Date:
November 10th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 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 2884)
---------------------------------------
Vector Time (GMT): 2009/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1087988
82 A = 6726350
10 meter
Y = 6634521
76 meter E =
0006036
Z = 54507
42 I = 51
33265
XDOT = -4756
976207 Wp = 136
81427
YDOT = -727
505470 meter/sec RA = 279
68471 deg
ZDOT = -6012
835961 TA = 42
59080
MA = 42
54400
Ha = 186
479 n
mi
Hp = 182
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3569517
11 X = -1162361
12
Y = 21766803
67 feet Y = 6621939
39 meter
Z = 178830
13 Z = 49041
44
XDOT = -15606
877320 XDOT = -4719
277909
YDOT = -2386
828971 feet/sec YDOT = -780
489832 meter/sec
ZDOT = -19727
152102 ZDOT = -6035
854105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13794015
29 X = -4204415
86
Y = -17212422
98 feet Y = -5246346
52 meter
Z = 157518
92 Z = 48011
77
XDOT = 10880
461244 XDOT = 3316
364587
YDOT = -8914
173326 feet/sec YDOT = -2717
040030 meter/sec
ZDOT = -19817
963592 ZDOT = -6040
515303
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 09313
53181450
00016717 00000-0 10270-3 0 9000
2 25544 51
6422 280
2424 0006347 311
8936 48
1687 15
76048375 28858
Satellite: ISS
Catalog Number: 25544
Epoch time: 09313
53181450 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 280
2424 deg
Eccentricity:
0006347
Arg of perigee: 311
8936 deg
Mean anomaly: 48
1687 deg
Mean motion: 15
76048375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2885
Checksum: 312
Coasting Arc #2 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2009/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4090039
13 A = 6714412
59 meter
Y = 1154269
46 meter E =
0006242
Z = 5200456
22 I = 51
28855
XDOT = -1190
792664 Wp = 343
86887
YDOT = 7574
412734 meter/sec RA = 274
50444 deg
ZDOT = -738
943714 TA = 113
22574
MA = 113
16000
Ha = 186
509 n
mi
Hp = 182
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13418763
55 X = 4051564
65
Y = 3786973
30 feet Y = 1199791
54 meter
Z = 17061864
24 Z = 5220232
48
XDOT = -3906
800079 XDOT = -1271
812856
YDOT = 24850
435478 feet/sec YDOT = 7560
643584 meter/sec
ZDOT = -2424
356018 ZDOT = -744
925426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11594980
76 X = -3534150
13
Y = 7569115
83 feet Y = 2307066
50 meter
Z = 17139909
57 Z = 5224244
44
XDOT = -15652
400765 XDOT = -4770
851753
YDOT = -18392
795842 feet/sec YDOT = -5606
124173 meter/sec
ZDOT = -2447
656303 ZDOT = -746
045641
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 09314
54632124
00016717 00000-0 10270-3 0 9012
2 25544 51
6421 275
0172 0006348 315
4235 44
6418 15
76060943 29019
Satellite: ISS
Catalog Number: 25544
Epoch time: 09314
54632124 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 275
0172 deg
Eccentricity:
0006348
Arg of perigee: 315
4235 deg
Mean anomaly: 44
6418 deg
Mean motion: 15
76060943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 285
Coasting Arc #3 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2009/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 996615
16 A = 6725374
41 meter
Y = -6505980
40 meter E =
0014166
Z = 1337441
21 I = 51
32492
XDOT = 4679
490897 Wp = 34
06779
YDOT = 1916
671854 meter/sec RA = 269
34841 deg
ZDOT = 5818
559170 TA = 340
70976
MA = 340
76333
Ha = 186
568 n
mi
Hp = 181
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3269734
77 X = 1062794
93
Y = -21345080
05 feet Y = -6494465
62 meter
Z = 4387930
49 Z = 1342443
66
XDOT = 15352
660423 XDOT = 4629
444507
YDOT = 6288
293483 feet/sec YDOT = 1968
720897 meter/sec
ZDOT = 19089
761055 ZDOT = 5841
170982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14264676
25 X = 4347873
32
Y = 16206522
02 feet Y = 4939747
91 meter
Z = 4407402
55 Z = 1343376
30
XDOT = -13432
856310 XDOT = -4094
334603
YDOT = 6591
495285 feet/sec YDOT = 2009
087763 meter/sec
ZDOT = 19179
023568 ZDOT = 5845
766384
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 09315
56080674
00016717 00000-0 10270-3 0 9023
2 25544 51
6421 269
7911 0006290 318
6179 41
4508 15
76118544 29171
Satellite: ISS
Catalog Number: 25544
Epoch time: 09315
56080674 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 269
7911 deg
Eccentricity:
0006290
Arg of perigee: 318
6179 deg
Mean anomaly: 41
4508 deg
Mean motion: 15
76118544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2917
Checksum: 318
Coasting Arc #4 (Orbit 2931)
---------------------------------------
Vector Time (GMT): 2009/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4122156
38 A = 6715834
81 meter
Y = -2178176
66 meter E =
0007988
Z = -4840005
41 I = 51
29484
XDOT = 1120
816985 Wp = 78
79678
YDOT = -7256
345920 meter/sec RA = 264
14142 deg
ZDOT = 2315
794006 TA = 213
84928
MA = 213
90029
Ha = 186
719 n
mi
Hp = 181
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13524135
10 X = -4073980
83
Y = -7146248
90 feet Y = -2224003
72 meter
Z = -15879282
84 Z = -4859914
28
XDOT = 3677
221081 XDOT = 1190
625434
YDOT = -23806
909187 feet/sec YDOT = -7243
421948 meter/sec
ZDOT = 7597
749363 ZDOT = 2321
408682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14008374
73 X = 4269752
62
Y = -5935795
27 feet Y = -1809230
40 meter
Z = -15957897
69 Z = -4863967
22
XDOT = 15776
398682 XDOT = 4808
646318
YDOT = 16789
129676 feet/sec YDOT = 5117
326725 meter/sec
ZDOT = 7619
601137 ZDOT = 2322
454427
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 09316
51187078
00016717 00000-0 10270-3 0 9036
2 25544 51
6425 264
8918 0006430 322
7347 37
3371 15
76121757 29326
Satellite: ISS
Catalog Number: 25544
Epoch time: 09316
51187078 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 264
8918 deg
Eccentricity:
0006430
Arg of perigee: 322
7347 deg
Mean anomaly: 37
3371 deg
Mean motion: 15
76121757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2932
Checksum: 316
Coasting Arc #5 (Orbit 2947)
---------------------------------------
Vector Time (GMT): 2009/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1005191
32 A = 6722862
13 meter
Y = 6084100
37 meter E =
0002726
Z = -2682044
12 I = 51
32404
XDOT = -4809
387263 Wp = 10
81283
YDOT = -3072
721364 meter/sec RA = 259
00742 deg
ZDOT = -5166
053626 TA = 199
90975
MA = 199
92039
Ha = 186
895 n
mi
Hp = 181
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3297871
79 X = -1060120
83
Y = 19960959
24 feet Y = 6072552
62 meter
Z = -8799357
36 Z = -2687060
88
XDOT = -15778
829604 XDOT = -4749
573646
YDOT = -10081
106836 feet/sec YDOT = -3126
168309 meter/sec
ZDOT = -16948
994837 ZDOT = -5189
273011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13721970
03 X = -4182456
46
Y = -14855273
25 feet Y = -4527887
29 meter
Z = -8818896
58 Z = -2687999
68
XDOT = 16517
888826 XDOT = 5034
652514
YDOT = -5137
973676 feet/sec YDOT = -1566
054377 meter/sec
ZDOT = -17040
706610 ZDOT = -5194
007375
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 09317
52631937
00016717 00000-0 10270-3 0 9047
2 25544 51
6433 259
6656 0006466 326
9410 33
1349 15
76168583 29486
Satellite: ISS
Catalog Number: 25544
Epoch time: 09317
52631937 = yrday
fracday
Element set: 904
Inclination: 51
6433 deg
RA of node: 259
6656 deg
Eccentricity:
0006466
Arg of perigee: 326
9410 deg
Mean anomaly: 33
1349 deg
Mean motion: 15
76168583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2948
Checksum: 337
Coasting Arc #6 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2009/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4315570
23 A = 6718596
37 meter
Y = 3140820
93 meter E =
0010764
Z = 4080145
63 I = 51
31731
XDOT = -1225
568885 Wp = 40
65821
YDOT = 6602
751629 meter/sec RA = 253
78420 deg
ZDOT = -3772
746932 TA = 88
26512
MA = 88
14184
Ha = 186
934 n
mi
Hp = 181
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14158694
98 X = 4260307
04
Y = 10304530
60 feet Y = 3188771
09 meter
Z = 13386304
55 Z = 4100977
16
XDOT = -4020
895293 XDOT = -1280
983020
YDOT = 21662
570960 feet/sec YDOT = 6588
736850 meter/sec
ZDOT = -12377
778647 ZDOT = -3778
835375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16707680
98 X = -5092501
16
Y = 5029439
06 feet Y = 1532973
03 meter
Z = 13468603
60 Z = 4105230
38
XDOT = -14543
768246 XDOT = -4432
940561
YDOT = -14984
204130 feet/sec YDOT = -4567
185419 meter/sec
ZDOT = -12401
524537 ZDOT = -3779
984679
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 09318
54074858
00016717 00000-0 10270-3 0 9054
2 25544 51
6437 254
4398 0006452 330
4579 29
6220 15
76193251 29643
Satellite: ISS
Catalog Number: 25544
Epoch time: 09318
54074858 = yrday
fracday
Element set: 905
Inclination: 51
6437 deg
RA of node: 254
4398 deg
Eccentricity:
0006452
Arg of perigee: 330
4579 deg
Mean anomaly: 29
6220 deg
Mean motion: 15
76193251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 331
Coasting Arc #7 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2009/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1193633
93 A = 6719400
82 meter
Y = -5379285
24 meter E =
0009339
Z = 3835170
66 I = 51
33012
XDOT = 5110
301210 Wp = 64
65003
YDOT = 4060
769701 meter/sec RA = 248
66104 deg
ZDOT = 4101
405840 TA = 342
37778
MA = 342
41016
Ha = 186
978 n
mi
Hp = 181
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3916121
83 X = 1235066
15
Y = -17648573
62 feet Y = -5365705
84 meter
Z = 12582580
91 Z = 3841069
91
XDOT = 16766
080086 XDOT = 5044
588625
YDOT = 13322
735239 feet/sec YDOT = 4117
548489 meter/sec
ZDOT = 13456
055905 ZDOT = 4126
073063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12004564
65 X = 3658991
31
Y = 13495108
36 feet Y = 4113309
03 meter
Z = 12605632
92 Z = 3842196
91
XDOT = -19609
077228 XDOT = -5976
846739
YDOT = 4771
380542 feet/sec YDOT = 1454
316789 meter/sec
ZDOT = 13553
527191 ZDOT = 4131
115088
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 09319
55515797
00016717 00000-0 10270-3 0 9069
2 25544 51
6440 249
2136 0006413 334
1895 25
8949 15
76226698 29804
Satellite: ISS
Catalog Number: 25544
Epoch time: 09319
55515797 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 249
2136 deg
Eccentricity:
0006413
Arg of perigee: 334
1895 deg
Mean anomaly: 25
8949 deg
Mean motion: 15
76226698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 347
Coasting Arc #8 (Orbit 2994)
---------------------------------------
Vector Time (GMT): 2009/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4607277
86 A = 6721819
78 meter
Y = -3869739
92 meter E =
0007674
Z = -2989160
95 I = 51
35080
XDOT = 1577
440217 Wp = 13
86813
YDOT = -5691
819375 meter/sec RA = 243
43648 deg
ZDOT = 4947
186091 TA = 311
40306
MA = 311
46900
Ha = 187
063 n
mi
Hp = 180
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15115741
00 X = -4549142
06
Y = -12695997
12 feet Y = -3920935
96 meter
Z = -9806958
48 Z = -3011402
86
XDOT = 5175
328797 XDOT = 1616
936600
YDOT = -18673
948082 feet/sec YDOT = -5673
959018 meter/sec
ZDOT = 16230
925496 ZDOT = 4954
945081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19043871
75 X = 5804572
11
Y = -5027234
10 feet Y = -1532300
95 meter
Z = -9894860
77 Z = -3015953
56
XDOT = 11996
052251 XDOT = 3656
396726
YDOT = 13500
164435 feet/sec YDOT = 4114
850120 meter/sec
ZDOT = 16261
304577 ZDOT = 4956
445635
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 09320
50614959
00016717 00000-0 10270-3 0 9077
2 25544 51
6440 244
3141 0006506 337
6587 22
4293 15
76245799 29959
Satellite: ISS
Catalog Number: 25544
Epoch time: 09320
50614959 = yrday
fracday
Element set: 907
Inclination: 51
6440 deg
RA of node: 244
3141 deg
Eccentricity:
0006506
Arg of perigee: 337
6587 deg
Mean anomaly: 22
4293 deg
Mean motion: 15
76245799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2995
Checksum: 330
Coasting Arc #9 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2009/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1642482
29 A = 6715958
19 meter
Y = 4509682
50 meter E =
0013136
Z = -4709460
40 I = 51
34657
XDOT = -5433
357004 Wp = 41
73293
YDOT = -4757
569909 meter/sec RA = 238
30856 deg
ZDOT = -2655
384904 TA = 202
01362
MA = 202
07009
Ha = 187
224 n
mi
Hp = 180
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5388721
42 X = -1669909
90
Y = 14795546
26 feet Y = 4491162
36 meter
Z = -15450985
56 Z = -4717506
03
XDOT = -17825
974424 XDOT = -5366
853451
YDOT = -15608
825160 feet/sec YDOT = -4817
956834 meter/sec
ZDOT = -8711
892729 ZDOT = -2681
619798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9282881
30 X = -2829422
22
Y = -12680627
57 feet Y = -3865055
28 meter
Z = -15482547
01 Z = -4719080
33
XDOT = 21964
798585 XDOT = 6694
870609
YDOT = -5294
235627 feet/sec YDOT = -1613
683019 meter/sec
ZDOT = -8815
592931 ZDOT = -2686
992725
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 09321
52052159
00016717 00000-0 10270-3 0 9089
2 25544 51
6447 239
0878 0006496 342
3809 17
7129 15
76297057 30111
Satellite: ISS
Catalog Number: 25544
Epoch time: 09321
52052159 = yrday
fracday
Element set: 908
Inclination: 51
6447 deg
RA of node: 239
0878 deg
Eccentricity:
0006496
Arg of perigee: 342
3809 deg
Mean anomaly: 17
7129 deg
Mean motion: 15
76297057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3011
Checksum: 324
Coasting Arc #10 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2009/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4860606
19 A = 6724499
06 meter
Y = 4364136
22 meter E =
0010993
Z = 1586308
05 I = 51
39215
XDOT = -2261
453353 Wp = 90
73886
YDOT = 4615
890415 meter/sec RA = 233
10047 deg
ZDOT = -5735
535740 TA = 71
68428
MA = 71
56472
Ha = 187
306 n
mi
Hp = 180
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15946870
72 X = 4803738
22
Y = 14318032
22 feet Y = 4418172
26 meter
Z = 5204422
74 Z = 1609783
78
XDOT = -7419
466382 XDOT = -2285
038073
YDOT = 15143
997426 feet/sec YDOT = 4590
470224 meter/sec
ZDOT = -18817
374474 ZDOT = -5746
578977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20686951
09 X = -6305382
69
Y = 5512180
98 feet Y = 1680112
76 meter
Z = 5297231
73 Z = 1614596
23
XDOT = -8291
115398 XDOT = -2527
131973
YDOT = -12885
401894 feet/sec YDOT = -3927
470497 meter/sec
ZDOT = -18860
762843 ZDOT = -5748
760515
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 09322
53487467
00016717 00000-0 10270-3 0 9096
2 25544 51
6444 233
8615 0006460 345
6503 14
4477 15
76301501 30274
Satellite: ISS
Catalog Number: 25544
Epoch time: 09322
53487467 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 233
8615 deg
Eccentricity:
0006460
Arg of perigee: 345
6503 deg
Mean anomaly: 14
4477 deg
Mean motion: 15
76301501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 304
Coasting Arc #11 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2009/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2370360
90 A = 6713663
95 meter
Y = -3550756
60 meter E =
0004748
Z = 5179331
88 I = 51
37498
XDOT = 5657
927935 Wp = 20
86762
YDOT = 5147
522773 meter/sec RA = 227
95257 deg
ZDOT = 943
666769 TA = 60
13912
MA = 60
09195
Ha = 187
210 n
mi
Hp = 180
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7776774
61 X = 2384729
13
Y = -11649463
90 feet Y = -3524170
04 meter
Z = 16992558
66 Z = 5190881
86
XDOT = 18562
755692 XDOT = 5595
362665
YDOT = 16888
198074 feet/sec YDOT = 5210
443137 meter/sec
ZDOT = 3096
019583 ZDOT = 971
002137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5784112
98 X = 1762997
64
Y = 12695908
03 feet Y = 3869712
77 meter
Z = 17037993
97 Z = 5193180
56
XDOT = -23237
376290 XDOT = -7082
752293
YDOT = 6304
811106 feet/sec YDOT = 1921
706425 meter/sec
ZDOT = 3204
104640 ZDOT = 976
611094
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 09323
54920693
00016717 00000-0 10270-3 0 9103
2 25544 51
6442 228
6349 0006487 348
4584 11
6431 15
76367317 30431
Satellite: ISS
Catalog Number: 25544
Epoch time: 09323
54920693 = yrday
fracday
Element set: 910
Inclination: 51
6442 deg
RA of node: 228
6349 deg
Eccentricity:
0006487
Arg of perigee: 348
4584 deg
Mean anomaly: 11
6431 deg
Mean motion: 15
76367317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 318
Coasting Arc #12 (Orbit 3057)
---------------------------------------
Vector Time (GMT): 2009/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4949106
24 A = 6725474
06 meter
Y = -4538782
28 meter E =
0017023
Z = -36763
93 I = 51
43592
XDOT = 3228
835152 Wp = 27
17613
YDOT = -3560
589305 meter/sec RA = 222
77375 deg
ZDOT = 6028
542020 TA = 332
42271
MA = 332
51291
Ha = 187
427 n
mi
Hp = 180
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16237225
20 X = -4897806
36
Y = -14891017
98 feet Y = -4593839
27 meter
Z = -120616
55 Z = -60682
96
XDOT = 10593
291182 XDOT = 3239
124245
YDOT = -11681
723441 feet/sec YDOT = -3524
425669 meter/sec
ZDOT = 19778
681168 ZDOT = 6044
252588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21140947
14 X = 6443760
69
Y = -6198264
78 feet Y = -1889231
10 meter
Z = -215208
87 Z = -65595
66
XDOT = 4129
407663 XDOT = 1258
643456
YDOT = 13466
392425 feet/sec YDOT = 4104
556411 meter/sec
ZDOT = 19840
540592 ZDOT = 6047
396773
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 09324
50012842
00016717 00000-0 10270-3 0 9119
2 25544 51
6443 223
7348 0006605 352
5465 7
5601 15
76358578 30581
Satellite: ISS
Catalog Number: 25544
Epoch time: 09324
50012842 = yrday
fracday
Element set: 911
Inclination: 51
6443 deg
RA of node: 223
7348 deg
Eccentricity:
0006605
Arg of perigee: 352
5465 deg
Mean anomaly: 7
5601 deg
Mean motion: 15
76358578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3058
Checksum: 304
Coasting Arc #13 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2009/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3312208
20 A = 6713478
39 meter
Y = 2683212
56 meter E =
0014971
Z = -5198128
36 I = 51
41909
XDOT = -5598
271721 Wp = 71
27371
YDOT = -5204
520653 meter/sec RA = 217
59812 deg
ZDOT = 887
476969 TA = 207
17096
MA = 207
24938
Ha = 187
457 n
mi
Hp = 179
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10866824
79 X = -3316714
25
Y = 8803190
83 feet Y = 2646148
80 meter
Z = -17054226
89 Z = -5214229
98
XDOT = -18367
033205 XDOT = -5543
969046
YDOT = -17075
198994 feet/sec YDOT = -5266
820292 meter/sec
ZDOT = 2911
669846 ZDOT = 860
411585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2204407
56 X = -671903
43
Y = -13731591
74 feet Y = -4185389
16 meter
Z = -17117671
58 Z = -5217466
30
XDOT = 22997
104926 XDOT = 7009
517582
YDOT = -7160
298305 feet/sec YDOT = -2182
458923 meter/sec
ZDOT = 2804
615238 ZDOT = 854
846724
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 09325
51442520
00016717 00000-0 10270-3 0 9122
2 25544 51
6445 218
5079 0006590 356
1017 4
0095 15
76409611 30744
Satellite: ISS
Catalog Number: 25544
Epoch time: 09325
51442520 = yrday
fracday
Element set: 912
Inclination: 51
6445 deg
RA of node: 218
5079 deg
Eccentricity:
0006590
Arg of perigee: 356
1017 deg
Mean anomaly: 4
0095 deg
Mean motion: 15
76409611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 290
Coasting Arc #14 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2009/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4734241
71 A = 6724304
35 meter
Y = 4505895
22 meter E =
0004811
Z = -1585139
86 I = 51
47995
XDOT = -4407
588626 Wp = 90
76139
YDOT = 2615
561801 meter/sec RA = 212
45304 deg
ZDOT = -5743
968216 TA = 106
77171
MA = 106
71892
Ha = 187
554 n
mi
Hp = 179
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15532289
07 X = 4691204
56
Y = 14783120
78 feet Y = 4558595
80 meter
Z = -5200590
08 Z = -1562244
79
XDOT = -14460
592606 XDOT = -4408
605205
YDOT = 8581
239505 feet/sec YDOT = 2566
268335 meter/sec
ZDOT = -18845
040079 ZDOT = -5765
382804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20492563
06 X = -6246133
22
Y = 6386034
11 feet Y = 1946463
20 meter
Z = -5110012
57 Z = -1557531
83
XDOT = -34
668602 XDOT = -10
566990
YDOT = -15218
136071 feet/sec YDOT = -4638
487874 meter/sec
ZDOT = -18929
466452 ZDOT = -5769
701375
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 09326
52870417
00016717 00000-0 10270-3 0 9135
2 25544 51
6444 213
2807 0006469 358
9220 1
1929 15
76395614 30904
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326
52870417 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 213
2807 deg
Eccentricity:
0006469
Arg of perigee: 358
9220 deg
Mean anomaly: 1
1929 deg
Mean motion: 15
76395614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 313
Coasting Arc #15 (Orbit 3105)
---------------------------------------
Vector Time (GMT): 2009/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4387005
37 A = 6715347
13 meter
Y = -1945427
41 meter E =
0012474
Z = 4695786
56 I = 51
47687
XDOT = 5145
043405 Wp = 34
20479
YDOT = 5063
635546 meter/sec RA = 207
25152 deg
ZDOT = -2695
274417 TA = 82
42294
MA = 82
28126
Ha = 187
467 n
mi
Hp = 179
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14393062
23 X = 4385621
86
Y = -6382635
86 feet Y = -1896377
38 meter
Z = 15406123
87 Z = 4717095
40
XDOT = 16880
063666 XDOT = 5101
131871
YDOT = 16612
977514 feet/sec YDOT = 5120
925116 meter/sec
ZDOT = -8842
763835 ZDOT = -2670
385807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1127836
81 X = -343764
66
Y = 15621446
67 feet Y = 4761416
94 meter
Z = 15490168
55 Z = 4721403
37
XDOT = -21499
946700 XDOT = -6553
183754
YDOT = 7162
615561 feet/sec YDOT = 2183
165223 meter/sec
ZDOT = -8744
278170 ZDOT = -2665
255986
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 09327
54296264
00016717 00000-0 10270-3 0 9141
2 25544 51
6444 208
0532 0006723 2
2172 357
9021 15
76497828 31062
Satellite: ISS
Catalog Number: 25544
Epoch time: 09327
54296264 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 208
0532 deg
Eccentricity:
0006723
Arg of perigee: 2
2172 deg
Mean anomaly: 357
9021 deg
Mean motion: 15
76497828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3106
Checksum: 307
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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