: 25544
Epoch time: 08121
54762496 = yrday
fracday
Element set: 905
Inclination: 51
6377 deg
RA of node: 261
8976 deg
Eccentricity:
0007262
Arg of perigee: 158
0740 deg
Mean anomaly: 202
0736 deg
Mean motion: 15
75832867 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2101
Checksum: 299
Coasting Arc #7 (Orbit 2116)
---------------------------------------
Vector Time (GMT): 2008/122/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4261607
07 A = 6718846
70 meter
Y = 2913305
49 meter E =
0012099
Z = 4288328
10 I = 51
31510
XDOT = -1163
480678 Wp = 108
20650
YDOT = 6794
740086 meter/sec RA = 256
05225 deg
ZDOT = -3455
595807 TA = 16
84881
MA = 16
80866
Ha = 189
039 n
mi
Hp = 179
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13981650
50 X = 4207881
17
Y = 9558088
86 feet Y = 2960660
82 meter
Z = 14069317
93 Z = 4308900
70
XDOT = -3817
193824 XDOT = -1222
587225
YDOT = 22292
454350 feet/sec YDOT = 6781
398899 meter/sec
ZDOT = -11337
256586 ZDOT = -3461
391621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16498723
26 X = 5028810
85
Y = -3521282
12 feet Y = -1073286
79 meter
Z = 14148569
67 Z = 4312484
03
XDOT = 13348
904820 XDOT = 4068
746189
YDOT = 16850
188351 feet/sec YDOT = 5135
937410 meter/sec
ZDOT = -11358
780487 ZDOT = -3462
156293
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
56226621
00020000 00000-0 20000-3 0 9068
2 25544 51
6383 256
6727 0007274 161
3439 198
7993 15
75830691 21172
Satellite: ISS
Catalog Number: 25544
Epoch time: 08122
56226621 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 256
6727 deg
Eccentricity:
0007274
Arg of perigee: 161
3439 deg
Mean anomaly: 198
7993 deg
Mean motion: 15
75830691 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2117
Checksum: 312
Coasting Arc #8 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2008/123/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1015912
30 A = 6721343
51 meter
Y = -5642204
01 meter E =
0015860
Z = 3503658
93 I = 51
33366
XDOT = 5064
999678 Wp = 118
14428
YDOT = 3702
313206 meter/sec RA = 250
93018 deg
ZDOT = 4470
727813 TA = 283
75862
MA = 283
93510
Ha = 188
861 n
mi
Hp = 179
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3333045
62 X = 1061908
40
Y = -18511168
00 feet Y = -5630586
31 meter
Z = 11494944
00 Z = 3508706
04
XDOT = 16617
453012 XDOT = 5001
505065
YDOT = 12146
696871 feet/sec YDOT = 3758
597919 meter/sec
ZDOT = 14667
742170 ZDOT = 4495
179725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11451788
98 X = -3490505
28
Y = -14906280
41 feet Y = -4543434
27 meter
Z = 11513713
77 Z = 3509379
96
XDOT = 19035
496695 XDOT = 5802
019393
YDOT = -3164
269021 feet/sec YDOT = -964
469198 meter/sec
ZDOT = 14761
967409 ZDOT = 4499
447666
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
57688507
00020000 00000-0 20000-3 0 9076
2 25544 51
6393 251
4471 0007154 166
1961 193
9400 15
75925728 21336
Satellite: ISS
Catalog Number: 25544
Epoch time: 08123
57688507 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 251
4471 deg
Eccentricity:
0007154
Arg of perigee: 166
1961 deg
Mean anomaly: 193
9400 deg
Mean motion: 15
75925728 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2133
Checksum: 304
Coasting Arc #9 (Orbit 2147)
---------------------------------------
Vector Time (GMT): 2008/124/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4598937
86 A = 6721565
17 meter
Y = -3508226
88 meter E =
0009467
Z = -3436150
40 I = 51
34535
XDOT = 1243
471454 Wp = 138
61535
YDOT = -6081
605018 meter/sec RA = 245
70689 deg
ZDOT = 4545
046931 TA = 180
54035
MA = 180
54138
Ha = 188
735 n
mi
Hp = 179
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15088378
80 X = -4542673
96
Y = -11509930
71 feet Y = -3559340
21 meter
Z = -11273459
31 Z = -3458355
88
XDOT = 4079
630753 XDOT = 1289
305012
YDOT = -19952
772369 feet/sec YDOT = -6067
443593 meter/sec
ZDOT = 14911
571296 ZDOT = 4551
199105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18573775
70 X = -5661286
83
Y = 3635312
33 feet Y = 1108043
20 meter
Z = -11359045
95 Z = -3462237
20
XDOT = -12040
064023 XDOT = -3669
811514
YDOT = -14852
191051 feet/sec YDOT = -4526
947832 meter/sec
ZDOT = 14934
535443 ZDOT = 4552
046403
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
52807691
00020000 00000-0 20000-3 0 9080
2 25544 51
6395 246
5488 0006888 169
7813 190
3493 15
75897335 21480
Satellite: ISS
Catalog Number: 25544
Epoch time: 08124
52807691 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 246
5488 deg
Eccentricity:
0006888
Arg of perigee: 169
7813 deg
Mean anomaly: 190
3493 deg
Mean motion: 15
75897335 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2148
Checksum: 342
Coasting Arc #10 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2008/125/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1229002
85 A = 6718306
54 meter
Y = 4950364
35 meter E =
0010081
Z = -4378534
33 I = 51
34832
XDOT = -5465
152587 Wp = 111
26859
YDOT = -4285
484003 meter/sec RA = 240
58560 deg
ZDOT = -3320
894234 TA = 125
24790
MA = 125
15351
Ha = 188
567 n
mi
Hp = 180
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4032161
58 X = -1262996
59
Y = 16241352
86 feet Y = 4936431
04 meter
Z = -14365270
11 Z = -4384587
36
XDOT = -17930
290639 XDOT = -5400
692737
YDOT = -14059
986887 feet/sec YDOT = -4346
237923 meter/sec
ZDOT = -10895
322289 ZDOT = -3347
288206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9788073
55 X = 2983404
82
Y = 13549191
47 feet Y = 4129793
56 meter
Z = -14387976
99 Z = -4385455
39
XDOT = -21306
455593 XDOT = -6494
207665
YDOT = 3748
007169 feet/sec YDOT = 1142
392585 meter/sec
ZDOT = -10997
067646 ZDOT = -3351
906218
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
54266243
00020000 00000-0 20000-3 0 9096
2 25544 51
6401 241
3232 0006940 173
7247 186
4006 15
75931933 21640
Satellite: ISS
Catalog Number: 25544
Epoch time: 08125
54266243 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 241
3232 deg
Eccentricity:
0006940
Arg of perigee: 173
7247 deg
Mean anomaly: 186
4006 deg
Mean motion: 15
75931933 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2164
Checksum: 278
Coasting Arc #11 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2008/126/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4945410
70 A = 6724224
60 meter
Y = 3904779
80 meter E =
0017619
Z = 2316662
24 I = 51
38397
XDOT = -1613
431651 Wp = 128
40367
YDOT = 5259
483199 meter/sec RA = 235
37132 deg
ZDOT = -5403
893265 TA = 25
38771
MA = 25
30125
Ha = 188
406 n
mi
Hp = 180
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16225100
71 X = 4890125
06
Y = 12810957
36 feet Y = 3959772
92 meter
Z = 7600597
91 Z = 2340553
68
XDOT = -5293
410929 XDOT = -1645
872281
YDOT = 17255
522305 feet/sec YDOT = 5241
259906 meter/sec
ZDOT = -17729
308612 ZDOT = -5411
809925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20177955
23 X = 6150240
75
Y = -4337747
33 feet Y = -1322145
39 meter
Z = 7692703
10 Z = 2344735
90
XDOT = 9695
884422 XDOT = 2955
305572
YDOT = 13510
937968 feet/sec YDOT = 4118
133893 meter/sec
ZDOT = -17759
140814 ZDOT = -5412
986120
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
55723018
00020000 00000-0 20000-3 0 9108
2 25544 51
6399 236
0985 0006897 176
2509 183
8708 15
75955991 21800
Satellite: ISS
Catalog Number: 25544
Epoch time: 08126
55723018 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 236
0985 deg
Eccentricity:
0006897
Arg of perigee: 176
2509 deg
Mean anomaly: 183
8708 deg
Mean motion: 15
75955991 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2180
Checksum: 330
Coasting Arc #12 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2008/127/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1651164
67 A = 6715620
45 meter
Y = -4213221
16 meter E =
0011136
Z = 4960952
00 I = 51
37369
XDOT = 5860
240960 Wp = 154
84321
YDOT = 4606
756434 meter/sec RA = 230
23887 deg
ZDOT = 1950
389685 TA = 276
18761
MA = 276
31446
Ha = 188
175 n
mi
Hp = 180
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5417206
91 X = 1674054
88
Y = -13822904
06 feet Y = -4194629
45 meter
Z = 16276089
25 Z = 4969028
68
XDOT = 19226
512336 XDOT = 5798
817081
YDOT = 15114
030295 feet/sec YDOT = 4671
945344 meter/sec
ZDOT = 6398
916289 ZDOT = 1978
710701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7500303
80 X = -2286092
60
Y = -12773740
44 feet Y = -3893436
09 meter
Z = 16306651
61 Z = 4970267
41
XDOT = 22844
140590 XDOT = 6962
894052
YDOT = -5056
948311 feet/sec YDOT = -1541
357845 meter/sec
ZDOT = 6508
104133 ZDOT = 1983
670140
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
57177735
00020000 00000-0 20000-3 0 9111
2 25544 51
6404 230
8727 0006741 180
9817 179
1336 15
76033524 21967
Satellite: ISS
Catalog Number: 25544
Epoch time: 08127
57177735 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 230
8727 deg
Eccentricity:
0006741
Arg of perigee: 180
9817 deg
Mean anomaly: 179
1336 deg
Mean motion: 15
76033524 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2196
Checksum: 300
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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