Date:
March 4th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7857 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3392)
---------------------------------------
Vector Time (GMT): 2007/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4062044
64 A = 6706400
84 meter
Y = 1171289
71 meter E =
0018453
Z = 5222048
82 I = 51
32489
XDOT = -2788
777035 Wp = 265
71724
YDOT = 7149
779038 meter/sec RA = 294
69250 deg
ZDOT = 565
974031 TA = 178
87909
MA = 178
87495
Ha = 183
923 n
mi
Hp = 174
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13326918
12 X = 4023278
17
Y = 3842814
00 feet Y = 1216497
33 meter
Z = 17132706
11 Z = 5241687
44
XDOT = -9149
530955 XDOT = -2871
268942
YDOT = 23457
280310 feet/sec YDOT = 7118
132174 meter/sec
ZDOT = 1856
870182 ZDOT = 552
225737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10999745
25 X = 3352722
35
Y = 8297044
06 feet Y = 2528939
03 meter
Z = 17206633
86 Z = 5244582
00
XDOT = -16298
214505 XDOT = -4967
695781
YDOT = 17864
004996 feet/sec YDOT = 5444
948723 meter/sec
ZDOT = 1806
157901 ZDOT = 550
516928
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 07061
54837053
00020000 00000-0 20000-3 0 9008
2 25544 51
6350 295
0644 0020978 269
6183 90
2579 15
78858434 33936
Satellite: ISS
Catalog Number: 25544
Epoch time: 07061
54837053 = yrday
fracday
Element set: 900
Inclination: 51
6350 deg
RA of node: 295
0644 deg
Eccentricity:
0020978
Arg of perigee: 269
6183 deg
Mean anomaly: 90
2579 deg
Mean motion: 15
78858434 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3393
Checksum: 316
Coasting Arc #2 (Orbit 3408)
---------------------------------------
Vector Time (GMT): 2007/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3047816
03 A = 6717626
39 meter
Y = -5871694
94 meter E =
0012797
Z = 1141252
42 I = 51
35171
XDOT = 3872
639077 Wp = 312
70080
YDOT = 3142
702146 meter/sec RA = 289
50315 deg
ZDOT = 5876
992469 TA = 59
87138
MA = 59
74462
Ha = 183
883 n
mi
Hp = 174
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9999396
43 X = 3107703
79
Y = -19264091
02 feet Y = -5837277
62 meter
Z = 3744266
47 Z = 1156204
26
XDOT = 12705
508784 XDOT = 3808
660466
YDOT = 10310
702578 feet/sec YDOT = 3185
650903 meter/sec
ZDOT = 19281
471355 ZDOT = 5895
649622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15926101
28 X = 4854275
67
Y = -14732092
74 feet Y = -4490341
87 meter
Z = 3799658
49 Z = 1158135
91
XDOT = 7274
905051 XDOT = 2217
391059
YDOT = 12813
908987 feet/sec YDOT = 3905
679459 meter/sec
ZDOT = 19351
974433 ZDOT = 5898
481807
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 07062
56105944
00020000 00000-0 20000-3 0 9019
2 25544 51
6340 289
8242 0021153 273
6160 86
2586 15
78921910 34097
Satellite: ISS
Catalog Number: 25544
Epoch time: 07062
56105944 = yrday
fracday
Element set: 901
Inclination: 51
6340 deg
RA of node: 289
8242 deg
Eccentricity:
0021153
Arg of perigee: 273
6160 deg
Mean anomaly: 86
2586 deg
Mean motion: 15
78921910 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3409
Checksum: 288
Coasting Arc #3 (Orbit 3423)
---------------------------------------
Vector Time (GMT): 2007/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2660502
64 A = 6709137
65 meter
Y = -4185794
22 meter E =
0011513
Z = -4508673
27 I = 51
31398
XDOT = 4008
220233 Wp = 265
82062
YDOT = -5843
224574 meter/sec RA = 284
27248 deg
ZDOT = 3052
077640 TA = 34
66722
MA = 34
59223
Ha = 183
861 n
mi
Hp = 174
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8728683
19 X = -2591596
89
Y = -13732920
66 feet Y = -4215160
58 meter
Z = -14792235
15 Z = -4521429
98
XDOT = 13150
328849 XDOT = 4058
435976
YDOT = -19170
684299 feet/sec YDOT = -5798
121370 meter/sec
ZDOT = 10013
378084 ZDOT = 3071
671660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3742405
20 X = -1140685
11
Y = -15790529
24 feet Y = -4812953
31 meter
Z = -14840715
29 Z = -4523450
02
XDOT = 17437
372324 XDOT = 5314
911084
YDOT = -13635
286913 feet/sec YDOT = -4156
035451 meter/sec
ZDOT = 10086
204880 ZDOT = 3074
275247
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 07063
51043297
00020000 00000-0 20000-3 0 9028
2 25544 51
6330 284
9116 0021189 277
3686 82
5072 15
78953821 34247
Satellite: ISS
Catalog Number: 25544
Epoch time: 07063
51043297 = yrday
fracday
Element set: 902
Inclination: 51
6330 deg
RA of node: 284
9116 deg
Eccentricity:
0021189
Arg of perigee: 277
3686 deg
Mean anomaly: 82
5072 deg
Mean motion: 15
78953821 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3424
Checksum: 297
Coasting Arc #4 (Orbit 3439)
---------------------------------------
Vector Time (GMT): 2007/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3802632
22 A = 6711266
18 meter
Y = 3895755
52 meter E =
0015581
Z = -3917255
44 I = 51
31456
XDOT = -2236
095907 Wp = 293
52639
YDOT = -6210
676270 meter/sec RA = 279
12507 deg
ZDOT = -3987
277891 TA = 294
91175
MA = 295
07360
Ha = 184
007 n
mi
Hp = 174
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12475827
48 X = -3826883
48
Y = 12781350
13 feet Y = 3853096
40 meter
Z = -12851887
93 Z = -3935787
60
XDOT = -7336
272661 XDOT = -2147
111876
YDOT = -20376
234481 feet/sec YDOT = -6235
184381 meter/sec
ZDOT = -13081
620376 ZDOT = -3997
923953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15728648
41 X = -4794092
04
Y = 8356917
39 feet Y = 2547188
42 meter
Z = -12920981
26 Z = -3938315
09
XDOT = -48
752028 XDOT = -14
859618
YDOT = -20475
001495 feet/sec YDOT = -6240
780456 meter/sec
ZDOT = -13122
447357 ZDOT = -3999
721954
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 07064
52307182
00020000 00000-0 20000-3 0 9037
2 25544 51
6320 279
6724 0021272 281
3457 78
5319 15
78974807 34400
Satellite: ISS
Catalog Number: 25544
Epoch time: 07064
52307182 = yrday
fracday
Element set: 903
Inclination: 51
6320 deg
RA of node: 279
6724 deg
Eccentricity:
0021272
Arg of perigee: 281
3457 deg
Mean anomaly: 78
5319 deg
Mean motion: 15
78974807 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3440
Checksum: 299
Coasting Arc #5 (Orbit 3455)
---------------------------------------
Vector Time (GMT): 2007/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1233133
16 A = 6715933
05 meter
Y = 6272117
36 meter E =
0007345
Z = 2067821
70 I = 51
32841
XDOT = -4618
757085 Wp = 275
89287
YDOT = 2725
026679 meter/sec RA = 273
88216 deg
ZDOT = -5527
246165 TA = 240
88942
MA = 240
96298
Ha = 184
132 n
mi
Hp = 174
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4045712
47 X = 1152860
81
Y = 20577812
87 feet Y = 6285458
31 meter
Z = 6784191
93 Z = 2073616
66
XDOT = -15153
402510 XDOT = -4622
035381
YDOT = 8940
376244 feet/sec YDOT = 2673
358332 meter/sec
ZDOT = -18134
009727 ZDOT = -5549
692041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2143643
97 X = -653382
68
Y = 20854534
06 feet Y = 6356461
98 meter
Z = 6806807
73 Z = 2074715
00
XDOT = -15479
801900 XDOT = -4718
243619
YDOT = 4337
926946 feet/sec YDOT = 1322
200133 meter/sec
ZDOT = -18217
960133 ZDOT = -5552
834248
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 07065
53568319
00020000 00000-0 20000-3 0 9041
2 25544 51
6324 274
4320 0021307 285
6996 74
1819 15
79059478 34566
Satellite: ISS
Catalog Number: 25544
Epoch time: 07065
53568319 = yrday
fracday
Element set: 904
Inclination: 51
6324 deg
RA of node: 274
4320 deg
Eccentricity:
0021307
Arg of perigee: 285
6996 deg
Mean anomaly: 74
1819 deg
Mean motion: 15
79059478 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3456
Checksum: 319
Coasting Arc #6 (Orbit 3471)
---------------------------------------
Vector Time (GMT): 2007/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4173891
51 A = 6705887
26 meter
Y = -632331
87 meter E =
0018471
Z = 5224965
47 I = 51
29251
XDOT = 562
103938 Wp = 288
79991
YDOT = 7660
791920 meter/sec RA = 268
70593 deg
ZDOT = 485
358773 TA = 156
60701
MA = 156
52287
Ha = 184
290 n
mi
Hp = 174
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13693869
77 X = 4155270
36
Y = -2074579
61 feet Y = -585760
78 meter
Z = 17142275
16 Z = 5245196
91
XDOT = 1844
173025 XDOT = 474
040320
YDOT = 25133
831759 feet/sec YDOT = 7666
585331 meter/sec
ZDOT = 1592
384427 ZDOT = 487
874947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13646272
75 X = 4159383
93
Y = 1731106
80 feet Y = 527641
35 meter
Z = 17218189
71 Z = 5248104
22
XDOT = -4996
346861 XDOT = -1522
886523
YDOT = 23679
502814 feet/sec YDOT = 7217
512458 meter/sec
ZDOT = 1602
873847 ZDOT = 488
555949
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 07066
54827019
00020000 00000-0 20000-3 0 9059
2 25544 51
6314 269
1904 0021183 289
3017 70
5857 15
79031382 34725
Satellite: ISS
Catalog Number: 25544
Epoch time: 07066
54827019 = yrday
fracday
Element set: 905
Inclination: 51
6314 deg
RA of node: 269
1904 deg
Eccentricity:
0021183
Arg of perigee: 289
3017 deg
Mean anomaly: 70
5857 deg
Mean motion: 15
79031382 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3472
Checksum: 296
Coasting Arc #7 (Orbit 3487)
---------------------------------------
Vector Time (GMT): 2007/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 276277
93 A = 6716969
40 meter
Y = -6580648
61 meter E =
0017241
Z = 1271882
25 I = 51
33180
XDOT = 4857
240399 Wp = 333
77661
YDOT = 1324
659019 meter/sec RA = 263
51445 deg
ZDOT = 5843
911117 TA = 40
27756
MA = 40
14996
Ha = 184
409 n
mi
Hp = 174
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 906423
65 X = 343664
60
Y = -21590054
48 feet Y = -6577182
25 meter
Z = 4172842
01 Z = 1273388
49
XDOT = 15935
828080 XDOT = 4813
678328
YDOT = 4345
994158 feet/sec YDOT = 1378
732198 meter/sec
ZDOT = 19172
936735 ZDOT = 5867
401591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6411876
17 X = 1954339
86
Y = -20634924
30 feet Y = -6289524
93 meter
Z = 4177608
18 Z = 1273334
97
XDOT = 12671
738663 XDOT = 3862
345944
YDOT = 7806
960604 feet/sec YDOT = 2379
561592 meter/sec
ZDOT = 19261
360834 ZDOT = 5870
862782
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 07067
56082690
00020000 00000-0 20000-3 0 9061
2 25544 51
6305 263
9487 0021279 293
0529 66
8393 15
79111975 34886
Satellite: ISS
Catalog Number: 25544
Epoch time: 07067
56082690 = yrday
fracday
Element set: 906
Inclination: 51
6305 deg
RA of node: 263
9487 deg
Eccentricity:
0021279
Arg of perigee: 293
0529 deg
Mean anomaly: 66
8393 deg
Mean motion: 15
79111975 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3488
Checksum: 329
Coasting Arc #8 (Orbit 3502)
---------------------------------------
Vector Time (GMT): 2007/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4187975
27 A = 6708945
00 meter
Y = -2823091
24 meter E =
0011701
Z = -4404055
34 I = 51
30919
XDOT = 1228
039451 Wp = 301
67794
YDOT = -6891
048754 meter/sec RA = 258
27908 deg
ZDOT = 3249
286653 TA =
96914
MA =
96687
Ha = 184
472 n
mi
Hp = 174
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13740076
34 X = -4134701
76
Y = -9262110
36 feet Y = -2869625
85 meter
Z = -14449000
46 Z = -4424270
93
XDOT = 4029
000823 XDOT = 1289
220476
YDOT = -22608
427669 feet/sec YDOT = -6876
973904 meter/sec
ZDOT = 10660
389283 ZDOT = 3255
401367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11027310
70 X = -3361124
30
Y = -12278568
96 feet Y = -3742507
82 meter
Z = -14525328
33 Z = -4427320
08
XDOT = 8401
456719 XDOT = 2560
764008
YDOT = -20183
314622 feet/sec YDOT = -6151
874297 meter/sec
ZDOT = 10682
425870 ZDOT = 3256
003405
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 07068
51007555
00020000 00000-0 20000-3 0 9075
2 25544 51
6299 259
0348 0021190 296
7019 63
1978 15
79152457 35033
Satellite: ISS
Catalog Number: 25544
Epoch time: 07068
51007555 = yrday
fracday
Element set: 907
Inclination: 51
6299 deg
RA of node: 259
0348 deg
Eccentricity:
0021190
Arg of perigee: 296
7019 deg
Mean anomaly: 63
1978 deg
Mean motion: 15
79152457 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3503
Checksum: 310
Coasting Arc #9 (Orbit 3518)
---------------------------------------
Vector Time (GMT): 2007/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1920986
67 A = 6710030
14 meter
Y = 4957673
48 meter E =
0017316
Z = -4093299
17 I = 51
32029
XDOT = -4620
246514 Wp = 321
23809
YDOT = -4901
387526 meter/sec RA = 253
13095 deg
ZDOT = -3746
242985 TA = 270
15441
MA = 270
35284
Ha = 184
770 n
mi
Hp = 174
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6302449
71 X = -1956396
88
Y = 16265332
94 feet Y = 4935993
83 meter
Z = -13429459
23 Z = -4102717
44
XDOT = -15158
289089 XDOT = -4546
896607
YDOT = -16080
667737 feet/sec YDOT = -4952
643689 meter/sec
ZDOT = -12290
823442 ZDOT = -3768
509755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9713774
82 X = -2960758
57
Y = 14456521
06 feet Y = 4406347
62 meter
Z = -13464170
27 Z = -4103879
10
XDOT = -10048
738447 XDOT = -3062
855479
YDOT = -18344
398132 feet/sec YDOT = -5591
372551 meter/sec
ZDOT = -12375
144128 ZDOT = -3771
943930
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 07069
52258018
00020000 00000-0 20000-3 0 9080
2 25544 51
6298 253
7949 0021160 301
0513 58
8575 15
79208300 35196
Satellite: ISS
Catalog Number: 25544
Epoch time: 07069
52258018 = yrday
fracday
Element set: 908
Inclination: 51
6298 deg
RA of node: 253
7949 deg
Eccentricity:
0021160
Arg of perigee: 301
0513 deg
Mean anomaly: 58
8575 deg
Mean motion: 15
79208300 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3519
Checksum: 298
Coasting Arc #10 (Orbit 3534)
---------------------------------------
Vector Time (GMT): 2007/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3678183
54 A = 6715824
19 meter
Y = 5347785
23 meter E =
0007908
Z = 1744255
40 I = 51
35051
XDOT = -3239
424592 Wp = 322
88716
YDOT = 4075
410893 meter/sec RA = 247
89018 deg
ZDOT = -5671
001552 TA = 197
70381
MA = 197
73139
Ha = 185
032 n
mi
Hp = 174
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12067531
30 X = 3609637
24
Y = 17545227
14 feet Y = 5388533
50 meter
Z = 5722622
72 Z = 1761957
34
XDOT = -10628
033437 XDOT = -3257
207124
YDOT = 13370
770647 feet/sec YDOT = 4039
086330 meter/sec
ZDOT = -18605
648136 ZDOT = -5686
781832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8137610
62 X = 2480343
72
Y = 19658726
56 feet Y = 5991979
85 meter
Z = 5789860
25 Z = 1764749
40
XDOT = -11633
592398 XDOT = -3545
918963
YDOT = 10305
845482 feet/sec YDOT = 3141
221703 meter/sec
ZDOT = -18664
384185 ZDOT = -5688
904300
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 07070
53505475
00020000 00000-0 20000-3 0 9096
2 25544 51
6299 248
5531 0021466 304
8639 55
0509 15
79281195 35352
Satellite: ISS
Catalog Number: 25544
Epoch time: 07070
53505475 = yrday
fracday
Element set: 909
Inclination: 51
6299 deg
RA of node: 248
5531 deg
Eccentricity:
0021466
Arg of perigee: 304
8639 deg
Mean anomaly: 55
0509 deg
Mean motion: 15
79281195 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3535
Checksum: 310
Coasting Arc #11 (Orbit 3550)
---------------------------------------
Vector Time (GMT): 2007/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3728985
20 A = 6705248
77 meter
Y = -1923676
50 meter E =
0019234
Z = 5242173
02 I = 51
32556
XDOT = 3535
778962 Wp = 313
26401
YDOT = 6839
457882 meter/sec RA = 242
70826 deg
ZDOT = 7
683404 TA = 136
73838
MA = 136
58718
Ha = 185
206 n
mi
Hp = 174
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12234203
41 X = 3724753
59
Y = -6311274
59 feet Y = -1882000
53 meter
Z = 17198730
39 Z = 5260278
00
XDOT = 11600
324677 XDOT = 3458
999053
YDOT = 22439
166279 feet/sec YDOT = 6878
567641 meter/sec
ZDOT = 25
208017 ZDOT = 24
673514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13117967
49 X = 3998356
49
Y = -3884739
51 feet Y = -1184068
60 meter
Z = 17266498
63 Z = 5262828
78
XDOT = 6831
903830 XDOT = 2082
364287
YDOT = 23280
799175 feet/sec YDOT = 7095
987589 meter/sec
ZDOT = 89
982663 ZDOT = 27
426716
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 07071
54750599
00020000 00000-0 20000-3 0 9109
2 25544 51
6292 243
3110 0021058 308
9417 50
9872 15
79228758 35518
Satellite: ISS
Catalog Number: 25544
Epoch time: 07071
54750599 = yrday
fracday
Element set: 910
Inclination: 51
6292 deg
RA of node: 243
3110 deg
Eccentricity:
0021058
Arg of perigee: 308
9417 deg
Mean anomaly: 50
9872 deg
Mean motion: 15
79228758 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3551
Checksum: 299
Coasting Arc #12 (Orbit 3566)
---------------------------------------
Vector Time (GMT): 2007/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2226149
73 A = 6715770
53 meter
Y = -6080307
25 meter E =
0020457
Z = 1735309
33 I = 51
37659
XDOT = 5205
467554 Wp = 352
38638
YDOT = -289
483993 meter/sec RA = 237
52709 deg
ZDOT = 5691
148405 TA = 26
96382
MA = 26
85767
Ha = 185
350 n
mi
Hp = 173
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7303640
85 X = -2166423
12
Y = -19948514
58 feet Y = -6104867
34 meter
Z = 5693272
09 Z = 1724639
96
XDOT = 17078
305622 XDOT = 5180
671527
YDOT = -949
750632 feet/sec YDOT = -231
412150 meter/sec
ZDOT = 18671
746737 ZDOT = 5716
375998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3763036
48 X = -1146973
52
Y = -20918659
74 feet Y = -6376007
49 meter
Z = 5652343
06 Z = 1722834
16
XDOT = 15356
091081 XDOT = 4680
536562
YDOT = 2283
778575 feet/sec YDOT = 696
095710 meter/sec
ZDOT = 18766
510631 ZDOT = 5720
032440
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 07072
55992300
00020000 00000-0 20000-3 0 9110
2 25544 51
6294 238
0692 0021096 312
5958 47
3428 15
79327324 35672
Satellite: ISS
Catalog Number: 25544
Epoch time: 07072
55992300 = yrday
fracday
Element set: 911
Inclination: 51
6294 deg
RA of node: 238
0692 deg
Eccentricity:
0021096
Arg of perigee: 312
5958 deg
Mean anomaly: 47
3428 deg
Mean motion: 15
79327324 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3567
Checksum: 304
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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