Date:
May 8th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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 2179)
---------------------------------------
Vector Time (GMT): 2008/126/13:14:53
461
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4999957
56 A = 6723743
27 meter
Y = -3780042
28 meter E =
0005186
Z = -2441663
59 I = 51
38541
XDOT = 1455
177335 Wp = 124
03607
YDOT = -5361
573634 meter/sec RA = 235
21714 deg
ZDOT = 5325
826284 TA = 208
28339
MA = 208
31156
Ha = 188
204 n
mi
Hp = 180
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16404060
23 X = -4945455
45
Y = -12401713
52 feet Y = -3835649
74 meter
Z = -8010707
33 Z = -2465821
92
XDOT = 4774
203855 XDOT = 1489
150564
YDOT = -17590
464680 feet/sec YDOT = -5345
111463 meter/sec
ZDOT = 17473
183345 ZDOT = 5332
977832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18666565
10 X = -5689569
04
Y = 8541341
08 feet Y = 2603400
76 meter
Z = -8103823
93 Z = -2470045
53
XDOT = -12660
736680 XDOT = -3858
992540
YDOT = -11081
628998 feet/sec YDOT = -3377
680519 meter/sec
ZDOT = 17500
068539 ZDOT = 5334
020891
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
55693765
00020000 00000-0 20000-3 0 9002
2 25544 51
6419 236
1081 0006454 177
5338 182
5859 15
76029830 21802
Satellite: ISS
Catalog Number: 25544
Epoch time: 08126
55693765 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 236
1081 deg
Eccentricity:
0006454
Arg of perigee: 177
5338 deg
Mean anomaly: 182
5859 deg
Mean motion: 15
76029830 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2180
Checksum: 306
Coasting Arc #2 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2008/127/13:14:53
461
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1566872
83 A = 6715610
35 meter
Y = 4280259
51 meter E =
0012605
Z = -4941421
17 I = 51
37530
XDOT = -5895
761700 Wp = 104
49130
YDOT = -4506
076073 meter/sec RA = 230
08612 deg
ZDOT = -2041
123541 TA = 145
70471
MA = 145
62326
Ha = 188
013 n
mi
Hp = 180
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5140658
90 X = -1590613
83
Y = 14042846
16 feet Y = 4262605
65 meter
Z = -16212011
73 Z = -4949090
41
XDOT = -19343
050196 XDOT = -5835
020227
YDOT = -14783
714151 feet/sec YDOT = -4571
666000 meter/sec
ZDOT = -6696
599545 ZDOT = -2069
618767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10170905
15 X = 3100091
89
Y = 10919694
38 feet Y = 3328322
85 meter
Z = -16241003
34 Z = -4950257
82
XDOT = -21187
590790 XDOT = -6457
977673
YDOT = 9647
652397 feet/sec YDOT = 2940
604451 meter/sec
ZDOT = -6806
445900 ZDOT = -2074
604710
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
57143121
00020000 00000-0 20000-3 0 9012
2 25544 51
6412 230
8827 0006494 181
4056 178
7091 15
76075111 21964
Satellite: ISS
Catalog Number: 25544
Epoch time: 08127
57143121 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 230
8827 deg
Eccentricity:
0006494
Arg of perigee: 181
4056 deg
Mean anomaly: 178
7091 deg
Mean motion: 15
76075111 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2196
Checksum: 278
Coasting Arc #3 (Orbit 2211)
---------------------------------------
Vector Time (GMT): 2008/128/13:14:53
461
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5266068
59 A = 6725604
53 meter
Y = 4021891
30 meter E =
0017840
Z = 1087477
91 I = 51
42866
XDOT = -2182
965298 Wp = 141
29406
YDOT = 4463
007692 meter/sec RA = 224
89067 deg
ZDOT = -5896
742349 TA = 26
75103
MA = 26
65912
Ha = 187
823 n
mi
Hp = 180
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17277127
91 X = 5215420
92
Y = 13195181
42 feet Y = 4080496
15 meter
Z = 3567840
91 Z = 1112938
42
XDOT = -7161
959640 XDOT = -2204
063319
YDOT = 14642
413687 feet/sec YDOT = 4438
479354 meter/sec
ZDOT = -19346
267549 ZDOT = -5907
398022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19470857
87 X = 5934717
48
Y = -9632631
58 feet Y = -2936026
11 meter
Z = 3665999
56 Z = 1117396
67
XDOT = 9305
568158 XDOT = 2836
337175
YDOT = 11385
145925 feet/sec YDOT = 3470
192478 meter/sec
ZDOT = -19386
710306 ZDOT = -5909
069301
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 08128
58590121
00020000 00000-0 20000-3 0 9021
2 25544 51
6406 225
6572 0006357 183
7606 176
3511 15
76123944 22128
Satellite: ISS
Catalog Number: 25544
Epoch time: 08128
58590121 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 225
6572 deg
Eccentricity:
0006357
Arg of perigee: 183
7606 deg
Mean anomaly: 176
3511 deg
Mean motion: 15
76123944 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2212
Checksum: 281
Coasting Arc #4 (Orbit 2227)
---------------------------------------
Vector Time (GMT): 2008/129/13:14:53
461
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2298711
61 A = 6713928
07 meter
Y = -3520092
01 meter E =
0007302
Z = 5233836
41 I = 51
41159
XDOT = 6129
316315 Wp = 168
35629
YDOT = 4650
627855 meter/sec RA = 219
73766 deg
ZDOT = 428
683552 TA = 277
52097
MA = 277
60393
Ha = 187
546 n
mi
Hp = 180
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7541704
74 X = 2312477
70
Y = -11548858
30 feet Y = -3494310
27 meter
Z = 17171379
29 Z = 5245036
61
XDOT = 20109
305494 XDOT = 6074
774231
YDOT = 15257
965402 feet/sec YDOT = 4718
864352 meter/sec
ZDOT = 1406
442100 ZDOT = 458
328241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7262187
00 X = -2213514
60
Y = -11663961
10 feet Y = -3555175
34 meter
Z = 17214016
29 Z = 5246832
16
XDOT = 21531
906006 XDOT = 6562
924951
YDOT = -11127
223907 feet/sec YDOT = -3391
577847 meter/sec
ZDOT = 1520
745404 ZDOT = 463
523199
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 08129
60034541
00020000 00000-0 20000-3 0 9035
2 25544 51
6406 220
4308 0006277 189
3410 170
7639 15
76192120 22282
Satellite: ISS
Catalog Number: 25544
Epoch time: 08129
60034541 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 220
4308 deg
Eccentricity:
0006277
Arg of perigee: 189
3410 deg
Mean anomaly: 170
7639 deg
Mean motion: 15
76192120 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2228
Checksum: 269
Coasting Arc #5 (Orbit 2243)
---------------------------------------
Vector Time (GMT): 2008/130/13:14:53
461
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5358034
83 A = 6725971
65 meter
Y = -4045642
17 meter E =
0008851
Z = 365438
69 I = 51
47437
XDOT = 3160
689918 Wp = 72
49504
YDOT = -3632
627656 meter/sec RA = 214
57129 deg
ZDOT = 6009
616065 TA = 291
48864
MA = 291
58299
Ha = 187
465 n
mi
Hp = 180
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17578854
44 X = -5314172
85
Y = -13273104
25 feet Y = -4105313
59 meter
Z = 1198945
82 Z = 339515
25
XDOT = 10369
717580 XDOT = 3171
881872
YDOT = -11918
069737 feet/sec YDOT = -3597
221223 meter/sec
ZDOT = 19716
588141 ZDOT = 6024
997474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19334337
96 X = -5893106
21
Y = 10564303
86 feet Y = 3219999
82 meter
Z = 1098976
94 Z = 334968
17
XDOT = -5869
952607 XDOT = -1789
161555
YDOT = -12843
541010 feet/sec YDOT = -3914
711300 meter/sec
ZDOT = 19775
273362 ZDOT = 6027
503321
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 08130
61477042
00020000 00000-0 20000-3 0 9046
2 25544 51
6397 215
2046 0005951 192
1704 167
9317 15
76167599 22449
Satellite: ISS
Catalog Number: 25544
Epoch time: 08130
61477042 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 215
2046 deg
Eccentricity:
0005951
Arg of perigee: 192
1704 deg
Mean anomaly: 167
9317 deg
Mean motion: 15
76167599 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2244
Checksum: 297
Coasting Arc #6 (Orbit 2258)
---------------------------------------
Vector Time (GMT): 2008/131/13:14:53
461
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3263026
84 A = 6714314
40 meter
Y = 2858496
37 meter E =
0014783
Z = -5136933
14 I = 51
45976
XDOT = -6046
361078 Wp = 123
46879
YDOT = -4581
513422 meter/sec RA = 209
39209 deg
ZDOT = 1285
909073 TA = 158
89914
MA = 158
83809
Ha = 187
230 n
mi
Hp = 180
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10705468
63 X = -3269794
17
Y = 9378268
91 feet Y = 2821970
07 meter
Z = -16853455
17 Z = -5152801
05
XDOT = -19837
142644 XDOT = -6000
927214
YDOT = -15031
212013 feet/sec YDOT = -4648
873397 meter/sec
ZDOT = 4218
861789 ZDOT = 1256
645679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4412811
55 X = 1345024
96
Y = 13455052
12 feet Y = 4101099
89 meter
Z = -16914094
84 Z = -5155416
11
XDOT = -20683
779624 XDOT = -6304
416030
YDOT = 11967
218274 feet/sec YDOT = 3647
608130 meter/sec
ZDOT = 4105
993424 ZDOT = 1251
506796
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 08131
56576962
00020000 00000-0 20000-3 0 9053
2 25544 51
6390 210
3044 0005938 196
3418 163
7556 15
76216501 22592
Satellite: ISS
Catalog Number: 25544
Epoch time: 08131
56576962 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 210
3044 deg
Eccentricity:
0005938
Arg of perigee: 196
3418 deg
Mean anomaly: 163
7556 deg
Mean motion: 15
76216501 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2259
Checksum: 297
Coasting Arc #7 (Orbit 2274)
---------------------------------------
Vector Time (GMT): 2008/132/13:14:53
461
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5118010
90 A = 6724238
57 meter
Y = 3931717
16 meter E =
0011520
Z = -1864471
74 I = 51
52031
XDOT = -4329
399545 Wp = 167
09349
YDOT = 2968
368547 meter/sec RA = 204
25673 deg
ZDOT = -5642
436639 TA = 33
67163
MA = 33
59849
Ha = 187
093 n
mi
Hp = 180
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16791374
34 X = 5082722
70
Y = 12899334
53 feet Y = 3988752
55 meter
Z = -6117033
28 Z = -1839693
83
XDOT = -14204
066749 XDOT = -4334
860615
YDOT = 9738
741952 feet/sec YDOT = 2919
924689 meter/sec
ZDOT = -18511
931231 ZDOT = -5663
481857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18325181
41 X = 5585515
29
Y = -10662602
58 feet Y = -3249961
27 meter
Z = -6021446
02 Z = -1835336
75
XDOT = 2873
760353 XDOT = 875
922156
YDOT = 15405
246165 feet/sec YDOT = 4695
519031 meter/sec
ZDOT = -18592
448587 ZDOT = -5666
978329
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 08132
58014862
00020000 00000-0 20000-3 0 9063
2 25544 51
6395 205
0775 0005811 198
8396 161
2554 15
76276284 22754
Satellite: ISS
Catalog Number: 25544
Epoch time: 08132
58014862 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 205
0775 deg
Eccentricity:
0005811
Arg of perigee: 198
8396 deg
Mean anomaly: 161
2554 deg
Mean motion: 15
76276284 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2275
Checksum: 309
Coasting Arc #8 (Orbit 2290)
---------------------------------------
Vector Time (GMT): 2008/133/13:14:53
461
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4281902
17 A = 6716246
01 meter
Y = -2380106
55 meter E =
0005311
Z = 4589259
44 I = 51
52114
XDOT = 5600
136125 Wp = 108
42151
YDOT = 4405
862633 meter/sec RA = 199
05624 deg
ZDOT = -2938
970439 TA = 10
73231
MA = 10
72098
Ha = 186
693 n
mi
Hp = 180
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14048235
45 X = 4285904
84
Y = -7808748
53 feet Y = -2332201
80 meter
Z = 15056625
45 Z = 4610070
50
XDOT = 18373
150018 XDOT = 5564
729860
YDOT = 14454
929898 feet/sec YDOT = 4468
288791 meter/sec
ZDOT = -9642
291467 ZDOT = -2911
850661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2190710
42 X = -667728
54
Y = -15846902
45 feet Y = -4830135
87 meter
Z = 15136311
09 Z = 4613547
62
XDOT = 19015
417581 XDOT = 5795
899279
YDOT = -11742
175505 feet/sec YDOT = -3579
015094 meter/sec
ZDOT = -9537
646371 ZDOT = -2907
074614
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 08133
59450390
00020000 00000-0 20000-3 0 9076
2 25544 51
6393 199
8507 0005751 204
3561 155
7332 15
76334272 22917
Satellite: ISS
Catalog Number: 25544
Epoch time: 08133
59450390 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 199
8507 deg
Eccentricity:
0005751
Arg of perigee: 204
3561 deg
Mean anomaly: 155
7332 deg
Mean motion: 15
76334272 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2291
Checksum: 295
Coasting Arc #9 (Orbit 2306)
---------------------------------------
Vector Time (GMT): 2008/134/13:14:53
461
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4547804
16 A = 6721140
04 meter
Y = -3758306
31 meter E =
0011362
Z = 3215461
50 I = 51
56513
XDOT = 5486
746559 Wp = 112
38559
YDOT = -2540
592110 meter/sec RA = 193
94318 deg
ZDOT = 4773
066407 TA = 285
27148
MA = 285
39705
Ha = 186
745 n
mi
Hp = 180
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14920617
31 X = -4521060
37
Y = -12330401
30 feet Y = -3809013
10 meter
Z = 10549414
35 Z = 3193432
94
XDOT = 18001
137005 XDOT = 5491
561289
YDOT = -8335
275953 feet/sec YDOT = -2479
209504 meter/sec
ZDOT = 15659
666691 ZDOT = 4799
732685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16772073
95 X = -5112128
14
Y = 9754378
29 feet Y = 2973134
50 meter
Z = 10464387
22 Z = 3189545
23
XDOT = -871
202617 XDOT = -265
542558
YDOT = -18469
681495 feet/sec YDOT = -5629
558920 meter/sec
ZDOT = 15761
832544 ZDOT = 4804
206559
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 08134
60884050
00020000 00000-0 20000-3 0 9084
2 25544 51
6390 194
6231 0005546 205
8018 154
2870 15
76325608 23078
Satellite: ISS
Catalog Number: 25544
Epoch time: 08134
60884050 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 194
6231 deg
Eccentricity:
0005546
Arg of perigee: 205
8018 deg
Mean anomaly: 154
2870 deg
Mean motion: 15
76325608 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2307
Checksum: 284
Coasting Arc #10 (Orbit 2321)
---------------------------------------
Vector Time (GMT): 2008/135/13:14:53
461
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5255463
81 A = 6719552
38 meter
Y = 2103166
35 meter E =
0006512
Z = -3628387
43 I = 51
59045
XDOT = -4714
059254 Wp = 154
22295
YDOT = -4231
564104 meter/sec RA = 188
73403 deg
ZDOT = 4372
356922 TA = 162
25163
MA = 162
22887
Ha = 186
474 n
mi
Hp = 180
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17242335
33 X = -5260964
95
Y = 6900152
08 feet Y = 2044366
17 meter
Z = -11904158
23 Z = -3653931
94
XDOT = -15466
073667 XDOT = -4687
631171
YDOT = -13883
084331 feet/sec YDOT = -4284
131854 meter/sec
ZDOT = 14345
003026 ZDOT = 4349
519828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 811806
36 X = 247438
58
Y = 18490823
34 feet Y = 5636002
95 meter
Z = -12002067
83 Z = -3658230
28
XDOT = -16906
291360 XDOT = -5153
037607
YDOT = 10002
070584 feet/sec YDOT = 3048
631114 meter/sec
ZDOT = 14256
812944 ZDOT = 4345
476585
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 08135
55975955
00020000 00000-0 20000-3 0 9095
2 25544 51
6400 189
7226 0005499 209
5596 150
5259 15
76390300 23226
Satellite: ISS
Catalog Number: 25544
Epoch time: 08135
55975955 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 189
7226 deg
Eccentricity:
0005499
Arg of perigee: 209
5596 deg
Mean anomaly: 150
5259 deg
Mean motion: 15
76390300 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2322
Checksum: 313
Coasting Arc #11 (Orbit 2337)
---------------------------------------
Vector Time (GMT): 2008/136/13:14:53
461
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3593461
27 A = 6717222
95 meter
Y = 3668320
25 meter E =
0005401
Z = -4333900
79 I = 51
61176
XDOT = -6494
013520 Wp = 105
63245
YDOT = 2312
674611 meter/sec RA = 183
62832 deg
ZDOT = -3431
978199 TA = 129
73901
MA = 129
69141
Ha = 186
341 n
mi
Hp = 181
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11789571
08 X = 3573228
03
Y = 12035171
42 feet Y = 3708391
49 meter
Z = -14218834
60 Z = -4316492
49
XDOT = -21305
818634 XDOT = -6502
719418
YDOT = 7587
515129 feet/sec YDOT = 2240
006339 meter/sec
ZDOT = -11259
770994 ZDOT = -3463
547543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15165304
41 X = 4622384
79
Y = -7467364
59 feet Y = -2276052
73 meter
Z = -14151558
32 Z = -4313394
98
XDOT = -45
563414 XDOT = -13
887729
YDOT = 21444
491870 feet/sec YDOT = 6536
281122 meter/sec
ZDOT = -11380
812076 ZDOT = -3468
871521
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 08136
57405304
00020000 00000-0 20000-3 0 9106
2 25544 51
6402 184
4952 0005472 213
9832 146
0983 15
76407099 23384
Satellite: ISS
Catalog Number: 25544
Epoch time: 08136
57405304 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 184
4952 deg
Eccentricity:
0005472
Arg of perigee: 213
9832 deg
Mean anomaly: 146
0983 deg
Mean motion: 15
76407099 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2338
Checksum: 292
Coasting Arc #12 (Orbit 2353)
---------------------------------------
Vector Time (GMT): 2008/137/13:14:53
461
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5998252
74 A = 6722884
90 meter
Y = -1972282
94 meter E =
0013084
Z = 2284865
31 I = 51
65931
XDOT = 3465
065549 Wp = 129
85051
YDOT = 4214
289346 meter/sec RA = 178
42918 deg
ZDOT = -5446
526856 TA = 24
43856
MA = 24
37659
Ha = 186
021 n
mi
Hp = 181
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19679306
89 X = 6008761
66
Y = -6470744
57 feet Y = -1905148
44 meter
Z = 7496277
27 Z = 2314030
70
XDOT = 11368
325292 XDOT = 3444
141852
YDOT = 13826
408616 feet/sec YDOT = 4252
921062 meter/sec
ZDOT = -17869
182600 ZDOT = -5429
743833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -301229
60 X = -91814
78
Y = -20672819
89 feet Y = -6301075
50 meter
Z = 7608127
64 Z = 2318957
31
XDOT = 15116
570506 XDOT = 4607
530690
YDOT = -6787
260366 feet/sec YDOT = -2068
756959 meter/sec
ZDOT = -17804
248623 ZDOT = -5426
734980
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 08137
58832532
00020000 00000-0 20000-3 0 9116
2 25544 51
6387 179
2676 0005330 217
9960 142
0829 15
76445634 23540
Satellite: ISS
Catalog Number: 25544
Epoch time: 08137
58832532 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 179
2676 deg
Eccentricity:
0005330
Arg of perigee: 217
9960 deg
Mean anomaly: 142
0829 deg
Mean motion: 15
76445634 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2354
Checksum: 308
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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