Date:
February 3rd 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9956 62 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 2950)
---------------------------------------
Vector Time (GMT): 2007/033/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1669676
86 A = 6716359
44 meter
Y = 5544493
64 meter E =
0028841
Z = 3406773
56 I = 51
94951
XDOT = -4480
910934 Wp = 135
95263
YDOT = -4220
234743 meter/sec RA = 79
33982 deg
ZDOT = 4628
691076 TA = 264
13435
MA = 264
46319
Ha = 191
320 n
mi
Hp = 172
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5477942
44 X = -1748101
00
Y = 18190595
95 feet Y = 5525383
76 meter
Z = 11177078
61 Z = 3398472
28
XDOT = -14701
151357 XDOT = -4455
871214
YDOT = -13845
914512 feet/sec YDOT = -4270
202961 meter/sec
ZDOT = 15185
994343 ZDOT = 4606
984215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16921906
67 X = -5157797
15
Y = 8673812
86 feet Y = 2643778
16 meter
Z = 11146603
31 Z = 3397484
69
XDOT = 294
552917 XDOT = 89
779729
YDOT = -19019
523222 feet/sec YDOT = -5797
150678 meter/sec
ZDOT = 15103
960771 ZDOT = 4603
687243
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 07033
56319645
00020000 00000-0 20000-3 0 9001
2 25544 51
6333 79
7080 0021992 160
3479 199
8538 15
77801348 29511
Satellite: ISS
Catalog Number: 25544
Epoch time: 07033
56319645 = yrday
fracday
Element set: 900
Inclination: 51
6333 deg
RA of node: 79
7080 deg
Eccentricity:
0021992
Arg of perigee: 160
3479 deg
Mean anomaly: 199
8538 deg
Mean motion: 15
77801348 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2951
Checksum: 314
Coasting Arc #2 (Orbit 2965)
---------------------------------------
Vector Time (GMT): 2007/034/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3819145
80 A = 6717049
31 meter
Y = 4605463
12 meter E =
0022443
Z = -3086019
13 I = 51
94677
XDOT = -2481
884250 Wp = 152
06681
YDOT = 5358
324421 meter/sec RA = 74
14565 deg
ZDOT = 4920
045773 TA = 172
33094
MA = 172
29656
Ha = 191
061 n
mi
Hp = 172
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12530005
91 X = 3782353
84
Y = 15109787
13 feet Y = 4647965
27 meter
Z = -10124734
67 Z = -3067555
63
XDOT = -8142
664863 XDOT = -2565
517246
YDOT = 17579
804532 feet/sec YDOT = 5330
102923 meter/sec
ZDOT = 16141
882458 ZDOT = 4907
786114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1763194
37 X = -537421
64
Y = 19585927
61 feet Y = 5969790
74 meter
Z = -10054827
33 Z = -3064711
37
XDOT = -16816
324775 XDOT = -5125
615791
YDOT = 6758
142069 feet/sec YDOT = 2059
881703 meter/sec
ZDOT = 16096
521264 ZDOT = 4906
219681
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 07034
51322335
00020000 00000-0 20000-3 0 9018
2 25544 51
6340 74
8002 0021996 163
8093 196
3780 15
77885645 29662
Satellite: ISS
Catalog Number: 25544
Epoch time: 07034
51322335 = yrday
fracday
Element set: 901
Inclination: 51
6340 deg
RA of node: 74
8002 deg
Eccentricity:
0021996
Arg of perigee: 163
8093 deg
Mean anomaly: 196
3780 deg
Mean motion: 15
77885645 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2966
Checksum: 302
Coasting Arc #3 (Orbit 2981)
---------------------------------------
Vector Time (GMT): 2007/035/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2739445
52 A = 6710594
03 meter
Y = -3648132
68 meter E =
0024535
Z = -4929629
54 I = 51
91624
XDOT = 4177
753417 Wp = 136
74587
YDOT = 6081
448746 meter/sec RA = 69
04251 deg
ZDOT = -2202
783480 TA = 112
07223
MA = 111
81150
Ha = 190
941 n
mi
Hp = 172
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8987682
17 X = 2803982
40
Y = -11968939
24 feet Y = -3617137
85 meter
Z = -16173325
25 Z = -4916164
93
XDOT = 13706
540081 XDOT = 4120
139701
YDOT = 19952
259666 feet/sec YDOT = 6127
844569 meter/sec
ZDOT = -7226
979922 ZDOT = -2182
628530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14842042
13 X = 4523854
44
Y = -2316417
77 feet Y = -706044
14 meter
Z = -16123224
90 Z = -4914358
95
XDOT = -4120
453588 XDOT = -1255
914254
YDOT = 22822
645452 feet/sec YDOT = 6956
342334 meter/sec
ZDOT = -7150
533914 ZDOT = -2179
482737
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 07035
52655681
00020000 00000-0 20000-3 0 9024
2 25544 51
6343 69
5648 0021884 167
8640 192
3057 15
77886671 29821
Satellite: ISS
Catalog Number: 25544
Epoch time: 07035
52655681 = yrday
fracday
Element set: 902
Inclination: 51
6343 deg
RA of node: 69
5648 deg
Eccentricity:
0021884
Arg of perigee: 167
8640 deg
Mean anomaly: 192
3057 deg
Mean motion: 15
77886671 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2982
Checksum: 327
Coasting Arc #4 (Orbit 2997)
---------------------------------------
Vector Time (GMT): 2007/036/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3381702
49 A = 6720849
38 meter
Y = -5747629
92 meter E =
0032899
Z = 645122
41 I = 51
93877
XDOT = 3823
973374 Wp = 155
07577
YDOT = -2936
473931 meter/sec RA = 63
87313 deg
ZDOT = -6036
146006 TA = 17
89962
MA = 17
78402
Ha = 190
695 n
mi
Hp = 172
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11094824
45 X = -3320314
15
Y = -18857053
55 feet Y = -5785102
76 meter
Z = 2116543
33 Z = 628843
73
XDOT = 12545
844404 XDOT = 3885
846996
YDOT = -9634
100824 feet/sec YDOT = -2893
366279 meter/sec
ZDOT = -19803
628629 ZDOT = -6017
419283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4725163
60 X = 1440229
86
Y = -21368537
88 feet Y = -6513130
35 meter
Z = 2054695
03 Z = 626271
05
XDOT = 14268
843214 XDOT = 4349
143412
YDOT = 1231
452974 feet/sec YDOT = 375
346866 meter/sec
ZDOT = -19733
679529 ZDOT = -6014
825521
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 07036
53986075
00020000 00000-0 20000-3 0 9031
2 25544 51
6334 64
3296 0021834 171
3587 188
7959 15
77936139 29980
Satellite: ISS
Catalog Number: 25544
Epoch time: 07036
53986075 = yrday
fracday
Element set: 903
Inclination: 51
6334 deg
RA of node: 64
3296 deg
Eccentricity:
0021834
Arg of perigee: 171
3587 deg
Mean anomaly: 188
7959 deg
Mean motion: 15
77936139 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2998
Checksum: 343
Coasting Arc #5 (Orbit 3013)
---------------------------------------
Vector Time (GMT): 2007/037/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3941172
84 A = 6708921
69 meter
Y = 1420822
96 meter E =
0020621
Z = 5233842
25 I = 51
88483
XDOT = -3459
872035 Wp = 166
75009
YDOT = -6851
587911 meter/sec RA = 58
72612 deg
ZDOT = -764
439182 TA = 290
37552
MA = 290
59692
Ha = 190
510 n
mi
Hp = 172
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12930357
09 X = -3982192
29
Y = 4661492
64 feet Y = 1376521
32 meter
Z = 17171398
45 Z = 5214596
77
XDOT = -11351
286204 XDOT = -3379
286032
YDOT = -22478
962962 feet/sec YDOT = -6889
827567 meter/sec
ZDOT = -2508
002567 ZDOT = -781
051002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12800729
85 X = -3901662
46
Y = -5247422
92 feet Y = -1599414
50 meter
Z = 17099311
12 Z = 5211870
03
XDOT = 6225
303017 XDOT = 1897
472360
YDOT = -23359
955757 feet/sec YDOT = -7120
114515 meter/sec
ZDOT = -2571
237670 ZDOT = -783
713242
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 07037
55313454
00020000 00000-0 20000-3 0 9040
2 25544 51
6329 59
0945 0021711 175
1706 184
9673 15
77996222 30145
Satellite: ISS
Catalog Number: 25544
Epoch time: 07037
55313454 = yrday
fracday
Element set: 904
Inclination: 51
6329 deg
RA of node: 59
0945 deg
Eccentricity:
0021711
Arg of perigee: 175
1706 deg
Mean anomaly: 184
9673 deg
Mean motion: 15
77996222 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3014
Checksum: 297
Coasting Arc #6 (Orbit 3029)
---------------------------------------
Vector Time (GMT): 2007/038/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2464488
80 A = 6718985
32 meter
Y = 5941015
79 meter E =
0021228
Z = 1966298
17 I = 51
90353
XDOT = -5249
226572 Wp = 140
22279
YDOT = 301
912794 meter/sec RA = 53
60257 deg
ZDOT = 5617
799986 TA = 241
58484
MA = 241
79895
Ha = 190
165 n
mi
Hp = 173
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8085593
17 X = 2388320
59
Y = 19491521
60 feet Y = 5968149
23 meter
Z = 6451109
48 Z = 1978085
34
XDOT = -17221
871957 XDOT = -5279
502264
YDOT = 990
527540 feet/sec YDOT = 243
043827 meter/sec
ZDOT = 18431
102316 ZDOT = 5592
226137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6710673
93 X = -2045413
41
Y = 19992009
72 feet Y = 6093564
56 meter
Z = 6496110
20 Z = 1980014
39
XDOT = -12267
455328 XDOT = -3739
120384
YDOT = -10127
591523 feet/sec YDOT = -3086
889896 meter/sec
ZDOT = 18335
112771 ZDOT = 5588
542373
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 07038
56637879
00020000 00000-0 20000-3 0 9053
2 25544 51
6331 53
8592 0021642 179
2192 180
9010 15
78045240 30300
Satellite: ISS
Catalog Number: 25544
Epoch time: 07038
56637879 = yrday
fracday
Element set: 905
Inclination: 51
6331 deg
RA of node: 53
8592 deg
Eccentricity:
0021642
Arg of perigee: 179
2192 deg
Mean anomaly: 180
9010 deg
Mean motion: 15
78045240 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3030
Checksum: 285
Coasting Arc #7 (Orbit 3044)
---------------------------------------
Vector Time (GMT): 2007/039/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5167541
18 A = 6712983
91 meter
Y = 823823
96 meter E =
0025186
Z = -4226335
42 I = 51
86544
XDOT = 1950
362476 Wp = 164
53638
YDOT = 6492
316961 meter/sec RA = 48
40948 deg
ZDOT = 3631
405370 TA = 142
44591
MA = 142
26974
Ha = 189
953 n
mi
Hp = 173
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16953875
28 X = 5178475
49
Y = 2702834
53 feet Y = 881671
41 meter
Z = -13865929
84 Z = -4201205
30
XDOT = 6398
827022 XDOT = 1859
979044
YDOT = 21300
252496 feet/sec YDOT = 6513
621664 meter/sec
ZDOT = 11914
059613 ZDOT = 3640
660523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11306708
77 X = 3446284
83
Y = 13019533
04 feet Y = 3968353
67 meter
Z = -13771467
16 Z = -4197543
19
XDOT = -7894
416544 XDOT = -2406
218163
YDOT = 19561
383058 feet/sec YDOT = 5962
309556 meter/sec
ZDOT = 11949
616107 ZDOT = 3642
242989
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 07039
51626857
00020000 00000-0 20000-3 0 9064
2 25544 51
6334 48
9506 0021511 182
8621 177
2425 15
78059899 30455
Satellite: ISS
Catalog Number: 25544
Epoch time: 07039
51626857 = yrday
fracday
Element set: 906
Inclination: 51
6334 deg
RA of node: 48
9506 deg
Eccentricity:
0021511
Arg of perigee: 182
8621 deg
Mean anomaly: 177
2425 deg
Mean motion: 15
78059899 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3045
Checksum: 311
Coasting Arc #8 (Orbit 3060)
---------------------------------------
Vector Time (GMT): 2007/040/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -761108
30 A = 6712899
09 meter
Y = -5207716
03 meter E =
0019289
Z = -4158965
20 I = 51
84495
XDOT = 6432
786703 Wp = 164
41422
YDOT = 2027
542936 meter/sec RA = 43
30763 deg
ZDOT = -3738
217634 TA = 67
62836
MA = 67
42407
Ha = 189
703 n
mi
Hp = 173
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2497074
47 X = -682615
05
Y = -17085682
50 feet Y = -5215788
25 meter
Z = -13644898
95 Z = -4162472
01
XDOT = 21104
943251 XDOT = 6427
795699
YDOT = 6652
043752 feet/sec YDOT = 2099
450074 meter/sec
ZDOT = -12264
493551 ZDOT = -3706
979639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8876805
69 X = 2705650
38
Y = -14798014
59 feet Y = -4510434
85 meter
Z = -13658707
10 Z = -4163173
92
XDOT = 11181
261498 XDOT = 3408
048505
YDOT = 17851
924999 feet/sec YDOT = 5441
266740 meter/sec
ZDOT = -12146
948627 ZDOT = -3702
389941
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 07040
52945530
00020000 00000-0 20000-3 0 9070
2 25544 51
6324 43
7141 0021517 186
6854 173
4027 15
78113599 30610
Satellite: ISS
Catalog Number: 25544
Epoch time: 07040
52945530 = yrday
fracday
Element set: 907
Inclination: 51
6324 deg
RA of node: 43
7141 deg
Eccentricity:
0021517
Arg of perigee: 186
6854 deg
Mean anomaly: 173
4027 deg
Mean motion: 15
78113599 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3061
Checksum: 282
Coasting Arc #9 (Orbit 3076)
---------------------------------------
Vector Time (GMT): 2007/041/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5851076
21 A = 6718488
29 meter
Y = -2529027
71 meter E =
0027674
Z = 2063466
03 I = 51
84242
XDOT = 330
560587 Wp = 160
05480
YDOT = -5321
412358 meter/sec RA = 38
11089 deg
ZDOT = -5588
471921 TA = 356
88613
MA = 356
90332
Ha = 189
409 n
mi
Hp = 173
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19196444
25 X = -5832385
22
Y = -8297335
00 feet Y = -2594353
25 meter
Z = 6769901
66 Z = 2035087
17
XDOT = 1084
516363 XDOT = 417
188271
YDOT = -17458
701961 feet/sec YDOT = -5317
231340 meter/sec
ZDOT = -18334
881629 ZDOT = -5586
655799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10035807
19 X = -3058914
03
Y = -18386609
13 feet Y = -5604238
46 meter
Z = 6663031
39 Z = 2030891
97
XDOT = 10351
355865 XDOT = 3155
093268
YDOT = -12287
501471 feet/sec YDOT = -3745
230448 meter/sec
ZDOT = -18328
711465 ZDOT = -5586
591255
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 07041
54261128
00020000 00000-0 20000-3 0 9088
2 25544 51
6324 38
4784 0021334 190
6230 169
4487 15
78188295 30771
Satellite: ISS
Catalog Number: 25544
Epoch time: 07041
54261128 = yrday
fracday
Element set: 908
Inclination: 51
6324 deg
RA of node: 38
4784 deg
Eccentricity:
0021334
Arg of perigee: 190
6230 deg
Mean anomaly: 169
4487 deg
Mean motion: 15
78188295 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3077
Checksum: 301
Coasting Arc #10 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2007/042/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1461136
09 A = 6708351
99 meter
Y = 3954224
37 meter E =
0022399
Z = 5223015
36 I = 51
78458
XDOT = -6755
320436 Wp = 186
16592
YDOT = -3611
488532 meter/sec RA = 32
98140 deg
ZDOT = 822
857876 TA = 255
89657
MA = 256
14560
Ha = 189
149 n
mi
Hp = 173
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4793753
58 X = -1530616
31
Y = 12973177
08 feet Y = 3937496
43 meter
Z = 17135877
16 Z = 5215748
66
XDOT = -22163
124790 XDOT = -6718
431430
YDOT = -11848
715655 feet/sec YDOT = -3686
824070 meter/sec
ZDOT = 2699
664949 ZDOT = 790
130430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11718639
13 X = -3571841
21
Y = 7407761
24 feet Y = 2257885
63 meter
Z = 17109069
32 Z = 5214844
33
XDOT = -10020
128991 XDOT = -3054
135316
YDOT = -21964
899893 feet/sec YDOT = -6694
901487 meter/sec
ZDOT = 2576
332871 ZDOT = 785
266259
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 07042
55573759
00020000 00000-0 20000-3 0 9097
2 25544 51
6318 33
2423 0021349 194
6416 165
4133 15
78207193 30934
Satellite: ISS
Catalog Number: 25544
Epoch time: 07042
55573759 = yrday
fracday
Element set: 909
Inclination: 51
6318 deg
RA of node: 33
2423 deg
Eccentricity:
0021349
Arg of perigee: 194
6416 deg
Mean anomaly: 165
4133 deg
Mean motion: 15
78207193 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3093
Checksum: 293
Coasting Arc #11 (Orbit 3108)
---------------------------------------
Vector Time (GMT): 2007/043/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5633332
93 A = 6719651
10 meter
Y = 3607776
53 meter E =
0013018
Z = 713148
17 I = 51
79907
XDOT = -3121
775011 Wp = 161
38079
YDOT = 3682
182221 meter/sec RA = 27
82448 deg
ZDOT = 5989
702405 TA = 206
37164
MA = 206
43796
Ha = 188
853 n
mi
Hp = 173
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18482063
40 X = 5589107
29
Y = 11836537
18 feet Y = 3670524
29 meter
Z = 2339724
96 Z = 740407
20
XDOT = -10242
043998 XDOT = -3191
814077
YDOT = 12080
650331 feet/sec YDOT = 3646
880867 meter/sec
ZDOT = 19651
254611 ZDOT = 5974
367152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7960356
53 X = 2426316
67
Y = 20440924
40 feet Y = 6230393
76 meter
Z = 2442524
65 Z = 744481
51
XDOT = -13988
696127 XDOT = -4263
754579
YDOT = 3090
535411 feet/sec YDOT = 941
995193 meter/sec
ZDOT = 19594
110995 ZDOT = 5972
285031
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 07043
56882960
00020000 00000-0 20000-3 0 9108
2 25544 51
6318 28
0059 0021567 198
2470 161
7924 15
78324783 31093
Satellite: ISS
Catalog Number: 25544
Epoch time: 07043
56882960 = yrday
fracday
Element set: 910
Inclination: 51
6318 deg
RA of node: 28
0059 deg
Eccentricity:
0021567
Arg of perigee: 198
2470 deg
Mean anomaly: 161
7924 deg
Mean motion: 15
78324783 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3109
Checksum: 303
Coasting Arc #12 (Orbit 3123)
---------------------------------------
Vector Time (GMT): 2007/044/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3959126
73 A = 6709913
52 meter
Y = -2476037
82 meter E =
0023525
Z = -4830128
45 I = 51
73979
XDOT = 5776
625100 Wp = 171
48810
YDOT = 4476
052313 meter/sec RA = 22
63785 deg
ZDOT = 2419
078190 TA = 122
21799
MA = 121
98971
Ha = 188
613 n
mi
Hp = 174
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12989260
94 X = 4009983
28
Y = -8123483
65 feet Y = -2431480
02 meter
Z = -15846878
13 Z = -4810772
04
XDOT = 18952
182088 XDOT = 5714
392727
YDOT = 14685
211001 feet/sec YDOT = 4540
301661 meter/sec
ZDOT = 7936
608235 ZDOT = 2446
989526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15370333
24 X = 4684877
57
Y = 868293
69 feet Y = 264655
92 meter
Z = -15774484
30 Z = -4808062
82
XDOT = 7096
136906 XDOT = 2162
902529
YDOT = 21763
595730 feet/sec YDOT = 6633
543978 meter/sec
ZDOT = 8041
966744 ZDOT = 2451
191463
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 07044
51857974
00020000 00000-0 20000-3 0 9112
2 25544 51
6319 23
0959 0021247 202
2013 157
8235 15
78291198 31243
Satellite: ISS
Catalog Number: 25544
Epoch time: 07044
51857974 = yrday
fracday
Element set: 911
Inclination: 51
6319 deg
RA of node: 23
0959 deg
Eccentricity:
0021247
Arg of perigee: 202
2013 deg
Mean anomaly: 157
8235 deg
Mean motion: 15
78291198 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3124
Checksum: 287
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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