Date:
April 16th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 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 3608)
---------------------------------------
Vector Time (GMT): 2009/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2434367
42 A = 6732521
50 meter
Y = 5319814
77 meter E =
0005324
Z = -3324477
48 I = 51
31186
XDOT = -3933
066288 Wp = 215
00435
YDOT = -4706
811631 meter/sec RA = 267
52000 deg
ZDOT = -4652
426516 TA = 4
26384
MA = 4
25930
Ha = 192
251 n
mi
Hp = 189
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7986769
77 X = -2477523
75
Y = 17453460
52 feet Y = 5292351
04 meter
Z = -10907078
35 Z = -3336408
39
XDOT = -12903
760787 XDOT = -3857
540841
YDOT = -15442
295376 feet/sec YDOT = -4750
371065 meter/sec
ZDOT = -15263
866523 ZDOT = -4671
350131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -468469
90 X = -142789
63
Y = 19161990
76 feet Y = 5840574
78 meter
Z = -10953299
93 Z = -3338565
82
XDOT = -16435
722015 XDOT = -5009
608070
YDOT = -9168
166487 feet/sec YDOT = -2794
457145 meter/sec
ZDOT = -15338
093865 ZDOT = -4675
051010
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 09105
52486064
00010596 00000-0 82463-4 0 9000
2 25544 51
6391 268
1377 0008883 241
9957 118
0307 15
72179612 36094
Satellite: ISS
Catalog Number: 25544
Epoch time: 09105
52486064 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 268
1377 deg
Eccentricity:
0008883
Arg of perigee: 241
9957 deg
Mean anomaly: 118
0307 deg
Mean motion: 15
72179612 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3609
Checksum: 324
Coasting Arc #2 (Orbit 3624)
---------------------------------------
Vector Time (GMT): 2009/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3988710
62 A = 6728903
69 meter
Y = 3149820
56 meter E =
0000617
Z = 4409253
48 I = 51
30133
XDOT = -1727
149587 Wp = 135
68652
YDOT = 6754
016013 meter/sec RA = 262
32505 deg
ZDOT = -3262
580798 TA = 347
20901
MA = 347
21058
Ha = 192
123 n
mi
Hp = 189
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13086320
92 X = 3931772
92
Y = 10334056
95 feet Y = 3194106
20 meter
Z = 14466054
74 Z = 4428492
46
XDOT = -5666
501270 XDOT = -1786
696686
YDOT = 22158
845188 feet/sec YDOT = 6734
369140 meter/sec
ZDOT = -10704
005242 ZDOT = -3271
115819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16081765
75 X = 4901722
20
Y = 4151550
66 feet Y = 1265392
64 meter
Z = 14541413
45 Z = 4432222
82
XDOT = 4196
506835 XDOT = 1279
095283
YDOT = 21349
682261 feet/sec YDOT = 6507
383153 meter/sec
ZDOT = -10736
861289 ZDOT = -3272
595321
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 09106
54187486
00010596 00000-0 82463-4 0 9010
2 25544 51
6384 262
9284 0008959 245
2035 114
8195 15
72155277 36251
Satellite: ISS
Catalog Number: 25544
Epoch time: 09106
54187486 = yrday
fracday
Element set: 901
Inclination: 51
6384 deg
RA of node: 262
9284 deg
Eccentricity:
0008959
Arg of perigee: 245
2035 deg
Mean anomaly: 114
8195 deg
Mean motion: 15
72155277 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3625
Checksum: 331
Coasting Arc #3 (Orbit 3640)
---------------------------------------
Vector Time (GMT): 2009/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 508200
09 A = 6734825
89 meter
Y = -6286643
65 meter E =
0005011
Z = 2356229
90 I = 51
32801
XDOT = 4954
537312 Wp = 81
90925
YDOT = 2416
420208 meter/sec RA = 257
22439 deg
ZDOT = 5369
570280 TA = 304
72161
MA = 304
76879
Ha = 191
936 n
mi
Hp = 189
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1667323
12 X = 567014
47
Y = -20625471
30 feet Y = -6280631
84 meter
Z = 7730413
06 Z = 2358841
54
XDOT = 16255
043675 XDOT = 4901
063831
YDOT = 7927
887820 feet/sec YDOT = 2471
525699 meter/sec
ZDOT = 17616
700393 ZDOT = 5393
509584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7242069
48 X = -2207382
78
Y = -19380186
74 feet Y = -5907080
92 meter
Z = 7740162
19 Z = 2359201
43
XDOT = 16576
694322 XDOT = 5052
576429
YDOT = 890
663741 feet/sec YDOT = 271
474308 meter/sec
ZDOT = 17710
373065 ZDOT = 5398
121710
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 09107
55887419
00010596 00000-0 82463-4 0 9026
2 25544 51
6393 257
7193 0009010 249
0833 110
9366 15
72222668 36413
Satellite: ISS
Catalog Number: 25544
Epoch time: 09107
55887419 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 257
7193 deg
Eccentricity:
0009010
Arg of perigee: 249
0833 deg
Mean anomaly: 110
9366 deg
Mean motion: 15
72222668 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3641
Checksum: 319
Coasting Arc #4 (Orbit 3655)
---------------------------------------
Vector Time (GMT): 2009/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4475694
24 A = 6726626
15 meter
Y = -1028129
96 meter E =
0007067
Z = -4920296
51 I = 51
30864
XDOT = -620
997905 Wp = 148
04296
YDOT = -7374
911076 meter/sec RA = 252
04260 deg
ZDOT = 2101
389236 TA = 142
46533
MA = 142
41598
Ha = 191
630 n
mi
Hp = 189
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14684036
23 X = -4439962
95
Y = -3373129
79 feet Y = -1077980
02 meter
Z = -16142705
09 Z = -4941952
65
XDOT = -2037
394700 XDOT = -548
692433
YDOT = -24195
902479 feet/sec YDOT = -7381
451145 meter/sec
ZDOT = 6894
321640 ZDOT = 2098
548093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14594054
88 X = -4448267
93
Y = 3357374
89 feet Y = 1023327
87 meter
Z = -16227367
27 Z = -4946101
54
XDOT = -12219
362870 XDOT = -3724
461803
YDOT = -19777
978391 feet/sec YDOT = -6028
327814 meter/sec
ZDOT = 6882
685674 ZDOT = 2097
842593
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 09108
51230171
00010596 00000-0 82463-4 0 9031
2 25544 51
6397 252
8368 0008901 253
1540 106
8646 15
72223767 36568
Satellite: ISS
Catalog Number: 25544
Epoch time: 09108
51230171 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 252
8368 deg
Eccentricity:
0008901
Arg of perigee: 253
1540 deg
Mean anomaly: 106
8646 deg
Mean motion: 15
72223767 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3656
Checksum: 309
Coasting Arc #5 (Orbit 3671)
---------------------------------------
Vector Time (GMT): 2009/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1596367
13 A = 6736422
93 meter
Y = 6406736
79 meter E =
0009560
Z = -1303237
38 I = 51
35184
XDOT = -5034
214129 Wp = 200
02878
YDOT = 68
622100 meter/sec RA = 246
92700 deg
ZDOT = -5825
429993 TA = 354
32728
MA = 354
33810
Ha = 191
359 n
mi
Hp = 190
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5237424
95 X = 1530938
18
Y = 21019477
67 feet Y = 6424222
44 meter
Z = -4275713
17 Z = -1295641
27
XDOT = -16516
450554 XDOT = -5006
308388
YDOT = 225
138125 feet/sec YDOT = 12
482494 meter/sec
ZDOT = -19112
303127 ZDOT = -5849
818459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14219543
52 X = 4334116
86
Y = 16349634
21 feet Y = 4983368
51 meter
Z = -4245565
71 Z = -1294048
43
XDOT = -13328
563171 XDOT = -4062
546055
YDOT = 6601
154326 feet/sec YDOT = 2012
031839 meter/sec
ZDOT = -19207
562164 ZDOT = -5854
464948
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 09109
52927744
00010596 00000-0 82463-4 0 9043
2 25544 51
6394 247
6269 0008888 258
0058 102
0108 15
72254332 36720
Satellite: ISS
Catalog Number: 25544
Epoch time: 09109
52927744 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 247
6269 deg
Eccentricity:
0008888
Arg of perigee: 258
0058 deg
Mean anomaly: 102
0108 deg
Mean motion: 15
72254332 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3672
Checksum: 323
Coasting Arc #6 (Orbit 3687)
---------------------------------------
Vector Time (GMT): 2009/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4125062
97 A = 6725352
38 meter
Y = -1113231
26 meter E =
0005905
Z = 5198870
92 I = 51
32822
XDOT = 2990
786487 Wp = 274
58632
YDOT = 7035
787185 meter/sec RA = 241
76380 deg
ZDOT = -866
861919 TA = 183
70867
MA = 183
71305
Ha = 191
061 n
mi
Hp = 190
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13533671
17 X = 4111949
45
Y = -3652333
52 feet Y = -1067175
54 meter
Z = 17056663
11 Z = 5218878
73
XDOT = 9812
291625 XDOT = 2916
099927
YDOT = 23083
291289 feet/sec YDOT = 7068
814281 meter/sec
ZDOT = -2844
035168 ZDOT = -852
514271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10156761
40 X = 3095780
87
Y = -9522110
92 feet Y = -2902339
41 meter
Z = 17134735
29 Z = 5222667
32
XDOT = 18805
513676 XDOT = 5731
920568
YDOT = 15045
199503 feet/sec YDOT = 4585
776808 meter/sec
ZDOT = -2787
458110 ZDOT = -849
617232
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 09110
54624210
00010596 00000-0 82463-4 0 9050
2 25544 51
6403 242
4178 0008825 262
2150 97
8010 15
72242176 36887
Satellite: ISS
Catalog Number: 25544
Epoch time: 09110
54624210 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 242
4178 deg
Eccentricity:
0008825
Arg of perigee: 262
2150 deg
Mean anomaly: 97
8010 deg
Mean motion: 15
72242176 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3688
Checksum: 287
Coasting Arc #7 (Orbit 3703)
---------------------------------------
Vector Time (GMT): 2009/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3557218
21 A = 6737068
43 meter
Y = -5711056
66 meter E =
0007996
Z = 213484
57 I = 51
38403
XDOT = 4180
891423 Wp = 3
16773
YDOT = -2379
370058 meter/sec RA = 236
63042 deg
ZDOT = 6009
885182 TA = 359
15844
MA = 359
15978
Ha = 190
839 n
mi
Hp = 190
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11670663
41 X = -3494128
91
Y = -18737062
54 feet Y = -5750482
79 meter
Z = 700408
71 Z = 196356
96
XDOT = 13716
835376 XDOT = 4177
992033
YDOT = -7806
332212 feet/sec YDOT = -2332
632849 meter/sec
ZDOT = 19717
471071 ZDOT = 6030
189170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19281638
46 X = -5877043
40
Y = -10751284
42 feet Y = -3276991
49 meter
Z = 633064
80 Z = 192958
15
XDOT = 7344
822035 XDOT = 2238
701756
YDOT = -12006
111893 feet/sec YDOT = -3659
462905 meter/sec
ZDOT = 19796
605225 ZDOT = 6034
005273
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 09111
56319215
00010596 00000-0 82463-4 0 9060
2 25544 51
6412 237
2085 0008854 266
4139 93
6011 15
72277490 37042
Satellite: ISS
Catalog Number: 25544
Epoch time: 09111
56319215 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 237
2085 deg
Eccentricity:
0008854
Arg of perigee: 266
4139 deg
Mean anomaly: 93
6011 deg
Mean motion: 15
72277490 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3704
Checksum: 302
Coasting Arc #8 (Orbit 3718)
---------------------------------------
Vector Time (GMT): 2009/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3018906
77 A = 6724966
20 meter
Y = 2940889
21 meter E =
0006122
Z = -5245734
81 I = 51
36121
XDOT = -5016
582914 Wp = 81
52312
YDOT = -5821
670766 meter/sec RA = 231
49114 deg
ZDOT = -376
227926 TA = 184
88472
MA = 184
89070
Ha = 190
585 n
mi
Hp = 190
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9904549
76 X = -3026084
75
Y = 9648586
64 feet Y = 2907089
67 meter
Z = -17210416
05 Z = -5260418
41
XDOT = -16458
605360 XDOT = -4949
283497
YDOT = -19099
969705 feet/sec YDOT = -5877
392850 meter/sec
ZDOT = -1234
343589 ZDOT = -400
435081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3686411
25 X = -1123618
15
Y = 13252764
45 feet Y = 4039442
60 meter
Z = -17267552
15 Z = -5263149
90
XDOT = -22818
526252 XDOT = -6955
086801
YDOT = -8081
506154 feet/sec YDOT = -2463
243076 meter/sec
ZDOT = -1329
357825 ZDOT = -405
188265
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 09112
51657205
00010596 00000-0 82463-4 0 9071
2 25544 51
6415 232
3259 0008886 270
7621 89
2523 15
72312080 37193
Satellite: ISS
Catalog Number: 25544
Epoch time: 09112
51657205 = yrday
fracday
Element set: 907
Inclination: 51
6415 deg
RA of node: 232
3259 deg
Eccentricity:
0008886
Arg of perigee: 270
7621 deg
Mean anomaly: 89
2523 deg
Mean motion: 15
72312080 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3719
Checksum: 304
Coasting Arc #9 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2009/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5082399
00 A = 6736643
40 meter
Y = 4328881
34 meter E =
0007576
Z = 862656
81 I = 51
42032
XDOT = -2554
051813 Wp = 163
35629
YDOT = 4182
745894 meter/sec RA = 226
33874 deg
ZDOT = -5936
286308 TA = 7
20865
MA = 7
19776
Ha = 190
830 n
mi
Hp = 190
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16674537
39 X = 5029424
27
Y = 14202366
62 feet Y = 4385419
53 meter
Z = 2830238
88 Z = 887218
74
XDOT = -8379
435083 XDOT = -2571
796225
YDOT = 13722
919599 feet/sec YDOT = 4154
085593 meter/sec
ZDOT = -19476
004947 ZDOT = -5948
737351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21587167
21 X = 6579768
56
Y = 3631433
72 feet Y = 1106861
00 meter
Z = 2926528
29 Z = 892005
82
XDOT = 219
187507 XDOT = 66
808352
YDOT = 14446
040510 feet/sec YDOT = 4403
153147 meter/sec
ZDOT = -19524
325412 ZDOT = -5951
014385
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 09113
53349930
00010596 00000-0 82463-4 0 9088
2 25544 51
6418 227
1164 0008892 274
3194 85
6952 15
72310421 37356
Satellite: ISS
Catalog Number: 25544
Epoch time: 09113
53349930 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 227
1164 deg
Eccentricity:
0008892
Arg of perigee: 274
3194 deg
Mean anomaly: 85
6952 deg
Mean motion: 15
72310421 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3735
Checksum: 314
Coasting Arc #10 (Orbit 3750)
---------------------------------------
Vector Time (GMT): 2009/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1341080
29 A = 6725616
11 meter
Y = -4210138
45 meter E =
0005020
Z = 5074992
24 I = 51
40586
XDOT = 6414
741300 Wp = 252
59805
YDOT = 3945
615585 meter/sec RA = 221
22151 deg
ZDOT = 1577
915925 TA = 182
18979
MA = 182
19199
Ha = 190
959 n
mi
Hp = 189
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4399869
71 X = 1363405
14
Y = -13812790
19 feet Y = -4195016
83 meter
Z = 16650237
00 Z = 5081561
62
XDOT = 21045
739174 XDOT = 6362
478600
YDOT = 12944
933021 feet/sec YDOT = 4017
056766 meter/sec
ZDOT = 5176
889518 ZDOT = 1608
952443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3642507
25 X = -1110236
21
Y = -14001413
51 feet Y = -4267630
84 meter
Z = 16675580
32 Z = 5082716
88
XDOT = 23661
159640 XDOT = 7211
921458
YDOT = 155
659789 feet/sec YDOT = 47
445104 meter/sec
ZDOT = 5298
448667 ZDOT = 1614
967154
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 09114
55041264
00010596 00000-0 82463-4 0 9091
2 25544 51
6427 221
9070 0008939 278
9912 81
0238 15
72368276 37510
Satellite: ISS
Catalog Number: 25544
Epoch time: 09114
55041264 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 221
9070 deg
Eccentricity:
0008939
Arg of perigee: 278
9912 deg
Mean anomaly: 81
0238 deg
Mean motion: 15
72368276 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3751
Checksum: 321
Coasting Arc #11 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2009/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5963150
49 A = 6735355
49 meter
Y = -2487478
57 meter E =
0008773
Z = -1881359
69 I = 51
46149
XDOT = 411
154516 Wp = 331
03556
YDOT = -5242
133788 meter/sec RA = 216
05403 deg
ZDOT = 5624
432453 TA = 8
02271
MA = 8
00869
Ha = 191
316 n
mi
Hp = 189
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19564142
02 X = -5925752
36
Y = -8161018
91 feet Y = -2553952
85 meter
Z = -6172439
91 Z = -1910238
58
XDOT = 1348
932140 XDOT = 442
419240
YDOT = -17198
601667 feet/sec YDOT = -5237
361314 meter/sec
ZDOT = 18452
862377 ZDOT = 5626
505735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20830844
11 X = -6349241
29
Y = 3745099
25 feet Y = 1141506
25 meter
Z = -6285464
36 Z = -1915809
54
XDOT = -8018
574665 XDOT = -2444
061558
YDOT = -13599
700420 feet/sec YDOT = -4145
188688 meter/sec
ZDOT = 18460
564732 ZDOT = 5626
780130
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 09115
50376017
00010596 00000-0 82463-4 0 9106
2 25544 51
6427 217
0240 0008985 284
1715 75
8449 15
72324076 37667
Satellite: ISS
Catalog Number: 25544
Epoch time: 09115
50376017 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 217
0240 deg
Eccentricity:
0008985
Arg of perigee: 284
1715 deg
Mean anomaly: 75
8449 deg
Mean motion: 15
72324076 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3766
Checksum: 313
Coasting Arc #12 (Orbit 3781)
---------------------------------------
Vector Time (GMT): 2009/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 658914
64 A = 6727262
98 meter
Y = 4766556
46 meter E =
0006573
Z = -4705670
08 I = 51
45859
XDOT = -7003
712409 Wp = 17
60603
YDOT = -1697
594753 meter/sec RA = 210
95740 deg
ZDOT = -2695
075142 TA = 225
76161
MA = 225
81559
Ha = 191
517 n
mi
Hp = 189
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2161793
45 X = 628425
06
Y = 15638308
58 feet Y = 4773754
58 meter
Z = -15438550
12 Z = -4702542
82
XDOT = -22978
059084 XDOT = -6971
116592
YDOT = -5569
536590 feet/sec YDOT = -1775
731963 meter/sec
ZDOT = -8842
110045 ZDOT = -2729
020873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10582045
88 X = 3225407
59
Y = 11731947
03 feet Y = 3575897
45 meter
Z = -15425971
60 Z = -4701836
14
XDOT = -21286
114942 XDOT = -6488
007834
YDOT = 7376
589491 feet/sec YDOT = 2248
384477 meter/sec
ZDOT = -8974
883470 ZDOT = -2735
544482
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 09116
52065159
00010596 00000-0 82463-4 0 9112
2 25544 51
6422 211
8154 0008968 287
2328 72
7853 15
72358501 37826
Satellite: ISS
Catalog Number: 25544
Epoch time: 09116
52065159 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 211
8154 deg
Eccentricity:
0008968
Arg of perigee: 287
2328 deg
Mean anomaly: 72
7853 deg
Mean motion: 15
72358501 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3782
Checksum: 318
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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