Date:
May 20th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 2399)
---------------------------------------
Vector Time (GMT): 2008/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5172740
88 A = 6722772
56 meter
Y = 3547472
72 meter E =
0000405
Z = -2418907
57 I = 51
74261
XDOT = -4599
696491 Wp = 291
29757
YDOT = -3042
073142 meter/sec RA = 163
26175 deg
ZDOT = 5374
318090 TA = 41
42950
MA = 41
42643
Ha = 185
714 n
mi
Hp = 181
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16970934
64 X = -5200273
97
Y = 11638690
02 feet Y = 3489474
53 meter
Z = -7936048
44 Z = -2444103
68
XDOT = -15090
867754 XDOT = -4591
445677
YDOT = -9980
554928 feet/sec YDOT = -3093
464131 meter/sec
ZDOT = 17632
277197 ZDOT = 5351
991967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 463555
47 X = 141291
71
Y = 20535734
28 feet Y = 6259291
81 meter
Z = -8032516
83 Z = -2448311
13
XDOT = -15174
480607 XDOT = -4625
181689
YDOT = 7206
412090 feet/sec YDOT = 2196
514405 meter/sec
ZDOT = 17546
158192 ZDOT = 5348
069017
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 08140
50488158
00020000 00000-0 20000-3 0 9001
2 25544 51
6380 164
2528 0005628 231
6193 128
4466 15
76387894 24004
Satellite: ISS
Catalog Number: 25544
Epoch time: 08140
50488158 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 164
2528 deg
Eccentricity:
0005628
Arg of perigee: 231
6193 deg
Mean anomaly: 128
4466 deg
Mean motion: 15
76387894 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2400
Checksum: 297
Coasting Arc #2 (Orbit 2415)
---------------------------------------
Vector Time (GMT): 2008/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3446706
34 A = 6714630
30 meter
Y = 2869495
48 meter E =
0007923
Z = -5004062
91 I = 51
74178
XDOT = -6213
377095 Wp = 88
97136
YDOT = 4121
344571 meter/sec RA = 158
15250 deg
ZDOT = -1918
804252 TA = 162
53660
MA = 162
50933
Ha = 185
583 n
mi
Hp = 181
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11308091
66 X = 3438672
29
Y = 9414355
24 feet Y = 2907994
32 meter
Z = -16417529
22 Z = -4987337
60
XDOT = -20385
095456 XDOT = -6249
679450
YDOT = 13521
471689 feet/sec YDOT = 4051
660337 meter/sec
ZDOT = -6295
289541 ZDOT = -1949
076972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14044661
10 X = 4280812
70
Y = -4622425
94 feet Y = -1408915
43 meter
Z = -16352949
59 Z = -4984379
03
XDOT = 246
186690 XDOT = 75
037703
YDOT = 23400
608235 feet/sec YDOT = 7132
505390 meter/sec
ZDOT = -6411
227483 ZDOT = -1954
142137
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 08141
51919112
00020000 00000-0 20000-3 0 9013
2 25544 51
6374 159
0251 0005656 236
9262 123
1360 15
76364477 24162
Satellite: ISS
Catalog Number: 25544
Epoch time: 08141
51919112 = yrday
fracday
Element set: 901
Inclination: 51
6374 deg
RA of node: 159
0251 deg
Eccentricity:
0005656
Arg of perigee: 236
9262 deg
Mean anomaly: 123
1360 deg
Mean motion: 15
76364477 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2416
Checksum: 277
Coasting Arc #3 (Orbit 2431)
---------------------------------------
Vector Time (GMT): 2008/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5580612
54 A = 6725024
41 meter
Y = -3631381
11 meter E =
0012332
Z = 889763
81 I = 51
80269
XDOT = 3294
233220 Wp = 149
31840
YDOT = 3593
375225 meter/sec RA = 152
98328 deg
ZDOT = -5970
227294 TA = 20
97824
MA = 20
92769
Ha = 185
335 n
mi
Hp = 181
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18309096
24 X = 5616482
07
Y = -11913980
02 feet Y = -3568775
09 meter
Z = 2919172
61 Z = 916961
39
XDOT = 10807
851773 XDOT = 3282
809415
YDOT = 11789
288797 feet/sec YDOT = 3630
150300 meter/sec
ZDOT = -19587
359887 ZDOT = -5954
250843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -696030
87 X = -212150
21
Y = -21818852
96 feet Y = -6650386
38 meter
Z = 3023357
50 Z = 921519
37
XDOT = 14152
226525 XDOT = 4313
598645
YDOT = -3168
313250 feet/sec YDOT = -965
701879 meter/sec
ZDOT = -19525
581013 ZDOT = -5951
397093
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 08142
53348893
00020000 00000-0 20000-3 0 9029
2 25544 51
6362 153
7971 0005511 240
9279 119
1334 15
76388414 24323
Satellite: ISS
Catalog Number: 25544
Epoch time: 08142
53348893 = yrday
fracday
Element set: 902
Inclination: 51
6362 deg
RA of node: 153
7971 deg
Eccentricity:
0005511
Arg of perigee: 240
9279 deg
Mean anomaly: 119
1334 deg
Mean motion: 15
76388414 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2432
Checksum: 294
Coasting Arc #4 (Orbit 2447)
---------------------------------------
Vector Time (GMT): 2008/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2301521
61 A = 6713257
31 meter
Y = -3458884
86 meter E =
0003707
Z = 5275565
83 I = 51
78821
XDOT = 6481
193808 Wp = 226
63401
YDOT = -4162
645682 meter/sec RA = 147
84994 deg
ZDOT = 95
828403 TA = 222
44450
MA = 222
47317
Ha = 185
189 n
mi
Hp = 181
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7550923
93 X = -2288300
79
Y = -11348047
43 feet Y = -3484548
75 meter
Z = 17308286
84 Z = 5264416
45
XDOT = 21263
759213 XDOT = 6526
793945
YDOT = -13656
974022 feet/sec YDOT = -4089
914319 meter/sec
ZDOT = 314
397649 ZDOT = 127
424473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13656530
00 X = -4162510
34
Y = 887576
96 feet Y = 270533
46 meter
Z = 17265075
19 Z = 5262394
92
XDOT = -1015
417243 XDOT = -309
499176
YDOT = -24250
989822 feet/sec YDOT = -7391
701698 meter/sec
ZDOT = 435
456503 ZDOT = 132
727142
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 08143
54777419
00020000 00000-0 20000-3 0 9032
2 25544 51
6357 148
5688 0005554 245
8770 114
1813 15
76406053 24485
Satellite: ISS
Catalog Number: 25544
Epoch time: 08143
54777419 = yrday
fracday
Element set: 903
Inclination: 51
6357 deg
RA of node: 148
5688 deg
Eccentricity:
0005554
Arg of perigee: 245
8770 deg
Mean anomaly: 114
1813 deg
Mean motion: 15
76406053 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2448
Checksum: 309
Coasting Arc #5 (Orbit 2463)
---------------------------------------
Vector Time (GMT): 2008/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5644174
59 A = 6724942
16 meter
Y = 3573369
50 meter E =
0008142
Z = 733314
37 I = 51
85270
XDOT = -2001
388201 Wp = 41
45363
YDOT = -4398
950880 meter/sec RA = 142
71561 deg
ZDOT = 5999
686432 TA = 326
52201
MA = 326
57344
Ha = 184
880 n
mi
Hp = 182
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18517633
17 X = -5687275
41
Y = 11723653
23 feet Y = 3510012
01 meter
Z = 2405887
06 Z = 705790
67
XDOT = -6566
234255 XDOT = -1981
195295
YDOT = -14432
253542 feet/sec YDOT = -4421
219642 meter/sec
ZDOT = 19684
010604 ZDOT = 5990
011932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1163333
15 X = 354583
94
Y = 21897256
54 feet Y = 6674283
79 meter
Z = 2300410
29 Z = 701165
06
XDOT = -14257
728114 XDOT = -4345
755529
YDOT = -1317
897698 feet/sec YDOT = -401
695218 meter/sec
ZDOT = 19646
373339 ZDOT = 5988
214594
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 08144
56204570
00020000 00000-0 20000-3 0 9049
2 25544 51
6361 143
3417 0005661 248
8779 111
1780 15
76472979 24642
Satellite: ISS
Catalog Number: 25544
Epoch time: 08144
56204570 = yrday
fracday
Element set: 904
Inclination: 51
6361 deg
RA of node: 143
3417 deg
Eccentricity:
0005661
Arg of perigee: 248
8779 deg
Mean anomaly: 111
1780 deg
Mean motion: 15
76472979 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2464
Checksum: 303
Coasting Arc #6 (Orbit 2478)
---------------------------------------
Vector Time (GMT): 2008/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1228764
09 A = 6714208
74 meter
Y = 4256887
80 meter E =
0008964
Z = -5052551
38 I = 51
83825
XDOT = -6371
055856 Wp = 120
46144
YDOT = 3942
173109 meter/sec RA = 137
55413 deg
ZDOT = 1769
812785 TA = 166
55162
MA = 166
52772
Ha = 184
702 n
mi
Hp = 182
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4031378
23 X = 1205616
05
Y = 13966167
31 feet Y = 4270499
91 meter
Z = -16576612
14 Z = -5046637
57
XDOT = -20902
414226 XDOT = -6423
261807
YDOT = 12933
638810 feet/sec YDOT = 3870
636140 meter/sec
ZDOT = 5806
472391 ZDOT = 1738
735881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14253145
36 X = 4344358
70
Y = 2986820
84 feet Y = 910382
99 meter
Z = -16553448
54 Z = -5045491
12
XDOT = 1683
583655 XDOT = 513
156298
YDOT = 23525
060509 feet/sec YDOT = 7170
438443 meter/sec
ZDOT = 5687
353790 ZDOT = 1733
505435
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 08145
51291792
00020000 00000-0 20000-3 0 9058
2 25544 51
6357 138
4401 0005590 254
9661 105
0885 15
76419532 24794
Satellite: ISS
Catalog Number: 25544
Epoch time: 08145
51291792 = yrday
fracday
Element set: 905
Inclination: 51
6357 deg
RA of node: 138
4401 deg
Eccentricity:
0005590
Arg of perigee: 254
9661 deg
Mean anomaly: 105
0885 deg
Mean motion: 15
76419532 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2479
Checksum: 304
Coasting Arc #7 (Orbit 2494)
---------------------------------------
Vector Time (GMT): 2008/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5418670
37 A = 6722893
84 meter
Y = -3222886
04 meter E =
0005394
Z = -2323911
31 I = 51
88846
XDOT = 866
331595 Wp = 194
51599
YDOT = 5380
983829 meter/sec RA = 132
45043 deg
ZDOT = -5444
925759 TA = 11
56011
MA = 11
54773
Ha = 184
586 n
mi
Hp = 182
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17777789
93 X = 5465595
62
Y = -10573773
10 feet Y = -3162028
66 meter
Z = -7624380
95 Z = -2297473
84
XDOT = 2842
295260 XDOT = 832
546710
YDOT = 17654
146421 feet/sec YDOT = 5390
483526 meter/sec
ZDOT = -17863
929656 ZDOT = -5440
798402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1219913
72 X = -371829
70
Y = -20685783
70 feet Y = -6305026
87 meter
Z = -7523020
69 Z = -2293016
71
XDOT = 15528
837683 XDOT = 4733
189726
YDOT = 5572
100172 feet/sec YDOT = 1698
376133 meter/sec
ZDOT = -17847
524413 ZDOT = -5439
925441
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 08146
52716796
00020000 00000-0 20000-3 0 9067
2 25544 51
6356 133
2117 0005506 259
3150 100
7395 15
76459468 24957
Satellite: ISS
Catalog Number: 25544
Epoch time: 08146
52716796 = yrday
fracday
Element set: 906
Inclination: 51
6356 deg
RA of node: 133
2117 deg
Eccentricity:
0005506
Arg of perigee: 259
3150 deg
Mean anomaly: 100
7395 deg
Mean motion: 15
76459468 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2495
Checksum: 306
Coasting Arc #8 (Orbit 2510)
---------------------------------------
Vector Time (GMT): 2008/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -352656
52 A = 6716978
69 meter
Y = -5131176
41 meter E =
0004349
Z = 4318757
76 I = 51
88752
XDOT = 5993
475380 Wp = 54
19256
YDOT = -3354
249096 meter/sec RA = 127
26884 deg
ZDOT = -3490
895531 TA = 70
99197
MA = 70
94485
Ha = 184
324 n
mi
Hp = 182
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1157009
57 X = -316232
46
Y = -16834568
28 feet Y = -5134916
91 meter
Z = 14169152
75 Z = 4317132
37
XDOT = 19663
633136 XDOT = 6047
495832
YDOT = -11004
754252 feet/sec YDOT = -3286
924139 meter/sec
ZDOT = -11453
069328 ZDOT = -3461
648394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15637892
77 X = -4766429
72
Y = -6355243
25 feet Y = -1937078
14 meter
Z = 14162395
37 Z = 4316698
11
XDOT = -1579
444206 XDOT = -481
414594
YDOT = -21422
341104 feet/sec YDOT = -6529
529568 meter/sec
ZDOT = -11340
905075 ZDOT = -3456
707867
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 08147
54140475
00020000 00000-0 20000-3 0 9076
2 25544 51
6354 127
9837 0005665 264
3884 95
6634 15
76487582 25115
Satellite: ISS
Catalog Number: 25544
Epoch time: 08147
54140475 = yrday
fracday
Element set: 907
Inclination: 51
6354 deg
RA of node: 127
9837 deg
Eccentricity:
0005665
Arg of perigee: 264
3884 deg
Mean anomaly: 95
6634 deg
Mean motion: 15
76487582 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2511
Checksum: 323
Coasting Arc #9 (Orbit 2526)
---------------------------------------
Vector Time (GMT): 2008/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5009726
61 A = 6719116
25 meter
Y = 2527240
78 meter E =
0006249
Z = 3692283
54 I = 51
91212
XDOT = -9
665253 Wp = 103
09214
YDOT = -6367
541730 meter/sec RA = 122
18368 deg
ZDOT = 4337
759477 TA = 301
20774
MA = 301
26897
Ha = 184
220 n
mi
Hp = 181
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16436110
93 X = -5055550
78
Y = 8291472
36 feet Y = 2470962
52 meter
Z = 12113791
14 Z = 3667835
19
XDOT = -31
710146 XDOT = 40
466211
YDOT = -20890
884941 feet/sec YDOT = -6367
369992 meter/sec
ZDOT = 14231
494347 ZDOT = 4337
833590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 431159
44 X = 131417
40
Y = 18465427
08 feet Y = 5628262
17 meter
Z = 12019995
70 Z = 3663694
69
XDOT = -17583
151888 XDOT = -5359
344696
YDOT = -8869
273299 feet/sec YDOT = -2703
354502 meter/sec
ZDOT = 14231
153814 ZDOT = 4337
655683
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 08148
55562834
00020000 00000-0 20000-3 0 9086
2 25544 51
6358 122
7559 0005755 267
2490 92
8016 15
76537215 25277
Satellite: ISS
Catalog Number: 25544
Epoch time: 08148
55562834 = yrday
fracday
Element set: 908
Inclination: 51
6358 deg
RA of node: 122
7559 deg
Eccentricity:
0005755
Arg of perigee: 267
2490 deg
Mean anomaly: 92
8016 deg
Mean motion: 15
76537215 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2527
Checksum: 315
Coasting Arc #10 (Orbit 2541)
---------------------------------------
Vector Time (GMT): 2008/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -261954
20 A = 6720752
07 meter
Y = 5934279
98 meter E =
0001658
Z = -3141548
48 I = 51
93180
XDOT = -5481
240770 Wp = 317
13193
YDOT = 2341
060652 meter/sec RA = 116
99757 deg
ZDOT = 4878
925608 TA = 6
43806
MA = 6
43593
Ha = 184
248 n
mi
Hp = 181
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -859429
79 X = -313031
62
Y = 19469422
52 feet Y = 5931065
38 meter
Z = -10306917
58 Z = -3142944
54
XDOT = -17983
073394 XDOT = -5530
712578
YDOT = 7680
645185 feet/sec YDOT = 2279
489190 meter/sec
ZDOT = 16006
973779 ZDOT = 4852
177641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17407259
63 X = 5305732
73
Y = 8757029
93 feet Y = 2669142
72 meter
Z = -10311708
00 Z = -3143008
60
XDOT = 183
854820 XDOT = 56
038949
YDOT = 18363
591591 feet/sec YDOT = 5597
222717 meter/sec
ZDOT = 15904
307394 ZDOT = 4847
632894
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 08149
50645368
00020000 00000-0 20000-3 0 9097
2 25544 51
6356 117
8541 0005591 272
8227 87
2298 15
76502821 25421
Satellite: ISS
Catalog Number: 25544
Epoch time: 08149
50645368 = yrday
fracday
Element set: 909
Inclination: 51
6356 deg
RA of node: 117
8541 deg
Eccentricity:
0005591
Arg of perigee: 272
8227 deg
Mean anomaly: 87
2298 deg
Mean motion: 15
76502821 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2542
Checksum: 310
Coasting Arc #11 (Orbit 2557)
---------------------------------------
Vector Time (GMT): 2008/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4564549
89 A = 6715403
40 meter
Y = -1462602
76 meter E =
0006482
Z = -4709456
26 I = 51
92665
XDOT = -552
435184 Wp = 48
57678
YDOT = 7166
732523 meter/sec RA = 111
90886 deg
ZDOT = -2759
425560 TA = 194
33224
MA = 194
35063
Ha = 184
232 n
mi
Hp = 182
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14975557
38 X = 4603443
62
Y = -4798565
48 feet Y = -1411341
44 meter
Z = -15450971
99 Z = -4687187
11
XDOT = -1812
451391 XDOT = -619
128727
YDOT = 23512
901978 feet/sec YDOT = 7160
182231 meter/sec
ZDOT = -9053
233464 ZDOT = -2762
270650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1568719
54 X = 478145
72
Y = -15731126
05 feet Y = -4794847
22 meter
Z = -15365444
26 Z = -4683387
41
XDOT = 19739
321590 XDOT = 6016
545221
YDOT = 10826
900262 feet/sec YDOT = 3300
039200 meter/sec
ZDOT = -9063
484138 ZDOT = -2762
549965
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 08150
52065342
00020000 00000-0 20000-3 0 9101
2 25544 51
6361 112
6253 0005652 276
7710 83
2811 15
76538327 25582
Satellite: ISS
Catalog Number: 25544
Epoch time: 08150
52065342 = yrday
fracday
Element set: 910
Inclination: 51
6361 deg
RA of node: 112
6253 deg
Eccentricity:
0005652
Arg of perigee: 276
7710 deg
Mean anomaly: 83
2811 deg
Mean motion: 15
76538327 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2558
Checksum: 275
Coasting Arc #12 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2008/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 641683
61 A = 6723777
25 meter
Y = -6492822
25 meter E =
0008749
Z = 1605022
61 I = 51
96512
XDOT = 5005
485809 Wp = 127
07326
YDOT = -938
633523 meter/sec RA = 106
73931 deg
ZDOT = -5781
964000 TA = 35
27165
MA = 35
21379
Ha = 184
321 n
mi
Hp = 181
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2105261
19 X = 706442
65
Y = -21301910
28 feet Y = -6485284
65 meter
Z = 5265822
22 Z = 1608296
62
XDOT = 16422
197536 XDOT = 5043
697900
YDOT = -3079
506309 feet/sec YDOT = -882
445087 meter/sec
ZDOT = -18969
698162 ZDOT = -5757
554249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18907418
46 X = -5762981
15
Y = -10029295
80 feet Y = -3056929
36 meter
Z = 5277797
19 Z = 1608672
58
XDOT = 2714
521987 XDOT = 827
386302
YDOT = -15078
725099 feet/sec YDOT = -4595
995410 meter/sec
ZDOT = -18875
880120 ZDOT = -5753
368260
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 08151
53484002
00020000 00000-0 20000-3 0 9112
2 25544 51
6363 107
3969 0005712 281
2940 78
7583 15
76559814 25749
Satellite: ISS
Catalog Number: 25544
Epoch time: 08151
53484002 = yrday
fracday
Element set: 911
Inclination: 51
6363 deg
RA of node: 107
3969 deg
Eccentricity:
0005712
Arg of perigee: 281
2940 deg
Mean anomaly: 78
7583 deg
Mean motion: 15
76559814 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2574
Checksum: 303
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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