Date:
April 14th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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
112/05:52:08
641 -2
1 3
1 3
1
N/A 2
3 0
1 186
0
000/00:04:57
282 -0
3 0
2 177
8
Coasting Arc #1 (Orbit 1786)
---------------------------------------
Vector Time (GMT): 2008/101/14:42:39
881
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6055196
25 A = 6720104
14 meter
Y = 1515633
71 meter E =
0013056
Z = 2475156
48 I = 51
67653
XDOT = -3308
953349 Wp = 98
86442
YDOT = -4471
936741 meter/sec RA = 4
21326 deg
ZDOT = -5334
831986 TA = 53
11081
MA = 52
99123
Ha = 184
915 n
mi
Hp = 178
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19866129
44 X = -6083718
21
Y = 4972551
54 feet Y = 1447761
47 meter
Z = 8120592
12 Z = 2445670
91
XDOT = -10856
146158 XDOT = -3232
785697
YDOT = -14671
708468 feet/sec YDOT = -4508
513264 meter/sec
ZDOT = -17502
729612 ZDOT = -5350
722155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5952743
80 X = -1814396
31
Y = 19641181
31 feet Y = 5986632
06 meter
Z = 8007635
23 Z = 2440727
22
XDOT = -16680
421755 XDOT = -5084
192551
YDOT = 2135
004533 feet/sec YDOT = 650
749382 meter/sec
ZDOT = -17564
116535 ZDOT = -5353
542720
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
64953554
00020000 00000-0 20000-3 0 9000
2 25544 51
6418 4
5357 0001648 340
9658 19
1445 15
77336162 17873
Satellite: ISS
Catalog Number: 25544
Epoch time: 08101
64953554 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 4
5357 deg
Eccentricity:
0001648
Arg of perigee: 340
9658 deg
Mean anomaly: 19
1445 deg
Mean motion: 15
77336162 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1787
Checksum: 295
Coasting Arc #2 (Orbit 1802)
---------------------------------------
Vector Time (GMT): 2008/102/14:42:39
881
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1898639
94 A = 6711440
65 meter
Y = 3977342
79 meter E =
0003802
Z = 5058843
81 I = 51
61745
XDOT = -7393
686627 Wp = 110
86608
YDOT = 1426
043453 meter/sec RA = 359
08730 deg
ZDOT = 1651
430098 TA = 323
26106
MA = 323
28712
Ha = 184
835 n
mi
Hp = 178
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6229133
66 X = 1829448
58
Y = 13049024
91 feet Y = 3998187
41 meter
Z = 16597256
58 Z = 5067899
50
XDOT = -24257
502057 XDOT = -7417
105711
YDOT = 4678
620251 feet/sec YDOT = 1343
232020 meter/sec
ZDOT = 5418
077748 ZDOT = 1615
454688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14370319
66 X = 4380073
43
Y = 1185723
49 feet Y = 361408
52 meter
Z = 16632379
75 Z = 5069549
35
XDOT = -7963
495777 XDOT = -2427
273513
YDOT = 22339
895111 feet/sec YDOT = 6809
200030 meter/sec
ZDOT = 5280
211194 ZDOT = 1609
408372
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
66321510
00020000 00000-0 20000-3 0 9015
2 25544 51
6410 359
3033 0001596 342
2905 17
8204 15
77343421 18032
Satellite: ISS
Catalog Number: 25544
Epoch time: 08102
66321510 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 359
3033 deg
Eccentricity:
0001596
Arg of perigee: 342
2905 deg
Mean anomaly: 17
8204 deg
Mean motion: 15
77343421 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1803
Checksum: 249
Coasting Arc #3 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2008/103/14:42:39
881
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6638427
32 A = 6722456
81 meter
Y = -964980
28 meter E =
0012527
Z = -321933
25 I = 51
62498
XDOT = 969
544403 Wp = 35
59636
YDOT = 4699
933716 meter/sec RA = 353
90720 deg
ZDOT = 6031
581315 TA = 320
89808
MA = 320
98855
Ha = 184
768 n
mi
Hp = 178
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21779617
21 X = 6650288
39
Y = -3165945
81 feet Y = -890679
27 meter
Z = -1056211
44 Z = -289655
08
XDOT = 3180
919957 XDOT = 887
616712
YDOT = 15419
730039 feet/sec YDOT = 4710
317491 meter/sec
ZDOT = 19788
652607 ZDOT = 6036
092457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7760723
99 X = 2365468
67
Y = -20600780
74 feet Y = -6279117
97 meter
Z = -932479
05 Z = -284219
62
XDOT = 13479
196842 XDOT = 4108
459197
YDOT = 4202
708279 feet/sec YDOT = 1280
985484 meter/sec
ZDOT = 19806
414214 ZDOT = 6036
995052
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
61350884
00020000 00000-0 20000-3 0 9028
2 25544 51
6400 354
3977 0001665 339
5262 20
5836 15
77408658 18187
Satellite: ISS
Catalog Number: 25544
Epoch time: 08103
61350884 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 354
3977 deg
Eccentricity:
0001665
Arg of perigee: 339
5262 deg
Mean anomaly: 20
5836 deg
Mean motion: 15
77408658 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1818
Checksum: 297
Coasting Arc #4 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2008/104/14:42:39
881
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 245985
90 A = 6710557
30 meter
Y = -4254578
10 meter E =
0013945
Z = -5195590
00 I = 51
55537
XDOT = 7600
557548 Wp = 91
38875
YDOT = -734
303517 meter/sec RA = 348
73553 deg
ZDOT = 963
042807 TA = 187
79358
MA = 187
81527
Ha = 184
677 n
mi
Hp = 178
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 807040
36 X = 318782
07
Y = -13958589
57 feet Y = -4251420
31 meter
Z = -17045898
95 Z = -5194218
20
XDOT = 24936
212428 XDOT = 7603
525493
YDOT = -2409
132272 feet/sec YDOT = -649
293146 meter/sec
ZDOT = 3159
589262 ZDOT = 999
973319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11909913
02 X = -3630141
49
Y = -7335716
60 feet Y = -2235926
42 meter
Z = -17041051
66 Z = -5194112
55
XDOT = 9006
033744 XDOT = 2745
039085
YDOT = -22276
142566 feet/sec YDOT = -6789
768254 meter/sec
ZDOT = 3301
193622 ZDOT = 1006
203816
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 08104
62712593
00020000 00000-0 20000-3 0 9030
2 25544 51
6390 349
1645 0001598 342
4300 17
6809 15
77472215 18345
Satellite: ISS
Catalog Number: 25544
Epoch time: 08104
62712593 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 349
1645 deg
Eccentricity:
0001598
Arg of perigee: 342
4300 deg
Mean anomaly: 17
6809 deg
Mean motion: 15
77472215 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1834
Checksum: 287
Coasting Arc #5 (Orbit 1849)
---------------------------------------
Vector Time (GMT): 2008/105/14:42:39
881
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6416273
25 A = 6720439
40 meter
Y = 251733
65 meter E =
0005234
Z = -1978817
05 I = 51
56068
XDOT = 1521
492884 Wp = 132
68813
YDOT = -5074
516826 meter/sec RA = 343
59526 deg
ZDOT = -5591
771799 TA = 69
39749
MA = 69
34136
Ha = 184
613 n
mi
Hp = 178
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21050765
25 X = -6408998
62
Y = 825897
80 feet Y = 180023
85 meter
Z = -6492181
92 Z = -2009969
47
XDOT = 4991
774554 XDOT = 1605
287513
YDOT = -16648
677251 feet/sec YDOT = -5057
034221 meter/sec
ZDOT = -18345
708002 ZDOT = -5584
176784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8783989
19 X = -2677359
91
Y = 19107397
74 feet Y = 5823934
83 meter
Z = -6611666
68 Z = -2015236
01
XDOT = -11139
938641 XDOT = -3395
453298
YDOT = -11445
125877 feet/sec YDOT = -3488
474367 meter/sec
ZDOT = -18317
070571 ZDOT = -5583
043110
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 08105
64071156
00020000 00000-0 20000-3 0 9047
2 25544 51
6389 343
9329 0001643 343
2090 16
9020 15
77507329 18500
Satellite: ISS
Catalog Number: 25544
Epoch time: 08105
64071156 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 343
9329 deg
Eccentricity:
0001643
Arg of perigee: 343
2090 deg
Mean anomaly: 16
9020 deg
Mean motion: 15
77507329 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1850
Checksum: 279
Coasting Arc #6 (Orbit 1865)
---------------------------------------
Vector Time (GMT): 2008/106/14:42:39
881
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2325849
83 A = 6714024
35 meter
Y = 4598547
97 meter E =
0009929
Z = 4299006
80 I = 51
51155
XDOT = -6882
969357 Wp = 61
88806
YDOT = -233
967797 meter/sec RA = 338
38144 deg
ZDOT = -3462
896883 TA = 63
18690
MA = 63
08538
Ha = 184
576 n
mi
Hp = 178
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7630740
93 X = -2397982
39
Y = 15087099
65 feet Y = 4572135
85 meter
Z = 14104353
03 Z = 4287532
46
XDOT = -22581
920463 XDOT = -6863
019456
YDOT = -767
610881 feet/sec YDOT = -310
825690 meter/sec
ZDOT = -11361
210245 ZDOT = -3496
285780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10190839
62 X = 3106167
92
Y = 13535970
82 feet Y = 4125763
90 meter
Z = 14060790
85 Z = 4285729
05
XDOT = -9557
742854 XDOT = -2913
200022
YDOT = 19166
973680 feet/sec YDOT = 5842
093578 meter/sec
ZDOT = -11489
320254 ZDOT = -3501
944814
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 08106
65426495
00020000 00000-0 20000-3 0 9050
2 25544 51
6388 338
6994 0001634 341
8635 18
2471 15
77564951 18663
Satellite: ISS
Catalog Number: 25544
Epoch time: 08106
65426495 = yrday
fracday
Element set: 905
Inclination: 51
6388 deg
RA of node: 338
6994 deg
Eccentricity:
0001634
Arg of perigee: 341
8635 deg
Mean anomaly: 18
2471 deg
Mean motion: 15
77564951 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1866
Checksum: 325
Coasting Arc #7 (Orbit 1881)
---------------------------------------
Vector Time (GMT): 2008/107/14:42:39
881
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5401960
14 A = 6715119
65 meter
Y = 759912
65 meter E =
0010462
Z = 3907285
97 I = 51
48821
XDOT = -3685
583922 Wp = 92
59912
YDOT = 5445
103318 meter/sec RA = 333
25884 deg
ZDOT = 4026
748321 TA = 315
48879
MA = 315
57279
Ha = 184
368 n
mi
Hp = 178
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17722966
35 X = 5374080
28
Y = 2493151
75 feet Y = 820164
78 meter
Z = 12819179
70 Z = 3933460
97
XDOT = -12091
810768 XDOT = -3765
759239
YDOT = 17864
512197 feet/sec YDOT = 5403
440936 meter/sec
ZDOT = 13211
116538 ZDOT = 4008
648704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9710499
52 X = 2959760
25
Y = -14947881
61 feet Y = -4556114
31 meter
Z = 12919665
03 Z = 3937913
90
XDOT = 9969
047095 XDOT = 3038
565555
YDOT = 17862
447015 feet/sec YDOT = 5444
473850 meter/sec
ZDOT = 13142
227535 ZDOT = 4005
750953
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 08107
66778765
00020000 00000-0 20000-3 0 9063
2 25544 51
6378 333
4659 0001592 344
3713 15
7403 15
77619824 18826
Satellite: ISS
Catalog Number: 25544
Epoch time: 08107
66778765 = yrday
fracday
Element set: 906
Inclination: 51
6378 deg
RA of node: 333
4659 deg
Eccentricity:
0001592
Arg of perigee: 344
3713 deg
Mean anomaly: 15
7403 deg
Mean motion: 15
77619824 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1882
Checksum: 321
Coasting Arc #8 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2008/108/14:42:39
881
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3943161
10 A = 6719079
27 meter
Y = -4821368
22 meter E =
0006247
Z = -2515749
33 I = 51
47583
XDOT = 5356
558800 Wp = 37
45128
YDOT = 1624
907612 meter/sec RA = 328
03551 deg
ZDOT = 5293
466033 TA = 293
94776
MA = 294
01317
Ha = 184
519 n
mi
Hp = 178
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12936880
25 X = 4009002
46
Y = -15818137
21 feet Y = -4776905
53 meter
Z = -8253770
78 Z = -2496433
15
XDOT = 17574
011812 XDOT = 5312
275852
YDOT = 5331
061719 feet/sec YDOT = 1684
560399 meter/sec
ZDOT = 17367
014543 ZDOT = 5319
380706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9175129
42 X = -2796579
45
Y = -18292159
47 feet Y = -5575450
21 meter
Z = -8180157
07 Z = -2493311
87
XDOT = 10639
906571 XDOT = 3243
043523
YDOT = -13130
433576 feet/sec YDOT = -4002
156154 meter/sec
ZDOT = 17466
584132 ZDOT = 5323
814843
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 08108
61793728
00020000 00000-0 20000-3 0 9076
2 25544 51
6375 328
5592 0001479 352
3433 7
7709 15
77653368 18973
Satellite: ISS
Catalog Number: 25544
Epoch time: 08108
61793728 = yrday
fracday
Element set: 907
Inclination: 51
6375 deg
RA of node: 328
5592 deg
Eccentricity:
0001479
Arg of perigee: 352
3433 deg
Mean anomaly: 7
7709 deg
Mean motion: 15
77653368 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1897
Checksum: 331
Coasting Arc #9 (Orbit 1912)
---------------------------------------
Vector Time (GMT): 2008/109/14:42:39
881
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3829255
54 A = 6710317
48 meter
Y = -2178359
15 meter E =
0014244
Z = -5074260
93 I = 51
42261
XDOT = 5179
382008 Wp = 72
18427
YDOT = -5475
523244 meter/sec RA = 322
89374 deg
ZDOT = -1557
251930 TA = 182
81151
MA = 182
81952
Ha = 184
481 n
mi
Hp = 177
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12563174
33 X = -3779962
06
Y = -7146847
60 feet Y = -2220904
69 meter
Z = -16647837
69 Z = -5092743
82
XDOT = 16992
723122 XDOT = 5247
790152
YDOT = -17964
315106 feet/sec YDOT = -5417
222013 meter/sec
ZDOT = -5109
094260 ZDOT = -1531
923803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11450077
41 X = -3489983
59
Y = 8685254
28 feet Y = 2647265
50 meter
Z = -16718952
27 Z = -5095936
65
XDOT = -9253
127208 XDOT = -2820
353173
YDOT = -21852
154836 feet/sec YDOT = -6660
536794 meter/sec
ZDOT = -5012
488135 ZDOT = -1527
806383
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 08109
63139931
00020000 00000-0 20000-3 0 9080
2 25544 51
6373 323
3263 0001487
4806 359
6360 15
77712059 19137
Satellite: ISS
Catalog Number: 25544
Epoch time: 08109
63139931 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 323
3263 deg
Eccentricity:
0001487
Arg of perigee:
4806 deg
Mean anomaly: 359
6360 deg
Mean motion: 15
77712059 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1913
Checksum: 289
Coasting Arc #10 (Orbit 1928)
---------------------------------------
Vector Time (GMT): 2008/110/14:42:39
881
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4906850
83 A = 6721388
69 meter
Y = 4585180
24 meter E =
0011228
Z = 111578
29 I = 51
43792
XDOT = -3358
319897 Wp = 127
53638
YDOT = -3437
443820 meter/sec RA = 317
69984 deg
ZDOT = -6024
325495 TA = 51
24628
MA = 51
14599
Ha = 184
332 n
mi
Hp = 177
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16098591
95 X = -4958300
37
Y = 15043242
24 feet Y = 4530021
36 meter
Z = 366070
52 Z = 87615
34
XDOT = -11018
109897 XDOT = -3290
366732
YDOT = -11277
702821 feet/sec YDOT = -3474
618703 meter/sec
ZDOT = -19764
847423 ZDOT = -6040
475300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7912320
04 X = 2411675
15
Y = 20564960
16 feet Y = 6268199
86 meter
Z = 274613
53 Z = 83702
20
XDOT = -13043
398172 XDOT = -3975
627763
YDOT = 5306
883725 feet/sec YDOT = 1617
538159 meter/sec
ZDOT = -19827
136121 ZDOT = -6043
311090
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 08110
64482790
00020000 00000-0 20000-3 0 9098
2 25544 51
6370 318
0917 0001758 356
9632 3
1522 15
77798338 19290
Satellite: ISS
Catalog Number: 25544
Epoch time: 08110
64482790 = yrday
fracday
Element set: 909
Inclination: 51
6370 deg
RA of node: 318
0917 deg
Eccentricity:
0001758
Arg of perigee: 356
9632 deg
Mean anomaly: 3
1522 deg
Mean motion: 15
77798338 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1929
Checksum: 310
Coasting Arc #11 (Orbit 1944)
---------------------------------------
Vector Time (GMT): 2008/111/14:42:39
881
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2024385
99 A = 6710009
35 meter
Y = 3839136
21 meter E =
0005458
Z = 5114925
53 I = 51
37791
XDOT = -5856
172157 Wp = 42
68032
YDOT = 4839
941191 meter/sec RA = 312
50801 deg
ZDOT = -1310
209646 TA = 59
91040
MA = 59
85629
Ha = 184
414 n
mi
Hp = 177
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6641686
32 X = 1956457
88
Y = 12595591
25 feet Y = 3861394
29 meter
Z = 16781251
74 Z = 5124595
14
XDOT = -19213
163244 XDOT = -5903
493012
YDOT = 15879
072149 feet/sec YDOT = 4774
189529 meter/sec
ZDOT = -4298
588078 ZDOT = -1338
774429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14105677
00 X = 4299410
35
Y = -1591154
09 feet Y = -484983
77 meter
Z = 16818722
64 Z = 5126346
66
XDOT = 7821
084475 XDOT = 2383
866548
YDOT = 22579
512975 feet/sec YDOT = 6882
235555 meter/sec
ZDOT = -4407
671052 ZDOT = -1343
458137
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 08111
65822942
00020000 00000-0 20000-3 0 9109
2 25544 51
6366 312
8574 0001488 7
0593 353
0593 15
77756635 19453
Satellite: ISS
Catalog Number: 25544
Epoch time: 08111
65822942 = yrday
fracday
Element set: 910
Inclination: 51
6366 deg
RA of node: 312
8574 deg
Eccentricity:
0001488
Arg of perigee: 7
0593 deg
Mean anomaly: 353
0593 deg
Mean motion: 15
77756635 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1945
Checksum: 304
Coasting Arc #12 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2008/112/05:54:37
282
Vector Time (MET): N/A
Weight (LBS) : 630355
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2266242
46 A = 6711389
21 meter
Y = 3694304
99 meter E =
0007324
Z = 5120054
56 I = 51
36848
XDOT = -5557
110406 Wp = 54
15366
YDOT = 5189
583255 meter/sec RA = 309
23119 deg
ZDOT = -1279
272643 TA = 48
14015
MA = 48
07767
Ha = 186
006 n
mi
Hp = 177
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7435178
69 X = 2199890
96
Y = 12120423
19 feet Y = 3719276
39 meter
Z = 16798079
28 Z = 5130903
03
XDOT = -18231
989521 XDOT = -5608
513524
YDOT = 17026
191783 feet/sec YDOT = 5127
153067 meter/sec
ZDOT = -4197
088725 ZDOT = -1306
394430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7343439
99 X = -2238280
51
Y = 12118101
95 feet Y = 3693597
48 meter
Z = 16840056
48 Z = 5132849
21
XDOT = -22638
794632 XDOT = -6900
304604
YDOT = -7717
438329 feet/sec YDOT = -2352
275203 meter/sec
ZDOT = -4300
603433 ZDOT = -1310
823926
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 08112
29160850
00020000 00000-0 20000-3 0 9114
2 25544 51
6394 309
5913 0003055 54
1758 305
9690 15
77259864 19559
Satellite: ISS
Catalog Number: 25544
Epoch time: 08112
29160850 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 309
5913 deg
Eccentricity:
0003055
Arg of perigee: 54
1758 deg
Mean anomaly: 305
9690 deg
Mean motion: 15
77259864 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1955
Checksum: 305
Coasting Arc #13 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2008/113/05:54:37
282
Vector Time (MET): N/A
Weight (LBS) : 630355
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4852267
40 A = 6720788
55 meter
Y = -4111496
27 meter E =
0017088
Z = 2146843
30 I = 51
38308
XDOT = 1861
242884 Wp = 68
12954
YDOT = 5080
158088 meter/sec RA = 304
08189 deg
ZDOT = 5493
870281 TA = 316
03343
MA = 316
16925
Ha = 186
014 n
mi
Hp = 177
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15919512
47 X = 4887452
98
Y = -13489160
99 feet Y = -4057038
77 meter
Z = 7043449
14 Z = 2170501
42
XDOT = 6106
439907 XDOT = 1777
608693
YDOT = 16667
185327 feet/sec YDOT = 5100
503800 meter/sec
ZDOT = 18024
508796 ZDOT = 5502
709355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19440966
46 X = 5925606
58
Y = 7493757
80 feet Y = 2284097
38 meter
Z = 7133788
22 Z = 2174378
65
XDOT = -11219
295595 XDOT = -3419
641297
YDOT = 11826
561486 feet/sec YDOT = 3604
735941 meter/sec
ZDOT = 18058
914726 ZDOT = 5504
357209
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 08113
30533346
00020000 00000-0 20000-3 0 9122
2 25544 51
6395 304
3593 0003086 56
9497 303
1964 15
77286125 19713
Satellite: ISS
Catalog Number: 25544
Epoch time: 08113
30533346 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 304
3593 deg
Eccentricity:
0003086
Arg of perigee: 56
9497 deg
Mean anomaly: 303
1964 deg
Mean motion: 15
77286125 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1971
Checksum: 297
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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