Date:
April 4th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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 1642)
---------------------------------------
Vector Time (GMT): 2008/092/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3957382
56 A = 6712498
33 meter
Y = 1573503
89 meter E =
0004214
Z = 5186798
93 I = 51
87250
XDOT = -4051
009111 Wp = 38
94377
YDOT = -6459
373784 meter/sec RA = 51
24072 deg
ZDOT = -1127
542523 TA = 61
79523
MA = 61
75267
Ha = 185
724 n
mi
Hp = 179
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12983538
58 X = -3999879
93
Y = 5162414
32 feet Y = 1529012
78 meter
Z = 17017056
85 Z = 5167470
83
XDOT = -13290
712308 XDOT = -3973
000955
YDOT = -21192
171206 feet/sec YDOT = -6504
238364 meter/sec
ZDOT = -3699
286494 ZDOT = -1147
032412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12896789
73 X = -3930941
51
Y = 5604287
56 feet Y = 1708186
85 meter
Z = 16943075
14 Z = 5164249
30
XDOT = -13573
964892 XDOT = -4137
344499
YDOT = -19788
110338 feet/sec YDOT = -6031
416031 meter/sec
ZDOT = -3774
732195 ZDOT = -1150
538373
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 08092
52478759
00020000 00000-0 20000-3 0 9005
2 25544 51
6381 51
6004 0001202 331
8903 28
2197 15
76824082 16430
Satellite: ISS
Catalog Number: 25544
Epoch time: 08092
52478759 = yrday
fracday
Element set: 900
Inclination: 51
6381 deg
RA of node: 51
6004 deg
Eccentricity:
0001202
Arg of perigee: 331
8903 deg
Mean anomaly: 28
2197 deg
Mean motion: 15
76824082 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1643
Checksum: 277
Coasting Arc #2 (Orbit 1658)
---------------------------------------
Vector Time (GMT): 2008/093/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3265731
92 A = 6722314
47 meter
Y = 5550582
41 meter E =
0014048
Z = 1902765
23 I = 51
88758
XDOT = -5127
059866 Wp = 62
67237
YDOT = 1068
954170 meter/sec RA = 46
12774 deg
ZDOT = 5656
025852 TA = 318
43577
MA = 318
54249
Ha = 185
471 n
mi
Hp = 179
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10714343
57 X = 3194178
50
Y = 18210572
23 feet Y = 5586701
74 meter
Z = 6242668
07 Z = 1918455
89
XDOT = -16821
062551 XDOT = -5166
107783
YDOT = 3507
067488 feet/sec YDOT = 1011
402484 meter/sec
ZDOT = 18556
515261 ZDOT = 5631
023860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11597097
10 X = 3534795
19
Y = 17639924
68 feet Y = 5376649
04 meter
Z = 6303443
49 Z = 1921289
58
XDOT = -15438
072193 XDOT = -4705
524404
YDOT = 3523
369978 feet/sec YDOT = 1073
923169 meter/sec
ZDOT = 18460
714196 ZDOT = 5626
825687
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 08093
53877605
00020000 00000-0 20000-3 0 9011
2 25544 51
6385 46
3708 0001087 330
3242 29
7861 15
76907813 16592
Satellite: ISS
Catalog Number: 25544
Epoch time: 08093
53877605 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 46
3708 deg
Eccentricity:
0001087
Arg of perigee: 330
3242 deg
Mean anomaly: 29
7861 deg
Mean motion: 15
76907813 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1659
Checksum: 305
Coasting Arc #3 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2008/094/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4988651
37 A = 6715227
88 meter
Y = -343106
92 meter E =
0008851
Z = -4490674
19 I = 51
84279
XDOT = 3296
190112 Wp = 104
50984
YDOT = 6180
653021 meter/sec RA = 40
94481 deg
ZDOT = 3192
516636 TA = 197
30689
MA = 197
33708
Ha = 185
514 n
mi
Hp = 179
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16366966
44 X = 5013932
08
Y = -1125678
87 feet Y = -287179
98 meter
Z = -14733183
05 Z = -4466377
99
XDOT = 10814
272022 XDOT = 3211
323496
YDOT = 20277
733009 feet/sec YDOT = 6217
038649 meter/sec
ZDOT = 10474
135944 ZDOT = 3208
322822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16334902
79 X = 4978878
37
Y = -2247738
95 feet Y = -685110
83 meter
Z = -14640015
26 Z = -4462276
65
XDOT = 11951
958975 XDOT = 3642
957095
YDOT = 18303
792935 feet/sec YDOT = 5578
996086 meter/sec
ZDOT = 10535
418679 ZDOT = 3211
195613
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 08094
48936426
00020000 00000-0 20000-3 0 9024
2 25544 51
6389 41
4677 0001264 335
4058 24
7046 15
76910231 16740
Satellite: ISS
Catalog Number: 25544
Epoch time: 08094
48936426 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 41
4677 deg
Eccentricity:
0001264
Arg of perigee: 335
4058 deg
Mean anomaly: 24
7046 deg
Mean motion: 15
76910231 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1674
Checksum: 296
Coasting Arc #4 (Orbit 1689)
---------------------------------------
Vector Time (GMT): 2008/095/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2348450
61 A = 6718041
29 meter
Y = -5175947
10 meter E =
0005378
Z = -3587564
08 I = 51
83127
XDOT = 6282
029541 Wp = 67
23859
YDOT = 228
448153 meter/sec RA = 35
85010 deg
ZDOT = -4445
079914 TA = 155
52022
MA = 155
49468
Ha = 185
400 n
mi
Hp = 179
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7704890
45 X = -2272970
05
Y = -16981453
73 feet Y = -5201787
11 meter
Z = -11770223
35 Z = -3598789
05
XDOT = 20610
333140 XDOT = 6300
601535
YDOT = 749
501814 feet/sec YDOT = 298
800833 meter/sec
ZDOT = -14583
595517 ZDOT = -4414
516679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9062236
07 X = -2762169
55
Y = -16265999
17 feet Y = -4957876
55 meter
Z = -11813822
99 Z = -3600853
25
XDOT = 19494
961974 XDOT = 5942
064410
YDOT = -362
071970 feet/sec YDOT = -110
359536 meter/sec
ZDOT = -14466
330889 ZDOT = -4409
337655
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 08095
50329350
00020000 00000-0 20000-3 0 9031
2 25544 51
6399 36
2376 0001279 339
5636 20
5478 15
76985200 16901
Satellite: ISS
Catalog Number: 25544
Epoch time: 08095
50329350 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 36
2376 deg
Eccentricity:
0001279
Arg of perigee: 339
5636 deg
Mean anomaly: 20
5478 deg
Mean motion: 15
76985200 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1690
Checksum: 304
Coasting Arc #5 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2008/096/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5911937
39 A = 6719419
93 meter
Y = -655724
15 meter E =
0012660
Z = 3114954
98 I = 51
81226
XDOT = -1959
360782 Wp = 89
46284
YDOT = -5629
375243 meter/sec RA = 30
65429 deg
ZDOT = -4886
659190 TA = 54
36354
MA = 54
24569
Ha = 185
414 n
mi
Hp = 179
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19396120
06 X = -5919297
61
Y = -2151325
96 feet Y = -721875
69 meter
Z = 10219668
56 Z = 3086216
74
XDOT = -6428
349023 XDOT = -1872
527905
YDOT = -18469
078881 feet/sec YDOT = -5650
800862 meter/sec
ZDOT = -16032
346423 ZDOT = -4895
966422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19571907
37 X = -5965517
37
Y = -143094
07 feet Y = -43615
07 meter
Z = 10109365
37 Z = 3081334
56
XDOT = -8209
975929 XDOT = -2502
400663
YDOT = -16293
778807 feet/sec YDOT = -4966
343780 meter/sec
ZDOT = -16068
630811 ZDOT = -4897
718671
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 08096
51719147
00020000 00000-0 20000-3 0 9041
2 25544 51
6406 31
0079 0001288 340
8576 19
2540 15
77032646 17062
Satellite: ISS
Catalog Number: 25544
Epoch time: 08096
51719147 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 31
0079 deg
Eccentricity:
0001288
Arg of perigee: 340
8576 deg
Mean anomaly: 19
2540 deg
Mean motion: 15
77032646 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1706
Checksum: 285
Coasting Arc #6 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2008/097/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 947110
09 A = 6713373
08 meter
Y = 4620864
95 meter E =
0006328
Z = 4773060
26 I = 51
76748
XDOT = -7171
217033 Wp = 113
31736
YDOT = -1186
898133 meter/sec RA = 25
55167 deg
ZDOT = 2566
895941 TA = 311
57358
MA = 311
62781
Ha = 185
192 n
mi
Hp = 179
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3107316
58 X = 872181
48
Y = 15160318
07 feet Y = 4631037
46 meter
Z = 15659646
53 Z = 4777479
06
XDOT = -23527
614938 XDOT = -7169
881660
YDOT = -3894
022747 feet/sec YDOT = -1267
083135 meter/sec
ZDOT = 8421
574610 ZDOT = 2532
061019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4811968
47 X = 1466687
99
Y = 14689780
86 feet Y = 4477445
21 meter
Z = 15677068
85 Z = 4778370
59
XDOT = -22800
518667 XDOT = -6949
598090
YDOT = -1393
969361 feet/sec YDOT = -424
881861 meter/sec
ZDOT = 8287
837029 ZDOT = 2526
132727
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 08097
53105660
00020000 00000-0 20000-3 0 9054
2 25544 51
6411 25
7783 0001198 335
8973 24
2136 15
77106154 17226
Satellite: ISS
Catalog Number: 25544
Epoch time: 08097
53105660 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 25
7783 deg
Eccentricity:
0001198
Arg of perigee: 335
8973 deg
Mean anomaly: 24
2136 deg
Mean motion: 15
77106154 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1722
Checksum: 282
Coasting Arc #7 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2008/098/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6461172
66 A = 6722691
78 meter
Y = 1342137
69 meter E =
0010033
Z = -1257796
87 I = 51
77167
XDOT = 104
614556 Wp = 30
94686
YDOT = 4979
395104 meter/sec RA = 20
36990 deg
ZDOT = 5879
722808 TA = 315
26437
MA = 315
34525
Ha = 185
289 n
mi
Hp = 179
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21198073
05 X = 6451794
71
Y = 4403338
89 feet Y = 1414337
73 meter
Z = -4126630
16 Z = -1226430
80
XDOT = 343
223609 XDOT = 20
363292
YDOT = 16336
598109 feet/sec YDOT = 4980
094128 meter/sec
ZDOT = 19290
429160 ZDOT = 5880
026183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21624038
65 X = 6591006
98
Y = 1458832
16 feet Y = 444652
04 meter
Z = -4006186
73 Z = -1221085
72
XDOT = 2572
751514 XDOT = 784
174661
YDOT = 14574
155687 feet/sec YDOT = 4442
202653 meter/sec
ZDOT = 19292
094998 ZDOT = 5880
230555
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 08098
48152890
00020000 00000-0 20000-3 0 9067
2 25544 51
6410 20
8747 0001315 343
1246 16
9875 15
77107855 17370
Satellite: ISS
Catalog Number: 25544
Epoch time: 08098
48152890 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 20
8747 deg
Eccentricity:
0001315
Arg of perigee: 343
1246 deg
Mean anomaly: 16
9875 deg
Mean motion: 15
77107855 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1737
Checksum: 299
Coasting Arc #8 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2008/099/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 849327
59 A = 6711085
10 meter
Y = -4082303
98 meter E =
0014850
Z = -5271200
31 I = 51
70606
XDOT = 7466
844788 Wp = 83
37948
YDOT = 1847
600473 meter/sec RA = 15
23124 deg
ZDOT = -226
643595 TA = 184
46330
MA = 184
47656
Ha = 185
173 n
mi
Hp = 179
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2786507
83 X = 920520
39
Y = -13393385
76 feet Y = -4072408
29 meter
Z = -17293964
27 Z = -5266901
25
XDOT = 24497
522271 XDOT = 7446
730688
YDOT = 6061
681341 feet/sec YDOT = 1930
986533 meter/sec
ZDOT = -743
581349 ZDOT = -190
417932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 790140
32 X = 240834
77
Y = -13677687
95 feet Y = -4168959
29 meter
Z = -17277880
05 Z = -5266297
84
XDOT = 24144
776486 XDOT = 7359
327873
YDOT = 2163
070580 feet/sec YDOT = 659
303913 meter/sec
ZDOT = -604
449926 ZDOT = -184
236338
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 08099
49533410
00020000 00000-0 20000-3 0 9071
2 25544 51
6417 15
6440 0001264 346
3708 13
7423 15
77172773 17533
Satellite: ISS
Catalog Number: 25544
Epoch time: 08099
49533410 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 15
6440 deg
Eccentricity:
0001264
Arg of perigee: 346
3708 deg
Mean anomaly: 13
7423 deg
Mean motion: 15
77172773 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1753
Checksum: 286
Coasting Arc #9 (Orbit 1768)
---------------------------------------
Vector Time (GMT): 2008/100/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6398627
02 A = 6722702
86 meter
Y = -1848399
48 meter E =
0008987
Z = -886302
82 I = 51
71740
XDOT = 2093
355203 Wp = 137
80840
YDOT = -4407
429856 meter/sec RA = 10
08379 deg
ZDOT = -5962
386528 TA = 51
86586
MA = 51
78489
Ha = 185
106 n
mi
Hp = 178
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20992870
82 X = -6373176
82
Y = -6064302
77 feet Y = -1919810
27 meter
Z = -2907817
65 Z = -917325
98
XDOT = 6867
963266 XDOT = 2171
448762
YDOT = -14460
071705 feet/sec YDOT = -4383
583986 meter/sec
ZDOT = -19561
635590 ZDOT = -5952
027281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21703564
08 X = -6615246
33
Y = -2392572
72 feet Y = -729256
17 meter
Z = -3026994
97 Z = -922628
07
XDOT = 4232
208344 XDOT = 1289
977103
YDOT = -13856
908291 feet/sec YDOT = -4223
585647 meter/sec
ZDOT = -19522
332026 ZDOT = -5950
406802
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 08100
50910791
00020000 00000-0 20000-3 0 9088
2 25544 51
6421 10
4133 0001210 346
3305 13
7827 15
77203966 17698
Satellite: ISS
Catalog Number: 25544
Epoch time: 08100
50910791 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 10
4133 deg
Eccentricity:
0001210
Arg of perigee: 346
3305 deg
Mean anomaly: 13
7827 deg
Mean motion: 15
77203966 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1769
Checksum: 258
Coasting Arc #10 (Orbit 1784)
---------------------------------------
Vector Time (GMT): 2008/101/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2786628
31 A = 6712435
10 meter
Y = 3647442
06 meter E =
0007143
Z = 4894883
39 I = 51
65384
XDOT = -6995
305762 Wp = 47
07548
YDOT = -2359
990789 meter/sec RA = 4
90039 deg
ZDOT = -2217
020064 TA = 64
47506
MA = 64
40121
Ha = 185
088 n
mi
Hp = 178
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9142481
32 X = -2850986
10
Y = 11966673
41 feet Y = 3615920
36 meter
Z = 16059328
69 Z = 4881189
65
XDOT = -22950
478222 XDOT = -6957
626103
YDOT = -7742
751931 feet/sec YDOT = -2438
005531 meter/sec
ZDOT = -7273
687874 ZDOT = -2250
912087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6823021
03 X = -2079656
81
Y = 13487239
96 feet Y = 4110910
74 meter
Z = 16007155
20 Z = 4878980
91
XDOT = -22971
499272 XDOT = -7001
712978
YDOT = -2807
134090 feet/sec YDOT = -855
614471 meter/sec
ZDOT = -7403
922794 ZDOT = -2256
715668
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 08101
52284927
00020000 00000-0 20000-3 0 9097
2 25544 51
6416 5
1826 0001337 347
9129 12
2004 15
77286378 17850
Satellite: ISS
Catalog Number: 25544
Epoch time: 08101
52284927 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 5
1826 deg
Eccentricity:
0001337
Arg of perigee: 347
9129 deg
Mean anomaly: 12
2004 deg
Mean motion: 15
77286378 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1785
Checksum: 289
Coasting Arc #11 (Orbit 1800)
---------------------------------------
Vector Time (GMT): 2008/102/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5606451
95 A = 6719023
51 meter
Y = 2277198
24 meter E =
0013432
Z = 2904919
52 I = 51
64763
XDOT = -4245
375320 Wp = 76
45510
YDOT = 4003
235173 meter/sec RA = 359
78233 deg
ZDOT = 5039
040558 TA = 317
03912
MA = 317
14393
Ha = 184
961 n
mi
Hp = 178
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18393871
21 X = 5566459
67
Y = 7471122
83 feet Y = 2339669
07 meter
Z = 9530575
87 Z = 2932058
67
XDOT = -13928
396719 XDOT = -4314
303391
YDOT = 13133
973666 feet/sec YDOT = 3955
375369 meter/sec
ZDOT = 16532
285295 ZDOT = 5018
249211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19480026
18 X = 5937511
98
Y = 3561076
39 feet Y = 1085416
08 meter
Z = 9634903
51 Z = 2936718
59
XDOT = -10778
767584 XDOT = -3285
368360
YDOT = 14304
386510 feet/sec YDOT = 4359
977008 meter/sec
ZDOT = 16452
915779 ZDOT = 5014
848730
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 08102
53656081
00020000 00000-0 20000-3 0 9105
2 25544 51
6420 359
9508 0001318 352
6244 7
4901 15
77306937 18017
Satellite: ISS
Catalog Number: 25544
Epoch time: 08102
53656081 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 359
9508 deg
Eccentricity:
0001318
Arg of perigee: 352
6244 deg
Mean anomaly: 7
4901 deg
Mean motion: 15
77306937 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1801
Checksum: 274
Coasting Arc #12 (Orbit 1815)
---------------------------------------
Vector Time (GMT): 2008/103/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4517571
85 A = 6716798
10 meter
Y = -3353009
08 meter E =
0005364
Z = -3673659
41 I = 51
61175
XDOT = 5669
644448 Wp = 86
42328
YDOT = 2904
492046 meter/sec RA = 354
57016 deg
ZDOT = 4326
830625 TA = 229
34688
MA = 229
39352
Ha = 184
944 n
mi
Hp = 178
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14821429
94 X = 4572575
89
Y = -11000685
95 feet Y = -3302183
37 meter
Z = -12052688
36 Z = -3651579
59
XDOT = 18601
195697 XDOT = 5615
725679
YDOT = 9529
173379 feet/sec YDOT = 2967
591661 meter/sec
ZDOT = 14195
638535 ZDOT = 4354
242794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12084671
11 X = 3683407
76
Y = -14024173
19 feet Y = -4274567
99 meter
Z = -11968310
83 Z = -3647941
14
XDOT = 19147
710649 XDOT = 5836
222206
YDOT = 4311
182025 feet/sec YDOT = 1314
048281 meter/sec
ZDOT = 14301
078658 ZDOT = 4358
968775
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 08103
48688558
00020000 00000-0 20000-3 0 9115
2 25544 51
6425 355
0462 0001343 351
1093 9
0048 15
77368117 18166
Satellite: ISS
Catalog Number: 25544
Epoch time: 08103
48688558 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 355
0462 deg
Eccentricity:
0001343
Arg of perigee: 351
1093 deg
Mean anomaly: 9
0048 deg
Mean motion: 15
77368117 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1816
Checksum: 283
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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