Date:
September 29th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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
276/12:01:12
220 -2
2 2
3 2
3
N/A -0
6 0
0 193
8
000/00:04:40
440 0
5 0
0 187
1
Coasting Arc #1 (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 = 5646008
97 A = 6731449
69 meter
Y = 529808
57 meter E =
0015384
Z = 3610105
86 I = 51
44691
XDOT = 2249
448109 Wp = 107
23596
YDOT = 5928
979089 meter/sec RA = 215
84813 deg
ZDOT = -4377
314697 TA = 29
39421
MA = 29
30778
Ha = 194
390 n
mi
Hp = 185
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18523651
47 X = 5622127
70
Y = 1738217
10 feet Y = 592812
26 meter
Z = 11844179
32 Z = 3637476
10
XDOT = 7380
079098 XDOT = 2204
246320
YDOT = 19452
031132 feet/sec YDOT = 5953
880636 meter/sec
ZDOT = -14361
268690 ZDOT = -4366
497146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18536534
32 X = -5649935
66
Y = -152662
72 feet Y = -46531
60 meter
Z = 11950114
46 Z = 3642394
89
XDOT = -9110
487408 XDOT = -2776
876562
YDOT = -17390
407864 feet/sec YDOT = -5300
596317 meter/sec
ZDOT = -14318
800502 ZDOT = -4364
370393
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
53953531
00020000 00000-0 20000-3 0 9000
2 25544 51
6389 216
6349 0006160 152
7145 207
4342 15
72231492 4487
Satellite: ISS
Catalog Number: 25544
Epoch time: 08270
53953531 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 216
6349 deg
Eccentricity:
0006160
Arg of perigee: 152
7145 deg
Mean anomaly: 207
4342 deg
Mean motion: 15
72231492 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 448
Checksum: 279
Coasting Arc #2 (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 = -3023397
58 A = 6732164
14 meter
Y = -4954170
41 meter E =
0016038
Z = 3404401
65 I = 51
47446
XDOT = 6154
389975 Wp = 111
37078
YDOT = -587
292645 meter/sec RA = 210
76498 deg
ZDOT = 4587
904569 TA = 288
92470
MA = 289
09848
Ha = 194
434 n
mi
Hp = 185
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9919283
39 X = -2984312
57
Y = -16253839
94 feet Y = -4987760
94 meter
Z = 11169296
75 Z = 3389809
33
XDOT = 20191
568161 XDOT = 6138
212461
YDOT = -1926
813139 feet/sec YDOT = -518
560726 meter/sec
ZDOT = 15052
180344 ZDOT = 4617
763475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11599509
63 X = 3535530
53
Y = 15142667
68 feet Y = 4615485
11 meter
Z = 11112320
98 Z = 3387035
44
XDOT = -18696
606783 XDOT = -5698
725747
YDOT = 3135
404462 feet/sec YDOT = 955
671280 meter/sec
ZDOT = 15167
630382 ZDOT = 4623
093740
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
55650769
00020000 00000-0 20000-3 0 9011
2 25544 51
6395 211
4260 0006232 157
2622 202
8817 15
72259784 4647
Satellite: ISS
Catalog Number: 25544
Epoch time: 08271
55650769 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 211
4260 deg
Eccentricity:
0006232
Arg of perigee: 157
2622 deg
Mean anomaly: 202
8817 deg
Mean motion: 15
72259784 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 464
Checksum: 290
Coasting Arc #3 (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 = -4928685
79 A = 6728819
77 meter
Y = 1478333
00 meter E =
0013869
Z = -4350228
10 I = 51
48972
XDOT = -4553
142221 Wp = 130
82808
YDOT = -5176
969652 meter/sec RA = 205
58161 deg
ZDOT = 3397
448312 TA = 173
57598
MA = 173
55818
Ha = 194
277 n
mi
Hp = 185
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16170228
96 X = -4923717
61
Y = 4850173
87 feet Y = 1423244
93 meter
Z = -14272401
90 Z = -4374159
96
XDOT = -14938
130645 XDOT = -4511
418460
YDOT = -16984
808570 feet/sec YDOT = -5227
651893 meter/sec
ZDOT = 11146
483962 ZDOT = 3375
430796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15391345
32 X = 4691282
05
Y = -6742407
52 feet Y = -2055085
81 meter
Z = -14364831
28 Z = -4378400
57
XDOT = 16436
662415 XDOT = 5009
894704
YDOT = 13943
071628 feet/sec YDOT = 4249
848232 meter/sec
ZDOT = 11060
753438 ZDOT = 3371
317648
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
50990646
00020000 00000-0 20000-3 0 9029
2 25544 51
6399 206
5421 0006119 160
7358 199
4037 15
72266376 4790
Satellite: ISS
Catalog Number: 25544
Epoch time: 08272
50990646 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 206
5421 deg
Eccentricity:
0006119
Arg of perigee: 160
7358 deg
Mean anomaly: 199
4037 deg
Mean motion: 15
72266376 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 479
Checksum: 311
Coasting Arc #4 (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 = 4835518
74 A = 6734326
13 meter
Y = 3945249
36 meter E =
0010929
Z = -2520608
06 I = 51
53629
XDOT = -4915
807283 Wp = 149
12116
YDOT = 2653
877625 meter/sec RA = 200
49607 deg
ZDOT = -5295
947344 TA = 59
45251
MA = 59
34470
Ha = 194
189 n
mi
Hp = 185
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15864562
80 X = 4803287
78
Y = 12943731
51 feet Y = 3999142
48 meter
Z = -8269711
48 Z = -2497195
42
XDOT = -16127
976649 XDOT = -4919
390874
YDOT = 8706
947588 feet/sec YDOT = 2598
885693 meter/sec
ZDOT = -17375
155328 ZDOT = -5319
837642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17533323
13 X = -5344156
89
Y = -10644432
28 feet Y = -3244422
96 meter
Z = -8178710
63 Z = -2492871
00
XDOT = 13909
625515 XDOT = 4239
653857
YDOT = -9539
875731 feet/sec YDOT = -2907
754123 meter/sec
ZDOT = -17467
302480 ZDOT = -5324
033796
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
52684988
00020000 00000-0 20000-3 0 9032
2 25544 51
6408 201
3329 0006096 164
4363 195
6988 15
72297694 4950
Satellite: ISS
Catalog Number: 25544
Epoch time: 08273
52684988 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 201
3329 deg
Eccentricity:
0006096
Arg of perigee: 164
4363 deg
Mean anomaly: 195
6988 deg
Mean motion: 15
72297694 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 495
Checksum: 334
Coasting Arc #5 (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 = 3507293
84 A = 6726597
68 meter
Y = -3042140
16 meter E =
0007232
Z = 4860661
44 I = 51
53841
XDOT = 6375
404956 Wp = 110
03211
YDOT = 3652
987534 meter/sec RA = 195
32730 deg
ZDOT = -2313
650195 TA = 2
52428
MA = 2
52063
Ha = 193
938 n
mi
Hp = 185
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11506869
54 X = 3517438
20
Y = -9980774
79 feet Y = -3002862
45 meter
Z = 15947051
95 Z = 4877725
08
XDOT = 20916
682926 XDOT = 6345
322331
YDOT = 11984
867239 feet/sec YDOT = 3724
112603 meter/sec
ZDOT = -7590
715862 ZDOT = -2282
751265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9743647
33 X = -2969863
71
Y = 11618327
69 feet Y = 3541266
28 meter
Z = 16012750
43 Z = 4880686
33
XDOT = -21707
097029 XDOT = -6616
323174
YDOT = -7906
547399 feet/sec YDOT = -2409
915647 meter/sec
ZDOT = -7470
777705 ZDOT = -2277
093044
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
54377794
00020000 00000-0 20000-3 0 9040
2 25544 51
6406 196
1245 0006071 168
5805 191
5496 15
72321122 5117
Satellite: ISS
Catalog Number: 25544
Epoch time: 08274
54377794 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 196
1245 deg
Eccentricity:
0006071
Arg of perigee: 168
5805 deg
Mean anomaly: 191
5496 deg
Mean motion: 15
72321122 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 511
Checksum: 289
Coasting Arc #6 (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 = -6135682
97 A = 6735982
72 meter
Y = -2324586
59 meter E =
0013160
Z = 1511131
13 I = 51
59856
XDOT = 2991
215007 Wp = 87
32442
YDOT = -4112
576247 meter/sec RA = 190
23146 deg
ZDOT = 5776
323121 TA = 289
31736
MA = 289
45963
Ha = 193
909 n
mi
Hp = 185
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20130193
46 X = -6116574
00
Y = -7626596
41 feet Y = -2393092
39 meter
Z = 4957779
30 Z = 1481369
91
XDOT = 9813
697530 XDOT = 3008
919240
YDOT = -13492
704223 feet/sec YDOT = -4079
027387 meter/sec
ZDOT = 18951
191342 ZDOT = 5790
898030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21164853
49 X = 6451047
34
Y = 4070575
74 feet Y = 1240711
48 meter
Z = 4842378
22 Z = 1475956
88
XDOT = -6960
326473 XDOT = -2121
507509
YDOT = 13408
931032 feet/sec YDOT = 4087
042179 meter/sec
ZDOT = 19007
153204 ZDOT = 5793
380297
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
56069072
00020000 00000-0 20000-3 0 9051
2 25544 51
6406 190
9147 0006040 172
5935 187
5318 15
72334605 5270
Satellite: ISS
Catalog Number: 25544
Epoch time: 08275
56069072 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 190
9147 deg
Eccentricity:
0006040
Arg of perigee: 172
5935 deg
Mean anomaly: 187
5318 deg
Mean motion: 15
72334605 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 527
Checksum: 293
Coasting Arc #7 (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 = -1641814
68 A = 6725458
63 meter
Y = 3978276
39 meter E =
0016337
Z = -5181631
51 I = 51
59213
XDOT = -7436
712591 Wp = 120
06382
YDOT = -1571
971244 meter/sec RA = 185
08188 deg
ZDOT = 1144
093248 TA = 160
91633
MA = 160
85505
Ha = 193
765 n
mi
Hp = 186
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5386531
11 X = -1661006
39
Y = 13052087
89 feet Y = 3959809
13 meter
Z = -17000103
38 Z = -5189654
42
XDOT = -24398
663357 XDOT = -7424
139761
YDOT = -5157
385970 feet/sec YDOT = -1655
062506 meter/sec
ZDOT = 3753
586773 ZDOT = 1107
995500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2746255
79 X = 837058
76
Y = -13812582
64 feet Y = -4210075
19 meter
Z = -17030733
12 Z = -5190967
45
XDOT = 23946
515184 XDOT = 7298
897828
YDOT = 283
836826 feet/sec YDOT = 86
513465 meter/sec
ZDOT = 3613
737283 ZDOT = 1101
467124
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
51403164
00020000 00000-0 20000-3 0 9062
2 25544 51
6411 186
0308 0005958 180
4745 179
6413 15
72265513 5421
Satellite: ISS
Catalog Number: 25544
Epoch time: 08276
51403164 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 186
0308 deg
Eccentricity:
0005958
Arg of perigee: 180
4745 deg
Mean anomaly: 179
6413 deg
Mean motion: 15
72265513 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 542
Checksum: 285
Coasting Arc #8 (Orbit 541)
---------------------------------------
Vector Time (GMT): 2008/276/12:03:32
440
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3171894
43 A = 6728088
32 meter
Y = 3526146
35 meter E =
0013386
Z = -4784099
21 I = 51
59793
XDOT = -6762
525374 Wp = 133
40850
YDOT = -2623
897606 meter/sec RA = 185
05899 deg
ZDOT = 2545
070072 TA = 161
60627
MA = 161
55782
Ha = 193
838 n
mi
Hp = 187
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10406477
78 X = -3187847
81
Y = 11568721
63 feet Y = 3490586
98 meter
Z = -15695863
55 Z = -4799547
53
XDOT = -22186
763037 XDOT = -6745
045686
YDOT = -8608
587946 feet/sec YDOT = -2699
422218 meter/sec
ZDOT = 8349
967427 ZDOT = 2512
259566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7753704
61 X = 2363329
16
Y = -13421685
15 feet Y = -4090929
63 meter
Z = -15755274
21 Z = -4802207
58
XDOT = 22539
944577 XDOT = 6870
175107
YDOT = 3351
366282 feet/sec YDOT = 1021
496443 meter/sec
ZDOT = 8222
728326 ZDOT = 2506
287594
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
51403161
00020000 00000-0 20000-3 0 9070
2 25544 51
6411 186
0308 0005686 194
0938 166
0067 15
71932794 5420
Satellite: ISS
Catalog Number: 25544
Epoch time: 08276
51403161 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 186
0308 deg
Eccentricity:
0005686
Arg of perigee: 194
0938 deg
Mean anomaly: 166
0067 deg
Mean motion: 15
71932794 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 542
Checksum: 292
Coasting Arc #9 (Orbit 557)
---------------------------------------
Vector Time (GMT): 2008/277/12:03:32
440
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6405413
97 A = 6736979
70 meter
Y = 1278968
96 meter E =
0012315
Z = -1620770
28 I = 51
65709
XDOT = -2357
455466 Wp = 165
99983
YDOT = 4548
116746 meter/sec RA = 179
97307 deg
ZDOT = -5748
654588 TA = 31
88225
MA = 31
80778
Ha = 193
806 n
mi
Hp = 187
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21015137
70 X = 6398509
85
Y = 4196092
38 feet Y = 1350559
35 meter
Z = -5317487
80 Z = -1589668
91
XDOT = -7734
433944 XDOT = -2380
211494
YDOT = 14921
642869 feet/sec YDOT = 4521
626926 meter/sec
ZDOT = -18860
415315 ZDOT = -5760
162756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21452913
11 X = -6538847
92
Y = 531660
22 feet Y = 162050
04 meter
Z = -5196993
08 Z = -1584043
49
XDOT = 4199
215729 XDOT = 1279
920954
YDOT = -14668
419338 feet/sec YDOT = -4470
934214 meter/sec
ZDOT = -18904
479873 ZDOT = -5762
085465
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
53119369
00020000 00000-0 20000-3 0 9088
2 25544 51
6412 180
8232 0005811 198
4890 161
6062 15
71932594 5585
Satellite: ISS
Catalog Number: 25544
Epoch time: 08277
53119369 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 180
8232 deg
Eccentricity:
0005811
Arg of perigee: 198
4890 deg
Mean anomaly: 161
6062 deg
Mean motion: 15
71932594 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 558
Checksum: 305
Coasting Arc #10 (Orbit 573)
---------------------------------------
Vector Time (GMT): 2008/278/12:03:32
440
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 867627
72 A = 6726128
17 meter
Y = -4196157
81 meter E =
0003268
Z = 5183411
00 I = 51
65037
XDOT = 7615
170579 Wp = 165
58390
YDOT = 198
369457 meter/sec RA = 174
83014 deg
ZDOT = -1117
038643 TA = 295
06030
MA = 295
09423
Ha = 193
433 n
mi
Hp = 187
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2846547
63 X = 889304
77
Y = -13766921
95 feet Y = -4186334
23 meter
Z = 17005941
61 Z = 5187678
73
XDOT = 24984
155442 XDOT = 7617
812879
YDOT = 650
818427 feet/sec YDOT = 283
541449 meter/sec
ZDOT = -3664
824944 ZDOT = -1080
036992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 585084
16 X = 178333
65
Y = 14026449
78 feet Y = 4275261
89 meter
Z = 17022027
10 Z = 5188313
86
XDOT = -23426
383254 XDOT = -7140
361616
YDOT = 5239
108387 feet/sec YDOT = 1596
880236 meter/sec
ZDOT = -3521
593614 ZDOT = -1073
381734
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
54833863
00020000 00000-0 20000-3 0 9093
2 25544 51
6408 175
6156 0005704 203
8085 156
2814 15
72019238 5740
Satellite: ISS
Catalog Number: 25544
Epoch time: 08278
54833863 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 175
6156 deg
Eccentricity:
0005704
Arg of perigee: 203
8085 deg
Mean anomaly: 156
2814 deg
Mean motion: 15
72019238 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 574
Checksum: 305
Coasting Arc #11 (Orbit 589)
---------------------------------------
Vector Time (GMT): 2008/279/12:03:32
440
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6660757
81 A = 6737825
90 meter
Y = 942412
27 meter E =
0007766
Z = 330458
54 I = 51
71885
XDOT = -370
283788 Wp = 63
61111
YDOT = -4767
764757 meter/sec RA = 169
72497 deg
ZDOT = 6027
928841 TA = 299
97244
MA = 300
04950
Ha = 193
328 n
mi
Hp = 187
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21852879
95 X = -6672406
31
Y = 3091903
76 feet Y = 867862
70 meter
Z = 1084181
55 Z = 298071
72
XDOT = -1214
841823 XDOT = -346
225450
YDOT = -15642
272826 feet/sec YDOT = -4771
770945 meter/sec
ZDOT = 19776
669427 ZDOT = 6026
188428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20363592
35 X = 6206822
95
Y = -8525741
62 feet Y = -2598646
05 meter
Z = 958914
49 Z = 292277
14
XDOT = 4623
745449 XDOT = 1409
317613
YDOT = 13311
262357 feet/sec YDOT = 4057
272766 meter/sec
ZDOT = 19769
444087 ZDOT = 6025
726558
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
56547107
00020000 00000-0 20000-3 0 9101
2 25544 51
6410 170
4072 0005654 207
4631 152
6233 15
72005454 5902
Satellite: ISS
Catalog Number: 25544
Epoch time: 08279
56547107 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 170
4072 deg
Eccentricity:
0005654
Arg of perigee: 207
4631 deg
Mean anomaly: 152
6233 deg
Mean motion: 15
72005454 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 590
Checksum: 265
Coasting Arc #12 (Orbit 604)
---------------------------------------
Vector Time (GMT): 2008/280/12:03:32
440
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1471594
02 A = 6725724
29 meter
Y = 3915908
72 meter E =
0012639
Z = -5276490
07 I = 51
70725
XDOT = -7329
765226 Wp = 108
97041
YDOT = 2298
568347 meter/sec RA = 164
60967 deg
ZDOT = -343
071296 TA = 157
79816
MA = 157
74339
Ha = 193
116 n
mi
Hp = 187
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4828064
36 X = 1453328
93
Y = 12847469
54 feet Y = 3932262
79 meter
Z = -17311319
12 Z = -5269385
33
XDOT = -24047
786174 XDOT = -7353
256818
YDOT = 7541
234735 feet/sec YDOT = 2216
471333 meter/sec
ZDOT = -1125
561995 ZDOT = -378
736878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8210725
51 X = -2502629
13
Y = -11041602
98 feet Y = -3365480
59 meter
Z = -17283415
15 Z = -5267984
94
XDOT = 20309
607335 XDOT = 6190
368316
YDOT = -13149
111043 feet/sec YDOT = -4007
849046 meter/sec
ZDOT = -1263
398124 ZDOT = -385
083748
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 08280
51901754
00020000 00000-0 20000-3 0 9111
2 25544 51
6412 165
5246 0005643 211
7138 148
3685 15
72046604 6052
Satellite: ISS
Catalog Number: 25544
Epoch time: 08280
51901754 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 165
5246 deg
Eccentricity:
0005643
Arg of perigee: 211
7138 deg
Mean anomaly: 148
3685 deg
Mean motion: 15
72046604 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 605
Checksum: 275
Coasting Arc #13 (Orbit 620)
---------------------------------------
Vector Time (GMT): 2008/281/12:03:32
440
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5947758
78 A = 6737451
48 meter
Y = -3005415
26 meter E =
0014869
Z = 927248
15 I = 51
77441
XDOT = 2913
665056 Wp = 147
90237
YDOT = 3918
909620 meter/sec RA = 159
48446 deg
ZDOT = -5956
343492 TA = 21
99383
MA = 21
93009
Ha = 193
091 n
mi
Hp = 187
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19513644
29 X = 5976419
31
Y = -9860286
30 feet Y = -2938743
74 meter
Z = 3042152
74 Z = 956212
35
XDOT = 9559
268557 XDOT = 2898
561808
YDOT = 12857
315025 feet/sec YDOT = 3951
407414 meter/sec
ZDOT = -19541
809358 ZDOT = -5942
225455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15856405
14 X = -4833032
29
Y = 15029605
32 feet Y = 4581023
70 meter
Z = 3153986
79 Z = 961335
17
XDOT = -11851
582896 XDOT = -3612
362467
YDOT = -8393
590962 feet/sec YDOT = -2558
366525 meter/sec
ZDOT = -19486
749348 ZDOT = -5939
561201
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 08281
53612098
00020000 00000-0 20000-3 0 9125
2 25544 51
6412 160
3168 0005764 214
4811 145
5978 15
72010310 6217
Satellite: ISS
Catalog Number: 25544
Epoch time: 08281
53612098 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 160
3168 deg
Eccentricity:
0005764
Arg of perigee: 214
4811 deg
Mean anomaly: 145
5978 deg
Mean motion: 15
72010310 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 621
Checksum: 264
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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