Date:
September 25th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
276/12:03:32
384 -3
9 4
5 4
5
N/A -1
6 0
0 193
9
000/00:09:20
767 1
5 0
1 188
5
Coasting Arc #1 (Orbit 415)
---------------------------------------
Vector Time (GMT): 2008/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5563804
20 A = 6734129
25 meter
Y = -2659163
30 meter E =
0008087
Z = -2716190
37 I = 51
40947
XDOT = 216
879700 Wp = 109
05050
YDOT = -5704
638104 meter/sec RA = 226
12416 deg
ZDOT = 5150
516510 TA = 219
90408
MA = 219
96355
Ha = 194
757 n
mi
Hp = 185
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18253950
80 X = -5520460
77
Y = -8724289
03 feet Y = -2721138
69 meter
Z = -8911385
74 Z = -2743113
90
XDOT = 711
547571 XDOT = 255
633560
YDOT = -18716
004277 feet/sec YDOT = -5701
996007 meter/sec
ZDOT = 16898
020046 ZDOT = 5151
664395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18625769
71 X = 5677134
61
Y = 7780031
81 feet Y = 2371353
70 meter
Z = -9015794
06 Z = -2748014
03
XDOT = 912
543451 XDOT = 278
143244
YDOT = 17364
649377 feet/sec YDOT = 5292
745130 meter/sec
ZDOT = 16901
877552 ZDOT = 5151
692278
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 08268
50554653
00020000 00000-0 20000-3 0 9006
2 25544 51
6373 227
0516 0006252 144
9924 215
1650 15
72163747 4162
Satellite: ISS
Catalog Number: 25544
Epoch time: 08268
50554653 = yrday
fracday
Element set: 900
Inclination: 51
6373 deg
RA of node: 227
0516 deg
Eccentricity:
0006252
Arg of perigee: 144
9924 deg
Mean anomaly: 215
1650 deg
Mean motion: 15
72163747 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 416
Checksum: 280
Coasting Arc #2 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2008/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 868118
72 A = 6729677
40 meter
Y = 5194552
21 meter E =
0011073
Z = -4197048
63 I = 51
41679
XDOT = -6525
018065 Wp = 103
43699
YDOT = -1836
385370 meter/sec RA = 221
03375 deg
ZDOT = -3633
033200 TA = 129
43275
MA = 129
33469
Ha = 194
611 n
mi
Hp = 185
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2848158
53 X = 830356
32
Y = 17042494
14 feet Y = 5204048
65 meter
Z = -13769844
59 Z = -4192923
33
XDOT = -21407
539584 XDOT = -6486
349789
YDOT = -6024
886383 feet/sec YDOT = -1909
135881 meter/sec
ZDOT = -11919
400263 ZDOT = -3664
637611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4086154
54 X = -1245459
90
Y = -16802260
32 feet Y = -5121328
94 meter
Z = -13753349
51 Z = -4192020
93
XDOT = 20475
865192 XDOT = 6241
043711
YDOT = 4848
810720 feet/sec YDOT = 1477
917507 meter/sec
ZDOT = -12041
841967 ZDOT = -3670
353432
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 08269
52255017
00020000 00000-0 20000-3 0 9012
2 25544 51
6382 221
8420 0006185 149
0888 211
0639 15
72203480 4327
Satellite: ISS
Catalog Number: 25544
Epoch time: 08269
52255017 = yrday
fracday
Element set: 901
Inclination: 51
6382 deg
RA of node: 221
8420 deg
Eccentricity:
0006185
Arg of perigee: 149
0888 deg
Mean anomaly: 211
0639 deg
Mean motion: 15
72203480 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 432
Checksum: 271
Coasting Arc #3 (Orbit 447)
---------------------------------------
Vector Time (GMT): 2008/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5644990
64 A = 6731459
55 meter
Y = 526772
79 meter E =
0015297
Z = 3612252
87 I = 51
44666
XDOT = 2253
146582 Wp = 107
21850
YDOT = 5929
219178 meter/sec RA = 215
84663 deg
ZDOT = -4374
976564 TA = 29
37977
MA = 29
29386
Ha = 194
371 n
mi
Hp = 185
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18520310
51 X = 5621132
97
Y = 1728257
18 feet Y = 589765
22 meter
Z = 11851223
33 Z = 3639618
23
XDOT = 7392
213195 XDOT = 2207
930475
YDOT = 19452
818824 feet/sec YDOT = 5954
162003 meter/sec
ZDOT = -14353
597650 ZDOT = -4364
141081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18532313
20 X = -5648649
06
Y = -143028
68 feet Y = -43595
14 meter
Z = 11957139
23 Z = 3644536
04
XDOT = -9121
897889 XDOT = -2780
354477
YDOT = -17390
465976 feet/sec YDOT = -5300
614029 meter/sec
ZDOT = -14311
060065 ZDOT = -4362
011108
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 08270
53954084
00020000 00000-0 20000-3 0 9026
2 25544 51
6387 216
6333 0006106 153
2490 206
8988 15
72225685 4483
Satellite: ISS
Catalog Number: 25544
Epoch time: 08270
53954084 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 216
6333 deg
Eccentricity:
0006106
Arg of perigee: 153
2490 deg
Mean anomaly: 206
8988 deg
Mean motion: 15
72225685 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 448
Checksum: 301
Coasting Arc #4 (Orbit 463)
---------------------------------------
Vector Time (GMT): 2008/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3028840
16 A = 6732200
70 meter
Y = -4953623
11 meter E =
0015962
Z = 3400458
26 I = 51
47427
XDOT = 6150
922725 Wp = 111
29944
YDOT = -593
092772 meter/sec RA = 210
76350 deg
ZDOT = 4591
744269 TA = 288
93955
MA = 289
11249
Ha = 194
419 n
mi
Hp = 185
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9937139
64 X = -2989741
72
Y = -16252044
31 feet Y = -4987274
42 meter
Z = 11156359
14 Z = 3385839
54
XDOT = 20180
192668 XDOT = 6134
791674
YDOT = -1945
842428 feet/sec YDOT = -524
399366 meter/sec
ZDOT = 15064
777787 ZDOT = 4621
586445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11617013
05 X = 3540865
58
Y = 15139055
48 feet Y = 4614384
11 meter
Z = 11099281
27 Z = 3383060
93
XDOT = -18683
529030 XDOT = -5694
739648
YDOT = 3151
881149 feet/sec YDOT = 960
693374 meter/sec
ZDOT = 15180
162489 ZDOT = 4626
913527
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 08271
55651798
00020000 00000-0 20000-3 0 9036
2 25544 51
6393 211
4244 0006176 157
7736 202
3695 15
72251077 4641
Satellite: ISS
Catalog Number: 25544
Epoch time: 08271
55651798 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 211
4244 deg
Eccentricity:
0006176
Arg of perigee: 157
7736 deg
Mean anomaly: 202
3695 deg
Mean motion: 15
72251077 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 464
Checksum: 299
Coasting Arc #5 (Orbit 478)
---------------------------------------
Vector Time (GMT): 2008/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4922136
52 A = 6728834
43 meter
Y = 1485858
12 meter E =
0013817
Z = -4355043
23 I = 51
48943
XDOT = -4562
443237 Wp = 130
85614
YDOT = -5174
137941 meter/sec RA = 205
58022 deg
ZDOT = 3389
349889 TA = 173
45459
MA = 173
43652
Ha = 194
267 n
mi
Hp = 185
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16148741
87 X = -4917229
58
Y = 4874862
59 feet Y = 1430842
95 meter
Z = -14288199
57 Z = -4378943
42
XDOT = -14968
645790 XDOT = -4520
711108
YDOT = -16975
518180 feet/sec YDOT = -5224
924145 meter/sec
ZDOT = 11119
914333 ZDOT = 3367
287209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15366965
99 X = 4683851
23
Y = -6764333
70 feet Y = -2061768
91 meter
Z = -14380505
63 Z = -4383178
12
XDOT = 16464
094428 XDOT = 5018
255982
YDOT = 13931
988877 feet/sec YDOT = 4246
470210 meter/sec
ZDOT = 11034
009377 ZDOT = 3363
166058
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 08272
50992292
00020000 00000-0 20000-3 0 9040
2 25544 51
6396 206
5406 0006061 161
2349 198
9038 15
72254890 4795
Satellite: ISS
Catalog Number: 25544
Epoch time: 08272
50992292 = yrday
fracday
Element set: 904
Inclination: 51
6396 deg
RA of node: 206
5406 deg
Eccentricity:
0006061
Arg of perigee: 161
2349 deg
Mean anomaly: 198
9038 deg
Mean motion: 15
72254890 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 479
Checksum: 307
Coasting Arc #6 (Orbit 494)
---------------------------------------
Vector Time (GMT): 2008/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4846229
49 A = 6734392
37 meter
Y = 3939431
12 meter E =
0010894
Z = -2509197
68 I = 51
53614
XDOT = -4902
126379 Wp = 149
40049
YDOT = 2665
089113 meter/sec RA = 200
49465 deg
ZDOT = -5302
995441 TA = 59
03194
MA = 58
92494
Ha = 194
182 n
mi
Hp = 185
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15899703
06 X = 4814007
36
Y = 12924642
78 feet Y = 3993444
06 meter
Z = -8232275
84 Z = -2485732
99
XDOT = -16083
091796 XDOT = -4905
802118
YDOT = 8743
730685 feet/sec YDOT = 2610
249653 meter/sec
ZDOT = -17398
279006 ZDOT = -5326
819501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17565307
47 X = -5353905
72
Y = -10620743
76 feet Y = -3237202
70 meter
Z = -8141074
21 Z = -2481399
42
XDOT = 13861
726092 XDOT = 4225
054113
YDOT = -9567
819886 feet/sec YDOT = -2916
271501 meter/sec
ZDOT = -17490
168698 ZDOT = -5331
003419
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 08273
52687478
00020000 00000-0 20000-3 0 9051
2 25544 51
6406 201
3314 0006035 164
9158 195
2186 15
72283179 4951
Satellite: ISS
Catalog Number: 25544
Epoch time: 08273
52687478 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 201
3314 deg
Eccentricity:
0006035
Arg of perigee: 164
9158 deg
Mean anomaly: 195
2186 deg
Mean motion: 15
72283179 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 495
Checksum: 304
Coasting Arc #7 (Orbit 510)
---------------------------------------
Vector Time (GMT): 2008/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3488061
63 A = 6726617
72 meter
Y = -3053270
57 meter E =
0007113
Z = 4867654
53 I = 51
53807
XDOT = 6389
218806 Wp = 110
01705
YDOT = 3640
774120 meter/sec RA = 195
32617 deg
ZDOT = -2294
373359 TA = 2
34148
MA = 2
33815
Ha = 193
935 n
mi
Hp = 185
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11443771
76 X = 3498297
91
Y = -10017291
89 feet Y = -3014207
41 meter
Z = 15969995
17 Z = 4884624
97
XDOT = 20962
003956 XDOT = 6359
178082
YDOT = 11944
796981 feet/sec YDOT = 3712
053898 meter/sec
ZDOT = -7527
471651 ZDOT = -2263
407217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9675553
27 X = -2949108
64
Y = 11644681
02 feet Y = 3549298
78 meter
Z = 16035331
84 Z = 4887569
14
XDOT = -21743
432316 XDOT = -6627
398170
YDOT = -7865
002396 feet/sec YDOT = -2397
252730 meter/sec
ZDOT = -7407
274739 ZDOT = -2257
737340
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 08274
54381319
00020000 00000-0 20000-3 0 9060
2 25544 51
6403 196
1230 0006007 169
0488 191
0806 15
72303989 5111
Satellite: ISS
Catalog Number: 25544
Epoch time: 08274
54381319 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 196
1230 deg
Eccentricity:
0006007
Arg of perigee: 169
0488 deg
Mean anomaly: 191
0806 deg
Mean motion: 15
72303989 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 511
Checksum: 283
Coasting Arc #8 (Orbit 526)
---------------------------------------
Vector Time (GMT): 2008/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6147779
21 A = 6736070
46 meter
Y = -2307821
91 meter E =
0013069
Z = 1487789
17 I = 51
59842
XDOT = 2958
645337 Wp = 86
78582
YDOT = -4124
917413 meter/sec RA = 190
23013 deg
ZDOT = 5784
254482 TA = 289
59146
MA = 289
73251
Ha = 193
909 n
mi
Hp = 185
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20169879
31 X = -6128743
42
Y = -7571594
19 feet Y = -2376463
39 meter
Z = 4881198
07 Z = 1457969
01
XDOT = 9706
841656 XDOT = 2976
451461
YDOT = -13533
193611 feet/sec YDOT = -4091
732195 meter/sec
ZDOT = 18977
212867 ZDOT = 5798
671412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21194126
25 X = 6459969
68
Y = 4009677
42 feet Y = 1222149
68 meter
Z = 4765570
68 Z = 1452545
94
XDOT = -6852
419864 XDOT = -2088
617575
YDOT = 13428
409818 feet/sec YDOT = 4092
979313 meter/sec
ZDOT = 19032
562158 ZDOT = 5801
124946
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 08275
56073827
00020000 00000-0 20000-3 0 9076
2 25544 51
6404 190
9133 0005974 173
0387 187
0859 15
72314245 5278
Satellite: ISS
Catalog Number: 25544
Epoch time: 08275
56073827 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 190
9133 deg
Eccentricity:
0005974
Arg of perigee: 173
0387 deg
Mean anomaly: 187
0859 deg
Mean motion: 15
72314245 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 527
Checksum: 306
Coasting Arc #9 (Orbit 541)
---------------------------------------
Vector Time (GMT): 2008/276/11:59:58
000
Vector Time (MET): N/A
Weight (LBS) : 628649
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1602598
73 A = 6725498
87 meter
Y = 3986544
07 meter E =
0016278
Z = -5187557
63 I = 51
59181
XDOT = -7447
839123 Wp = 119
68577
YDOT = -1544
598201 meter/sec RA = 185
08118 deg
ZDOT = 1108
563627 TA = 160
95020
MA = 160
88925
Ha = 193
772 n
mi
Hp = 186
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5257869
84 X = -1621857
01
Y = 13079212
82 feet Y = 3968514
97 meter
Z = -17019546
04 Z = -5195390
19
XDOT = -24435
167727 XDOT = -7435
398955
YDOT = -5067
579401 feet/sec YDOT = -1627
814630 meter/sec
ZDOT = 3637
019772 ZDOT = 1072
411501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2614682
80 X = 796955
32
Y = -13815065
60 feet Y = -4210831
99 meter
Z = -17049438
32 Z = -5196668
80
XDOT = 23964
683940 XDOT = 7304
435665
YDOT = 198
496350 feet/sec YDOT = 60
501687 meter/sec
ZDOT = 3496
962723 ZDOT = 1065
874238
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 08276
51409250
00020000 00000-0 20000-3 0 9086
2 25544 51
6408 186
0294 0005897 180
9455 179
1697 15
72242451 5421
Satellite: ISS
Catalog Number: 25544
Epoch time: 08276
51409250 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 186
0294 deg
Eccentricity:
0005897
Arg of perigee: 180
9455 deg
Mean anomaly: 179
1697 deg
Mean motion: 15
72242451 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 542
Checksum: 309
Coasting Arc #10 (Orbit 541)
---------------------------------------
Vector Time (GMT): 2008/276/12:08:12
767
Vector Time (MET): N/A
Weight (LBS) : 628360
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4846835
41 A = 6732812
69 meter
Y = 2644111
03 meter E =
0007138
Z = -3861192
09 I = 51
60936
XDOT = -5315
898239 Wp = 152
09021
YDOT = -3737
649101 meter/sec RA = 185
03537 deg
ZDOT = 4110
241338 TA = 160
92363
MA = 160
89689
Ha = 193
869 n
mi
Hp = 188
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15901690
99 X = -4857284
66
Y = 8674904
96 feet Y = 2589852
32 meter
Z = -12667953
06 Z = -3884764
05
XDOT = -17440
611019 XDOT = -5293
675410
YDOT = -12262
628283 feet/sec YDOT = -3796
970101 meter/sec
ZDOT = 13485
043761 ZDOT = 4084
470277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13496606
69 X = 4113765
72
Y = -11985286
10 feet Y = -3653115
20 meter
Z = -12758891
49 Z = -3888910
13
XDOT = 18936
476201 XDOT = 5771
837946
YDOT = 7064
591753 feet/sec YDOT = 2153
287566 meter/sec
ZDOT = 13384
928245 ZDOT = 4079
726129
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 08276
51409213
00020000 00000-0 20000-3 0 9096
2 25544 51
6408 186
0296 0005318 213
4928 146
5898 15
71479253 5420
Satellite: ISS
Catalog Number: 25544
Epoch time: 08276
51409213 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 186
0296 deg
Eccentricity:
0005318
Arg of perigee: 213
4928 deg
Mean anomaly: 146
5898 deg
Mean motion: 15
71479253 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 542
Checksum: 308
Coasting Arc #11 (Orbit 557)
---------------------------------------
Vector Time (GMT): 2008/277/12:08:12
767
Vector Time (MET): N/A
Weight (LBS) : 628360
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5568495
82 A = 6735603
84 meter
Y = 2346091
12 meter E =
0006055
Z = -2969043
69 I = 51
64804
XDOT = -4323
130152 Wp = 172
24407
YDOT = 3952
302713 meter/sec RA = 179
96817 deg
ZDOT = -4992
126650 TA = 41
97389
MA = 41
92751
Ha = 193
784 n
mi
Hp = 188
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18269343
23 X = 5556270
97
Y = 7697149
33 feet Y = 2408292
82 meter
Z = -9740956
98 Z = -2942021
10
XDOT = -14183
497873 XDOT = -4342
752753
YDOT = 12966
872418 feet/sec YDOT = 3903
849124 meter/sec
ZDOT = -16378
368275 ZDOT = -5013
176646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19635527
68 X = -5984908
84
Y = -3080938
32 feet Y = -939070
00 meter
Z = -9636136
39 Z = -2937094
37
XDOT = 10346
411804 XDOT = 3153
586318
YDOT = -14533
808703 feet/sec YDOT = -4429
904893 meter/sec
ZDOT = -16459
421477 ZDOT = -5016
831666
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 08277
53155419
00020000 00000-0 20000-3 0 9107
2 25544 51
6410 180
8241 0005384 218
4105 141
6674 15
71484426 5583
Satellite: ISS
Catalog Number: 25544
Epoch time: 08277
53155419 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 180
8241 deg
Eccentricity:
0005384
Arg of perigee: 218
4105 deg
Mean anomaly: 141
6674 deg
Mean motion: 15
71484426 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 558
Checksum: 282
Coasting Arc #12 (Orbit 573)
---------------------------------------
Vector Time (GMT): 2008/278/12:08:12
767
Vector Time (MET): N/A
Weight (LBS) : 628360
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2527477
50 A = 6729255
15 meter
Y = -4016849
72 meter E =
0002703
Z = 4768290
30 I = 51
65613
XDOT = 7113
698901 Wp = 95
74161
YDOT = 1406
656625 meter/sec RA = 174
80904 deg
ZDOT = -2584
718560 TA = 19
60993
MA = 19
59954
Ha = 193
404 n
mi
Hp = 188
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8292249
01 X = 2549042
75
Y = -13178640
81 feet Y = -3988465
37 meter
Z = 15643997
06 Z = 4780621
47
XDOT = 23338
907155 XDOT = 7109
997076
YDOT = 4615
015174 feet/sec YDOT = 1486
185381 meter/sec
ZDOT = -8480
047770 ZDOT = -2550
168533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4550339
31 X = -1386943
42
Y = 14840816
12 feet Y = 4523480
75 meter
Z = 15691309
70 Z = 4782711
20
XDOT = -22706
488539 XDOT = -6920
937707
YDOT = 1865
856825 feet/sec YDOT = 568
713160 meter/sec
ZDOT = -8346
180653 ZDOT = -2543
915863
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 08278
54900269
00020000 00000-0 20000-3 0 9111
2 25544 51
6404 175
6184 0005312 223
4242 136
6502 15
71541828 5745
Satellite: ISS
Catalog Number: 25544
Epoch time: 08278
54900269 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 175
6184 deg
Eccentricity:
0005312
Arg of perigee: 223
4242 deg
Mean anomaly: 136
6502 deg
Mean motion: 15
71541828 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 574
Checksum: 278
Coasting Arc #13 (Orbit 589)
---------------------------------------
Vector Time (GMT): 2008/279/12:08:12
767
Vector Time (MET): N/A
Weight (LBS) : 628360
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6563865
38 A = 6738307
33 meter
Y = -19553
26 meter E =
0009001
Z = 1507150
34 I = 51
71548
XDOT = 1349
378711 Wp = 70
13635
YDOT = -4887
827003 meter/sec RA = 169
72891 deg
ZDOT = 5788
443077 TA = 306
42857
MA = 306
51153
Ha = 193
336 n
mi
Hp = 189
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21534991
40 X = -6570480
48
Y = -64151
11 feet Y = -92991
17 meter
Z = 4944718
95 Z = 1475246
46
XDOT = 4427
095510 XDOT = 1375
815194
YDOT = -16036
177830 feet/sec YDOT = -4872
589636 meter/sec
ZDOT = 18990
954978 ZDOT = 5795
062706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20761881
86 X = 6328221
59
Y = -5823254
14 feet Y = -1774927
86 meter
Z = 4821222
70 Z = 1469508
68
XDOT = -202
332390 XDOT = -61
670913
YDOT = 15091
859555 feet/sec YDOT = 4599
998792 meter/sec
ZDOT = 19016
077585 ZDOT = 5796
100448
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 08279
56644001
00020000 00000-0 20000-3 0 9124
2 25544 51
6407 170
4120 0005281 227
4256 132
6461 15
71522448 5900
Satellite: ISS
Catalog Number: 25544
Epoch time: 08279
56644001 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 170
4120 deg
Eccentricity:
0005281
Arg of perigee: 227
4256 deg
Mean anomaly: 132
6461 deg
Mean motion: 15
71522448 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 590
Checksum: 266
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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