Date:
August 28th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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 3979)
---------------------------------------
Vector Time (GMT): 2008/240/17:24:57
822
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6619869
11 A = 6738654
44 meter
Y = 1191697
30 meter E =
0019290
Z = 212132
70 I = 51
71175
XDOT = -1043
834749 Wp = 48
36271
YDOT = 4663
070528 meter/sec RA = 8
77837 deg
ZDOT = 6039
564561 TA = 313
93894
MA = 314
09795
Ha = 195
795 n
mi
Hp = 185
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21718730
69 X = 6605020
88
Y = 3909768
05 feet Y = 1265641
46 meter
Z = 695973
41 Z = 244255
43
XDOT = -3424
654688 XDOT = -1125
238966
YDOT = 15298
787823 feet/sec YDOT = 4650
942388 meter/sec
ZDOT = 19814
844359 ZDOT = 6034
296147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15160522
26 X = -4620927
19
Y = 16029962
00 feet Y = 4885932
42 meter
Z = 820250
49 Z = 250012
35
XDOT = -9696
064481 XDOT = -2955
360454
YDOT = -10231
339796 feet/sec YDOT = -3118
512370 meter/sec
ZDOT = 19794
868380 ZDOT = 6033
475882
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 08240
78877468
00020000 00000-0 20000-3 0 9008
2 25544 51
6421 8
9481 0006585 51
0399 309
1349 15
71721140 39800
Satellite: ISS
Catalog Number: 25544
Epoch time: 08240
78877468 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 8
9481 deg
Eccentricity:
0006585
Arg of perigee: 51
0399 deg
Mean anomaly: 309
1349 deg
Mean motion: 15
71721140 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3980
Checksum: 300
Coasting Arc #2 (Orbit 3994)
---------------------------------------
Vector Time (GMT): 2008/241/17:24:57
822
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -363852
60 A = 6726578
26 meter
Y = -4196216
73 meter E =
0020695
Z = -5262296
40 I = 51
64324
XDOT = 7661
396647 Wp = 76
40206
YDOT = 44
668353 meter/sec RA = 3
66447 deg
ZDOT = -562
434652 TA = 188
22373
MA = 188
25770
Ha = 195
708 n
mi
Hp = 185
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1193742
13 X = -291340
00
Y = -13767115
25 feet Y = -4199880
06 meter
Z = -17264751
96 Z = -5263887
86
XDOT = 25135
815771 XDOT = 7663
059902
YDOT = 146
549716 feet/sec YDOT = 130
351806 meter/sec
ZDOT = -1845
258045 ZDOT = -525
212267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12231938
22 X = 3728294
77
Y = 6411975
89 feet Y = 1954370
25 meter
Z = -17271259
24 Z = -5264279
82
XDOT = -13060
076968 XDOT = -3980
711460
YDOT = 20305
765463 feet/sec YDOT = 6189
197313 meter/sec
ZDOT = -1701
361146 ZDOT = -518
574877
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 08241
74246556
00020000 00000-0 20000-3 0 9014
2 25544 51
6429 4
0663 0006441 55
3483 304
8285 15
71764597 39959
Satellite: ISS
Catalog Number: 25544
Epoch time: 08241
74246556 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 4
0663 deg
Eccentricity:
0006441
Arg of perigee: 55
3483 deg
Mean anomaly: 304
8285 deg
Mean motion: 15
71764597 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3995
Checksum: 305
Coasting Arc #3 (Orbit 4010)
---------------------------------------
Vector Time (GMT): 2008/242/17:24:57
822
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6536545
43 A = 6737827
36 meter
Y = 1100862
90 meter E =
0017750
Z = 1179207
60 I = 51
65225
XDOT = -1849
808766 Wp = 102
54527
YDOT = -4607
438354 meter/sec RA = 358
53056 deg
ZDOT = -5882
088891 TA = 64
55015
MA = 64
36660
Ha = 195
729 n
mi
Hp = 185
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21445359
01 X = -6554097
92
Y = 3611754
91 feet Y = 1027669
36 meter
Z = 3868791
34 Z = 1147410
98
XDOT = -6068
926397 XDOT = -1769
576560
YDOT = -15116
267565 feet/sec YDOT = -4627
675507 meter/sec
ZDOT = -19298
191900 ZDOT = -5890
880119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8040041
73 X = 2450604
72
Y = -20229710
63 feet Y = -6166015
80 meter
Z = 3745968
44 Z = 1141771
18
XDOT = 14540
184995 XDOT = 4431
848387
YDOT = 2154
806870 feet/sec YDOT = 656
785134 meter/sec
ZDOT = -19332
570938 ZDOT = -5892
567622
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 08242
75972599
00020000 00000-0 20000-3 0 9020
2 25544 51
6428 358
8592 0006622 58
5692 301
6116 15
71820071 40115
Satellite: ISS
Catalog Number: 25544
Epoch time: 08242
75972599 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 358
8592 deg
Eccentricity:
0006622
Arg of perigee: 58
5692 deg
Mean anomaly: 301
6116 deg
Mean motion: 15
71820071 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4011
Checksum: 297
Coasting Arc #4 (Orbit 4026)
---------------------------------------
Vector Time (GMT): 2008/243/17:24:57
822
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2815118
64 A = 6727757
85 meter
Y = 3605921
60 meter E =
0011096
Z = 4923621
57 I = 51
58886
XDOT = -6963
890756 Wp = 91
20386
YDOT = 2508
873115 meter/sec RA = 353
43878 deg
ZDOT = 2139
865567 TA = 338
01405
MA = 338
06162
Ha = 195
715 n
mi
Hp = 184
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9235953
54 X = 2750669
70
Y = 11830451
44 feet Y = 3637041
74 meter
Z = 16153614
09 Z = 4937140
52
XDOT = -22847
410618 XDOT = -7001
822740
YDOT = 8231
211007 feet/sec YDOT = 2430
786882 meter/sec
ZDOT = 7020
556321 ZDOT = 2105
943226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14825419
61 X = -4518787
90
Y = 1941175
05 feet Y = 591670
16 meter
Z = 16206185
24 Z = 4939645
26
XDOT = 4556
710811 XDOT = 1388
885455
YDOT = -22837
199595 feet/sec YDOT = -6960
778437 meter/sec
ZDOT = 6889
642868 ZDOT = 2099
963146
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 08243
77697595
00020000 00000-0 20000-3 0 9034
2 25544 51
6423 353
6525 0006705 62
7668 297
4177 15
71825733 40277
Satellite: ISS
Catalog Number: 25544
Epoch time: 08243
77697595 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 353
6525 deg
Eccentricity:
0006705
Arg of perigee: 62
7668 deg
Mean anomaly: 297
4177 deg
Mean motion: 15
71825733 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4027
Checksum: 323
Coasting Arc #5 (Orbit 4041)
---------------------------------------
Vector Time (GMT): 2008/244/17:24:57
822
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5389089
23 A = 6735553
31 meter
Y = -3158129
14 meter E =
0011943
Z = -2519014
62 I = 51
58762
XDOT = 4441
604798 Wp = 58
28731
YDOT = 3370
953170 meter/sec RA = 348
27830 deg
ZDOT = 5300
517824 TA = 273
20178
MA = 273
33842
Ha = 195
785 n
mi
Hp = 184
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17680738
93 X = 5436240
21
Y = -10361316
07 feet Y = -3097601
75 meter
Z = -8264483
66 Z = -2492719
95
XDOT = 14572
194218 XDOT = 4377
831425
YDOT = 11059
557644 feet/sec YDOT = 3420
265485 meter/sec
ZDOT = 17390
150340 ZDOT = 5321
939841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 376688
66 X = 114814
70
Y = 20530189
69 feet Y = 6257601
82 meter
Z = -8163118
70 Z = -2488118
58
XDOT = -15224
385498 XDOT = -4640
392700
YDOT = 7194
577556 feet/sec YDOT = 2192
907239 meter/sec
ZDOT = 17473
249846 ZDOT = 5325
846553
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 08244
73063750
00020000 00000-0 20000-3 0 9042
2 25544 51
6435 348
7716 0006741 66
3147 293
8722 15
71870117 40428
Satellite: ISS
Catalog Number: 25544
Epoch time: 08244
73063750 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 348
7716 deg
Eccentricity:
0006741
Arg of perigee: 66
3147 deg
Mean anomaly: 293
8722 deg
Mean motion: 15
71870117 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4042
Checksum: 292
Coasting Arc #6 (Orbit 4057)
---------------------------------------
Vector Time (GMT): 2008/245/17:24:57
822
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4759677
63 A = 6730264
28 meter
Y = -2113294
02 meter E =
0015425
Z = -4279165
70 I = 51
54097
XDOT = 5153
401755 Wp = 68
71972
YDOT = -4479
978640 meter/sec RA = 343
19981 deg
ZDOT = -3524
313258 TA = 165
44973
MA = 165
40527
Ha = 195
773 n
mi
Hp = 184
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15615740
26 X = -4714905
35
Y = -6933379
34 feet Y = -2166269
41 meter
Z = -14039257
56 Z = -4302179
25
XDOT = 16907
486072 XDOT = 5220
234996
YDOT = -14698
092652 feet/sec YDOT = -4421
976864 meter/sec
ZDOT = -11562
707540 ZDOT = -3499
115519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13463968
67 X = 4103817
65
Y = -10398741
62 feet Y = -3169536
45 meter
Z = -14128395
74 Z = -4306335
02
XDOT = 4148
336273 XDOT = 1264
412896
YDOT = 20928
369459 feet/sec YDOT = 6378
967011 meter/sec
ZDOT = -11465
704256 ZDOT = -3494
746657
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 08245
74786508
00020000 00000-0 20000-3 0 9058
2 25544 51
6430 343
5643 0006726 68
8895 291
2986 15
71856958 40583
Satellite: ISS
Catalog Number: 25544
Epoch time: 08245
74786508 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 343
5643 deg
Eccentricity:
0006726
Arg of perigee: 68
8895 deg
Mean anomaly: 291
2986 deg
Mean motion: 15
71856958 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4058
Checksum: 343
Coasting Arc #7 (Orbit 4073)
---------------------------------------
Vector Time (GMT): 2008/246/17:24:57
822
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3472774
43 A = 6732590
44 meter
Y = 4491741
12 meter E =
0018704
Z = 3605222
34 I = 51
51999
XDOT = -6204
388294 Wp = 80
48076
YDOT = -1257
151442 meter/sec RA = 338
02250 deg
ZDOT = -4387
832439 TA = 56
30267
MA = 56
12449
Ha = 195
801 n
mi
Hp = 184
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11393616
90 X = -3540257
23
Y = 14736683
46 feet Y = 4452529
44 meter
Z = 11828157
29 Z = 3588187
43
XDOT = -20355
604639 XDOT = -6168
554186
YDOT = -4124
512604 feet/sec YDOT = -1326
332374 meter/sec
ZDOT = -14395
775719 ZDOT = -4417
886265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7843791
14 X = -2390787
54
Y = -16941170
36 feet Y = -5163668
72 meter
Z = 11762709
63 Z = 3585273
89
XDOT = 11723
026159 XDOT = 3573
178373
YDOT = -15555
051649 feet/sec YDOT = -4741
179742 meter/sec
ZDOT = -14512
046261 ZDOT = -4423
271700
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 08246
76508095
00020000 00000-0 20000-3 0 9065
2 25544 51
6417 338
3569 0006784 71
2936 288
8962 15
71897629 40749
Satellite: ISS
Catalog Number: 25544
Epoch time: 08246
76508095 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 338
3569 deg
Eccentricity:
0006784
Arg of perigee: 71
2936 deg
Mean anomaly: 288
8962 deg
Mean motion: 15
71897629 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4074
Checksum: 346
Coasting Arc #8 (Orbit 4089)
---------------------------------------
Vector Time (GMT): 2008/247/17:24:57
822
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5848778
87 A = 6733321
11 meter
Y = -23594
04 meter E =
0019207
Z = 3317426
43 I = 51
49539
XDOT = -2641
328326 Wp = 83
94600
YDOT = 5525
218640 meter/sec RA = 332
94548 deg
ZDOT = 4674
952851 TA = 315
13703
MA = 315
29212
Ha = 195
683 n
mi
Hp = 184
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19188907
07 X = 5832492
49
Y = -77408
26 feet Y = 41719
46 meter
Z = 10883944
97 Z = 3345800
34
XDOT = -8665
775349 XDOT = -2725
626063
YDOT = 18127
357743 feet/sec YDOT = 5495
210654 meter/sec
ZDOT = 15337
771821 ZDOT = 4661
916231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8404041
80 X = -2561551
94
Y = 17181184
39 feet Y = 5236825
00 meter
Z = 10993606
73 Z = 3350851
33
XDOT = -11120
531122 XDOT = -3389
537886
YDOT = -15265
579278 feet/sec YDOT = -4652
948564 meter/sec
ZDOT = 15287
869355 ZDOT = 4659
742579
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 08247
78228664
00020000 00000-0 20000-3 0 9070
2 25544 51
6411 333
1500 0006743 74
9120 285
2787 15
71889326 40900
Satellite: ISS
Catalog Number: 25544
Epoch time: 08247
78228664 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 333
1500 deg
Eccentricity:
0006743
Arg of perigee: 74
9120 deg
Mean anomaly: 285
2787 deg
Mean motion: 15
71889326 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4090
Checksum: 302
Coasting Arc #9 (Orbit 4104)
---------------------------------------
Vector Time (GMT): 2008/248/17:24:57
822
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1097558
08 A = 6729557
37 meter
Y = -4912422
84 meter E =
0015756
Z = -4481043
68 I = 51
45692
XDOT = 6870
617185 Wp = 96
72754
YDOT = -1348
176234 meter/sec RA = 327
76595 deg
ZDOT = 3168
527248 TA = 205
04587
MA = 205
12239
Ha = 195
792 n
mi
Hp = 184
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3600912
34 X = 1174176
23
Y = -16116872
85 feet Y = -4899721
04 meter
Z = -14701586
88 Z = -4475525
48
XDOT = 22541
394963 XDOT = 6869
789852
YDOT = -4423
150374 feet/sec YDOT = -1271
349576 meter/sec
ZDOT = 10395
430603 ZDOT = 3201
902907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12994169
79 X = 3960622
95
Y = 10221827
14 feet Y = 3115612
91 meter
Z = -14680688
62 Z = -4474673
89
XDOT = -4867
818424 XDOT = -1483
711056
YDOT = 21266
739032 feet/sec YDOT = 6482
102057 meter/sec
ZDOT = 10524
305892 ZDOT = 3207
808436
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 08248
73590617
00020000 00000-0 20000-3 0 9087
2 25544 51
6411 328
2682 0006733 77
5252 282
6663 15
71879115 41056
Satellite: ISS
Catalog Number: 25544
Epoch time: 08248
73590617 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 328
2682 deg
Eccentricity:
0006733
Arg of perigee: 77
5252 deg
Mean anomaly: 282
6663 deg
Mean motion: 15
71879115 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4105
Checksum: 305
Coasting Arc #10 (Orbit 4120)
---------------------------------------
Vector Time (GMT): 2008/249/17:24:57
822
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5930891
14 A = 6735946
19 meter
Y = 2313448
76 meter E =
0011362
Z = -2204436
21 I = 51
45391
XDOT = -88
198754 Wp = 106
81805
YDOT = -5409
826570 meter/sec RA = 322
67546 deg
ZDOT = -5466
515072 TA = 97
91396
MA = 97
78498
Ha = 195
751 n
mi
Hp = 184
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19458304
28 X = -5945610
89
Y = 7590054
98 feet Y = 2247043
79 meter
Z = -7232402
26 Z = -2233284
40
XDOT = -289
365990 XDOT = -1
143167
YDOT = -17748
774837 feet/sec YDOT = -5410
326157 meter/sec
ZDOT = -17934
760735 ZDOT = -5466
732035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1081990
66 X = 329790
75
Y = -20819260
75 feet Y = -6345710
68 meter
Z = -7343695
30 Z = -2238358
33
XDOT = 14731
790564 XDOT = 4490
249764
YDOT = 7062
157623 feet/sec YDOT = 2152
545643 meter/sec
ZDOT = -17936
070945 ZDOT = -5466
914424
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 08249
75308991
00020000 00000-0 20000-3 0 9093
2 25544 51
6401 323
0597 0006814 81
3155 278
8779 15
71912927 41210
Satellite: ISS
Catalog Number: 25544
Epoch time: 08249
75308991 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 323
0597 deg
Eccentricity:
0006814
Arg of perigee: 81
3155 deg
Mean anomaly: 278
8779 deg
Mean motion: 15
71912927 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4121
Checksum: 315
Coasting Arc #11 (Orbit 4136)
---------------------------------------
Vector Time (GMT): 2008/250/17:24:57
822
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1217421
43 A = 6727091
59 meter
Y = 4309786
68 meter E =
0011810
Z = 5011177
32 I = 51
40123
XDOT = -6392
059046 Wp = 70
53775
YDOT = 3907
208669 meter/sec RA = 317
50594 deg
ZDOT = -1800
120777 TA = 36
89695
MA = 36
81576
Ha = 195
659 n
mi
Hp = 184
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3994164
80 X = 1144794
73
Y = 14139720
08 feet Y = 4322994
49 meter
Z = 16440870
46 Z = 5016915
18
XDOT = -20971
322331 XDOT = -6426
530313
YDOT = 12818
926080 feet/sec YDOT = 3835
536253 meter/sec
ZDOT = -5905
908060 ZDOT = -1831
257231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14527827
11 X = -4428081
70
Y = -2021187
66 feet Y = -616058
00 meter
Z = 16463423
02 Z = 5018051
34
XDOT = -3622
225386 XDOT = -1104
054298
YDOT = -23243
184299 feet/sec YDOT = -7084
522574 meter/sec
ZDOT = -6025
907343 ZDOT = -1836
696558
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 08250
77026158
00020000 00000-0 20000-3 0 9101
2 25544 51
6396 317
8520 0006674 83
9625 276
2297 15
71939889 41374
Satellite: ISS
Catalog Number: 25544
Epoch time: 08250
77026158 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 317
8520 deg
Eccentricity:
0006674
Arg of perigee: 83
9625 deg
Mean anomaly: 276
2297 deg
Mean motion: 15
71939889 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4137
Checksum: 327
Coasting Arc #12 (Orbit 4152)
---------------------------------------
Vector Time (GMT): 2008/251/17:24:57
822
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5008219
85 A = 6737487
23 meter
Y = -4401314
01 meter E =
0019598
Z = 916471
82 I = 51
41615
XDOT = 2578
642749 Wp = 65
91437
YDOT = 4187
132349 meter/sec RA = 312
39432 deg
ZDOT = 5925
425230 TA = 304
11806
MA = 304
30383
Ha = 195
610 n
mi
Hp = 184
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16431167
48 X = 5052611
76
Y = -14440006
59 feet Y = -4345061
01 meter
Z = 3006797
32 Z = 940909
56
XDOT = 8460
114007 XDOT = 2502
845220
YDOT = 13737
310857 feet/sec YDOT = 4215
544329 meter/sec
ZDOT = 19440
371489 ZDOT = 5937
768243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7112070
25 X = 2167759
01
Y = 20672227
31 feet Y = 6300894
88 meter
Z = 3100864
40 Z = 945143
47
XDOT = -14372
849476 XDOT = -4380
844520
YDOT = 1977
805247 feet/sec YDOT = 602
835039 meter/sec
ZDOT = 19488
444382 ZDOT = 5940
077848
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 08251
78742089
00020000 00000-0 20000-3 0 9112
2 25544 51
6396 312
6449 0006722 89
3747 270
8185 15
72003834 41533
Satellite: ISS
Catalog Number: 25544
Epoch time: 08251
78742089 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 312
6449 deg
Eccentricity:
0006722
Arg of perigee: 89
3747 deg
Mean anomaly: 270
8185 deg
Mean motion: 15
72003834 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4153
Checksum: 307
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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