Date:
May 26th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 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 2463)
---------------------------------------
Vector Time (GMT): 2008/144/12:23:29
943
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1488663
28 A = 6713593
70 meter
Y = -3996881
51 meter E =
0002249
Z = 5186653
94 I = 51
81192
XDOT = 6550
993734 Wp = 276
26149
YDOT = -3895
144356 meter/sec RA = 142
61786 deg
ZDOT = -1121
551983 TA = 184
41205
MA = 184
41403
Ha = 184
928 n
mi
Hp = 182
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4884065
87 X = -1469054
89
Y = -13113128
32 feet Y = -4013419
82 meter
Z = 17016581
16 Z = 5179468
92
XDOT = 21492
761595 XDOT = 6599
511300
YDOT = -12779
345001 feet/sec YDOT = -3821
615936 meter/sec
ZDOT = -3679
632490 ZDOT = -1089
609816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14012843
15 X = -4271114
59
Y = -633600
39 feet Y = -193121
40 meter
Z = 16988556
32 Z = 5178111
97
XDOT = -3235
916246 XDOT = -986
307272
YDOT = -23796
753658 feet/sec YDOT = -7253
250515 meter/sec
ZDOT = -3557
197883 ZDOT = -1084
233915
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 08144
56204941
00020000 00000-0 20000-3 0 9007
2 25544 51
6336 143
3443 0005688 251
0919 108
9629 15
76422474 24645
Satellite: ISS
Catalog Number: 25544
Epoch time: 08144
56204941 = yrday
fracday
Element set: 900
Inclination: 51
6336 deg
RA of node: 143
3443 deg
Eccentricity:
0005688
Arg of perigee: 251
0919 deg
Mean anomaly: 108
9629 deg
Mean motion: 15
76422474 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2464
Checksum: 294
Coasting Arc #2 (Orbit 2479)
---------------------------------------
Vector Time (GMT): 2008/145/12:23:29
943
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5607788
31 A = 6723775
86 meter
Y = 3248769
30 meter E =
0008466
Z = 1774419
69 I = 51
86956
XDOT = -1116
548397 Wp = 59
43263
YDOT = -5053
325188 meter/sec RA = 137
50432 deg
ZDOT = 5707
597682 TA = 320
18326
MA = 320
24535
Ha = 184
637 n
mi
Hp = 182
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18398255
62 X = -5652319
62
Y = 10658691
94 feet Y = 3185810
54 meter
Z = 5821586
92 Z = 1747069
29
XDOT = -3663
216527 XDOT = -1087
684920
YDOT = -16579
150879 feet/sec YDOT = -5065
650589 meter/sec
ZDOT = 18725
714179 ZDOT = 5702
242778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2830204
17 X = 862646
23
Y = 21102211
73 feet Y = 6431954
14 meter
Z = 5716730
06 Z = 1742459
32
XDOT = -15225
767602 XDOT = -4640
813965
YDOT = -3039
450732 feet/sec YDOT = -926
424583 meter/sec
ZDOT = 18704
620957 ZDOT = 5701
168468
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 08145
57630880
00020000 00000-0 20000-3 0 9015
2 25544 51
6338 138
1167 0005781 253
7300 106
3228 15
76493036 24806
Satellite: ISS
Catalog Number: 25544
Epoch time: 08145
57630880 = yrday
fracday
Element set: 901
Inclination: 51
6338 deg
RA of node: 138
1167 deg
Eccentricity:
0005781
Arg of perigee: 253
7300 deg
Mean anomaly: 106
3228 deg
Mean motion: 15
76493036 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2480
Checksum: 283
Coasting Arc #3 (Orbit 2494)
---------------------------------------
Vector Time (GMT): 2008/146/12:23:29
943
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 515738
74 A = 6715885
91 meter
Y = 4838250
31 meter E =
0006483
Z = -4635134
23 I = 51
86334
XDOT = -6235
661952 Wp = 135
53747
YDOT = 3453
989344 meter/sec RA = 132
32734 deg
ZDOT = 2909
426872 TA = 163
18740
MA = 163
16590
Ha = 184
476 n
mi
Hp = 182
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1692056
24 X = 484115
02
Y = 15873524
65 feet Y = 4843841
45 meter
Z = -15207133
29 Z = -4632704
88
XDOT = -20458
208505 XDOT = -6287
955049
YDOT = 11331
986036 feet/sec YDOT = 3383
965801 meter/sec
ZDOT = 9545
363754 ZDOT = 2879
007443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15426873
30 X = 4702110
98
Y = 4140292
53 feet Y = 1261961
16 meter
Z = -15197312
26 Z = -4632140
78
XDOT = 3361
597774 XDOT = 1024
615002
YDOT = 22108
735199 feet/sec YDOT = 6738
742489 meter/sec
ZDOT = 9428
711477 ZDOT = 2873
871258
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 08146
52716762
00020000 00000-0 20000-3 0 9026
2 25544 51
6338 133
2149 0005649 259
9177 100
1350 15
76441525 24955
Satellite: ISS
Catalog Number: 25544
Epoch time: 08146
52716762 = yrday
fracday
Element set: 902
Inclination: 51
6338 deg
RA of node: 133
2149 deg
Eccentricity:
0005649
Arg of perigee: 259
9177 deg
Mean anomaly: 100
1350 deg
Mean motion: 15
76441525 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2495
Checksum: 293
Coasting Arc #4 (Orbit 2510)
---------------------------------------
Vector Time (GMT): 2008/147/12:23:29
943
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5236204
65 A = 6720582
02 meter
Y = -2682096
81 meter E =
0001578
Z = -3246614
36 I = 51
89870
XDOT = 124
951986 Wp = 220
43188
YDOT = 6035
280314 meter/sec RA = 127
23685 deg
ZDOT = -4784
235665 TA = 357
44667
MA = 357
44748
Ha = 184
359 n
mi
Hp = 182
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17179149
11 X = 5281578
59
Y = -8799530
22 feet Y = -2623288
47 meter
Z = -10651621
92 Z = -3221066
97
XDOT = 409
947460 XDOT = 80
696226
YDOT = 19800
788432 feet/sec YDOT = 6036
430756 meter/sec
ZDOT = -15696
311236 ZDOT = -4783
735382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2228150
82 X = -679140
37
Y = -19226761
44 feet Y = -5860316
89 meter
Z = -10553621
85 Z = -3216743
94
XDOT = 17327
419755 XDOT = 5281
397541
YDOT = 6606
529115 feet/sec YDOT = 2013
670074 meter/sec
ZDOT = -15693
792275 ZDOT = -4783
467885
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 08147
54140095
00020000 00000-0 20000-3 0 9030
2 25544 51
6342 127
9863 0005610 264
3341 95
7184 15
76491877 25112
Satellite: ISS
Catalog Number: 25544
Epoch time: 08147
54140095 = yrday
fracday
Element set: 903
Inclination: 51
6342 deg
RA of node: 127
9863 deg
Eccentricity:
0005610
Arg of perigee: 264
3341 deg
Mean anomaly: 95
7184 deg
Mean motion: 15
76491877 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2511
Checksum: 294
Coasting Arc #5 (Orbit 2526)
---------------------------------------
Vector Time (GMT): 2008/148/12:23:29
943
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 221183
75 A = 6719368
94 meter
Y = -5667550
05 meter E =
0006317
Z = 3598065
80 I = 51
91153
XDOT = 5734
434117 Wp = 83
42185
YDOT = -2600
139829 meter/sec RA = 122
05011 deg
ZDOT = -4440
845459 TA = 53
68713
MA = 53
62882
Ha = 184
162 n
mi
Hp = 181
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 725668
46 X = 267063
94
Y = -18594324
32 feet Y = -5664820
52 meter
Z = 11804677
81 Z = 3599251
13
XDOT = 18813
760225 XDOT = 5784
655976
YDOT = -8530
642482 feet/sec YDOT = -2535
732811 meter/sec
ZDOT = -14569
702948 ZDOT = -4412
865793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17314479
18 X = -5277453
26
Y = -6811004
56 feet Y = -2075994
19 meter
Z = 11808680
59 Z = 3599285
84
XDOT = -2250
087916 XDOT = -685
826797
YDOT = -19395
873289 feet/sec YDOT = -5911
862178 meter/sec
ZDOT = -14462
330844 ZDOT = -4408
118441
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 08148
55561910
00020000 00000-0 20000-3 0 9046
2 25544 51
6340 122
7582 0005752 269
1343 90
9162 15
76518967 25273
Satellite: ISS
Catalog Number: 25544
Epoch time: 08148
55561910 = yrday
fracday
Element set: 904
Inclination: 51
6340 deg
RA of node: 122
7582 deg
Eccentricity:
0005752
Arg of perigee: 269
1343 deg
Mean anomaly: 90
9162 deg
Mean motion: 15
76518967 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2527
Checksum: 301
Coasting Arc #6 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2008/149/12:23:29
943
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4760963
59 A = 6716528
37 meter
Y = 1753983
29 meter E =
0004294
Z = 4400185
70 I = 51
91744
XDOT = 562
872855 Wp = 136
12645
YDOT = -6910
661533 meter/sec RA = 116
96513 deg
ZDOT = 3358
753263 TA = 280
21659
MA = 280
26501
Ha = 184
153 n
mi
Hp = 181
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15619959
30 X = -4801598
50
Y = 5754538
34 feet Y = 1700515
83 meter
Z = 14436304
79 Z = 4376958
26
XDOT = 1846
695718 XDOT = 623
790812
YDOT = -22672
774057 feet/sec YDOT = -6904
026886 meter/sec
ZDOT = 11019
531702 ZDOT = 3361
635009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 486737
67 X = 148357
64
Y = 16716095
76 feet Y = 5095065
99 meter
Z = 14347123
92 Z = 4373003
37
XDOT = -19722
361116 XDOT = -6011
375668
YDOT = -8906
605385 feet/sec YDOT = -2714
733321 meter/sec
ZDOT = 11029
941907 ZDOT = 3361
926293
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 08149
56982136
00020000 00000-0 20000-3 0 9056
2 25544 51
6347 117
5301 0005870 271
8574 88
1919 15
76571789 25436
Satellite: ISS
Catalog Number: 25544
Epoch time: 08149
56982136 = yrday
fracday
Element set: 905
Inclination: 51
6347 deg
RA of node: 117
5301 deg
Eccentricity:
0005870
Arg of perigee: 271
8574 deg
Mean anomaly: 88
1919 deg
Mean motion: 15
76571789 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2543
Checksum: 324
Coasting Arc #7 (Orbit 2557)
---------------------------------------
Vector Time (GMT): 2008/150/12:23:29
943
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -692435
48 A = 6722856
74 meter
Y = 6319513
87 meter E =
0005513
Z = -2175264
25 I = 51
95050
XDOT = -5194
907112 Wp = 343
95884
YDOT = 1333
890249 meter/sec RA = 111
78675 deg
ZDOT = 5530
712165 TA = 351
76667
MA = 351
77571
Ha = 184
212 n
mi
Hp = 181
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2271769
95 X = -752482
66
Y = 20733313
21 feet Y = 6311435
12 meter
Z = -7136693
73 Z = -2178773
40
XDOT = -17043
658503 XDOT = -5236
304263
YDOT = 4376
280345 feet/sec YDOT = 1275
565844 meter/sec
ZDOT = 18145
381118 ZDOT = 5505
374609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19106591
64 X = 5823689
13
Y = 8353757
01 feet Y = 2546225
14 meter
Z = -7149581
29 Z = -2179192
38
XDOT = -365
104867 XDOT = -111
283963
YDOT = 16276
251408 feet/sec YDOT = 4961
001429 meter/sec
ZDOT = 18048
036632 ZDOT = 5501
041566
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 08150
52062455
00020000 00000-0 20000-3 0 9068
2 25544 51
6344 112
6278 0005738 276
9872 83
0639 15
76549255 25584
Satellite: ISS
Catalog Number: 25544
Epoch time: 08150
52062455 = yrday
fracday
Element set: 906
Inclination: 51
6344 deg
RA of node: 112
6278 deg
Eccentricity:
0005738
Arg of perigee: 276
9872 deg
Mean anomaly: 83
0639 deg
Mean motion: 15
76549255 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2558
Checksum: 314
Coasting Arc #8 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2008/151/12:23:29
943
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4329902
07 A = 6713555
22 meter
Y = -493430
00 meter E =
0008730
Z = -5114428
02 I = 51
92974
XDOT = -976
777725 Wp = 63
44660
YDOT = 7478
297627 meter/sec RA = 106
68486 deg
ZDOT = -1546
635683 TA = 191
75879
MA = 191
77920
Ha = 184
264 n
mi
Hp = 182
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14205715
44 X = 4359943
21
Y = -1618864
82 feet Y = -444842
08 meter
Z = -16779619
49 Z = -5093320
11
XDOT = -3204
651328 XDOT = -1052
815238
YDOT = 24535
097200 feet/sec YDOT = 7466
949745 meter/sec
ZDOT = -5074
264053 ZDOT = -1551
564898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2506557
11 X = 763998
61
Y = -14172411
88 feet Y = -4319751
14 meter
Z = -16698461
54 Z = -5089691
08
XDOT = 21591
345997 XDOT = 6581
042260
YDOT = 9825
866143 feet/sec YDOT = 2994
924000 meter/sec
ZDOT = -5092
512832 ZDOT = -1552
197911
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 08151
53479850
00020000 00000-0 20000-3 0 9072
2 25544 51
6351 107
3988 0005822 280
9258 79
1251 15
76580185 25749
Satellite: ISS
Catalog Number: 25544
Epoch time: 08151
53479850 = yrday
fracday
Element set: 907
Inclination: 51
6351 deg
RA of node: 107
3988 deg
Eccentricity:
0005822
Arg of perigee: 280
9258 deg
Mean anomaly: 79
1251 deg
Mean motion: 15
76580185 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2574
Checksum: 313
Coasting Arc #9 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2008/152/12:23:29
943
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 970547
26 A = 6724690
41 meter
Y = -6631981
83 meter E =
0008233
Z = 479696
87 I = 51
97536
XDOT = 4771
093281 Wp = 147
59121
YDOT = 258
107098 meter/sec RA = 101
53400 deg
ZDOT = -6044
098409 TA = 27
20948
MA = 27
16637
Ha = 184
384 n
mi
Hp = 181
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3184210
16 X = 1042304
66
Y = -21758470
57 feet Y = -6620727
45 meter
Z = 1573808
64 Z = 484585
40
XDOT = 15653
193178 XDOT = 4797
214196
YDOT = 846
808065 feet/sec YDOT = 311
606959 meter/sec
ZDOT = -19829
719191 ZDOT = -6020
856501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20118169
89 X = -6132018
18
Y = -8875353
74 feet Y = -2705207
82 meter
Z = 1591994
32 Z = 485239
87
XDOT = 4382
675576 XDOT = 1335
839516
YDOT = -13498
892347 feet/sec YDOT = -4114
462387 meter/sec
ZDOT = -19740
276362 ZDOT = -6016
836235
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 08152
54895733
00020000 00000-0 20000-3 0 9087
2 25544 51
6358 102
1701 0005825 284
8879 75
1640 15
76599186 25904
Satellite: ISS
Catalog Number: 25544
Epoch time: 08152
54895733 = yrday
fracday
Element set: 908
Inclination: 51
6358 deg
RA of node: 102
1701 deg
Eccentricity:
0005825
Arg of perigee: 284
8879 deg
Mean anomaly: 75
1640 deg
Mean motion: 15
76599186 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2590
Checksum: 323
Coasting Arc #10 (Orbit 2605)
---------------------------------------
Vector Time (GMT): 2008/153/12:23:29
943
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4043834
88 A = 6712638
98 meter
Y = -974549
55 meter E =
0004212
Z = 5271339
21 I = 51
94023
XDOT = 1218
958320 Wp = 312
58524
YDOT = -7591
993469 meter/sec RA = 96
40215 deg
ZDOT = -465
923444 TA = 141
83532
MA = 141
80548
Ha = 184
587 n
mi
Hp = 181
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13267174
81 X = -4058244
53
Y = -3197341
03 feet Y = -1019851
38 meter
Z = 17294419
96 Z = 5251658
68
XDOT = 3999
207086 XDOT = 1306
026010
YDOT = -24908
115056 feet/sec YDOT = -7577
875490 meter/sec
ZDOT = -1528
620224 ZDOT = -459
791255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6445482
67 X = -1964583
12
Y = 12137261
62 feet Y = 3699437
34 meter
Z = 17218609
49 Z = 5248232
17
XDOT = -22223
177114 XDOT = -6773
624384
YDOT = -9653
552929 feet/sec YDOT = -2942
402933 meter/sec
ZDOT = -1505
722451 ZDOT = -458
944203
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 08153
56309975
00020000 00000-0 20000-3 0 9099
2 25544 51
6363 96
9418 0005932 289
0490 71
0032 15
76646215 26064
Satellite: ISS
Catalog Number: 25544
Epoch time: 08153
56309975 = yrday
fracday
Element set: 909
Inclination: 51
6363 deg
RA of node: 96
9418 deg
Eccentricity:
0005932
Arg of perigee: 289
0490 deg
Mean anomaly: 71
0032 deg
Mean motion: 15
76646215 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2606
Checksum: 305
Coasting Arc #11 (Orbit 2621)
---------------------------------------
Vector Time (GMT): 2008/154/12:23:29
943
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1152041
71 A = 6723935
34 meter
Y = 6490781
16 meter E =
0011513
Z = 1287002
14 I = 51
98062
XDOT = -4561
110324 Wp = 34
55103
YDOT = -1980
478110 meter/sec RA = 91
28478 deg
ZDOT = 5889
216635 TA = 339
52589
MA = 339
57200
Ha = 184
719 n
mi
Hp = 181
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3779664
41 X = -1230789
18
Y = 21295213
78 feet Y = 6477457
83 meter
Z = 4222447
95 Z = 1281215
32
XDOT = -14964
272716 XDOT = -4567
234638
YDOT = -6497
631596 feet/sec YDOT = -2031
518384 meter/sec
ZDOT = 19321
576885 ZDOT = 5867
043064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19814137
43 X = 6039349
09
Y = 8680703
69 feet Y = 2645878
49 meter
Z = 4200761
96 Z = 1280392
25
XDOT = -9211
191775 XDOT = -2807
571253
YDOT = 11690
464176 feet/sec YDOT = 3563
253481 meter/sec
ZDOT = 19236
079731 ZDOT = 5863
157102
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 08154
57722804
00020000 00000-0 20000-3 0 9103
2 25544 51
6365 91
7123 0005925 293
1210 66
9329 15
76652170 26227
Satellite: ISS
Catalog Number: 25544
Epoch time: 08154
57722804 = yrday
fracday
Element set: 910
Inclination: 51
6365 deg
RA of node: 91
7123 deg
Eccentricity:
0005925
Arg of perigee: 293
1210 deg
Mean anomaly: 66
9329 deg
Mean motion: 15
76652170 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2622
Checksum: 282
Coasting Arc #12 (Orbit 2636)
---------------------------------------
Vector Time (GMT): 2008/155/12:23:29
943
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3961842
99 A = 6714453
09 meter
Y = 2457309
68 meter E =
0006161
Z = -4837655
60 I = 51
94923
XDOT = -1441
239429 Wp = 98
61448
YDOT = 7154
508125 meter/sec RA = 86
12033 deg
ZDOT = 2455
584889 TA = 195
26519
MA = 195
28379
Ha = 184
893 n
mi
Hp = 181
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12998172
53 X = 3957571
32
Y = 8062039
65 feet Y = 2501590
43 meter
Z = -15871573
48 Z = -4818418
51
XDOT = -4728
475817 XDOT = -1533
064115
YDOT = 23472
795686 feet/sec YDOT = 7137
877418 meter/sec
ZDOT = 8056
380869 ZDOT = 2448
361724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10712524
94 X = 3265177
60
Y = -11024608
09 feet Y = -3360300
54 meter
Z = -15797330
25 Z = -4815026
26
XDOT = 21071
362764 XDOT = 6422
551370
YDOT = 8977
896288 feet/sec YDOT = 2736
462789 meter/sec
ZDOT = 8029
210309 ZDOT = 2447
303302
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 08155
52795862
00020000 00000-0 20000-3 0 9114
2 25544 51
6375 86
8104 0005935 296
9059 63
1498 15
76678865 26376
Satellite: ISS
Catalog Number: 25544
Epoch time: 08155
52795862 = yrday
fracday
Element set: 911
Inclination: 51
6375 deg
RA of node: 86
8104 deg
Eccentricity:
0005935
Arg of perigee: 296
9059 deg
Mean anomaly: 63
1498 deg
Mean motion: 15
76678865 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2637
Checksum: 342
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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