Date:
May 29th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 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 2541)
---------------------------------------
Vector Time (GMT): 2008/149/11:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1775283
29 A = 6723784
50 meter
Y = -6269352
48 meter E =
0009153
Z = 1637705
08 I = 51
94089
XDOT = 5108
728670 Wp = 130
77642
YDOT = -64
066750 meter/sec RA = 117
15961 deg
ZDOT = -5768
180444 TA = 31
18933
MA = 31
13505
Ha = 184
150 n
mi
Hp = 181
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5824420
23 X = 1837300
51
Y = -20568741
73 feet Y = -6249153
65 meter
Z = 5373048
17 Z = 1646479
48
XDOT = 16760
920833 XDOT = 5137
086321
YDOT = -210
192748 feet/sec YDOT = -6
778898 meter/sec
ZDOT = -18924
476521 ZDOT = -5743
293217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13632766
58 X = -4155267
25
Y = -16455620
64 feet Y = -5015673
17 meter
Z = 5406188
95 Z = 1647806
39
XDOT = 8212
524259 XDOT = 2503
177394
YDOT = -13005
593078 feet/sec YDOT = -3964
104770 meter/sec
ZDOT = -18828
745676 ZDOT = -5739
001682
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
50644650
00020000 00000-0 20000-3 0 9001
2 25544 51
6344 117
8609 0005717 273
1706 86
8804 15
76537762 25429
Satellite: ISS
Catalog Number: 25544
Epoch time: 08149
50644650 = yrday
fracday
Element set: 900
Inclination: 51
6344 deg
RA of node: 117
8609 deg
Eccentricity:
0005717
Arg of perigee: 273
1706 deg
Mean anomaly: 86
8804 deg
Mean motion: 15
76537762 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2542
Checksum: 302
Coasting Arc #2 (Orbit 2557)
---------------------------------------
Vector Time (GMT): 2008/150/11:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4178354
92 A = 6713185
43 meter
Y = -588044
55 meter E =
0003021
Z = 5223871
23 I = 51
91710
XDOT = 2187
113355 Wp = 247
21180
YDOT = -7328
320205 meter/sec RA = 112
04861 deg
ZDOT = 923
715381 TA = 194
02131
MA = 194
02970
Ha = 184
339 n
mi
Hp = 181
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13708513
51 X = -4196845
65
Y = -1929280
03 feet Y = -634873
18 meter
Z = 17138685
15 Z = 5203527
61
XDOT = 7175
568749 XDOT = 2264
409945
YDOT = -24043
045291 feet/sec YDOT = -7303
430550 meter/sec
ZDOT = 3030
562273 ZDOT = 934
527559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9254733
26 X = -2820842
70
Y = 10424672
97 feet Y = 3177440
32 meter
Z = 17060366
31 Z = 5199999
65
XDOT = -15290
088331 XDOT = -4660
418923
YDOT = -18604
559805 feet/sec YDOT = -5670
669828 meter/sec
ZDOT = 3071
446427 ZDOT = 936
176871
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
52064834
00020000 00000-0 20000-3 0 9016
2 25544 51
6343 112
6325 0005766 276
7756 83
2753 15
76531728 25581
Satellite: ISS
Catalog Number: 25544
Epoch time: 08150
52064834 = yrday
fracday
Element set: 901
Inclination: 51
6343 deg
RA of node: 112
6325 deg
Eccentricity:
0005766
Arg of perigee: 276
7756 deg
Mean anomaly: 83
2753 deg
Mean motion: 15
76531728 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2558
Checksum: 299
Coasting Arc #3 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2008/151/11:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1993156
32 A = 6724858
42 meter
Y = 6415735
86 meter E =
0010092
Z = 52611
37 I = 51
96662
XDOT = -4519
526378 Wp = 18
90022
YDOT = -1456
398088 meter/sec RA = 106
90731 deg
ZDOT = 6069
529552 TA = 341
66943
MA = 341
70578
Ha = 184
267 n
mi
Hp = 181
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6539226
76 X = -2065005
53
Y = 21049002
17 feet Y = 6393045
51 meter
Z = 172609
47 Z = 42754
57
XDOT = -14827
842449 XDOT = -4532
389925
YDOT = -4778
208951 feet/sec YDOT = -1507
010543 meter/sec
ZDOT = 19913
154698 ZDOT = 6047
541967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14192337
48 X = 4325824
46
Y = 16864490
00 feet Y = 5140296
55 meter
Z = 135302
57 Z = 41240
22
XDOT = -10855
329472 XDOT = -3308
704423
YDOT = 8965
759123 feet/sec YDOT = 2732
763381 meter/sec
ZDOT = 19828
426171 ZDOT = 6043
704297
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
53483742
00020000 00000-0 20000-3 0 9022
2 25544 51
6342 107
4036 0005668 279
5141 80
5383 15
76578459 25740
Satellite: ISS
Catalog Number: 25544
Epoch time: 08151
53483742 = yrday
fracday
Element set: 902
Inclination: 51
6342 deg
RA of node: 107
4036 deg
Eccentricity:
0005668
Arg of perigee: 279
5141 deg
Mean anomaly: 80
5383 deg
Mean motion: 15
76578459 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2574
Checksum: 304
Coasting Arc #4 (Orbit 2588)
---------------------------------------
Vector Time (GMT): 2008/152/11:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3755552
97 A = 6713171
04 meter
Y = 1975795
09 meter E =
0008775
Z = -5209353
14 I = 51
93509
XDOT = -2354
418611 Wp = 93
63550
YDOT = 7253
727600 meter/sec RA = 101
76437 deg
ZDOT = 1054
792100 TA = 186
38040
MA = 186
39158
Ha = 184
496 n
mi
Hp = 182
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12321368
02 X = 3758486
78
Y = 6482267
34 feet Y = 2017808
84 meter
Z = -17091053
60 Z = -5191100
95
XDOT = -7724
470508 XDOT = -2440
480036
YDOT = 23798
318898 feet/sec YDOT = 7226
917826 meter/sec
ZDOT = 3460
604003 ZDOT = 1043
145914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12037137
97 X = 3668919
65
Y = -7165536
27 feet Y = -2184055
46 meter
Z = -17020646
66 Z = -5187893
10
XDOT = 15665
554915 XDOT = 4774
861138
YDOT = 18208
283693 feet/sec YDOT = 5549
884870 meter/sec
ZDOT = 3416
478635 ZDOT = 1041
342688
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
48563171
00020000 00000-0 20000-3 0 9033
2 25544 51
6349 102
5014 0005799 284
8013 75
2508 15
76560020 25892
Satellite: ISS
Catalog Number: 25544
Epoch time: 08152
48563171 = yrday
fracday
Element set: 903
Inclination: 51
6349 deg
RA of node: 102
5014 deg
Eccentricity:
0005799
Arg of perigee: 284
8013 deg
Mean anomaly: 75
2508 deg
Mean motion: 15
76560020 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2589
Checksum: 287
Coasting Arc #5 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2008/153/11:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2109783
09 A = 6723463
10 meter
Y = -6130256
51 meter E =
0004112
Z = -1771099
93 I = 51
97575
XDOT = 4142
779526 Wp = 193
01256
YDOT = 3077
486053 meter/sec RA = 96
65667 deg
ZDOT = -5718
386227 TA = 6
53158
MA = 6
52622
Ha = 184
587 n
mi
Hp = 181
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6921860
53 X = 2186779
65
Y = -20112390
14 feet Y = -6106232
94 meter
Z = -5810695
30 Z = -1760664
25
XDOT = 13591
796345 XDOT = 4135
838175
YDOT = 10096
739020 feet/sec YDOT = 3123
775017 meter/sec
ZDOT = -18761
109669 ZDOT = -5698
276572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13746940
57 X = -4190067
49
Y = -16245015
37 feet Y = -4951480
68 meter
Z = -5771106
54 Z = -1759033
27
XDOT = 14489
033193 XDOT = 4416
257317
YDOT = -5625
216207 feet/sec YDOT = -1714
565900 meter/sec
ZDOT = -18683
455205 ZDOT = -5694
717146
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
49980053
00020000 00000-0 20000-3 0 9048
2 25544 51
6358 97
2728 0005866 289
3318 70
7212 15
76591359 26057
Satellite: ISS
Catalog Number: 25544
Epoch time: 08153
49980053 = yrday
fracday
Element set: 904
Inclination: 51
6358 deg
RA of node: 97
2728 deg
Eccentricity:
0005866
Arg of perigee: 289
3318 deg
Mean anomaly: 70
7212 deg
Mean motion: 15
76591359 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2605
Checksum: 317
Coasting Arc #6 (Orbit 2620)
---------------------------------------
Vector Time (GMT): 2008/154/11:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3529954
11 A = 6715545
78 meter
Y = -3361693
01 meter E =
0006241
Z = 4620212
71 I = 51
95191
XDOT = 2482
161679 Wp = 19
51281
YDOT = -6669
500757 meter/sec RA = 91
48618 deg
ZDOT = -2949
444292 TA = 99
61320
MA = 99
54269
Ha = 184
783 n
mi
Hp = 181
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11581214
26 X = -3514545
38
Y = -11029176
54 feet Y = -3401081
67 meter
Z = 15158178
18 Z = 4603100
65
XDOT = 8143
575062 XDOT = 2570
884763
YDOT = -21881
564163 feet/sec YDOT = -6641
247189 meter/sec
ZDOT = -9676
654501 ZDOT = -2937
171408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15360947
98 X = -4682016
95
Y = 4670057
12 feet Y = 1423433
41 meter
Z = 15092033
26 Z = 4600051
74
XDOT = -14604
353652 XDOT = -4451
406993
YDOT = -16842
902998 feet/sec YDOT = -5133
716834 meter/sec
ZDOT = -9630
028091 ZDOT = -2935
232562
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
51395864
00020000 00000-0 20000-3 0 9053
2 25544 51
6365 92
0446 0005892 293
0681 66
9862 15
76604706 26216
Satellite: ISS
Catalog Number: 25544
Epoch time: 08154
51395864 = yrday
fracday
Element set: 905
Inclination: 51
6365 deg
RA of node: 92
0446 deg
Eccentricity:
0005892
Arg of perigee: 293
0681 deg
Mean anomaly: 66
9862 deg
Mean motion: 15
76604706 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2621
Checksum: 311
Coasting Arc #7 (Orbit 2636)
---------------------------------------
Vector Time (GMT): 2008/155/11:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2250565
51 A = 6719970
70 meter
Y = 5395377
95 meter E =
0008020
Z = 3304530
72 I = 51
96732
XDOT = -4001
584453 Wp = 68
31896
YDOT = -4575
195148 meter/sec RA = 86
40091 deg
ZDOT = 4738
511741 TA = 330
34494
MA = 330
39038
Ha = 184
941 n
mi
Hp = 181
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7383745
11 X = -2326783
27
Y = 17701371
23 feet Y = 5369783
98 meter
Z = 10841636
21 Z = 3293413
31
XDOT = -13128
557917 XDOT = -3973
145679
YDOT = -15010
482768 feet/sec YDOT = -4619
785153 meter/sec
ZDOT = 15546
298363 ZDOT = 4719
139842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11947424
56 X = 3641575
00
Y = 15034390
64 feet Y = 4582482
27 meter
Z = 10799326
62 Z = 3291634
75
XDOT = -18418
182510 XDOT = -5613
862029
YDOT = 3508
541370 feet/sec YDOT = 1069
403410 meter/sec
ZDOT = 15471
351041 ZDOT = 4715
667797
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
52810507
00020000 00000-0 20000-3 0 9062
2 25544 51
6372 86
8160 0005908 296
5616 63
4943 15
76633160 26377
Satellite: ISS
Catalog Number: 25544
Epoch time: 08155
52810507 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 86
8160 deg
Eccentricity:
0005908
Arg of perigee: 296
5616 deg
Mean anomaly: 63
4943 deg
Mean motion: 15
76633160 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2637
Checksum: 301
Coasting Arc #8 (Orbit 2651)
---------------------------------------
Vector Time (GMT): 2008/156/11:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3486632
56 A = 6719359
85 meter
Y = 4538091
09 meter E =
0002621
Z = -3518691
01 I = 51
96230
XDOT = -2721
945210 Wp = 359
78749
YDOT = 5603
264996 meter/sec RA = 81
21721 deg
ZDOT = 4531
993367 TA = 318
52923
MA = 318
54911
Ha = 185
159 n
mi
Hp = 181
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11439083
20 X = 3452721
08
Y = 14888750
31 feet Y = 4576891
81 meter
Z = -11544261
83 Z = -3501834
14
XDOT = -8930
266438 XDOT = -2806
415279
YDOT = 18383
415340 feet/sec YDOT = 5572
353318 meter/sec
ZDOT = 14868
744642 ZDOT = 4518
566144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18531857
09 X = 5648510
04
Y = -3255828
37 feet Y = -992376
49 meter
Z = -11478995
86 Z = -3498797
94
XDOT = 11840
337110 XDOT = 3608
934751
YDOT = 15181
851032 feet/sec YDOT = 4627
428195 meter/sec
ZDOT = 14817
549987 ZDOT = 4516
389236
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 08156
47885828
00020000 00000-0 20000-3 0 9076
2 25544 51
6374 81
9144 0006017 300
8876 59
1696 15
76629282 26520
Satellite: ISS
Catalog Number: 25544
Epoch time: 08156
47885828 = yrday
fracday
Element set: 907
Inclination: 51
6374 deg
RA of node: 81
9144 deg
Eccentricity:
0006017
Arg of perigee: 300
8876 deg
Mean anomaly: 59
1696 deg
Mean motion: 15
76629282 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2652
Checksum: 328
Coasting Arc #9 (Orbit 2667)
---------------------------------------
Vector Time (GMT): 2008/157/11:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2561655
31 A = 6715856
95 meter
Y = -4293327
91 meter E =
0008123
Z = -4491516
13 I = 51
94606
XDOT = 4001
302792 Wp = 31
81356
YDOT = 5743
663001 meter/sec RA = 76
13302 deg
ZDOT = -3204
009916 TA = 206
25884
MA = 206
30005
Ha = 185
197 n
mi
Hp = 181
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8404380
95 X = 2631292
57
Y = -14085721
48 feet Y = -4264291
64 meter
Z = -14735945
31 Z = -4478903
41
XDOT = 13127
633832 XDOT = 3952
343369
YDOT = 18844
038716 feet/sec YDOT = 5788
134830 meter/sec
ZDOT = -10511
843555 ZDOT = -3184
689203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8759372
88 X = -2669856
85
Y = -13918773
44 feet Y = -4242442
14 meter
Z = -14687763
12 Z = -4476830
20
XDOT = 21747
520514 XDOT = 6628
644253
YDOT = -2658
160099 feet/sec YDOT = -810
207198 meter/sec
ZDOT = -10436
988837 ZDOT = -3181
194198
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 08157
49298395
00020000 00000-0 20000-3 0 9087
2 25544 51
6383 76
6858 0005972 305
4452 54
6155 15
76670128 26685
Satellite: ISS
Catalog Number: 25544
Epoch time: 08157
49298395 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 76
6858 deg
Eccentricity:
0005972
Arg of perigee: 305
4452 deg
Mean anomaly: 54
6155 deg
Mean motion: 15
76670128 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2668
Checksum: 334
Coasting Arc #10 (Orbit 2683)
---------------------------------------
Vector Time (GMT): 2008/158/11:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3501125
76 A = 6722898
32 meter
Y = -5380771
68 meter E =
0008559
Z = 1986323
75 I = 51
96169
XDOT = 3212
894335 Wp = 100
18366
YDOT = -4172
924887 meter/sec RA = 70
95819 deg
ZDOT = -5622
118358 TA = 57
77304
MA = 57
69011
Ha = 185
341 n
mi
Hp = 181
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11486633
06 X = -3450346
06
Y = -17653450
39 feet Y = -5419639
76 meter
Z = 6516810
22 Z = 1969437
60
XDOT = 10540
991913 XDOT = 3286
628943
YDOT = -13690
698448 feet/sec YDOT = -4136
583035 meter/sec
ZDOT = -18445
270205 ZDOT = -5606
331951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20907138
37 X = -6372495
78
Y = 2706929
64 feet Y = 825072
16 meter
Z = 6451353
51 Z = 1966372
55
XDOT = -7506
670170 XDOT = -2288
033068
YDOT = -14013
132648 feet/sec YDOT = -4271
202831 meter/sec
ZDOT = -18384
854159 ZDOT = -5603
703548
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 08158
50709877
00020000 00000-0 20000-3 0 9093
2 25544 51
6385 71
4573 0006008 309
0127 51
0502 15
76672906 26845
Satellite: ISS
Catalog Number: 25544
Epoch time: 08158
50709877 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 71
4573 deg
Eccentricity:
0006008
Arg of perigee: 309
0127 deg
Mean anomaly: 51
0502 deg
Mean motion: 15
76672906 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2684
Checksum: 300
Coasting Arc #11 (Orbit 2699)
---------------------------------------
Vector Time (GMT): 2008/159/11:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3111464
56 A = 6712878
14 meter
Y = 2952323
66 meter E =
0002014
Z = 5164527
49 I = 51
91748
XDOT = -3999
330219 Wp = 324
94992
YDOT = -6459
378293 meter/sec RA = 65
85213 deg
ZDOT = 1284
919407 TA = 112
82924
MA = 112
80798
Ha = 185
490 n
mi
Hp = 181
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10208217
05 X = -3169334
80
Y = 9686101
24 feet Y = 2917204
98 meter
Z = 16943987
83 Z = 5149272
07
XDOT = -13121
162135 XDOT = -3933
045052
YDOT = -21192
186001 feet/sec YDOT = -6503
730704 meter/sec
ZDOT = 4215
614853 ZDOT = 1265
650647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4477102
89 X = 1364620
96
Y = 13414996
94 feet Y = 4088891
07 meter
Z = 16885508
08 Z = 5146702
86
XDOT = -23771
743743 XDOT = -7245
627493
YDOT = 2729
097070 feet/sec YDOT = 831
828787 meter/sec
ZDOT = 4140
891231 ZDOT = 1262
143647
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 08159
52120104
00020000 00000-0 20000-3 0 9108
2 25544 51
6384 66
2283 0006090 311
7831 48
2813 15
76721660 27001
Satellite: ISS
Catalog Number: 25544
Epoch time: 08159
52120104 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 66
2283 deg
Eccentricity:
0006090
Arg of perigee: 311
7831 deg
Mean anomaly: 48
2813 deg
Mean motion: 15
76721660 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2700
Checksum: 261
Coasting Arc #12 (Orbit 2714)
---------------------------------------
Vector Time (GMT): 2008/160/11:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 629858
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3433581
81 A = 6724508
52 meter
Y = 5767521
64 meter E =
0013674
Z = -219940
37 I = 51
94341
XDOT = -3985
615744 Wp = 16
64177
YDOT = 2600
046105 meter/sec RA = 60
70332 deg
ZDOT = 6064
973463 TA = 340
97450
MA = 341
02553
Ha = 185
680 n
mi
Hp = 181
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11265032
17 X = 3369901
70
Y = 18922315
10 feet Y = 5805561
90 meter
Z = -721589
13 Z = -203413
93
XDOT = -13076
167140 XDOT = -4043
855973
YDOT = 8530
334991 feet/sec YDOT = 2555
150094 meter/sec
ZDOT = 19898
206901 ZDOT = 6045
470419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21860066
43 X = 6662948
25
Y = -2679713
83 feet Y = -816776
77 meter
Z = -657478
93 Z = -200399
58
XDOT = 2290
699353 XDOT = 698
205163
YDOT = 13915
477395 feet/sec YDOT = 4241
437510 meter/sec
ZDOT = 19823
341878 ZDOT = 6042
154605
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 08160
47191437
00020000 00000-0 20000-3 0 9112
2 25544 51
6386 61
3259 0006149 316
7697 43
2984 15
76692609 27152
Satellite: ISS
Catalog Number: 25544
Epoch time: 08160
47191437 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 61
3259 deg
Eccentricity:
0006149
Arg of perigee: 316
7697 deg
Mean anomaly: 43
2984 deg
Mean motion: 15
76692609 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2715
Checksum: 316
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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