Date:
January 24th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11474 33 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 523)
---------------------------------------
Vector Time (GMT): 2008/021/14:14:00
847
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -67460
55 A = 6716538
45 meter
Y = -5547068
72 meter E =
0005713
Z = -3792501
74 I = 51
90794
XDOT = 5788
838329 Wp = 18
26373
YDOT = 2818
929401 meter/sec RA = 56
89877 deg
ZDOT = -4222
446094 TA = 207
55111
MA = 207
58140
Ha = 184
483 n
mi
Hp = 180
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -221327
25 X = 12995
43
Y = -18199044
34 feet Y = -5547372
75 meter
Z = -12442591
03 Z = -3792634
76
XDOT = 18992
251735 XDOT = 5777
397721
YDOT = 9248
456039 feet/sec YDOT = 2883
600063 meter/sec
ZDOT = -13853
169600 ZDOT = -4194
352087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8103146
11 X = 2469838
93
Y = -16296232
23 feet Y = -4967091
58 meter
Z = -12443637
34 Z = -3792820
66
XDOT = 11630
269376 XDOT = 3544
906106
YDOT = 16287
962749 feet/sec YDOT = 4964
571046 meter/sec
ZDOT = -13745
451282 ZDOT = -4189
613551
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 08021
61665162
00020000 00000-0 20000-3 0 9003
2 25544 51
6372 57
3549 0005708 312
6203 47
4480 15
77296667 5240
Satellite: ISS
Catalog Number: 25544
Epoch time: 08021
61665162 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 57
3549 deg
Eccentricity:
0005708
Arg of perigee: 312
6203 deg
Mean anomaly: 47
4480 deg
Mean motion: 15
77296667 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 524
Checksum: 285
Coasting Arc #2 (Orbit 539)
---------------------------------------
Vector Time (GMT): 2008/022/14:14:00
847
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5252776
52 A = 6719259
32 meter
Y = -3118280
87 meter E =
0009596
Z = 2793393
40 I = 51
90022
XDOT = 639
062039 Wp = 78
34983
YDOT = -5699
858368 meter/sec RA = 51
70676 deg
ZDOT = -5144
399283 TA = 69
74845
MA = 69
64531
Ha = 184
595 n
mi
Hp = 179
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17233518
77 X = -5231086
41
Y = -10230580
28 feet Y = -3176899
42 meter
Z = 9164676
51 Z = 2767928
55
XDOT = 2096
660234 XDOT = 727
741027
YDOT = -18700
322730 feet/sec YDOT = -5692
215648 meter/sec
ZDOT = -16877
950403 ZDOT = -5141
080013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11072081
07 X = -3374770
31
Y = -16758555
55 feet Y = -5108007
73 meter
Z = 9066977
12 Z = 2763614
63
XDOT = 8925
977762 XDOT = 2720
638022
YDOT = -15052
157574 feet/sec YDOT = -4587
897628 meter/sec
ZDOT = -16865
809143 ZDOT = -5140
698627
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 08022
63033830
00020000 00000-0 20000-3 0 9018
2 25544 51
6368 52
1227 0005877 317
6324 42
4387 15
77375306 5404
Satellite: ISS
Catalog Number: 25544
Epoch time: 08022
63033830 = yrday
fracday
Element set: 901
Inclination: 51
6368 deg
RA of node: 52
1227 deg
Eccentricity:
0005877
Arg of perigee: 317
6324 deg
Mean anomaly: 42
4387 deg
Mean motion: 15
77375306 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 540
Checksum: 274
Coasting Arc #3 (Orbit 555)
---------------------------------------
Vector Time (GMT): 2008/023/14:14:00
847
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1288817
06 A = 6711795
93 meter
Y = 4319574
78 meter E =
0001730
Z = 4971357
07 I = 51
85553
XDOT = -6149
650697 Wp = 44
62876
YDOT = -4176
691846 meter/sec RA = 46
60183 deg
ZDOT = 2035
590136 TA = 25
75351
MA = 25
74490
Ha = 184
762 n
mi
Hp = 179
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4228402
42 X = -1361172
61
Y = 14171833
28 feet Y = 4304757
57 meter
Z = 16310226
59 Z = 4964920
76
XDOT = -20176
019348 XDOT = -6112
377453
YDOT = -13703
057236 feet/sec YDOT = -4245
252481 meter/sec
ZDOT = 6678
445328 ZDOT = 2005
806301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9894019
54 X = -3015697
15
Y = 11028024
45 feet Y = 3361341
85 meter
Z = 16286030
55 Z = 4963982
11
XDOT = -11745
437220 XDOT = -3580
009265
YDOT = -20227
662953 feet/sec YDOT = -6165
391668 meter/sec
ZDOT = 6564
117585 ZDOT = 2000
743040
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 08023
64399977
00020000 00000-0 20000-3 0 9028
2 25544 51
6362 46
8902 0005855 321
3010 38
7734 15
77383169 5565
Satellite: ISS
Catalog Number: 25544
Epoch time: 08023
64399977 = yrday
fracday
Element set: 902
Inclination: 51
6362 deg
RA of node: 46
8902 deg
Eccentricity:
0005855
Arg of perigee: 321
3010 deg
Mean anomaly: 38
7734 deg
Mean motion: 15
77383169 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 556
Checksum: 305
Coasting Arc #4 (Orbit 570)
---------------------------------------
Vector Time (GMT): 2008/024/14:14:00
847
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5337981
56 A = 6722171
92 meter
Y = 4017790
94 meter E =
0013473
Z = -662696
91 I = 51
87015
XDOT = -2403
289385 Wp = 16
14904
YDOT = 4178
587489 meter/sec RA = 41
43352 deg
ZDOT = 6017
217809 TA = 336
64236
MA = 336
70351
Ha = 184
732 n
mi
Hp = 179
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17513062
87 X = 5295876
45
Y = 13181728
81 feet Y = 4077247
90 meter
Z = -2174202
46 Z = -636867
86
XDOT = -7884
807693 XDOT = -2479
066056
YDOT = 13709
276539 feet/sec YDOT = 4151
288581 meter/sec
ZDOT = 19741
528245 ZDOT = 6005
359110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10662979
37 X = 3250076
11
Y = 19162142
13 feet Y = 5840620
92 meter
Z = -2075013
68 Z = -632464
17
XDOT = -11476
831756 XDOT = -3498
138319
YDOT = 8503
780265 feet/sec YDOT = 2591
952225 meter/sec
ZDOT = 19696
579711 ZDOT = 6003
517496
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 08024
59428164
00020000 00000-0 20000-3 0 9035
2 25544 51
6361 41
9853 0005628 325
4439 34
6360 15
77460622 5710
Satellite: ISS
Catalog Number: 25544
Epoch time: 08024
59428164 = yrday
fracday
Element set: 903
Inclination: 51
6361 deg
RA of node: 41
9853 deg
Eccentricity:
0005628
Arg of perigee: 325
4439 deg
Mean anomaly: 34
6360 deg
Mean motion: 15
77460622 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 571
Checksum: 287
Coasting Arc #5 (Orbit 586)
---------------------------------------
Vector Time (GMT): 2008/025/14:14:00
847
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2961148
51 A = 6710389
08 meter
Y = -2955786
95 meter E =
0012491
Z = -5256176
95 I = 51
80784
XDOT = 5908
348540 Wp = 71
89088
YDOT = 4901
315451 meter/sec RA = 36
28632 deg
ZDOT = 577
244344 TA = 203
55512
MA = 203
61237
Ha = 184
902 n
mi
Hp = 179
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9715054
17 X = 3019513
38
Y = -9697463
75 feet Y = -2922347
25 meter
Z = -17244675
02 Z = -5241650
37
XDOT = 19384
345605 XDOT = 5850
298086
YDOT = 16080
431271 feet/sec YDOT = 4967
061376 meter/sec
ZDOT = 1893
846274 ZDOT = 605
805457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12819000
85 X = 3907231
46
Y = -5098973
32 feet Y = -1554167
07 meter
Z = -17189403
29 Z = -5239330
12
XDOT = 11189
592143 XDOT = 3410
587685
YDOT = 21431
250524 feet/sec YDOT = 6532
245160 meter/sec
ZDOT = 2003
572282 ZDOT = 610
688831
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 08025
60788957
00020000 00000-0 20000-3 0 9048
2 25544 51
6364 36
7520 0005834 329
7267 30
3561 15
77456296 5876
Satellite: ISS
Catalog Number: 25544
Epoch time: 08025
60788957 = yrday
fracday
Element set: 904
Inclination: 51
6364 deg
RA of node: 36
7520 deg
Eccentricity:
0005834
Arg of perigee: 329
7267 deg
Mean anomaly: 30
3561 deg
Mean motion: 15
77456296 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 587
Checksum: 316
Coasting Arc #6 (Orbit 602)
---------------------------------------
Vector Time (GMT): 2008/026/14:14:00
847
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4781939
19 A = 6720920
52 meter
Y = -4419873
38 meter E =
0002275
Z = -1663657
77 I = 51
82053
XDOT = 4411
669659 Wp = 110
55150
YDOT = -2612
835146 meter/sec RA = 31
15710 deg
ZDOT = -5746
194485 TA = 87
80330
MA = 87
77725
Ha = 184
941 n
mi
Hp = 179
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15688776
86 X = -4724078
51
Y = -14500896
92 feet Y = -4473024
21 meter
Z = -5458194
80 Z = -1686747
43
XDOT = 14473
981820 XDOT = 4468
472256
YDOT = -8572
293787 feet/sec YDOT = -2563
183680 meter/sec
ZDOT = -18852
344112 ZDOT = -5724
625129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9090280
49 X = -2770717
49
Y = -19308128
74 feet Y = -5885117
64 meter
Z = -5546943
88 Z = -1690708
49
XDOT = 15321
418304 XDOT = 4669
968299
YDOT = -1827
516837 feet/sec YDOT = -557
027132 meter/sec
ZDOT = -18770
102239 ZDOT = -5721
127162
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 08026
62146937
00020000 00000-0 20000-3 0 9058
2 25544 51
6371 31
5191 0005926 334
1433 25
9435 15
77522754 6030
Satellite: ISS
Catalog Number: 25544
Epoch time: 08026
62146937 = yrday
fracday
Element set: 905
Inclination: 51
6371 deg
RA of node: 31
5191 deg
Eccentricity:
0005926
Arg of perigee: 334
1433 deg
Mean anomaly: 25
9435 deg
Mean motion: 15
77522754 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 603
Checksum: 280
Coasting Arc #7 (Orbit 618)
---------------------------------------
Vector Time (GMT): 2008/027/14:14:00
847
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4695798
59 A = 6713304
47 meter
Y = 1657775
82 meter E =
0010724
Z = 4501823
41 I = 51
76942
XDOT = -4832
816150 Wp = 33
27700
YDOT = -5110
914799 meter/sec RA = 25
96683 deg
ZDOT = -3146
666940 TA = 88
10620
MA = 87
98339
Ha = 185
053 n
mi
Hp = 178
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15406163
36 X = -4735855
75
Y = 5438897
03 feet Y = 1605040
70 meter
Z = 14769761
85 Z = 4478914
36
XDOT = -15855
696031 XDOT = -4760
020268
YDOT = -16768
093171 feet/sec YDOT = -5164
551041 meter/sec
ZDOT = -10323
710432 ZDOT = -3169
967576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16409854
42 X = -5001723
63
Y = -473262
15 feet Y = -144250
30 meter
Z = 14682303
51 Z = 4475166
11
XDOT = -8773
202023 XDOT = -2674
071977
YDOT = -20118
835064 feet/sec YDOT = -6132
220928 meter/sec
ZDOT = -10413
330887 ZDOT = -3173
983254
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 08027
63502107
00020000 00000-0 20000-3 0 9066
2 25544 51
6371 26
2866 0005958 337
2186 22
8714 15
77565469 6197
Satellite: ISS
Catalog Number: 25544
Epoch time: 08027
63502107 = yrday
fracday
Element set: 906
Inclination: 51
6371 deg
RA of node: 26
2866 deg
Eccentricity:
0005958
Arg of perigee: 337
2186 deg
Mean anomaly: 22
8714 deg
Mean motion: 15
77565469 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 619
Checksum: 305
Coasting Arc #8 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2008/028/14:14:00
847
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3445752
50 A = 6715843
51 meter
Y = 4422291
18 meter E =
0010590
Z = 3685651
96 I = 51
75301
XDOT = -6257
048278 Wp = 66
20515
YDOT = 1264
963308 meter/sec RA = 20
86265 deg
ZDOT = 4326
468857 TA = 338
18050
MA = 338
22557
Ha = 184
890 n
mi
Hp = 178
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11304962
27 X = 3378141
70
Y = 14508829
33 feet Y = 4460445
44 meter
Z = 12092034
00 Z = 3702227
05
XDOT = -20528
373615 XDOT = -6291
745151
YDOT = 4150
142086 feet/sec YDOT = 1194
799348 meter/sec
ZDOT = 14194
451630 ZDOT = 4295
988310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5592046
85 X = 1704455
88
Y = 17478262
79 feet Y = 5327374
50 meter
Z = 12155859
84 Z = 3705106
08
XDOT = -19509
685791 XDOT = -5946
552229
YDOT = -3561
571450 feet/sec YDOT = -1085
566978 meter/sec
ZDOT = 14077
997506 ZDOT = 4290
973640
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 08028
64854319
00020000 00000-0 20000-3 0 9074
2 25544 51
6380 21
0542 0005820 340
2515 19
8424 15
77638185 6357
Satellite: ISS
Catalog Number: 25544
Epoch time: 08028
64854319 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 21
0542 deg
Eccentricity:
0005820
Arg of perigee: 340
2515 deg
Mean anomaly: 19
8424 deg
Mean motion: 15
77638185 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 635
Checksum: 283
Coasting Arc #9 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2008/029/14:14:00
847
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6060656
38 A = 6718455
80 meter
Y = -615160
11 meter E =
0008498
Z = -2824508
18 I = 51
73363
XDOT = 2883
601722 Wp = 17
12620
YDOT = 4995
390108 meter/sec RA = 15
65700 deg
ZDOT = 5111
327315 TA = 310
47869
MA = 310
55273
Ha = 185
212 n
mi
Hp = 178
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19884043
26 X = 6080805
54
Y = -2018241
81 feet Y = -547273
64 meter
Z = -9266759
13 Z = -2795016
96
XDOT = 9460
635570 XDOT = 2802
698597
YDOT = 16389
075156 feet/sec YDOT = 5027
183654 meter/sec
ZDOT = 16769
446573 ZDOT = 5125
139337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19504826
76 X = 5945071
20
Y = 4592040
31 feet Y = 1399653
89 meter
Z = -9154026
43 Z = -2790147
26
XDOT = 3845
135113 XDOT = 1171
997182
YDOT = 17124
721806 feet/sec YDOT = 5219
615207 meter/sec
ZDOT = 16822
756666 ZDOT = 5127
576232
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 08029
59869610
00020000 00000-0 20000-3 0 9080
2 25544 51
6379 16
1482 0005975 345
1060 14
9928 15
77631235 6504
Satellite: ISS
Catalog Number: 25544
Epoch time: 08029
59869610 = yrday
fracday
Element set: 908
Inclination: 51
6379 deg
RA of node: 16
1482 deg
Eccentricity:
0005975
Arg of perigee: 345
1060 deg
Mean anomaly: 14
9928 deg
Mean motion: 15
77631235 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 650
Checksum: 306
Coasting Arc #10 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2008/030/14:14:00
847
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1417727
22 A = 6710801
97 meter
Y = -4273738
74 meter E =
0014727
Z = -4988502
08 I = 51
68090
XDOT = 7442
338420 Wp = 51
59298
YDOT = -184
580512 meter/sec RA = 10
53774 deg
ZDOT = -1951
863076 TA = 199
51919
MA = 199
57564
Ha = 185
121 n
mi
Hp = 178
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4651336
02 X = -1345599
30
Y = -14021452
58 feet Y = -4289189
04 meter
Z = -16366476
66 Z = -4995214
34
XDOT = 24417
120801 XDOT = 7453
330983
YDOT = -605
579106 feet/sec YDOT = -101
294487 meter/sec
ZDOT = -6403
750249 ZDOT = -1915
681936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8445
25 X = 2574
11
Y = -14743863
78 feet Y = -4493929
68 meter
Z = -16392560
11 Z = -4996452
32
XDOT = 22362
927525 XDOT = 6816
220310
YDOT = 6997
415335 feet/sec YDOT = 2132
812194 meter/sec
ZDOT = -6265
389395 ZDOT = -1909
690687
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 08030
61216284
00020000 00000-0 20000-3 0 9099
2 25544 51
6386 10
9148 0005928 348
8630 11
2403 15
77695933 6664
Satellite: ISS
Catalog Number: 25544
Epoch time: 08030
61216284 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 10
9148 deg
Eccentricity:
0005928
Arg of perigee: 348
8630 deg
Mean anomaly: 11
2403 deg
Mean motion: 15
77695933 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 666
Checksum: 295
Coasting Arc #11 (Orbit 681)
---------------------------------------
Vector Time (GMT): 2008/031/14:14:00
847
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6697872
76 A = 6721491
58 meter
Y = -254562
72 meter E =
0009549
Z = 470670
34 I = 51
68885
XDOT = -247
488720 Wp = 105
61436
YDOT = -4800
212835 meter/sec RA = 5
35693 deg
ZDOT = -6019
910588 TA = 69
26386
MA = 69
16155
Ha = 185
171 n
mi
Hp = 178
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21974648
16 X = -6696814
80
Y = -835179
54 feet Y = -329456
26 meter
Z = 1544194
01 Z = 438135
04
XDOT = -811
970867 XDOT = -164
550347
YDOT = -15748
729774 feet/sec YDOT = -4802
516263 meter/sec
ZDOT = -19750
362821 ZDOT = -6020
911737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20771059
10 X = -6331018
82
Y = -7246701
49 feet Y = -2208794
62 meter
Z = 1419733
40 Z = 432734
74
XDOT = 3421
795247 XDOT = 1042
963191
YDOT = -13746
674805 feet/sec YDOT = -4189
986481 meter/sec
ZDOT = -19754
651490 ZDOT = -6021
217774
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 08031
62560003
00020000 00000-0 20000-3 0 9104
2 25544 51
6392 5
6815 0005889 352
8588 7
2493 15
77733477 6824
Satellite: ISS
Catalog Number: 25544
Epoch time: 08031
62560003 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 5
6815 deg
Eccentricity:
0005889
Arg of perigee: 352
8588 deg
Mean anomaly: 7
2493 deg
Mean motion: 15
77733477 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 682
Checksum: 300
Coasting Arc #12 (Orbit 697)
---------------------------------------
Vector Time (GMT): 2008/032/14:14:00
847
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1023794
83 A = 6709580
49 meter
Y = 4114386
10 meter E =
0008174
Z = 5199087
97 I = 51
62013
XDOT = -7619
262593 Wp = 17
70283
YDOT = -742
171530 meter/sec RA =
19086 deg
ZDOT = -905
012698 TA = 80
95672
MA = 80
86423
Ha = 185
204 n
mi
Hp = 177
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3358906
93 X = -1094982
29
Y = 13498642
07 feet Y = 4102539
01 meter
Z = 17057375
23 Z = 5193941
86
XDOT = -24997
580685 XDOT = -7606
000917
YDOT = -2434
945964 feet/sec YDOT = -827
300237 meter/sec
ZDOT = -2969
201764 ZDOT = -941
994369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7057369
23 X = -2151086
14
Y = 12014442
80 feet Y = 3662002
16 meter
Z = 17038085
20 Z = 5193208
37
XDOT = -22453
828726 XDOT = -6843
926996
YDOT = -8740
728728 feet/sec YDOT = -2664
174116 meter/sec
ZDOT = -3110
718110 ZDOT = -948
146880
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 08032
63900612
00020000 00000-0 20000-3 0 9111
2 25544 51
6392
4485 0005922 356
1241 3
9877 15
77802488 6986
Satellite: ISS
Catalog Number: 25544
Epoch time: 08032
63900612 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node:
4485 deg
Eccentricity:
0005922
Arg of perigee: 356
1241 deg
Mean anomaly: 3
9877 deg
Mean motion: 15
77802488 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 698
Checksum: 289
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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