Date:
July 31st 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7265 64 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 3535)
---------------------------------------
Vector Time (GMT): 2008/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6184039
93 A = 6735587
28 meter
Y = 2532074
15 meter E =
0022018
Z = 732448
28 I = 51
80834
XDOT = -1201
003422 Wp = 34
98182
YDOT = -4688
826197 meter/sec RA = 152
78654 deg
ZDOT = 5998
629093 TA = 332
98684
MA = 333
10127
Ha = 194
692 n
mi
Hp = 184
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20288844
90 X = -6215452
41
Y = 8307329
88 feet Y = 2462744
91 meter
Z = 2403045
53 Z = 702330
89
XDOT = -3940
299942 XDOT = -1177
622651
YDOT = -15383
288049 feet/sec YDOT = -4702
126728 meter/sec
ZDOT = 19680
541644 ZDOT = 5992
850779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18996616
28 X = 5790168
64
Y = 10969127
76 feet Y = 3343390
14 meter
Z = 2287004
83 Z = 697079
07
XDOT = -8883
796637 XDOT = -2707
781215
YDOT = 11235
895164 feet/sec YDOT = 3424
700846 meter/sec
ZDOT = 19657
776542 ZDOT = 5991
690290
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 08212
56220515
00020000 00000-0 20000-3 0 9008
2 25544 51
6397 153
4413 0010125 11
0908 349
0476 15
72734210 35364
Satellite: ISS
Catalog Number: 25544
Epoch time: 08212
56220515 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 153
4413 deg
Eccentricity:
0010125
Arg of perigee: 11
0908 deg
Mean anomaly: 349
0476 deg
Mean motion: 15
72734210 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3536
Checksum: 254
Coasting Arc #2 (Orbit 3550)
---------------------------------------
Vector Time (GMT): 2008/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1863623
13 A = 6723729
68 meter
Y = 3740390
65 meter E =
0019729
Z = -5281862
88 I = 51
79502
XDOT = -6644
444059 Wp = 62
75579
YDOT = 3844
857199 meter/sec RA = 147
66217 deg
ZDOT = 388
314944 TA = 210
87218
MA = 210
98834
Ha = 194
785 n
mi
Hp = 183
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6114249
12 X = 1847316
69
Y = 12271622
88 feet Y = 3761140
29 meter
Z = -17328946
44 Z = -5272848
72
XDOT = -21799
357148 XDOT = -6688
830356
YDOT = 12614
360889 feet/sec YDOT = 3770
306982 meter/sec
ZDOT = 1273
999159 ZDOT = 355
929709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5686024
37 X = 1733100
23
Y = -12524523
85 feet Y = -3817474
87 meter
Z = -17293773
00 Z = -5271142
01
XDOT = 22570
141955 XDOT = 6879
379268
YDOT = 8704
801191 feet/sec YDOT = 2653
223403 meter/sec
ZDOT = 1149
313742 ZDOT = 350
310829
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 08213
51531176
00020000 00000-0 20000-3 0 9013
2 25544 51
6407 148
5559 0010159 14
4217 345
7233 15
72743238 35510
Satellite: ISS
Catalog Number: 25544
Epoch time: 08213
51531176 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 148
5559 deg
Eccentricity:
0010159
Arg of perigee: 14
4217 deg
Mean anomaly: 345
7233 deg
Mean motion: 15
72743238 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3551
Checksum: 275
Coasting Arc #3 (Orbit 3566)
---------------------------------------
Vector Time (GMT): 2008/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5330503
81 A = 6735709
81 meter
Y = -4118482
70 meter E =
0012143
Z = 36364
03 I = 51
86049
XDOT = 2937
652501 Wp = 85
52702
YDOT = 3733
513835 meter/sec RA = 142
55228 deg
ZDOT = -6049
648801 TA = 94
07973
MA = 93
94092
Ha = 194
846 n
mi
Hp = 183
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17488529
57 X = 5375984
53
Y = -13512082
35 feet Y = -4058619
65 meter
Z = 119304
58 Z = 62369
00
XDOT = 9637
967522 XDOT = 2925
072755
YDOT = 12249
061138 feet/sec YDOT = 3766
294635 meter/sec
ZDOT = -19847
929138 ZDOT = -6035
408229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21567896
07 X = -6573894
72
Y = -4818404
43 feet Y = -1468649
67 meter
Z = 219334
03 Z = 66853
01
XDOT = 2840
331587 XDOT = 865
733068
YDOT = -13754
920148 feet/sec YDOT = -4192
499661 meter/sec
ZDOT = -19792
565250 ZDOT = -6032
773888
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 08214
53194929
00020000 00000-0 20000-3 0 9028
2 25544 51
6416 143
3449 0010143 18
5144 341
6385 15
72757036 35679
Satellite: ISS
Catalog Number: 25544
Epoch time: 08214
53194929 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 143
3449 deg
Eccentricity:
0010143
Arg of perigee: 18
5144 deg
Mean anomaly: 341
6385 deg
Mean motion: 15
72757036 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3567
Checksum: 289
Coasting Arc #4 (Orbit 3582)
---------------------------------------
Vector Time (GMT): 2008/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3200337
66 A = 6723549
17 meter
Y = -2678414
89 meter E =
0010409
Z = 5265694
64 I = 51
84256
XDOT = 5392
500095 Wp = 36
92746
YDOT = -5480
882003 meter/sec RA = 137
44656 deg
ZDOT = 497
184423 TA = 48
40993
MA = 48
32076
Ha = 194
885 n
mi
Hp = 183
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10499795
47 X = -3195728
50
Y = -8787450
42 feet Y = -2714177
51 meter
Z = 17275901
06 Z = 5250158
79
XDOT = 17691
929447 XDOT = 5450
972240
YDOT = -17981
896335 feet/sec YDOT = -5420
253069 meter/sec
ZDOT = 1631
182489 ZDOT = 523
522169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 249188
31 X = 75952
60
Y = 13765234
65 feet Y = 4195643
52 meter
Z = 17215631
49 Z = 5247324
48
XDOT = -24159
521992 XDOT = -7363
822303
YDOT = -1697
757822 feet/sec YDOT = -517
476584 meter/sec
ZDOT = 1732
369472 ZDOT = 528
026215
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 08215
54857465
00020000 00000-0 20000-3 0 9032
2 25544 51
6416 138
1342 0010099 21
4202 338
7381 15
72819470 35833
Satellite: ISS
Catalog Number: 25544
Epoch time: 08215
54857465 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 138
1342 deg
Eccentricity:
0010099
Arg of perigee: 21
4202 deg
Mean anomaly: 338
7381 deg
Mean motion: 15
72819470 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3583
Checksum: 287
Coasting Arc #5 (Orbit 3597)
---------------------------------------
Vector Time (GMT): 2008/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3986713
90 A = 6735329
60 meter
Y = 5351052
13 meter E =
0020317
Z = -835990
40 I = 51
90265
XDOT = -4283
854233 Wp = 32
40309
YDOT = -2269
064253 meter/sec RA = 132
32425 deg
ZDOT = 5988
416373 TA = 318
50834
MA = 318
66241
Ha = 194
981 n
mi
Hp = 183
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13079770
03 X = -4042192
92
Y = 17555945
32 feet Y = 5306160
25 meter
Z = -2742750
64 Z = -855491
94
XDOT = -14054
639873 XDOT = -4287
252838
YDOT = -7444
436524 feet/sec YDOT = -2316
988067 meter/sec
ZDOT = 19647
035344 ZDOT = 5967
597484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21798898
93 X = 6644304
39
Y = -1919297
07 feet Y = -585001
75 meter
Z = -2817549
52 Z = -858789
10
XDOT = 3722
051674 XDOT = 1134
481350
YDOT = 13941
001203 feet/sec YDOT = 4249
217167 meter/sec
ZDOT = 19566
395230 ZDOT = 5963
837266
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 08216
50165464
00020000 00000-0 20000-3 0 9041
2 25544 51
6417 133
2486 0010234 25
2766 334
8896 15
72780734 35981
Satellite: ISS
Catalog Number: 25544
Epoch time: 08216
50165464 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 133
2486 deg
Eccentricity:
0010234
Arg of perigee: 25
2766 deg
Mean anomaly: 334
8896 deg
Mean motion: 15
72780734 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3598
Checksum: 304
Coasting Arc #6 (Orbit 3613)
---------------------------------------
Vector Time (GMT): 2008/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4149914
35 A = 6724099
35 meter
Y = 1234059
73 meter E =
0022048
Z = -5163188
04 I = 51
88458
XDOT = -3674
535767 Wp = 58
81612
YDOT = 6607
562636 meter/sec RA = 127
23530 deg
ZDOT = -1367
255786 TA = 198
07213
MA = 198
15063
Ha = 195
022 n
mi
Hp = 183
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13615204
56 X = 4160887
89
Y = 4048752
39 feet Y = 1280527
99 meter
Z = -16939593
31 Z = -5143001
39
XDOT = -12055
563539 XDOT = -3741
507716
YDOT = 21678
355104 feet/sec YDOT = 6566
097452 meter/sec
ZDOT = -4485
747328 ZDOT = -1385
268829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6316936
90 X = -1925402
37
Y = -12825846
27 feet Y = -3909317
94 meter
Z = -16861494
24 Z = -5139383
45
XDOT = 23157
458640 XDOT = 7058
393394
YDOT = -5387
840458 feet/sec YDOT = -1642
213772 meter/sec
ZDOT = -4554
676725 ZDOT = -1388
265466
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 08217
51826164
00020000 00000-0 20000-3 0 9055
2 25544 51
6423 128
0371 0010232 29
4986 330
6752 15
72826822 36144
Satellite: ISS
Catalog Number: 25544
Epoch time: 08217
51826164 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 128
0371 deg
Eccentricity:
0010232
Arg of perigee: 29
4986 deg
Mean anomaly: 330
6752 deg
Mean motion: 15
72826822 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3614
Checksum: 281
Coasting Arc #7 (Orbit 3629)
---------------------------------------
Vector Time (GMT): 2008/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2399920
43 A = 6734508
54 meter
Y = -6097941
78 meter E =
0018154
Z = 1542098
55 I = 51
93592
XDOT = 5040
340698 Wp = 83
84527
YDOT = 503
315824 meter/sec RA = 122
10166 deg
ZDOT = -5793
956585 TA = 79
24053
MA = 79
03620
Ha = 195
083 n
mi
Hp = 183
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7873754
71 X = 2460439
08
Y = -20006370
68 feet Y = -6070766
16 meter
Z = 5059378
46 Z = 1553904
04
XDOT = 16536
550846 XDOT = 5062
483593
YDOT = 1651
298635 feet/sec YDOT = 559
803799 meter/sec
ZDOT = -19009
043915 ZDOT = -5769
417099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19889828
38 X = -6062419
69
Y = 8135611
47 feet Y = 2479734
38 meter
Z = 5104384
83 Z = 1555816
50
XDOT = -9702
749448 XDOT = -2957
398032
YDOT = -11731
922597 feet/sec YDOT = -3575
890008 meter/sec
ZDOT = -18914
199297 ZDOT = -5765
047946
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 08218
53485885
00020000 00000-0 20000-3 0 9060
2 25544 51
6420 122
8254 0010165 33
2916 326
8884 15
72813737 36306
Satellite: ISS
Catalog Number: 25544
Epoch time: 08218
53485885 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 122
8254 deg
Eccentricity:
0010165
Arg of perigee: 33
2916 deg
Mean anomaly: 326
8884 deg
Mean motion: 15
72813737 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3630
Checksum: 298
Coasting Arc #8 (Orbit 3645)
---------------------------------------
Vector Time (GMT): 2008/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4541468
86 A = 6724956
27 meter
Y = 397082
71 meter E =
0012368
Z = 4932610
59 I = 51
91864
XDOT = 1743
605995 Wp = 67
79654
YDOT = -7183
939517 meter/sec RA = 117
02695 deg
ZDOT = 2183
912084 TA = 1
10861
MA = 1
10587
Ha = 195
239 n
mi
Hp = 182
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14899832
23 X = -4569533
11
Y = 1302764
80 feet Y = 346140
30 meter
Z = 16183105
62 Z = 4910480
16
XDOT = 5720
492111 XDOT = 1813
199400
YDOT = -23569
355372 feet/sec YDOT = -7164
052476 meter/sec
ZDOT = 7165
065892 ZDOT = 2192
551230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11461638
00 X = 3493507
26
Y = 9751490
53 feet Y = 2972254
31 meter
Z = 16097651
72 Z = 4906564
24
XDOT = -20049
436343 XDOT = -6111
068197
YDOT = 11684
977394 feet/sec YDOT = 3561
581110 meter/sec
ZDOT = 7197
742624 ZDOT = 2193
871952
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 08219
55144457
00020000 00000-0 20000-3 0 9071
2 25544 51
6421 117
6137 0010186 36
7360 323
4499 15
72851306 36469
Satellite: ISS
Catalog Number: 25544
Epoch time: 08219
55144457 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 117
6137 deg
Eccentricity:
0010186
Arg of perigee: 36
7360 deg
Mean anomaly: 323
4499 deg
Mean motion: 15
72851306 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3646
Checksum: 292
Coasting Arc #9 (Orbit 3660)
---------------------------------------
Vector Time (GMT): 2008/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -626796
83 A = 6733161
38 meter
Y = 6306571
43 meter E =
0016135
Z = -2260876
61 I = 51
95916
XDOT = -5204
916094 Wp = 41
38845
YDOT = 1437
917033 meter/sec RA = 111
88379 deg
ZDOT = 5487
888233 TA = 293
35796
MA = 293
52762
Ha = 195
134 n
mi
Hp = 182
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2056420
03 X = -686288
46
Y = 20690851
16 feet Y = 6299229
71 meter
Z = -7417574
18 Z = -2264065
76
XDOT = -17076
496370 XDOT = -5247
267293
YDOT = 4717
575566 feet/sec YDOT = 1379
475598 meter/sec
ZDOT = 18004
882654 ZDOT = 5462
500089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15908978
07 X = 4849056
52
Y = -13381728
23 feet Y = -4078750
77 meter
Z = -7429290
53 Z = -2264447
75
XDOT = 14603
232228 XDOT = 4451
065183
YDOT = 7481
253526 feet/sec YDOT = 2280
286075 meter/sec
ZDOT = 17906
938598 ZDOT = 5458
034885
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 08220
50448512
00020000 00000-0 20000-3 0 9088
2 25544 51
6425 112
7278 0010196 39
7911 320
3998 15
72869598 36610
Satellite: ISS
Catalog Number: 25544
Epoch time: 08220
50448512 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 112
7278 deg
Eccentricity:
0010196
Arg of perigee: 39
7911 deg
Mean anomaly: 320
3998 deg
Mean motion: 15
72869598 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3661
Checksum: 310
Coasting Arc #10 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2008/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4423723
48 A = 6726123
72 meter
Y = -2072144
19 meter E =
0020156
Z = -4643241
49 I = 51
94535
XDOT = 249
225554 Wp = 56
83296
YDOT = 7098
223028 meter/sec RA = 106
82048 deg
ZDOT = -2928
637219 TA = 184
20439
MA = 184
22135
Ha = 195
145 n
mi
Hp = 182
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14513528
47 X = 4469121
67
Y = -6798373
32 feet Y = -2022421
43 meter
Z = -15233731
93 Z = -4621641
00
XDOT = 817
669141 XDOT = 184
060294
YDOT = 23288
133293 feet/sec YDOT = 7100
645846 meter/sec
ZDOT = -9608
389826 ZDOT = -2927
584306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15280612
56 X = -4657530
71
Y = -5088515
43 feet Y = -1550979
50 meter
Z = -15150474
16 Z = -4617864
53
XDOT = 14991
698027 XDOT = 4569
469558
YDOT = -16409
487457 feet/sec YDOT = -5001
611777 meter/sec
ZDOT = -9603
651516 ZDOT = -2927
192982
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 08221
52105138
00020000 00000-0 20000-3 0 9096
2 25544 51
6427 107
5159 0010189 42
8811 317
3144 15
72888086 36777
Satellite: ISS
Catalog Number: 25544
Epoch time: 08221
52105138 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 107
5159 deg
Eccentricity:
0010189
Arg of perigee: 42
8811 deg
Mean anomaly: 317
3144 deg
Mean motion: 15
72888086 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3677
Checksum: 295
Coasting Arc #11 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2008/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1040411
77 A = 6731825
24 meter
Y = -6001545
04 meter E =
0021361
Z = 2855100
35 I = 51
97180
XDOT = 4750
592549 Wp = 76
86660
YDOT = -3268
701995 meter/sec RA = 101
67048 deg
ZDOT = -5103
301737 TA = 70
53082
MA = 70
30016
Ha = 195
247 n
mi
Hp = 182
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3413424
43 X = -987093
70
Y = -19690108
41 feet Y = -6012881
64 meter
Z = 9367127
12 Z = 2850175
07
XDOT = 15585
933561 XDOT = 4811
581416
YDOT = -10724
087910 feet/sec YDOT = -3215
236716 meter/sec
ZDOT = -16743
115936 ZDOT = -5080
075596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10717084
53 X = -3266567
37
Y = 16877870
92 feet Y = 5144375
06 meter
Z = 9347538
63 Z = 2849129
77
XDOT = -17580
563295 XDOT = -5358
555692
YDOT = -1873
418287 feet/sec YDOT = -571
017894 meter/sec
ZDOT = -16653
680226 ZDOT = -5076
041733
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 08222
53760889
00020000 00000-0 20000-3 0 9100
2 25544 51
6426 102
3040 0010253 47
1266 313
0756 15
72888368 36935
Satellite: ISS
Catalog Number: 25544
Epoch time: 08222
53760889 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 102
3040 deg
Eccentricity:
0010253
Arg of perigee: 47
1266 deg
Mean anomaly: 313
0756 deg
Mean motion: 15
72888368 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3693
Checksum: 287
Coasting Arc #12 (Orbit 3708)
---------------------------------------
Vector Time (GMT): 2008/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3759616
76 A = 6727578
27 meter
Y = 3601816
62 meter E =
0017880
Z = 4243308
79 I = 51
96236
XDOT = -2102
432506 Wp = 78
14888
YDOT = -6472
943849 meter/sec RA = 96
61416 deg
ZDOT = 3622
460719 TA = 335
18469
MA = 335
27057
Ha = 195
391 n
mi
Hp = 182
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12334700
66 X = -3820226
51
Y = 11816983
67 feet Y = 3559435
14 meter
Z = 13921616
76 Z = 4224897
81
XDOT = -6897
744442 XDOT = -2047
491896
YDOT = -21236
692418 feet/sec YDOT = -6496
147609 meter/sec
ZDOT = 11884
713646 ZDOT = 3612
380012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17126879
45 X = 5220272
86
Y = -650000
71 feet Y = -198120
22 meter
Z = 13850807
04 Z = 4221725
99
XDOT = -8871
869809 XDOT = -2704
145918
YDOT = 19285
038726 feet/sec YDOT = 5878
079804 meter/sec
ZDOT = 11845
167374 ZDOT = 3610
407016
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 08223
55415561
00020000 00000-0 20000-3 0 9118
2 25544 51
6428 97
0920 0010261 50
3169 309
8897 15
72888995 37094
Satellite: ISS
Catalog Number: 25544
Epoch time: 08223
55415561 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 97
0920 deg
Eccentricity:
0010261
Arg of perigee: 50
3169 deg
Mean anomaly: 309
8897 deg
Mean motion: 15
72888995 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3709
Checksum: 314
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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