Date:
July 2nd 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 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 810)
---------------------------------------
Vector Time (GMT): 2009/181/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -22553
90 A = 6725265
01 meter
Y = 5492304
66 meter E =
0009368
Z = -3883173
60 I = 51
36154
XDOT = -5874
360299 Wp = 126
87886
YDOT = -2881
778464 meter/sec RA = 235
82049 deg
ZDOT = -4054
099541 TA = 100
77465
MA = 100
66917
Ha = 191
618 n
mi
Hp = 182
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -73995
74 X = -65104
32
Y = 18019372
24 feet Y = 5491815
08 meter
Z = -12740070
88 Z = -3883385
75
XDOT = -19272
835626 XDOT = -5822
005043
YDOT = -9454
653752 feet/sec YDOT = -2947
175691 meter/sec
ZDOT = -13300
851513 ZDOT = -4082
510484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13405353
01 X = -4085951
60
Y = -12041021
09 feet Y = -3670103
23 meter
Z = -12740603
56 Z = -3883335
97
XDOT = 18982
860433 XDOT = 5785
975860
YDOT = -6984
671988 feet/sec YDOT = -2128
928022 meter/sec
ZDOT = -13412
420790 ZDOT = -4088
105857
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 09181
88395476
00010596 00000-0 82463-4 0 9009
2 25544 51
6396 236
5844 0007542 171
0204 189
1095 15
74122983 8112
Satellite: ISS
Catalog Number: 25544
Epoch time: 09181
88395476 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 236
5844 deg
Eccentricity:
0007542
Arg of perigee: 171
0204 deg
Mean anomaly: 189
1095 deg
Mean motion: 15
74122983 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 811
Checksum: 321
Coasting Arc #2 (Orbit 826)
---------------------------------------
Vector Time (GMT): 2009/182/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5337268
60 A = 6726459
55 meter
Y = 2098624
11 meter E =
0014629
Z = 3497133
36 I = 51
38303
XDOT = 489
670963 Wp = 118
63409
YDOT = 6247
406279 meter/sec RA = 230
61367 deg
ZDOT = -4489
136975 TA = 19
58174
MA = 19
52561
Ha = 191
454 n
mi
Hp = 182
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17510723
74 X = 5296416
25
Y = 6885249
69 feet Y = 2158079
59 meter
Z = 11473534
63 Z = 3522962
99
XDOT = 1606
532031 XDOT = 441
582492
YDOT = 20496
739761 feet/sec YDOT = 6252
613903 meter/sec
ZDOT = -14728
139681 ZDOT = -4486
873960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16632416
99 X = -5069560
70
Y = 8663568
18 feet Y = 2640655
58 meter
Z = 11574946
98 Z = 3528043
84
XDOT = -15958
815146 XDOT = -4864
246857
YDOT = -10941
221353 feet/sec YDOT = -3334
884268 meter/sec
ZDOT = -14718
923744 ZDOT = -4486
327957
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 09182
89971507
00010596 00000-0 82463-4 0 9017
2 25544 51
6393 231
3675 0007558 175
0583 185
0656 15
74102693 8276
Satellite: ISS
Catalog Number: 25544
Epoch time: 09182
89971507 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 231
3675 deg
Eccentricity:
0007558
Arg of perigee: 175
0583 deg
Mean anomaly: 185
0656 deg
Mean motion: 15
74102693 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 827
Checksum: 333
Coasting Arc #3 (Orbit 842)
---------------------------------------
Vector Time (GMT): 2009/183/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -862155
12 A = 6725117
05 meter
Y = -5374515
38 meter E =
0014596
Z = 3947263
42 I = 51
39828
XDOT = 6317
193754 Wp = 131
12254
YDOT = 1913
112155 meter/sec RA = 225
51113 deg
ZDOT = 3965
671990 TA = 277
57116
MA = 277
73694
Ha = 191
458 n
mi
Hp = 183
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2828592
91 X = -821167
43
Y = -17632924
47 feet Y = -5383928
03 meter
Z = 12950339
30 Z = 3943173
67
XDOT = 20725
701293 XDOT = 6276
066942
YDOT = 6276
614683 feet/sec YDOT = 1983
524054 meter/sec
ZDOT = 13010
734874 ZDOT = 3996
261433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15380330
50 X = 4687924
74
Y = 9098856
67 feet Y = 2773331
51 meter
Z = 12934005
27 Z = 3942284
81
XDOT = -17409
985295 XDOT = -5306
563518
YDOT = 10675
085836 feet/sec YDOT = 3253
766163 meter/sec
ZDOT = 13130
815635 ZDOT = 4002
272606
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 09183
91547470
00010596 00000-0 82463-4 0 9020
2 25544 51
6394 226
1499 0007490 178
9494 181
1686 15
74106707 8439
Satellite: ISS
Catalog Number: 25544
Epoch time: 09183
91547470 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 226
1499 deg
Eccentricity:
0007490
Arg of perigee: 178
9494 deg
Mean anomaly: 181
1686 deg
Mean motion: 15
74106707 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 843
Checksum: 339
Coasting Arc #4 (Orbit 857)
---------------------------------------
Vector Time (GMT): 2009/184/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5667425
45 A = 6726649
00 meter
Y = -1231337
47 meter E =
0009003
Z = -3419395
21 I = 51
42597
XDOT = -1452
748280 Wp = 149
09722
YDOT = -6012
504558 meter/sec RA = 220
30672 deg
ZDOT = 4570
683932 TA = 170
38888
MA = 170
37164
Ha = 191
292 n
mi
Hp = 183
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18593915
53 X = -5636624
42
Y = -4039821
11 feet Y = -1294541
07 meter
Z = -11218488
23 Z = -3446852
98
XDOT = -4766
234513 XDOT = -1407
611005
YDOT = -19726
064822 feet/sec YDOT = -6028
498540 meter/sec
ZDOT = 14995
682192 ZDOT = 4563
734966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14794658
76 X = 4509411
99
Y = -11863481
95 feet Y = -3615989
30 meter
Z = -11326261
32 Z = -3452244
45
XDOT = 17522
883340 XDOT = 5340
974842
YDOT = 7555
005436 feet/sec YDOT = 2302
765657 meter/sec
ZDOT = 14968
095235 ZDOT = 4562
275428
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 09184
86774897
00010596 00000-0 82463-4 0 9031
2 25544 51
6397 221
2585 0007449 182
7770 177
3353 15
74123436 8580
Satellite: ISS
Catalog Number: 25544
Epoch time: 09184
86774897 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 221
2585 deg
Eccentricity:
0007449
Arg of perigee: 182
7770 deg
Mean anomaly: 177
3353 deg
Mean motion: 15
74123436 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 858
Checksum: 351
Coasting Arc #5 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2009/185/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1655409
71 A = 6724746
63 meter
Y = 5112890
40 meter E =
0007781
Z = -4043855
59 I = 51
44304
XDOT = -6603
294142 Wp = 129
91228
YDOT = -901
253370 meter/sec RA = 215
20724 deg
ZDOT = -3852
462423 TA = 100
34117
MA = 100
25345
Ha = 191
138 n
mi
Hp = 183
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5431134
21 X = 1617757
70
Y = 16774574
81 feet Y = 5131192
45 meter
Z = -13267242
76 Z = -4035904
08
XDOT = -21664
350858 XDOT = -6574
010911
YDOT = -2956
868013 feet/sec YDOT = -974
930764 meter/sec
ZDOT = -12639
312413 ZDOT = -3884
470161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16610694
87 X = -5062939
80
Y = -5983526
92 feet Y = -1823779
01 meter
Z = -13235767
10 Z = -4034261
81
XDOT = 15183
335749 XDOT = 4627
880736
YDOT = -13984
850036 feet/sec YDOT = -4262
582291 meter/sec
ZDOT = -12764
931158 ZDOT = -3890
751017
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 09185
88350801
00010596 00000-0 82463-4 0 9040
2 25544 51
6399 216
0412 0007363 187
3259 172
7798 15
74122415 8747
Satellite: ISS
Catalog Number: 25544
Epoch time: 09185
88350801 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 216
0412 deg
Eccentricity:
0007363
Arg of perigee: 187
3259 deg
Mean anomaly: 172
7798 deg
Mean motion: 15
74122415 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 874
Checksum: 327
Coasting Arc #6 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2009/186/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5831775
03 A = 6726978
68 meter
Y = 314891
65 meter E =
0013454
Z = 3320752
69 I = 51
47491
XDOT = 2358
661234 Wp = 123
34701
YDOT = 5657
883621 meter/sec RA = 210
00702 deg
ZDOT = -4672
408995 TA = 17
46977
MA = 17
42353
Ha = 190
949 n
mi
Hp = 183
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19133120
19 X = 5811688
94
Y = 1033109
09 feet Y = 379993
00 meter
Z = 10894857
92 Z = 3349034
52
XDOT = 7738
389874 XDOT = 2317
916051
YDOT = 18562
610306 feet/sec YDOT = 5684
032669 meter/sec
ZDOT = -15329
425838 ZDOT = -4661
048541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12302295
23 X = -3749739
58
Y = 14607070
16 feet Y = 4452234
99 meter
Z = 11005842
31 Z = 3354580
74
XDOT = -18469
729580 XDOT = -5629
573576
YDOT = -4023
806526 feet/sec YDOT = -1226
456229 meter/sec
ZDOT = -15284
537844 ZDOT = -4658
727135
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 09186
89926804
00010596 00000-0 82463-4 0 9055
2 25544 51
6391 210
8240 0007346 190
5042 169
5968 15
74103772 8903
Satellite: ISS
Catalog Number: 25544
Epoch time: 09186
89926804 = yrday
fracday
Element set: 905
Inclination: 51
6391 deg
RA of node: 210
8240 deg
Eccentricity:
0007346
Arg of perigee: 190
5042 deg
Mean anomaly: 169
5968 deg
Mean motion: 15
74103772 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 890
Checksum: 328
Coasting Arc #7 (Orbit 905)
---------------------------------------
Vector Time (GMT): 2009/187/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2434973
13 A = 6724597
38 meter
Y = -4734234
06 meter E =
0012714
Z = 4107730
04 I = 51
49336
XDOT = 6716
776314 Wp = 139
05098
YDOT = -178
746150 meter/sec RA = 204
91001 deg
ZDOT = 3759
540298 TA = 272
26873
MA = 272
41430
Ha = 190
931 n
mi
Hp = 183
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7988757
00 X = -2401807
52
Y = -15532263
97 feet Y = -4761278
71 meter
Z = 13476804
59 Z = 4095980
71
XDOT = 22036
667698 XDOT = 6700
012929
YDOT = -586
437501 feet/sec YDOT = -103
729691 meter/sec
ZDOT = 12334
449796 ZDOT = 3792
129270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17306509
59 X = 5275024
12
Y = 2608434
71 feet Y = 795050
90 meter
Z = 13430432
54 Z = 4093595
84
XDOT = -12251
494257 XDOT = -3734
255450
YDOT = 16848
532518 feet/sec YDOT = 5135
432711 meter/sec
ZDOT = 12462
323431 ZDOT = 3798
516182
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 09187
91502665
00010596 00000-0 82463-4 0 9065
2 25544 51
6394 205
6060 0007261 195
0137 165
0812 15
74103641 9061
Satellite: ISS
Catalog Number: 25544
Epoch time: 09187
91502665 = yrday
fracday
Element set: 906
Inclination: 51
6394 deg
RA of node: 205
6060 deg
Eccentricity:
0007261
Arg of perigee: 195
0137 deg
Mean anomaly: 165
0812 deg
Mean motion: 15
74103641 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 906
Checksum: 296
Coasting Arc #8 (Orbit 920)
---------------------------------------
Vector Time (GMT): 2009/188/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5867839
77 A = 6727199
26 meter
Y = 630351
22 meter E =
0006711
Z = -3237837
28 I = 51
53006
XDOT = -3176
857666 Wp = 161
60570
YDOT = -5148
706790 meter/sec RA = 199
71339 deg
ZDOT = 4751
376634 TA = 160
48911
MA = 160
46341
Ha = 190
700 n
mi
Hp = 183
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19251442
81 X = -5858723
76
Y = 2068081
43 feet Y = 564785
17 meter
Z = -10622825
73 Z = -3266320
57
XDOT = -10422
761372 XDOT = -3142
128824
YDOT = -16892
082645 feet/sec YDOT = -5184
038961 meter/sec
ZDOT = 15588
506017 ZDOT = 4736
027097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9322021
91 X = 2841352
28
Y = -16899946
92 feet Y = -5151103
82 meter
Z = -10734576
80 Z = -3271899
01
XDOT = 18634
107230 XDOT = 5679
675884
YDOT = 408
069625 feet/sec YDOT = 124
379622 meter/sec
ZDOT = 15527
970475 ZDOT = 4732
925401
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 09188
86729968
00010596 00000-0 82463-4 0 9078
2 25544 51
6393 200
7143 0007241 200
1483 159
9395 15
74114343 9214
Satellite: ISS
Catalog Number: 25544
Epoch time: 09188
86729968 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 200
7143 deg
Eccentricity:
0007241
Arg of perigee: 200
1483 deg
Mean anomaly: 159
9395 deg
Mean motion: 15
74114343 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 921
Checksum: 322
Coasting Arc #9 (Orbit 936)
---------------------------------------
Vector Time (GMT): 2009/189/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3091081
20 A = 6724272
98 meter
Y = 4250009
57 meter E =
0005912
Z = -4196372
00 I = 51
54816
XDOT = -6663
358765 Wp = 130
85789
YDOT = 1253
662342 meter/sec RA = 194
61998 deg
ZDOT = -3645
732984 TA = 101
96628
MA = 101
90000
Ha = 190
588 n
mi
Hp = 184
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10141342
51 X = 3063712
01
Y = 13943600
95 feet Y = 4284423
52 meter
Z = -13767624
69 Z = -4181421
55
XDOT = -21861
413271 XDOT = -6659
172182
YDOT = 4113
065427 feet/sec YDOT = 1179
172784 meter/sec
ZDOT = -11961
066221 ZDOT = -3678
092669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17275724
52 X = -5265640
83
Y = 662825
02 feet Y = 202029
07 meter
Z = -13708695
43 Z = -4178410
37
XDOT = 8840
682340 XDOT = 2694
639977
YDOT = -19099
026990 feet/sec YDOT = -5821
383427 meter/sec
ZDOT = -12088
009422 ZDOT = -3684
425272
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 09189
88305804
00010596 00000-0 82463-4 0 9081
2 25544 51
6392 195
4965 0007284 205
0245 155
0566 15
74107918 9376
Satellite: ISS
Catalog Number: 25544
Epoch time: 09189
88305804 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 195
4965 deg
Eccentricity:
0007284
Arg of perigee: 205
0245 deg
Mean anomaly: 155
0566 deg
Mean motion: 15
74107918 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 937
Checksum: 337
Coasting Arc #10 (Orbit 952)
---------------------------------------
Vector Time (GMT): 2009/190/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5729152
23 A = 6727402
37 meter
Y = -1572371
10 meter E =
0011911
Z = 3139914
11 I = 51
58879
XDOT = 3905
977577 Wp = 126
92989
YDOT = 4543
704251 meter/sec RA = 189
42856 deg
ZDOT = -4846
021562 TA = 16
46249
MA = 16
42384
Ha = 190
254 n
mi
Hp = 184
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18796431
18 X = 5731056
07
Y = -5158697
82 feet Y = -1508294
18 meter
Z = 10301555
48 Z = 3167750
26
XDOT = 12814
887065 XDOT = 3878
419496
YDOT = 14907
166177 feet/sec YDOT = 4587
229806 meter/sec
ZDOT = -15899
020874 ZDOT = -4827
112911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5897748
82 X = -1797633
84
Y = 18516835
16 feet Y = 5643931
36 meter
Z = 10410735
24 Z = 3173192
10
XDOT = -18184
248602 XDOT = -5542
558974
YDOT = 3115
367429 feet/sec YDOT = 949
563992 meter/sec
ZDOT = -15824
525400 ZDOT = -4823
315342
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 09190
89881676
00010596 00000-0 82463-4 0 9091
2 25544 51
6395 190
2791 0007115 208
3540 151
7237 15
74136781 9532
Satellite: ISS
Catalog Number: 25544
Epoch time: 09190
89881676 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 190
2791 deg
Eccentricity:
0007115
Arg of perigee: 208
3540 deg
Mean anomaly: 151
7237 deg
Mean motion: 15
74136781 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 953
Checksum: 333
Coasting Arc #11 (Orbit 968)
---------------------------------------
Vector Time (GMT): 2009/191/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3693939
23 A = 6724119
46 meter
Y = -3665052
42 meter E =
0010628
Z = 4259310
81 I = 51
60619
XDOT = 6421
483292 Wp = 147
40194
YDOT = -2333
005888 meter/sec RA = 184
33805 deg
ZDOT = 3548
709658 TA = 266
51381
MA = 266
63537
Ha = 190
310 n
mi
Hp = 184
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12119223
18 X = -3673372
08
Y = -12024450
21 feet Y = -3706245
76 meter
Z = 13974116
84 Z = 4241415
43
XDOT = 21067
858569 XDOT = 6429
855387
YDOT = -7654
218794 feet/sec YDOT = -2261
150744 meter/sec
ZDOT = 11642
748222 ZDOT = 3579
924774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16667434
87 X = 5080234
15
Y = -3952758
42 feet Y = -1204800
77 meter
Z = 13903640
91 Z = 4237829
75
XDOT = -4954
056900 XDOT = -1509
996543
YDOT = 20643
377763 feet/sec YDOT = 6292
101542 meter/sec
ZDOT = 11765
157339 ZDOT = 3586
019957
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 09191
91457647
00010596 00000-0 82463-4 0 9104
2 25544 51
6391 185
0607 0007084 212
5155 147
5572 15
74088011 9694
Satellite: ISS
Catalog Number: 25544
Epoch time: 09191
91457647 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 185
0607 deg
Eccentricity:
0007084
Arg of perigee: 212
5155 deg
Mean anomaly: 147
5572 deg
Mean motion: 15
74088011 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 969
Checksum: 318
Coasting Arc #12 (Orbit 983)
---------------------------------------
Vector Time (GMT): 2009/192/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5453694
82 A = 6727715
05 meter
Y = 2496586
43 meter E =
0004573
Z = -3052850
20 I = 51
64823
XDOT = -4509
490459 Wp = 180
69417
YDOT = -3827
413093 meter/sec RA = 179
15074 deg
ZDOT = 4921
296681 TA = 143
96650
MA = 143
93566
Ha = 190
072 n
mi
Hp = 184
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17892699
53 X = -5466376
74
Y = 8190900
36 feet Y = 2435529
45 meter
Z = -10015912
73 Z = -3079374
44
XDOT = -14794
916203 XDOT = -4490
262971
YDOT = -12557
129570 feet/sec YDOT = -3877
733888 meter/sec
ZDOT = 16145
986486 ZDOT = 4899
436146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2194848
99 X = 668989
97
Y = -19502006
27 feet Y = -5944211
51 meter
Z = -10119903
28 Z = -3084546
52
XDOT = 17019
158239 XDOT = 5187
439431
YDOT = -6426
025850 feet/sec YDOT = -1958
652679 meter/sec
ZDOT = 16059
923971 ZDOT = 4895
064826
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 09192
86684883
00010596 00000-0 82463-4 0 9114
2 25544 51
6387 180
1687 0007239 217
3069 142
7592 15
74114201 9849
Satellite: ISS
Catalog Number: 25544
Epoch time: 09192
86684883 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 180
1687 deg
Eccentricity:
0007239
Arg of perigee: 217
3069 deg
Mean anomaly: 142
7592 deg
Mean motion: 15
74114201 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 984
Checksum: 333
Coasting Arc #13 (Orbit 999)
---------------------------------------
Vector Time (GMT): 2009/193/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4157849
03 A = 6723769
98 meter
Y = 3017618
82 meter E =
0004195
Z = -4339231
70 I = 51
66356
XDOT = -6016
354888 Wp = 124
35048
YDOT = 3356
668932 meter/sec RA = 174
06446 deg
ZDOT = -3435
222921 TA = 110
99895
MA = 110
95407
Ha = 189
996 n
mi
Hp = 185
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13641236
98 X = 4144875
49
Y = 9900324
21 feet Y = 3064042
21 meter
Z = -14236324
47 Z = -4319064
27
XDOT = -19738
697138 XDOT = -6036
755050
YDOT = 11012
693348 feet/sec YDOT = 3289
276805 meter/sec
ZDOT = -11270
416407 ZDOT = -3464
499319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15448127
94 X = -4708589
40
Y = 6907153
07 feet Y = 2105300
25 meter
Z = -14156951
65 Z = -4315038
86
XDOT = 843
787553 XDOT = 257
186446
YDOT = -21416
355703 feet/sec YDOT = -6527
705218 meter/sec
ZDOT = -11385
168437 ZDOT = -3470
199339
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 09193
88260753
00010596 00000-0 82463-4 0 9124
2 25544 51
6378 174
9511 0007244 221
2482 138
8135 15
74107484 10009
Satellite: ISS
Catalog Number: 25544
Epoch time: 09193
88260753 = yrday
fracday
Element set: 912
Inclination: 51
6378 deg
RA of node: 174
9511 deg
Eccentricity:
0007244
Arg of perigee: 221
2482 deg
Mean anomaly: 138
8135 deg
Mean motion: 15
74107484 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1000
Checksum: 303
Coasting Arc #14 (Orbit 1015)
---------------------------------------
Vector Time (GMT): 2009/194/20:39:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5012686
57 A = 6727850
49 meter
Y = -3363205
04 meter E =
0010322
Z = 2955694
29 I = 51
70836
XDOT = 5000
130705 Wp = 129
65491
YDOT = 3046
885274 meter/sec RA = 168
88282 deg
ZDOT = -5007
902151 TA = 16
26879
MA = 16
23568
Ha = 189
562 n
mi
Hp = 185
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16445822
09 X = 5035563
80
Y = -11034137
26 feet Y = -3307022
61 meter
Z = 9697159
74 Z = 2980101
04
XDOT = 16404
628297 XDOT = 4990
015646
YDOT = 9996
342761 feet/sec YDOT = 3102
743590 meter/sec
ZDOT = -16430
125166 ZDOT = -4983
635917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1664336
80 X = 507289
86
Y = 19687134
23 feet Y = 6000638
51 meter
Z = 9792797
60 Z = 2984844
71
XDOT = -15326
152891 XDOT = -4671
411401
YDOT = 9429
042653 feet/sec YDOT = 2873
972200 meter/sec
ZDOT = -16334
649465 ZDOT = -4978
801157
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 09194
89836502
00010596 00000-0 82463-4 0 9138
2 25544 51
6386 169
7335 0007179 226
4205 133
6363 15
74157333 10162
Satellite: ISS
Catalog Number: 25544
Epoch time: 09194
89836502 = yrday
fracday
Element set: 913
Inclination: 51
6386 deg
RA of node: 169
7335 deg
Eccentricity:
0007179
Arg of perigee: 226
4205 deg
Mean anomaly: 133
6363 deg
Mean motion: 15
74157333 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1016
Checksum: 320
Coasting Arc #15 (Orbit 1031)
---------------------------------------
Vector Time (GMT): 2009/195/20:43:09
674
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3079651
63 A = 6721069
19 meter
Y = -3235166
91 meter E =
0007948
Z = 5024984
53 I = 51
71213
XDOT = 6634
516628 Wp = 185
42934
YDOT = -3444
198986 meter/sec RA = 163
77599 deg
ZDOT = 1841
123788 TA = 246
78960
MA = 246
87333
Ha = 189
707 n
mi
Hp = 185
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10103843
92 X = -3067656
98
Y = -10614064
65 feet Y = -3269538
83 meter
Z = 16486169
72 Z = 5010052
40
XDOT = 21766
786837 XDOT = 6663
593322
YDOT = -11299
865441 feet/sec YDOT = -3369
845551 meter/sec
ZDOT = 6040
432376 ZDOT = 1873
424497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14097060
82 X = 4296784
14
Y = -4237381
96 feet Y = -1291554
02 meter
Z = 16427333
70 Z = 5007051
31
XDOT = -162
089317 XDOT = -49
404824
YDOT = 23465
135199 feet/sec YDOT = 7152
173209 meter/sec
ZDOT = 6167
075203 ZDOT = 1879
724522
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 09195
91412645
00010596 00000-0 82463-4 0 9141
2 25544 51
6372 164
5150 0007110 228
7140 131
3411 15
74071777 10327
Satellite: ISS
Catalog Number: 25544
Epoch time: 09195
91412645 = yrday
fracday
Element set: 914
Inclination: 51
6372 deg
RA of node: 164
5150 deg
Eccentricity:
0007110
Arg of perigee: 228
7140 deg
Mean anomaly: 131
3411 deg
Mean motion: 15
74071777 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1032
Checksum: 278
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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