Date:
July 1st 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 3061)
---------------------------------------
Vector Time (GMT): 2008/182/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4488926
30 A = 6718881
16 meter
Y = -669030
36 meter E =
0011116
Z = -4962339
01 I = 51
36395
XDOT = 3185
157236 Wp = 33
24628
YDOT = -6723
379230 meter/sec RA = 307
55425 deg
ZDOT = -1967
752337 TA = 217
60691
MA = 217
68470
Ha = 188
820 n
mi
Hp = 184
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14727448
48 X = -4457005
19
Y = -2194981
49 feet Y = -719048
54 meter
Z = -16280639
79 Z = -4984068
95
XDOT = 10449
990932 XDOT = 3269
661435
YDOT = -22058
330806 feet/sec YDOT = -6687
288061 meter/sec
ZDOT = -6455
880370 ZDOT = -1952
074954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3928889
98 X = -1197525
67
Y = 14266952
20 feet Y = 4348567
03 meter
Z = -16364376
33 Z = -4987861
91
XDOT = -19606
107408 XDOT = -5975
941538
YDOT = -12762
051375 feet/sec YDOT = -3889
873259 meter/sec
ZDOT = -6396
035104 ZDOT = -1949
511500
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 08182
47752302
00020000 00000-0 20000-3 0 9008
2 25544 51
6394 308
0305 0008843 312
6866 47
3552 15
74872017 30623
Satellite: ISS
Catalog Number: 25544
Epoch time: 08182
47752302 = yrday
fracday
Element set: 900
Inclination: 51
6394 deg
RA of node: 308
0305 deg
Eccentricity:
0008843
Arg of perigee: 312
6866 deg
Mean anomaly: 47
3552 deg
Mean motion: 15
74872017 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3062
Checksum: 283
Coasting Arc #2 (Orbit 3077)
---------------------------------------
Vector Time (GMT): 2008/183/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2512162
59 A = 6728816
46 meter
Y = 6077942
21 meter E =
0006057
Z = 1416248
13 I = 51
38036
XDOT = -5020
355034 Wp = 94
45950
YDOT = -720
733679 meter/sec RA = 302
36229 deg
ZDOT = -5791
297534 TA = 69
90927
MA = 69
84409
Ha = 189
024 n
mi
Hp = 184
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8242003
24 X = -2586820
26
Y = 19940755
28 feet Y = 6049432
00 meter
Z = 4646483
37 Z = 1403864
14
XDOT = -16470
981082 XDOT = -4983
789491
YDOT = -2364
611807 feet/sec YDOT = -776
668346 meter/sec
ZDOT = -19000
319995 ZDOT = -5815
597770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18988701
19 X = 5787756
12
Y = 10267916
81 feet Y = 3129661
04 meter
Z = 4599267
10 Z = 1401856
61
XDOT = -3279
947861 XDOT = -999
728108
YDOT = 14649
248664 feet/sec YDOT = 4465
090993 meter/sec
ZDOT = -19093
966874 ZDOT = -5819
841103
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 08183
49279367
00020000 00000-0 20000-3 0 9017
2 25544 51
6391 302
8087 0008889 316
1459 43
8998 15
74881019 30780
Satellite: ISS
Catalog Number: 25544
Epoch time: 08183
49279367 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 302
8087 deg
Eccentricity:
0008889
Arg of perigee: 316
1459 deg
Mean anomaly: 43
8998 deg
Mean motion: 15
74881019 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3078
Checksum: 339
Coasting Arc #3 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2008/184/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4295963
17 A = 6717951
81 meter
Y = 621169
70 meter E =
0005141
Z = 5128614
50 I = 51
33095
XDOT = -2542
231512 Wp = 331
61297
YDOT = 7158
724185 meter/sec RA = 297
22384 deg
ZDOT = 1267
417008 TA = 106
24782
MA = 106
19126
Ha = 189
048 n
mi
Hp = 183
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14094367
37 X = 4263784
19
Y = 2037958
33 feet Y = 669028
47 meter
Z = 16826163
05 Z = 5149406
11
XDOT = -8340
654566 XDOT = -2628
249388
YDOT = 23486
627903 feet/sec YDOT = 7129
814243 meter/sec
ZDOT = 4158
192285 ZDOT = 1254
859716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3225085
29 X = 983006
00
Y = -13773168
37 feet Y = -4198061
72 meter
Z = 16906297
25 Z = 5153039
40
XDOT = 21682
915174 XDOT = 6608
952545
YDOT = 10102
675493 feet/sec YDOT = 3079
295490 meter/sec
ZDOT = 4110
393868 ZDOT = 1252
848051
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 08184
50804855
00020000 00000-0 20000-3 0 9027
2 25544 51
6404 297
5879 0009026 320
0725 39
9774 15
74934885 30944
Satellite: ISS
Catalog Number: 25544
Epoch time: 08184
50804855 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 297
5879 deg
Eccentricity:
0009026
Arg of perigee: 320
0725 deg
Mean anomaly: 39
9774 deg
Mean motion: 15
74934885 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3094
Checksum: 323
Coasting Arc #4 (Orbit 3108)
---------------------------------------
Vector Time (GMT): 2008/185/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1905286
49 A = 6729301
81 meter
Y = -6394421
24 meter E =
0015516
Z = -792680
14 I = 51
35728
XDOT = 4846
436131 Wp = 5
03873
YDOT = 709
239833 meter/sec RA = 292
04240 deg
ZDOT = 5951
593729 TA = 346
27388
MA = 346
31602
Ha = 189
341 n
mi
Hp = 183
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6250939
93 X = 1980498
96
Y = -20979072
30 feet Y = -6372694
52 meter
Z = -2600656
64 Z = -783243
14
XDOT = 15900
381006 XDOT = 4809
233769
YDOT = 2326
902339 feet/sec YDOT = 763
226115 meter/sec
ZDOT = 19526
226146 ZDOT = 5975
047170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20503085
80 X = -6249340
55
Y = -7681426
16 feet Y = -2341298
69 meter
Z = -2564820
55 Z = -781757
30
XDOT = 2837
916934 XDOT = 864
997081
YDOT = -14098
196282 feet/sec YDOT = -4297
130227 meter/sec
ZDOT = 19616
629677 ZDOT = 5979
148726
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 08185
45983828
00020000 00000-0 20000-3 0 9031
2 25544 51
6409 292
6941 0009033 324
7193 35
3372 15
74917959 31097
Satellite: ISS
Catalog Number: 25544
Epoch time: 08185
45983828 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 292
6941 deg
Eccentricity:
0009033
Arg of perigee: 324
7193 deg
Mean anomaly: 35
3372 deg
Mean motion: 15
74917959 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3109
Checksum: 320
Coasting Arc #5 (Orbit 3124)
---------------------------------------
Vector Time (GMT): 2008/186/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4179702
33 A = 6717452
39 meter
Y = -647027
57 meter E =
0013446
Z = -5228166
36 I = 51
30782
XDOT = 1823
292597 Wp = 48
87513
YDOT = -7457
023274 meter/sec RA = 286
89117 deg
ZDOT = -526
940804 TA = 216
04603
MA = 216
13677
Ha = 189
429 n
mi
Hp = 183
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13712934
16 X = -4146759
53
Y = -2122793
86 feet Y = -693582
17 meter
Z = -17152776
79 Z = -5248391
09
XDOT = 5981
931092 XDOT = 1909
102436
YDOT = -24465
299457 feet/sec YDOT = -7436
154280 meter/sec
ZDOT = -1728
808412 ZDOT = -517
876459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2814582
89 X = -857884
86
Y = 13488814
06 feet Y = 4111390
53 meter
Z = -17230745
40 Z = -5251931
20
XDOT = -23144
221706 XDOT = -7054
358776
YDOT = -7026
567368 feet/sec YDOT = -2141
697734 meter/sec
ZDOT = -1694
503334 ZDOT = -516
484616
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 08186
47506540
00020000 00000-0 20000-3 0 9047
2 25544 51
6408 287
4743 0009101 328
6919 31
3702 15
74961299 31250
Satellite: ISS
Catalog Number: 25544
Epoch time: 08186
47506540 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 287
4743 deg
Eccentricity:
0009101
Arg of perigee: 328
6919 deg
Mean anomaly: 31
3702 deg
Mean motion: 15
74961299 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3125
Checksum: 299
Coasting Arc #6 (Orbit 3140)
---------------------------------------
Vector Time (GMT): 2008/187/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1279659
37 A = 6729395
87 meter
Y = 6605215
13 meter E =
0004834
Z = 110909
89 I = 51
34067
XDOT = -4740
514281 Wp = 96
73637
YDOT = -813
752592 meter/sec RA = 281
71997 deg
ZDOT = -6008
829136 TA = 82
05415
MA = 81
99930
Ha = 189
616 n
mi
Hp = 182
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4198357
51 X = -1353963
59
Y = 21670653
31 feet Y = 6590489
77 meter
Z = 363877
59 Z = 104514
05
XDOT = -15552
868375 XDOT = -4701
873232
YDOT = -2669
791968 feet/sec YDOT = -866
546684 meter/sec
ZDOT = -19714
006352 ZDOT = -6031
764375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21516197
81 X = 6558137
09
Y = 4930882
26 feet Y = 1502932
91 meter
Z = 339793
38 Z = 103569
02
XDOT = -2831
002125 XDOT = -862
889448
YDOT = 13771
981502 feet/sec YDOT = 4197
699962 meter/sec
ZDOT = -19802
437890 ZDOT = -6035
783069
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 08187
49027820
00020000 00000-0 20000-3 0 9050
2 25544 51
6405 282
2531 0009077 332
5155 27
5528 15
74974975 31419
Satellite: ISS
Catalog Number: 25544
Epoch time: 08187
49027820 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 282
2531 deg
Eccentricity:
0009077
Arg of perigee: 332
5155 deg
Mean anomaly: 27
5528 deg
Mean motion: 15
74974975 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3141
Checksum: 301
Coasting Arc #7 (Orbit 3156)
---------------------------------------
Vector Time (GMT): 2008/188/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4133691
99 A = 6717191
79 meter
Y = 787041
36 meter E =
0009127
Z = 5237274
44 I = 51
29565
XDOT = -1094
605620 Wp = 351
94601
YDOT = 7618
932817 meter/sec RA = 276
55233 deg
ZDOT = -272
133578 TA = 100
70042
MA = 100
59764
Ha = 189
643 n
mi
Hp = 182
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13561981
60 X = 4099142
68
Y = 2582156
69 feet Y = 833072
77 meter
Z = 17182658
93 Z = 5257271
74
XDOT = -3591
225789 XDOT = -1178
398431
YDOT = 24996
498745 feet/sec YDOT = 7606
223838 meter/sec
ZDOT = -892
826700 ZDOT = -277
653539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2805713
10 X = 855181
35
Y = -13418898
00 feet Y = -4090080
11 meter
Z = 17259773
94 Z = 5260779
10
XDOT = 23954
902195 XDOT = 7301
454189
YDOT = 3796
529708 feet/sec YDOT = 1157
182255 meter/sec
ZDOT = -913
438169 ZDOT = -278
415954
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 08188
50547535
00020000 00000-0 20000-3 0 9064
2 25544 51
6408 277
0317 0009237 336
6032 23
4711 15
75029759 31571
Satellite: ISS
Catalog Number: 25544
Epoch time: 08188
50547535 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 277
0317 deg
Eccentricity:
0009237
Arg of perigee: 336
6032 deg
Mean anomaly: 23
4711 deg
Mean motion: 15
75029759 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3157
Checksum: 297
Coasting Arc #8 (Orbit 3172)
---------------------------------------
Vector Time (GMT): 2008/189/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 628598
69 A = 6729177
23 meter
Y = -6662266
81 meter E =
0018617
Z = 582722
31 I = 51
33359
XDOT = 4764
704687 Wp = 23
13081
YDOT = 976
982477 meter/sec RA = 271
39442 deg
ZDOT = 5982
421963 TA = 343
24825
MA = 343
30966
Ha = 189
915 n
mi
Hp = 182
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2062331
66 X = 700219
78
Y = -21857830
73 feet Y = -6654837
07 meter
Z = 1911818
59 Z = 585949
15
XDOT = 15632
233226 XDOT = 4724
364699
YDOT = 3205
323088 feet/sec YDOT = 1030
037860 meter/sec
ZDOT = 19627
368645 ZDOT = 6005
470695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21859001
38 X = -6662623
62
Y = -2038771
27 feet Y = -621417
48 meter
Z = 1923667
61 Z = 586333
89
XDOT = 3047
794485 XDOT = 928
967759
YDOT = -13927
810470 feet/sec YDOT = -4245
196631 meter/sec
ZDOT = 19716
260795 ZDOT = 6009
516290
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 08189
52066073
00020000 00000-0 20000-3 0 9071
2 25544 51
6406 271
8108 0009298 341
3704 18
7118 15
75007582 31731
Satellite: ISS
Catalog Number: 25544
Epoch time: 08189
52066073 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 271
8108 deg
Eccentricity:
0009298
Arg of perigee: 341
3704 deg
Mean anomaly: 18
7118 deg
Mean motion: 15
75007582 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3173
Checksum: 294
Coasting Arc #9 (Orbit 3187)
---------------------------------------
Vector Time (GMT): 2008/190/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4207576
20 A = 6717488
98 meter
Y = -925519
12 meter E =
0013742
Z = -5163188
95 I = 51
29476
XDOT = 362
087783 Wp = 59
69401
YDOT = -7610
564416 meter/sec RA = 266
21344 deg
ZDOT = 1078
119017 TA = 220
59744
MA = 220
69999
Ha = 189
973 n
mi
Hp = 181
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13804383
85 X = -4171832
61
Y = -3036480
06 feet Y = -972370
22 meter
Z = -16939596
29 Z = -5183542
42
XDOT = 1187
952045 XDOT = 441
926159
YDOT = -24969
043361 feet/sec YDOT = -7606
069065 meter/sec
ZDOT = 3537
135882 ZDOT = 1080
071089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2792387
57 X = -851119
73
Y = 13759284
80 feet Y = 4193830
01 meter
Z = -17018102
14 Z = -5187117
53
XDOT = -23982
497353 XDOT = -7309
865193
YDOT = -520
026090 feet/sec YDOT = -158
503952 meter/sec
ZDOT = 3543
981427 ZDOT = 1080
205539
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 08190
47238224
00020000 00000-0 20000-3 0 9087
2 25544 51
6402 266
9166 0009347 344
8630 15
2253 15
75050405 31887
Satellite: ISS
Catalog Number: 25544
Epoch time: 08190
47238224 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 266
9166 deg
Eccentricity:
0009347
Arg of perigee: 344
8630 deg
Mean anomaly: 15
2253 deg
Mean motion: 15
75050405 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3188
Checksum: 286
Coasting Arc #10 (Orbit 3203)
---------------------------------------
Vector Time (GMT): 2008/191/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -27537
47 A = 6728419
53 meter
Y = 6600634
30 meter E =
0004121
Z = -1314711
97 I = 51
33409
XDOT = -4897
004530 Wp = 60
36863
YDOT = -1176
810884 meter/sec RA = 261
06829 deg
ZDOT = -5817
374132 TA = 134
11951
MA = 134
08560
Ha = 190
165 n
mi
Hp = 181
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -90346
03 X = -94958
17
Y = 21655624
33 feet Y = 6599949
54 meter
Z = -4313359
49 Z = -1315008
76
XDOT = -16066
287827 XDOT = -4855
221724
YDOT = -3860
928098 feet/sec YDOT = -1231
337716 meter/sec
ZDOT = -19085
873136 ZDOT = -5841
062270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21644653
06 X = 6597290
25
Y = -691707
21 feet Y = -210832
36 meter
Z = -4313911
54 Z = -1314880
24
XDOT = -3351
012562 XDOT = -1021
388629
YDOT = 14504
000541 feet/sec YDOT = 4420
819365 meter/sec
ZDOT = -19177
253422 ZDOT = -5845
226843
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 08191
48753953
00020000 00000-0 20000-3 0 9091
2 25544 51
6394 261
6949 0009315 348
8416 11
2539 15
75054814 32049
Satellite: ISS
Catalog Number: 25544
Epoch time: 08191
48753953 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 261
6949 deg
Eccentricity:
0009315
Arg of perigee: 348
8416 deg
Mean anomaly: 11
2539 deg
Mean motion: 15
75054814 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3204
Checksum: 312
Coasting Arc #11 (Orbit 3219)
---------------------------------------
Vector Time (GMT): 2008/192/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4383909
07 A = 6718145
53 meter
Y = 1117757
49 meter E =
0013104
Z = 4967144
40 I = 51
30658
XDOT = 290
296266 Wp = 15
19043
YDOT = 7453
366392 meter/sec RA = 255
87254 deg
ZDOT = -1919
815108 TA = 93
50850
MA = 93
35861
Ha = 190
156 n
mi
Hp = 181
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14382903
78 X = 4346954
90
Y = 3667183
36 feet Y = 1166573
64 meter
Z = 16296405
50 Z = 4988351
73
XDOT = 952
415572 XDOT = 216
256047
YDOT = 24453
301812 feet/sec YDOT = 7456
198908 meter/sec
ZDOT = -6298
605999 ZDOT = -1918
583778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2916926
61 X = 889079
23
Y = -14461475
23 feet Y = -4407857
65 meter
Z = 16378225
20 Z = 4992083
04
XDOT = 23313
883021 XDOT = 7106
071545
YDOT = -2475
196662 feet/sec YDOT = -754
439942 meter/sec
ZDOT = -6293
189530 ZDOT = -1918
164169
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 08192
50268114
00020000 00000-0 20000-3 0 9107
2 25544 51
6401 256
4726 0009495 352
2388 7
8627 15
75117321 32209
Satellite: ISS
Catalog Number: 25544
Epoch time: 08192
50268114 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 256
4726 deg
Eccentricity:
0009495
Arg of perigee: 352
2388 deg
Mean anomaly: 7
8627 deg
Mean motion: 15
75117321 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3220
Checksum: 278
Coasting Arc #12 (Orbit 3235)
---------------------------------------
Vector Time (GMT): 2008/193/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -514983
38 A = 6727281
84 meter
Y = -6381931
61 meter E =
0019309
Z = 2023907
06 I = 51
34510
XDOT = 5177
060784 Wp = 40
94860
YDOT = 1348
531759 meter/sec RA = 250
74105 deg
ZDOT = 5554
153580 TA = 341
75464
MA = 341
82382
Ha = 190
385 n
mi
Hp = 181
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1689578
01 X = -453413
09
Y = -20938095
85 feet Y = -6387346
48 meter
Z = 6640115
01 Z = 2021553
94
XDOT = 16985
107559 XDOT = 5134
615487
YDOT = 4424
316796 feet/sec YDOT = 1406
186529 meter/sec
ZDOT = 18222
288647 ZDOT = 5579
200794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20767914
90 X = -6330060
46
Y = 3174938
78 feet Y = 967721
34 meter
Z = 6630470
08 Z = 2020967
28
XDOT = 3474
937007 XDOT = 1059
160800
YDOT = -15632
511819 feet/sec YDOT = -4764
789602 meter/sec
ZDOT = 18318
930886 ZDOT = 5583
610134
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 08193
51781175
00020000 00000-0 20000-3 0 9117
2 25544 51
6396 251
2514 0009511 357
0343 3
0763 15
75099593 32369
Satellite: ISS
Catalog Number: 25544
Epoch time: 08193
51781175 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 251
2514 deg
Eccentricity:
0009511
Arg of perigee: 357
0343 deg
Mean anomaly: 3
0763 deg
Mean motion: 15
75099593 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3236
Checksum: 288
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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