Date:
February 7th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6888 9 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 2996)
---------------------------------------
Vector Time (GMT): 2007/036/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2948505
84 A = 6709679
41 meter
Y = -3161051
44 meter E =
0025519
Z = -5142312
69 I = 51
90109
XDOT = 4265
077386 Wp = 138
00908
YDOT = 6249
689586 meter/sec RA = 64
14322 deg
ZDOT = -1418
821339 TA = 118
57485
MA = 118
31781
Ha = 190
795 n
mi
Hp = 172
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9673575
59 X = 3008613
81
Y = -10370903
67 feet Y = -3127743
61 meter
Z = -16871104
61 Z = -5127843
16
XDOT = 13993
036044 XDOT = 4201
767681
YDOT = 20504
230925 feet/sec YDOT = 6297
030055 meter/sec
ZDOT = -4654
925652 ZDOT = -1398
256009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13835011
00 X = 4216911
35
Y = 3397522
77 feet Y = 1035564
94 meter
Z = -16817169
45 Z = -5125873
25
XDOT = -10700
609853 XDOT = -3261
545883
YDOT = 21286
472857 feet/sec YDOT = 6488
116927 meter/sec
ZDOT = -4576
917943 ZDOT = -1395
044589
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
47656942
00020000 00000-0 20000-3 0 9008
2 25544 51
6331 64
6589 0021841 171
7270 188
4259 15
77885476 29972
Satellite: ISS
Catalog Number: 25544
Epoch time: 07036
47656942 = yrday
fracday
Element set: 900
Inclination: 51
6331 deg
RA of node: 64
6589 deg
Eccentricity:
0021841
Arg of perigee: 171
7270 deg
Mean anomaly: 188
4259 deg
Mean motion: 15
77885476 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2997
Checksum: 332
Coasting Arc #2 (Orbit 3012)
---------------------------------------
Vector Time (GMT): 2007/037/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3404943
60 A = 6721015
96 meter
Y = -5770732
03 meter E =
0032043
Z = -70455
06 I = 51
92615
XDOT = 4130
992438 Wp = 160
98192
YDOT = -2372
901215 meter/sec RA = 58
98588 deg
ZDOT = -6080
272470 TA = 19
78338
MA = 19
65938
Ha = 190
516 n
mi
Hp = 173
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11171074
81 X = -3339819
14
Y = -18932847
86 feet Y = -5808443
88 meter
Z = -231151
76 Z = -86837
61
XDOT = 13553
124795 XDOT = 4186
755769
YDOT = -7785
108974 feet/sec YDOT = -2326
394491 meter/sec
ZDOT = -19948
400491 ZDOT = -6060
069043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10653643
69 X = 3247230
60
Y = -19227919
02 feet Y = -5860669
72 meter
Z = -293390
68 Z = -89425
48
XDOT = 12236
613103 XDOT = 3729
719674
YDOT = 7051
860363 feet/sec YDOT = 2149
407039 meter/sec
ZDOT = -19872
835430 ZDOT = -6057
240239
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
48987352
00020000 00000-0 20000-3 0 9013
2 25544 51
6332 59
4237 0021761 175
2491 184
8888 15
77936236 30139
Satellite: ISS
Catalog Number: 25544
Epoch time: 07037
48987352 = yrday
fracday
Element set: 901
Inclination: 51
6332 deg
RA of node: 59
4237 deg
Eccentricity:
0021761
Arg of perigee: 175
2491 deg
Mean anomaly: 184
8888 deg
Mean motion: 15
77936236 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3013
Checksum: 314
Coasting Arc #3 (Orbit 3028)
---------------------------------------
Vector Time (GMT): 2007/038/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4244611
37 A = 6709580
27 meter
Y = 972309
61 meter E =
0019327
Z = 5096442
43 I = 51
87140
XDOT = -3405
915374 Wp = 166
60591
YDOT = -6742
351983 meter/sec RA = 53
82482 deg
ZDOT = -1567
580350 TA = 298
26645
MA = 298
46137
Ha = 190
379 n
mi
Hp = 173
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13925890
33 X = -4279925
58
Y = 3189992
15 feet Y = 924646
63 meter
Z = 16720611
65 Z = 5075736
67
XDOT = -11174
263038 XDOT = -3322
653411
YDOT = -22120
577372 feet/sec YDOT = -6779
973315 meter/sec
ZDOT = -5142
980150 ZDOT = -1583
923646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10036796
07 X = -3059215
44
Y = -10293643
73 feet Y = -3137502
61 meter
Z = 16642984
97 Z = 5072781
82
XDOT = 12302
476066 XDOT = 3749
794705
YDOT = -20319
397895 feet/sec YDOT = -6193
352478 meter/sec
ZDOT = -5205
188848 ZDOT = -1586
541561
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
50315668
00020000 00000-0 20000-3 0 9023
2 25544 51
6325 54
1890 0021677 179
0216 181
0996 15
77983336 30290
Satellite: ISS
Catalog Number: 25544
Epoch time: 07038
50315668 = yrday
fracday
Element set: 902
Inclination: 51
6325 deg
RA of node: 54
1890 deg
Eccentricity:
0021677
Arg of perigee: 179
0216 deg
Mean anomaly: 181
0996 deg
Mean motion: 15
77983336 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3029
Checksum: 305
Coasting Arc #4 (Orbit 3044)
---------------------------------------
Vector Time (GMT): 2007/039/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2332757
21 A = 6717889
07 meter
Y = 5746543
79 meter E =
0022336
Z = 2598888
08 I = 51
88172
XDOT = -5608
698723 Wp = 145
62774
YDOT = -123
436909 meter/sec RA = 48
71060 deg
ZDOT = 5267
353829 TA = 243
79471
MA = 244
02452
Ha = 190
078 n
mi
Hp = 173
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7653402
92 X = 2255700
41
Y = 18853490
12 feet Y = 5772199
15 meter
Z = 8526535
71 Z = 2610033
25
XDOT = -18401
242529 XDOT = -5632
489079
YDOT = -404
976735 feet/sec YDOT = -186
289492 meter/sec
ZDOT = 17281
344582 ZDOT = 5240
049369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11830696
44 X = -3605996
28
Y = 16532866
59 feet Y = 5039217
74 meter
Z = 8569096
86 Z = 2611860
72
XDOT = -8375
349358 XDOT = -2552
806484
YDOT = -14964
761162 feet/sec YDOT = -4561
259202 meter/sec
ZDOT = 17178
804249 ZDOT = 5236
099535
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
51642082
00020000 00000-0 20000-3 0 9039
2 25544 51
6326 48
9533 0021544 182
6748 177
4306 15
77987294 30458
Satellite: ISS
Catalog Number: 25544
Epoch time: 07039
51642082 = yrday
fracday
Element set: 903
Inclination: 51
6326 deg
RA of node: 48
9533 deg
Eccentricity:
0021544
Arg of perigee: 182
6748 deg
Mean anomaly: 177
4306 deg
Mean motion: 15
77987294 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3045
Checksum: 309
Coasting Arc #5 (Orbit 3059)
---------------------------------------
Vector Time (GMT): 2007/040/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5458465
04 A = 6714621
73 meter
Y = 1091195
29 meter E =
0023015
Z = -3777182
51 I = 51
85212
XDOT = 1700
855382 Wp = 171
07923
YDOT = 6194
396258 meter/sec RA = 43
51162 deg
ZDOT = 4228
592656 TA = 143
36032
MA = 143
20271
Ha = 189
842 n
mi
Hp = 173
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17908349
86 X = 5464206
10
Y = 3580037
03 feet Y = 1152267
02 meter
Z = -12392331
06 Z = -3750651
65
XDOT = 5580
234194 XDOT = 1610
920862
YDOT = 20322
822369 feet/sec YDOT = 6212
913287 meter/sec
ZDOT = 13873
335487 ZDOT = 4236
636916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6915493
99 X = 2107842
57
Y = 16975395
22 feet Y = 5174100
46 meter
Z = -12292576
16 Z = -3746777
21
XDOT = -12691
376172 XDOT = -3868
331457
YDOT = 15284
069150 feet/sec YDOT = 4658
584277 meter/sec
ZDOT = 13904
302890 ZDOT = 4238
031521
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
46633534
00020000 00000-0 20000-3 0 9048
2 25544 51
6337 44
0451 0021513 186
4339 173
6553 15
78030588 30605
Satellite: ISS
Catalog Number: 25544
Epoch time: 07040
46633534 = yrday
fracday
Element set: 904
Inclination: 51
6337 deg
RA of node: 44
0451 deg
Eccentricity:
0021513
Arg of perigee: 186
4339 deg
Mean anomaly: 173
6553 deg
Mean motion: 15
78030588 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3060
Checksum: 275
Coasting Arc #6 (Orbit 3075)
---------------------------------------
Vector Time (GMT): 2007/041/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -466680
09 A = 6711622
15 meter
Y = -4921451
15 meter E =
0018535
Z = -4535566
60 I = 51
82002
XDOT = 6705
331782 Wp = 161
68201
YDOT = 2203
560826 meter/sec RA = 38
40768 deg
ZDOT = -3101
612018 TA = 77
63825
MA = 77
43084
Ha = 189
621 n
mi
Hp = 173
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1531102
65 X = -389580
34
Y = -16146493
26 feet Y = -4926238
62 meter
Z = -14880467
85 Z = -4537646
56
XDOT = 21999
120020 XDOT = 6695
259789
YDOT = 7229
530269 feet/sec YDOT = 2278
487349 meter/sec
ZDOT = -10175
892447 ZDOT = -3069
062314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12501794
59 X = 3810546
99
Y = -10320284
11 feet Y = -3145622
60 meter
Z = -14888878
78 Z = -4538130
25
XDOT = 5748
151939 XDOT = 1752
036711
YDOT = 21369
422229 feet/sec YDOT = 6513
399895 meter/sec
ZDOT = -10053
400500 ZDOT = -3064
276472
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
47955812
00020000 00000-0 20000-3 0 9057
2 25544 51
6329 38
8093 0021521 190
4203 169
6519 15
78061488 30760
Satellite: ISS
Catalog Number: 25544
Epoch time: 07041
47955812 = yrday
fracday
Element set: 905
Inclination: 51
6329 deg
RA of node: 38
8093 deg
Eccentricity:
0021521
Arg of perigee: 190
4203 deg
Mean anomaly: 169
6519 deg
Mean motion: 15
78061488 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3076
Checksum: 299
Coasting Arc #7 (Orbit 3091)
---------------------------------------
Vector Time (GMT): 2007/042/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6014066
45 A = 6719676
22 meter
Y = -2571951
47 meter E =
0028531
Z = 1453578
02 I = 51
82326
XDOT = 730
964947 Wp = 165
25372
YDOT = -5006
330075 meter/sec RA = 33
21720 deg
ZDOT = -5836
107413 TA = 358
72696
MA = 358
73421
Ha = 189
387 n
mi
Hp = 174
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19731189
16 X = -5991920
67
Y = -8438161
01 feet Y = -2639080
36 meter
Z = 4768956
76 Z = 1424415
77
XDOT = 2398
178960 XDOT = 815
242486
YDOT = -16424
967437 feet/sec YDOT = -4997
684559 meter/sec
ZDOT = -19147
334032 ZDOT = -5832
351931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4566719
76 X = -1391936
18
Y = -20992923
46 feet Y = -6398643
07 meter
Z = 4659138
39 Z = 1420105
38
XDOT = 13308
402989 XDOT = 4056
401231
YDOT = -7139
917365 feet/sec YDOT = -2176
246813 meter/sec
ZDOT = -19133
838794 ZDOT = -5831
994064
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
49276029
00020000 00000-0 20000-3 0 9067
2 25544 51
6322 33
5737 0021411 194
1172 165
9397 15
78096787 30925
Satellite: ISS
Catalog Number: 25544
Epoch time: 07042
49276029 = yrday
fracday
Element set: 906
Inclination: 51
6322 deg
RA of node: 33
5737 deg
Eccentricity:
0021411
Arg of perigee: 194
1172 deg
Mean anomaly: 165
9397 deg
Mean motion: 15
78096787 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3092
Checksum: 304
Coasting Arc #8 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2007/043/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1830104
81 A = 6708381
82 meter
Y = 3730862
37 meter E =
0020949
Z = 5270171
81 I = 51
76014
XDOT = -6839
564267 Wp = 191
45077
YDOT = -3545
623408 meter/sec RA = 28
07542 deg
ZDOT = 114
867375 TA = 257
34445
MA = 257
57875
Ha = 189
115 n
mi
Hp = 174
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6004280
88 X = -1897288
94
Y = 12240362
10 feet Y = 3710021
19 meter
Z = 17290589
93 Z = 5261118
32
XDOT = -22439
515311 XDOT = -6799
966268
YDOT = -11632
622730 feet/sec YDOT = -3621
885833 meter/sec
ZDOT = 376
861466 ZDOT = 81
737324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13472726
55 X = -4106487
05
Y = 2349998
86 feet Y = 716279
65 meter
Z = 17257041
99 Z = 5259946
40
XDOT = -3776
222482 XDOT = -1150
992612
YDOT = -23984
427807 feet/sec YDOT = -7310
453596 meter/sec
ZDOT = 252
022362 ZDOT = 76
816416
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
50594070
00020000 00000-0 20000-3 0 9070
2 25544 51
6316 28
3376 0021391 198
3314 161
7083 15
78122221 31087
Satellite: ISS
Catalog Number: 25544
Epoch time: 07043
50594070 = yrday
fracday
Element set: 907
Inclination: 51
6316 deg
RA of node: 28
3376 deg
Eccentricity:
0021391
Arg of perigee: 198
3314 deg
Mean anomaly: 161
7083 deg
Mean motion: 15
78122221 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3108
Checksum: 269
Coasting Arc #9 (Orbit 3123)
---------------------------------------
Vector Time (GMT): 2007/044/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5613414
07 A = 6719446
30 meter
Y = 3476328
68 meter E =
0013504
Z = 1288205
37 I = 51
77249
XDOT = -3530
374450 Wp = 162
43537
YDOT = 3518
582230 meter/sec RA = 22
92907 deg
ZDOT = 5860
065127 TA = 211
67357
MA = 211
75490
Ha = 188
811 n
mi
Hp = 174
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18416712
81 X = 5567866
33
Y = 11405277
81 feet Y = 3538846
26 meter
Z = 4226395
56 Z = 1315364
32
XDOT = -11582
593340 XDOT = -3597
923884
YDOT = 11543
904955 feet/sec YDOT = 3478
725594 meter/sec
ZDOT = 19225
935457 ZDOT = 5842
751058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2099952
42 X = 640065
50
Y = 21539956
23 feet Y = 6565378
66 meter
Z = 4328807
90 Z = 1319420
65
XDOT = -14698
444429 XDOT = -4480
085862
YDOT = -2436
177548 feet/sec YDOT = -742
546917 meter/sec
ZDOT = 19161
337193 ZDOT = 5840
375576
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
51909745
00020000 00000-0 20000-3 0 9082
2 25544 51
6315 23
1019 0021572 202
2419 157
7812 15
78215350 31244
Satellite: ISS
Catalog Number: 25544
Epoch time: 07044
51909745 = yrday
fracday
Element set: 908
Inclination: 51
6315 deg
RA of node: 23
1019 deg
Eccentricity:
0021572
Arg of perigee: 202
2419 deg
Mean anomaly: 157
7812 deg
Mean motion: 15
78215350 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3124
Checksum: 268
Coasting Arc #10 (Orbit 3138)
---------------------------------------
Vector Time (GMT): 2007/045/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4268467
25 A = 6711277
86 meter
Y = -2432989
72 meter E =
0022655
Z = -4583302
68 I = 51
71695
XDOT = 5662
290950 Wp = 178
71148
YDOT = 4279
651840 meter/sec RA = 17
73279 deg
ZDOT = 2979
585065 TA = 120
94537
MA = 120
72252
Ha = 188
590 n
mi
Hp = 174
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14004157
63 X = 4317620
31
Y = -7982249
73 feet Y = -2384982
27 meter
Z = -15037082
29 Z = -4562447
75
XDOT = 18577
070047 XDOT = 5599
540540
YDOT = 14040
852494 feet/sec YDOT = 4342
619730 meter/sec
ZDOT = 9775
541553 ZDOT = 3006
939551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15001358
71 X = 4572414
14
Y = 6093650
87 feet Y = 1857344
79 meter
Z = -14959052
16 Z = -4559519
10
XDOT = 928
183112 XDOT = 282
910212
YDOT = 22143
761554 feet/sec YDOT = 6749
418522 meter/sec
ZDOT = 9878
791419 ZDOT = 3011
055624
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 07045
46891665
00020000 00000-0 20000-3 0 9099
2 25544 51
6312 18
1920 0021257 206
0422 153
9676 15
78168566 31390
Satellite: ISS
Catalog Number: 25544
Epoch time: 07045
46891665 = yrday
fracday
Element set: 909
Inclination: 51
6312 deg
RA of node: 18
1920 deg
Eccentricity:
0021257
Arg of perigee: 206
0422 deg
Mean anomaly: 153
9676 deg
Mean motion: 15
78168566 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3139
Checksum: 301
Coasting Arc #11 (Orbit 3154)
---------------------------------------
Vector Time (GMT): 2007/046/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3986384
28 A = 6714059
11 meter
Y = -3901726
60 meter E =
0017634
Z = -3718367
22 I = 51
69943
XDOT = 6057
519481 Wp = 194
94330
YDOT = -2114
233852 meter/sec RA = 12
61822 deg
ZDOT = -4287
909697 TA = 30
03079
MA = 29
92977
Ha = 188
184 n
mi
Hp = 174
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13078688
59 X = -3924395
75
Y = -12800940
28 feet Y = -3945957
85 meter
Z = -12199367
51 Z = -3737582
04
XDOT = 19873
751579 XDOT = 6101
540190
YDOT = -6936
462769 feet/sec YDOT = -2046
249018 meter/sec
ZDOT = -14067
945200 ZDOT = -4258
376320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1651772
90 X = 503460
38
Y = -18177188
90 feet Y = -5540407
18 meter
Z = -12272008
18 Z = -3740508
09
XDOT = 16687
223708 XDOT = 5086
265786
YDOT = 10912
395984 feet/sec YDOT = 3326
098296 meter/sec
ZDOT = -13957
279685 ZDOT = -4254
178848
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 07046
48203393
00020000 00000-0 20000-3 0 9109
2 25544 51
6312 12
9551 0021215 209
8935 150
1020 15
78219107 31554
Satellite: ISS
Catalog Number: 25544
Epoch time: 07046
48203393 = yrday
fracday
Element set: 910
Inclination: 51
6312 deg
RA of node: 12
9551 deg
Eccentricity:
0021215
Arg of perigee: 209
8935 deg
Mean anomaly: 150
1020 deg
Mean motion: 15
78219107 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3155
Checksum: 255
Coasting Arc #12 (Orbit 3170)
---------------------------------------
Vector Time (GMT): 2007/047/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6038388
92 A = 6717157
01 meter
Y = 1295026
51 meter E =
0020735
Z = 2609876
26 I = 51
68187
XDOT = -3255
686138 Wp = 175
23861
YDOT = -4614
898999 meter/sec RA = 7
40531 deg
ZDOT = -5259
986255 TA = 335
01567
MA = 335
11588
Ha = 187
968 n
mi
Hp = 174
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19810987
29 X = -6065099
20
Y = 4248774
64 feet Y = 1227352
52 meter
Z = 8562586
16 Z = 2580477
88
XDOT = -10681
384966 XDOT = -3178
288503
YDOT = -15140
744746 feet/sec YDOT = -4650
873123 meter/sec
ZDOT = -17257
172752 ZDOT = -5275
613877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16090470
34 X = -4904375
36
Y = -12389516
91 feet Y = -3776324
76 meter
Z = 8452326
30 Z = 2576269
06
XDOT = 3788
740795 XDOT = 1154
808194
YDOT = -16694
751771 feet/sec YDOT = -5088
560340 meter/sec
ZDOT = -17316
433595 ZDOT = -5278
048960
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 07047
49512862
00020000 00000-0 20000-3 0 9116
2 25544 51
6313 7
7189 0021163 214
2158 145
7645 15
78267029 31710
Satellite: ISS
Catalog Number: 25544
Epoch time: 07047
49512862 = yrday
fracday
Element set: 911
Inclination: 51
6313 deg
RA of node: 7
7189 deg
Eccentricity:
0021163
Arg of perigee: 214
2158 deg
Mean anomaly: 145
7645 deg
Mean motion: 15
78267029 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3171
Checksum: 288
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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