Date:
August 1st 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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
213/08:19:06
328 2
6 4
1 4
1
N/A 2
1 -0
1 189
1
000/00:07:12
656 -2
3 0
2 187
8
Coasting Arc #1 (Orbit 1252)
---------------------------------------
Vector Time (GMT): 2009/209/21:07:30
343
Vector Time (MET): N/A
Weight (LBS) : 686751
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -340172
45 A = 6731719
94 meter
Y = 6714631
83 meter E =
0010973
Z = 132758
31 I = 51
99522
XDOT = -4731
721158 Wp = 15
47841
YDOT = -361
737171 meter/sec RA = 92
01609 deg
ZDOT = 6067
822237 TA = 345
95729
MA = 345
98777
Ha = 188
304 n
mi
Hp = 185
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1116051
34 X = -415876
24
Y = 22029632
00 feet Y = 6710404
53 meter
Z = 435558
75 Z = 130922
47
XDOT = -15524
019546 XDOT = -4756
800714
YDOT = -1186
801742 feet/sec YDOT = -414
790817 meter/sec
ZDOT = 19907
553270 ZDOT = 6044
774697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21713817
29 X = -6618371
51
Y = -3881538
58 feet Y = -1183092
96 meter
Z = 428677
91 Z = 130661
03
XDOT = 2861
823302 XDOT = 872
283742
YDOT = -13782
612675 feet/sec YDOT = -4200
940343 meter/sec
ZDOT = 19816
909801 ZDOT = 6040
194107
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 09209
94344807
00010596 00000-0 82463-4 0 9009
2 25544 51
6416 92
4632 0006463 287
9579 72
0880 15
74159271 12535
Satellite: ISS
Catalog Number: 25544
Epoch time: 09209
94344807 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 92
4632 deg
Eccentricity:
0006463
Arg of perigee: 287
9579 deg
Mean anomaly: 72
0880 deg
Mean motion: 15
74159271 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1253
Checksum: 324
Coasting Arc #2 (Orbit 1267)
---------------------------------------
Vector Time (GMT): 2009/210/21:07:30
343
Vector Time (MET): N/A
Weight (LBS) : 686751
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4149910
38 A = 6719565
44 meter
Y = 41173
06 meter E =
0009138
Z = -5292361
63 I = 51
95454
XDOT = 227
752474 Wp = 77
94159
YDOT = 7687
958357 meter/sec RA = 86
90032 deg
ZDOT = 240
610320 TA = 194
32094
MA = 194
34686
Ha = 188
487 n
mi
Hp = 185
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13615191
55 X = 4174850
75
Y = 135082
22 feet Y = 87719
79 meter
Z = -17363391
18 Z = -5272140
88
XDOT = 747
219403 XDOT = 140
598647
YDOT = 25222
960489 feet/sec YDOT = 7690
017891 meter/sec
ZDOT = 789
403938 ZDOT = 241
505847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1625472
67 X = -495444
07
Y = 13620005
01 feet Y = 4151377
53 meter
Z = -17283875
25 Z = -5268125
18
XDOT = -24160
971145 XDOT = -7364
264005
YDOT = -1886
029126 feet/sec YDOT = -574
861678 meter/sec
ZDOT = 793
299681 ZDOT = 241
797743
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 09210
89568327
00010596 00000-0 82463-4 0 9011
2 25544 51
6417 87
5727 0006541 291
5443 68
5023 15
74193273 12689
Satellite: ISS
Catalog Number: 25544
Epoch time: 09210
89568327 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 87
5727 deg
Eccentricity:
0006541
Arg of perigee: 291
5443 deg
Mean anomaly: 68
5023 deg
Mean motion: 15
74193273 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1268
Checksum: 320
Coasting Arc #3 (Orbit 1283)
---------------------------------------
Vector Time (GMT): 2009/211/21:07:30
343
Vector Time (MET): N/A
Weight (LBS) : 686751
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -729865
09 A = 6731583
83 meter
Y = -6681481
18 meter E =
0006149
Z = -296208
46 I = 51
99189
XDOT = 4746
422208 Wp = 161
00289
YDOT = -251
755155 meter/sec RA = 81
79214 deg
ZDOT = -6057
149866 TA = 22
20037
MA = 22
17376
Ha = 188
577 n
mi
Hp = 185
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2394570
50 X = -653658
46
Y = -21920870
00 feet Y = -6689216
83 meter
Z = -971812
52 Z = -299569
81
XDOT = 15572
251338 XDOT = 4778
308946
YDOT = -825
968357 feet/sec YDOT = -198
498875 meter/sec
ZDOT = -19872
538930 ZDOT = -6034
014480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22047559
73 X = 6720096
21
Y = -370313
11 feet Y = -112871
44 meter
Z = -985346
26 Z = -300333
54
XDOT = -641
551846 XDOT = -195
545003
YDOT = 14089
618115 feet/sec YDOT = 4294
515602 meter/sec
ZDOT = -19781
570301 ZDOT = -6029
422628
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 09211
91139159
00010596 00000-0 82463-4 0 9023
2 25544 51
6414 82
3555 0006494 294
9310 65
1178 15
74193704 12846
Satellite: ISS
Catalog Number: 25544
Epoch time: 09211
91139159 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 82
3555 deg
Eccentricity:
0006494
Arg of perigee: 294
9310 deg
Mean anomaly: 65
1178 deg
Mean motion: 15
74193704 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1284
Checksum: 309
Coasting Arc #4 (Orbit 1299)
---------------------------------------
Vector Time (GMT): 2009/212/21:07:30
343
Vector Time (MET): N/A
Weight (LBS) : 686751
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4133493
25 A = 6719438
78 meter
Y = 478157
86 meter E =
0005300
Z = 5279097
25 I = 51
94679
XDOT = -1437
120692 Wp = 321
52494
YDOT = -7551
242808 meter/sec RA = 76
67121 deg
ZDOT = -437
471528 TA = 132
63537
MA = 132
59067
Ha = 188
817 n
mi
Hp = 185
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13561329
55 X = -4164177
52
Y = 1568759
37 feet Y = 431762
48 meter
Z = 17319872
86 Z = 5258942
46
XDOT = -4714
962901 XDOT = -1350
449458
YDOT = -24774
418661 feet/sec YDOT = -7566
828874 meter/sec
ZDOT = -1435
274041 ZDOT = -444
243428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -547125
47 X = -166763
84
Y = -13740813
99 feet Y = -4188200
11 meter
Z = 17240630
66 Z = 5254944
22
XDOT = 24054
188545 XDOT = 7331
716669
YDOT = -2808
284933 feet/sec YDOT = -855
965248 meter/sec
ZDOT = -1462
252851 ZDOT = -445
694669
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 09212
92708726
00010596 00000-0 82463-4 0 9038
2 25544 51
6422 77
1375 0006646 299
4656 60
5844 15
74253647 13000
Satellite: ISS
Catalog Number: 25544
Epoch time: 09212
92708726 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 77
1375 deg
Eccentricity:
0006646
Arg of perigee: 299
4656 deg
Mean anomaly: 60
5844 deg
Mean motion: 15
74253647 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1300
Checksum: 318
Coasting Arc #5 (Orbit 1306)
---------------------------------------
Vector Time (GMT): 2009/213/08:22:42
656
Vector Time (MET): N/A
Weight (LBS) : 686430
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2104110
18 A = 6725929
34 meter
Y = -4779943
23 meter E =
0004362
Z = -4241281
15 I = 51
95688
XDOT = 4402
502247 Wp = 3
39084
YDOT = 5163
557872 meter/sec RA = 74
30382 deg
ZDOT = -3631
193087 TA = 229
78432
MA = 229
82250
Ha = 189
096 n
mi
Hp = 187
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6903248
63 X = 2178007
08
Y = -15682228
44 feet Y = -4756000
11 meter
Z = -13914964
39 Z = -4230880
62
XDOT = 14443
905011 XDOT = 4362
074730
YDOT = 16940
806668 feet/sec YDOT = 5212
563656 meter/sec
ZDOT = -11913
363145 ZDOT = -3609
903510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13338962
30 X = -4065715
71
Y = -10806936
74 feet Y = -3293954
32 meter
Z = -13874277
19 Z = -4228879
69
XDOT = 19332
902610 XDOT = 5892
668716
YDOT = -8658
400489 feet/sec YDOT = -2639
080469 meter/sec
ZDOT = -11829
399231 ZDOT = -3605
600886
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 09213
37146149
00010596 00000-0 82463-4 0 9044
2 25544 51
6414 74
8570 0007675 281
0392 78
9908 15
73465543 13079
Satellite: ISS
Catalog Number: 25544
Epoch time: 09213
37146149 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 74
8570 deg
Eccentricity:
0007675
Arg of perigee: 281
0392 deg
Mean anomaly: 78
9908 deg
Mean motion: 15
73465543 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1307
Checksum: 323
Coasting Arc #6 (Orbit 1322)
---------------------------------------
Vector Time (GMT): 2009/214/08:22:42
656
Vector Time (MET): N/A
Weight (LBS) : 686430
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4287299
11 A = 6729068
98 meter
Y = -3997657
08 meter E =
0005518
Z = 3301359
77 I = 51
95755
XDOT = 1757
278958 Wp = 74
02128
YDOT = -5805
607496 meter/sec RA = 69
14516 deg
ZDOT = -4740
004628 TA = 67
43673
MA = 67
37835
Ha = 189
349 n
mi
Hp = 187
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14065941
98 X = -4258315
15
Y = -13115672
84 feet Y = -4045438
53 meter
Z = 10831232
85 Z = 3280602
29
XDOT = 5765
350913 XDOT = 1845
093381
YDOT = -19047
268687 feet/sec YDOT = -5785
464979 meter/sec
ZDOT = -15551
196286 ZDOT = -4731
255330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16148078
60 X = -4921934
36
Y = 10529809
30 feet Y = 3209485
87 meter
Z = 10749412
85 Z = 3276421
04
XDOT = -16293
230350 XDOT = -4966
176611
YDOT = -9118
991453 feet/sec YDOT = -2779
468595 meter/sec
ZDOT = -15517
042692 ZDOT = -4729
594613
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 09214
38764566
00010596 00000-0 82463-4 0 9056
2 25544 51
6410 69
6429 0007701 284
6365 75
3944 15
73453269 13230
Satellite: ISS
Catalog Number: 25544
Epoch time: 09214
38764566 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 69
6429 deg
Eccentricity:
0007701
Arg of perigee: 284
6365 deg
Mean anomaly: 75
3944 deg
Mean motion: 15
73453269 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1323
Checksum: 326
Coasting Arc #7 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2009/215/08:22:42
656
Vector Time (MET): N/A
Weight (LBS) : 686430
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -944020
61 A = 6726604
96 meter
Y = 5293469
83 meter E =
0003186
Z = 4038831
88 I = 51
93819
XDOT = -5327
620963 Wp = 86
62975
YDOT = -3942
399720 meter/sec RA = 64
08544 deg
ZDOT = 3919
371272 TA = 323
08100
MA = 323
10293
Ha = 189
684 n
mi
Hp = 187
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3097180
48 X = -1022762
48
Y = 17367027
01 feet Y = 5282472
50 meter
Z = 13250760
75 Z = 4034055
27
XDOT = -17479
071401 XDOT = -5302
179657
YDOT = -12934
382283 feet/sec YDOT = -4001
834507 meter/sec
ZDOT = 12858
829632 ZDOT = 3893
551503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16203579
60 X = 4938851
06
Y = 7010103
71 feet Y = 2136679
61 meter
Z = 13232205
73 Z = 4033176
31
XDOT = -16049
302768 XDOT = -4891
827484
YDOT = 13001
941404 feet/sec YDOT = 3962
991740 meter/sec
ZDOT = 12757
097950 ZDOT = 3888
363455
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 09215
40381893
00010596 00000-0 82463-4 0 9069
2 25544 51
6414 64
4280 0007749 289
1899 70
8425 15
73472854 13398
Satellite: ISS
Catalog Number: 25544
Epoch time: 09215
40381893 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 64
4280 deg
Eccentricity:
0007749
Arg of perigee: 289
1899 deg
Mean anomaly: 70
8425 deg
Mean motion: 15
73472854 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1339
Checksum: 337
Coasting Arc #8 (Orbit 1353)
---------------------------------------
Vector Time (GMT): 2009/216/08:22:42
656
Vector Time (MET): N/A
Weight (LBS) : 686430
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4956788
43 A = 6728223
95 meter
Y = 2851600
75 meter E =
0003289
Z = -3540887
91 I = 51
93004
XDOT = -365
774909 Wp = 320
99379
YDOT = 6231
838414 meter/sec RA = 58
92321 deg
ZDOT = 4506
927718 TA = 357
03872
MA = 357
04067
Ha = 189
945 n
mi
Hp = 187
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16262429
23 X = 4941733
57
Y = 9355645
51 feet Y = 2906946
65 meter
Z = -11617086
31 Z = -3516844
61
XDOT = -1200
048914 XDOT = -457
326586
YDOT = 20445
664088 feet/sec YDOT = 6227
235753 meter/sec
ZDOT = 14786
508262 ZDOT = 4504
929082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12558697
03 X = 3827890
86
Y = -14016601
99 feet Y = -4272260
29 meter
Z = -11522386
86 Z = -3512023
52
XDOT = 18704
690881 XDOT = 5701
189780
YDOT = 4610
788516 feet/sec YDOT = 1405
368340 meter/sec
ZDOT = 14778
919361 ZDOT = 4504
614621
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 09216
35647158
00010596 00000-0 82463-4 0 9074
2 25544 51
6418 59
5393 0007862 292
9668 67
0665 15
73503743 13547
Satellite: ISS
Catalog Number: 25544
Epoch time: 09216
35647158 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 59
5393 deg
Eccentricity:
0007862
Arg of perigee: 292
9668 deg
Mean anomaly: 67
0665 deg
Mean motion: 15
73503743 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1354
Checksum: 341
Coasting Arc #9 (Orbit 1369)
---------------------------------------
Vector Time (GMT): 2009/217/08:22:42
656
Vector Time (MET): N/A
Weight (LBS) : 686430
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -305849
27 A = 6727161
37 meter
Y = -5519210
59 meter E =
0005394
Z = -3837418
90 I = 51
91040
XDOT = 5930
632923 Wp = 349
06445
YDOT = 2576
484158 meter/sec RA = 53
86270 deg
ZDOT = -4172
207194 TA = 237
36865
MA = 237
42072
Ha = 190
024 n
mi
Hp = 187
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1003442
47 X = -225468
70
Y = -18107646
30 feet Y = -5522181
03 meter
Z = -12589957
01 Z = -3838709
90
XDOT = 19457
457098 XDOT = 5921
648839
YDOT = 8453
032015 feet/sec YDOT = 2642
754088 meter/sec
ZDOT = -13688
343813 ZDOT = -4143
418422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17949723
38 X = -5471075
68
Y = -2562655
65 feet Y = -781097
44 meter
Z = -12595276
72 Z = -3839040
35
XDOT = 11858
535189 XDOT = 3614
481525
YDOT = -16242
297445 feet/sec YDOT = -4950
652261 meter/sec
ZDOT = -13574
987040 ZDOT = -4137
656050
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 09217
37262470
00010596 00000-0 82463-4 0 9088
2 25544 51
6419 54
3247 0008016 296
8122 63
2221 15
73513257 13704
Satellite: ISS
Catalog Number: 25544
Epoch time: 09217
37262470 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 54
3247 deg
Eccentricity:
0008016
Arg of perigee: 296
8122 deg
Mean anomaly: 63
2221 deg
Mean motion: 15
73513257 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1370
Checksum: 292
Coasting Arc #10 (Orbit 1385)
---------------------------------------
Vector Time (GMT): 2009/218/08:22:42
656
Vector Time (MET): N/A
Weight (LBS) : 686430
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5345254
43 A = 6727489
71 meter
Y = -1634669
52 meter E =
0007290
Z = 3744194
04 I = 51
89271
XDOT = -1075
014730 Wp = 41
67737
YDOT = -6307
473535 meter/sec RA = 48
69734 deg
ZDOT = -4278
403159 TA = 93
30855
MA = 93
22515
Ha = 190
221 n
mi
Hp = 186
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17536923
99 X = -5344766
23
Y = -5363088
98 feet Y = -1694440
79 meter
Z = 12284101
19 Z = 3718228
44
XDOT = -3526
951214 XDOT = -983
620327
YDOT = -20693
810809 feet/sec YDOT = -6318
983700 meter/sec
ZDOT = -14036
755771 ZDOT = -4283
403868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8361936
97 X = -2548718
39
Y = 16397717
45 feet Y = 4998024
28 meter
Z = 12181889
89 Z = 3713040
04
XDOT = -19781
864965 XDOT = -6029
512441
YDOT = 379
820971 feet/sec YDOT = 115
769432 meter/sec
ZDOT = -14056
703095 ZDOT = -4284
483103
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 09218
38876798
00010596 00000-0 82463-4 0 9095
2 25544 51
6416 49
1098 0007990 301
6267 58
4116 15
73542822 13868
Satellite: ISS
Catalog Number: 25544
Epoch time: 09218
38876798 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 49
1098 deg
Eccentricity:
0007990
Arg of perigee: 301
6267 deg
Mean anomaly: 58
4116 deg
Mean motion: 15
73542822 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1386
Checksum: 343
Coasting Arc #11 (Orbit 1401)
---------------------------------------
Vector Time (GMT): 2009/219/08:22:42
656
Vector Time (MET): N/A
Weight (LBS) : 686430
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1561940
05 A = 6727737
98 meter
Y = 5434178
18 meter E =
0006482
Z = 3638001
73 I = 51
87316
XDOT = -6216
478224 Wp = 55
09011
YDOT = -1158
303242 meter/sec RA = 43
63316 deg
ZDOT = 4397
312437 TA = 348
36963
MA = 348
38459
Ha = 190
446 n
mi
Hp = 186
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5124475
22 X = 1483385
64
Y = 17828668
55 feet Y = 5451205
34 meter
Z = 11935701
22 Z = 3645398
90
XDOT = -20395
269763 XDOT = -6224
424786
YDOT = -3800
207486 feet/sec YDOT = -1227
864159 meter/sec
ZDOT = 14426
878075 ZDOT = 4367
094030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18403729
95 X = 5609456
89
Y = -2173300
98 feet Y = -662422
14 meter
Z = 11965037
37 Z = 3646943
39
XDOT = -7147
608589 XDOT = -2178
591098
YDOT = 18278
829742 feet/sec YDOT = 5571
387305 meter/sec
ZDOT = 14307
959389 ZDOT = 4361
066022
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 09219
40490113
00010596 00000-0 82463-4 0 9104
2 25544 51
6418 43
8940 0008057 305
8718 54
1697 15
73526838 14024
Satellite: ISS
Catalog Number: 25544
Epoch time: 09219
40490113 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 43
8940 deg
Eccentricity:
0008057
Arg of perigee: 305
8718 deg
Mean anomaly: 54
1697 deg
Mean motion: 15
73526838 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1402
Checksum: 308
Coasting Arc #12 (Orbit 1416)
---------------------------------------
Vector Time (GMT): 2009/220/08:22:42
656
Vector Time (MET): N/A
Weight (LBS) : 686430
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5443592
43 A = 6726805
02 meter
Y = 380648
47 meter E =
0003242
Z = -3930919
89 I = 51
84758
XDOT = 2500
268486 Wp = 358
52617
YDOT = 6051
140452 meter/sec RA = 38
46470 deg
ZDOT = 4051
464100 TA = 313
46185
MA = 313
48881
Ha = 190
679 n
mi
Hp = 186
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17859555
22 X = 5458026
76
Y = 1248846
70 feet Y = 441602
71 meter
Z = -12896718
81 Z = -3904440
29
XDOT = 8202
980597 XDOT = 2412
736813
YDOT = 19852
823005 feet/sec YDOT = 6078
610416 meter/sec
ZDOT = 13292
205054 ZDOT = 4063
397730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3765844
55 X = 1147829
42
Y = -17578905
70 feet Y = -5358050
46 meter
Z = -12792543
77 Z = -3899167
34
XDOT = 19518
797335 XDOT = 5949
329428
YDOT = -5518
496962 feet/sec YDOT = -1682
037874 meter/sec
ZDOT = 13339
411676 ZDOT = 4065
852679
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 09220
35751470
00010596 00000-0 82463-4 0 9117
2 25544 51
6417 39
0049 0008257 308
6161 51
4262 15
73563379 14170
Satellite: ISS
Catalog Number: 25544
Epoch time: 09220
35751470 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 39
0049 deg
Eccentricity:
0008257
Arg of perigee: 308
6161 deg
Mean anomaly: 51
4262 deg
Mean motion: 15
73563379 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1417
Checksum: 297
Coasting Arc #13 (Orbit 1432)
---------------------------------------
Vector Time (GMT): 2009/221/08:22:42
656
Vector Time (MET): N/A
Weight (LBS) : 686430
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2771481
78 A = 6728219
31 meter
Y = -5073244
65 meter E =
0005963
Z = -3447199
56 I = 51
82819
XDOT = 6172
078890 Wp = 348
58377
YDOT = -250
007364 meter/sec RA = 33
39783 deg
ZDOT = -4587
227978 TA = 232
06890
MA = 232
12281
Ha = 190
721 n
mi
Hp = 186
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9092787
99 X = -2697800
24
Y = -16644503
44 feet Y = -5103824
97 meter
Z = -11309709
85 Z = -3460484
34
XDOT = 20249
602658 XDOT = 6196
699449
YDOT = -820
234133 feet/sec YDOT = -180
849847 meter/sec
ZDOT = -15049
960559 ZDOT = -4557
184582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17635569
10 X = -5375321
46
Y = 6893131
88 feet Y = 2101026
60 meter
Z = -11362185
54 Z = -3463194
15
XDOT = 2210
339354 XDOT = 673
711435
YDOT = -18995
653266 feet/sec YDOT = -5789
875115 meter/sec
ZDOT = -14931
798833 ZDOT = -4551
212284
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 09221
37362687
00010596 00000-0 82463-4 0 9129
2 25544 51
6415 33
7900 0008316 311
9349 48
1104 15
73560664 14336
Satellite: ISS
Catalog Number: 25544
Epoch time: 09221
37362687 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 33
7900 deg
Eccentricity:
0008316
Arg of perigee: 311
9349 deg
Mean anomaly: 48
1104 deg
Mean motion: 15
73560664 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1433
Checksum: 295
Coasting Arc #14 (Orbit 1448)
---------------------------------------
Vector Time (GMT): 2009/222/08:22:42
656
Vector Time (MET): N/A
Weight (LBS) : 686430
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5287404
91 A = 6726081
18 meter
Y = 806637
64 meter E =
0009710
Z = 4080457
93 I = 51
79644
XDOT = -3808
798240 Wp = 28
07929
YDOT = -5475
370041 meter/sec RA = 28
22619 deg
ZDOT = -3840
922760 TA = 101
39900
MA = 101
28991
Ha = 190
886 n
mi
Hp = 185
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17347128
98 X = -5315853
88
Y = 2646448
96 feet Y = 747351
68 meter
Z = 13387329
16 Z = 4054702
81
XDOT = -12496
057217 XDOT = -3728
630267
YDOT = -17963
812470 feet/sec YDOT = -5517
513985 meter/sec
ZDOT = -12601
452626 ZDOT = -3859
231079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 768510
09 X = 234241
88
Y = 17607869
93 feet Y = 5366878
75 meter
Z = 13286062
88 Z = 4049591
97
XDOT = -17905
223479 XDOT = -5457
512116
YDOT = 10374
595622 feet/sec YDOT = 3162
176746 meter/sec
ZDOT = -12673
700079 ZDOT = -3862
943784
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 09222
38972706
00010596 00000-0 82463-4 0 9131
2 25544 51
6421 28
5746 0008468 316
7248 43
3249 15
73639175 14490
Satellite: ISS
Catalog Number: 25544
Epoch time: 09222
38972706 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 28
5746 deg
Eccentricity:
0008468
Arg of perigee: 316
7248 deg
Mean anomaly: 43
3249 deg
Mean motion: 15
73639175 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1449
Checksum: 331
Coasting Arc #15 (Orbit 1464)
---------------------------------------
Vector Time (GMT): 2009/223/08:22:42
656
Vector Time (MET): N/A
Weight (LBS) : 686430
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3848560
02 A = 6728611
33 meter
Y = 4441086
74 meter E =
0010075
Z = 3263325
14 I = 51
77709
XDOT = -5851
803924 Wp = 46
35899
YDOT = 1573
110559 meter/sec RA = 23
15397 deg
ZDOT = 4758
113456 TA = 351
80843
MA = 351
82487
Ha = 191
029 n
mi
Hp = 185
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12626509
24 X = 3782760
40
Y = 14570494
56 feet Y = 4483755
64 meter
Z = 10706447
30 Z = 3281861
62
XDOT = -19198
831771 XDOT = -5892
073771
YDOT = 5161
123880 feet/sec YDOT = 1507
447020 meter/sec
ZDOT = 15610
608450 ZDOT = 4729
587699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15640015
27 X = 4767076
65
Y = -11204796
40 feet Y = -3415221
94 meter
Z = 10779541
79 Z = 3285604
34
XDOT = 2591
323653 XDOT = 789
835449
YDOT = 18534
455817 feet/sec YDOT = 5649
302133 meter/sec
ZDOT = 15498
480623 ZDOT = 4723
936894
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 09223
40581925
00010596 00000-0 82463-4 0 9145
2 25544 51
6412 23
3587 0008476 320
5980 39
4566 15
73602313 14651
Satellite: ISS
Catalog Number: 25544
Epoch time: 09223
40581925 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 23
3587 deg
Eccentricity:
0008476
Arg of perigee: 320
5980 deg
Mean anomaly: 39
4566 deg
Mean motion: 15
73602313 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1465
Checksum: 306
Coasting Arc #16 (Orbit 1479)
---------------------------------------
Vector Time (GMT): 2009/224/08:22:42
656
Vector Time (MET): N/A
Weight (LBS) : 686430
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4870325
84 A = 6725567
31 meter
Y = -1920066
95 meter E =
0004799
Z = -4221824
18 I = 51
73824
XDOT = 4967
819332 Wp = 33
34727
YDOT = 4624
818146 meter/sec RA = 17
97897 deg
ZDOT = 3633
437805 TA = 273
57190
MA = 273
62678
Ha = 191
238 n
mi
Hp = 185
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15978759
31 X = 4911943
23
Y = -6299432
25 feet Y = -1865371
28 meter
Z = -13851129
19 Z = -4198063
12
XDOT = 16298
619855 XDOT = 4898
084030
YDOT = 15173
287879 feet/sec YDOT = 4679
981194 meter/sec
ZDOT = 11920
727706 ZDOT = 3657
402211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5116280
30 X = -1559442
23
Y = -16474379
26 feet Y = -5021390
80 meter
Z = -13757757
07 Z = -4193364
35
XDOT = 15111
123664 XDOT = 4605
870493
YDOT = -14710
578286 feet/sec YDOT = -4483
784262 meter/sec
ZDOT = 12015
171913 ZDOT = 3662
224399
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 09224
35839397
00010596 00000-0 82463-4 0 9150
2 25544 51
6404 18
4689 0008423 323
8346 36
2247 15
73634483 14805
Satellite: ISS
Catalog Number: 25544
Epoch time: 09224
35839397 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 18
4689 deg
Eccentricity:
0008423
Arg of perigee: 323
8346 deg
Mean anomaly: 36
2247 deg
Mean motion: 15
73634483 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1480
Checksum: 325
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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