Date:
August 13th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 1482)
---------------------------------------
Vector Time (GMT): 2009/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -294957
26 A = 6721581
29 meter
Y = 4223497
64 meter E =
0005046
Z = 5221581
70 I = 51
71827
XDOT = -7480
998114 Wp = 338
75363
YDOT = -1598
859675 meter/sec RA = 17
24636 deg
ZDOT = 875
531817 TA = 102
94568
MA = 102
88933
Ha = 191
163 n
mi
Hp = 185
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -967707
55 X = -367528
70
Y = 13856619
55 feet Y = 4219793
31 meter
Z = 17131173
55 Z = 5219972
66
XDOT = -24543
957068 XDOT = -7466
816559
YDOT = -5245
602607 feet/sec YDOT = -1682
437322 meter/sec
ZDOT = 2872
479714 ZDOT = 839
223536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9671815
51 X = 2947969
37
Y = -9980437
42 feet Y = -3042037
32 meter
Z = 17125020
42 Z = 5219706
22
XDOT = 14819
782894 XDOT = 4517
069826
YDOT = 19017
692907 feet/sec YDOT = 5796
592798 meter/sec
ZDOT = 2729
613645 ZDOT = 831
986239
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
54904545
00010596 00000-0 82463-4 0 9003
2 25544 51
6387 17
4993 0007858 324
1680 35
8954 15
73558160 14838
Satellite: ISS
Catalog Number: 25544
Epoch time: 09224
54904545 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 17
4993 deg
Eccentricity:
0007858
Arg of perigee: 324
1680 deg
Mean anomaly: 35
8954 deg
Mean motion: 15
73558160 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1483
Checksum: 331
Coasting Arc #2 (Orbit 1497)
---------------------------------------
Vector Time (GMT): 2009/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6627259
98 A = 6733036
40 meter
Y = 703386
37 meter E =
0014714
Z = -889812
24 I = 51
72953
XDOT = 280
024820 Wp = 8
46397
YDOT = 4871
369261 meter/sec RA = 12
10475 deg
ZDOT = 5963
041032 TA = 341
83152
MA = 341
88404
Ha = 191
247 n
mi
Hp = 185
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21742978
93 X = 6623224
58
Y = 2307698
07 feet Y = 777473
77 meter
Z = -2919331
50 Z = -857626
77
XDOT = 918
716600 XDOT = 196
564147
YDOT = 15982
182616 feet/sec YDOT = 4874
033685 meter/sec
ZDOT = 19563
782912 ZDOT = 5964
198932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15536401
80 X = -4735495
27
Y = -15408635
15 feet Y = -4696551
99 meter
Z = -2792719
33 Z = -851220
85
XDOT = 8243
452569 XDOT = 2512
604343
YDOT = -11841
901219 feet/sec YDOT = -3609
411492 meter/sec
ZDOT = 19568
534320 ZDOT = 5964
489261
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 09225
50164011
00010596 00000-0 82463-4 0 9017
2 25544 51
6401 12
6106 0007785 327
5438 32
5245 15
73587728 14980
Satellite: ISS
Catalog Number: 25544
Epoch time: 09225
50164011 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 12
6106 deg
Eccentricity:
0007785
Arg of perigee: 327
5438 deg
Mean anomaly: 32
5245 deg
Mean motion: 15
73587728 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1498
Checksum: 297
Coasting Arc #3 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2009/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -769976
49 A = 6721590
40 meter
Y = -4223586
29 meter E =
0013915
Z = -5182383
17 I = 51
66210
XDOT = 7606
175887 Wp = 49
00540
YDOT = 23
310542 meter/sec RA = 6
99545 deg
ZDOT = -1142
125068 TA = 210
04184
MA = 210
12174
Ha = 191
327 n
mi
Hp = 185
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2526169
57 X = -697515
36
Y = -13856910
41 feet Y = -4231791
08 meter
Z = -17002569
45 Z = -5185948
02
XDOT = 24954
645300 XDOT = 7610
898142
YDOT = 76
478156 feet/sec YDOT = 108
393752 meter/sec
ZDOT = -3747
129488 ZDOT = -1105
162862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6558894
26 X = -1999150
97
Y = 12445630
73 feet Y = 3793428
25 meter
Z = -17016757
87 Z = -5186707
80
XDOT = -18800
894808 XDOT = -5730
512738
YDOT = -14864
002983 feet/sec YDOT = -4530
548109 meter/sec
ZDOT = -3601
756832 ZDOT = -1097
815482
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 09226
51773421
00010596 00000-0 82463-4 0 9021
2 25544 51
6403 7
3967 0007849 332
0253 28
0487 15
73618939 15141
Satellite: ISS
Catalog Number: 25544
Epoch time: 09226
51773421 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 7
3967 deg
Eccentricity:
0007849
Arg of perigee: 332
0253 deg
Mean anomaly: 28
0487 deg
Mean motion: 15
73618939 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1514
Checksum: 312
Coasting Arc #4 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2009/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6609081
21 A = 6732777
11 meter
Y = 654786
62 meter E =
0008155
Z = 1096713
44 I = 51
66947
XDOT = -1453
327398 Wp = 92
70614
YDOT = -4717
338361 meter/sec RA = 1
84369 deg
ZDOT = -5904
416512 TA = 75
30655
MA = 75
21617
Ha = 191
482 n
mi
Hp = 185
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21683337
31 X = -6621239
55
Y = 2148250
06 feet Y = 580811
92 meter
Z = 3598141
20 Z = 1064577
23
XDOT = -4768
134507 XDOT = -1371
786880
YDOT = -15476
831892 feet/sec YDOT = -4733
133874 meter/sec
ZDOT = -19371
445248 ZDOT = -5911
279097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18677996
97 X = 5693053
48
Y = 11260903
22 feet Y = 3432323
30 meter
Z = 3471772
38 Z = 1058196
22
XDOT = -4706
127475 XDOT = -1434
427654
YDOT = 13825
569703 feet/sec YDOT = 4214
033646 meter/sec
ZDOT = -19398
621736 ZDOT = -5912
699905
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 09227
53382029
00010596 00000-0 82463-4 0 9035
2 25544 51
6399 2
1802 0007911 335
1968 24
8814 15
73617057 15309
Satellite: ISS
Catalog Number: 25544
Epoch time: 09227
53382029 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 2
1802 deg
Eccentricity:
0007911
Arg of perigee: 335
1968 deg
Mean anomaly: 24
8814 deg
Mean motion: 15
73617057 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1530
Checksum: 304
Coasting Arc #5 (Orbit 1545)
---------------------------------------
Vector Time (GMT): 2009/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1757889
80 A = 6721658
18 meter
Y = 3970931
91 meter E =
0004992
Z = 5129047
54 I = 51
60385
XDOT = -7424
932823 Wp = 6
36268
YDOT = 1515
983291 meter/sec RA = 356
73253 deg
ZDOT = 1375
829996 TA = 70
48933
MA = 70
43542
Ha = 191
551 n
mi
Hp = 184
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5767354
98 X = 1688439
80
Y = 13027991
82 feet Y = 3990200
87 meter
Z = 16827583
79 Z = 5137418
95
XDOT = -24360
015825 XDOT = -7448
016429
YDOT = 4973
698460 feet/sec YDOT = 1432
824142 meter/sec
ZDOT = 4513
877941 ZDOT = 1339
704148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3011448
08 X = 917889
37
Y = -13885518
63 feet Y = -4232306
08 meter
Z = 16860666
75 Z = 5139131
23
XDOT = 21683
816329 XDOT = 6609
227217
YDOT = 9992
411849 feet/sec YDOT = 3045
687131 meter/sec
ZDOT = 4371
845933 ZDOT = 1332
538640
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 09228
54989777
00010596 00000-0 82463-4 0 9041
2 25544 51
6411 356
9650 0008005 338
7279 21
3550 15
73655517 15463
Satellite: ISS
Catalog Number: 25544
Epoch time: 09228
54989777 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 356
9650 deg
Eccentricity:
0008005
Arg of perigee: 338
7279 deg
Mean anomaly: 21
3550 deg
Mean motion: 15
73655517 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1546
Checksum: 334
Coasting Arc #6 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2009/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6290007
42 A = 6732527
53 meter
Y = -1980711
83 meter E =
0015236
Z = -1309745
24 I = 51
61102
XDOT = 2568
610376 Wp = 11
62502
YDOT = 4305
563943 meter/sec RA = 351
57432 deg
ZDOT = 5850
809060 TA = 333
98401
MA = 334
06051
Ha = 191
834 n
mi
Hp = 184
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20636507
30 X = 6318050
99
Y = -6498398
40 feet Y = -1910216
37 meter
Z = -4297064
44 Z = -1279120
94
XDOT = 8427
199396 XDOT = 2491
852229
YDOT = 14125
865955 feet/sec YDOT = 4333
858006 meter/sec
ZDOT = 19195
567782 ZDOT = 5863
101060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20678363
28 X = -6302765
13
Y = -6443598
60 feet Y = -1964008
85 meter
Z = -4176686
14 Z = -1273053
93
XDOT = 754
735141 XDOT = 230
043271
YDOT = -14838
148402 feet/sec YDOT = -4522
667633 meter/sec
ZDOT = 19244
088926 ZDOT = 5865
598305
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 09229
50246479
00010596 00000-0 82463-4 0 9054
2 25544 51
6418 352
0762 0008058 343
3549 16
7348 15
73629101 15611
Satellite: ISS
Catalog Number: 25544
Epoch time: 09229
50246479 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 352
0762 deg
Eccentricity:
0008058
Arg of perigee: 343
3549 deg
Mean anomaly: 16
7348 deg
Mean motion: 15
73629101 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1561
Checksum: 315
Coasting Arc #7 (Orbit 1576)
---------------------------------------
Vector Time (GMT): 2009/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2685064
45 A = 6721912
22 meter
Y = -3504159
84 meter E =
0015813
Z = -5081532
65 I = 51
54652
XDOT = 6911
467321 Wp = 46
89118
YDOT = -2968
679605 meter/sec RA = 346
46336 deg
ZDOT = -1597
338079 TA = 207
68479
MA = 207
76906
Ha = 191
872 n
mi
Hp = 184
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8809266
57 X = -2620996
13
Y = -11496587
41 feet Y = -3533827
31 meter
Z = -16671695
05 Z = -5094420
99
XDOT = 22675
417721 XDOT = 6951
909347
YDOT = -9739
762485 feet/sec YDOT = -2891
165312 meter/sec
ZDOT = -5240
610495 ZDOT = -1563
664812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 848494
29 X = 258621
06
Y = 14399895
51 feet Y = 4389088
15 meter
Z = -16722535
16 Z = -5097028
72
XDOT = -23237
594706 XDOT = -7082
818866
YDOT = -4591
443603 feet/sec YDOT = -1399
472010 meter/sec
ZDOT = -5108
278450 ZDOT = -1557
003271
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 09230
51852755
00010596 00000-0 82463-4 0 9068
2 25544 51
6421 346
8617 0008112 346
8153 13
2796 15
73648800 15778
Satellite: ISS
Catalog Number: 25544
Epoch time: 09230
51852755 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 346
8617 deg
Eccentricity:
0008112
Arg of perigee: 346
8153 deg
Mean anomaly: 13
2796 deg
Mean motion: 15
73648800 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1577
Checksum: 316
Coasting Arc #8 (Orbit 1592)
---------------------------------------
Vector Time (GMT): 2009/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5745983
07 A = 6732253
71 meter
Y = 3180726
35 meter E =
0011083
Z = 1474005
96 I = 51
55276
XDOT = -3518
752568 Wp = 83
56204
YDOT = -3657
886321 meter/sec RA = 341
29719 deg
ZDOT = -5785
182623 TA = 80
20078
MA = 80
07565
Ha = 192
013 n
mi
Hp = 184
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18851650
51 X = -5788283
74
Y = 10435453
90 feet Y = 3116234
85 meter
Z = 4835977
57 Z = 1445989
93
XDOT = -11544
463806 XDOT = -3449
485202
YDOT = -12000
939372 feet/sec YDOT = -3696
847664 meter/sec
ZDOT = -18980
257951 ZDOT = -5802
108164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21522591
13 X = 6560085
78
Y = 1453940
48 feet Y = 443161
06 meter
Z = 4725910
72 Z = 1440457
59
XDOT = 3216
758330 XDOT = 980
467939
YDOT = 14711
913611 feet/sec YDOT = 4484
191268 meter/sec
ZDOT = -19046
990254 ZDOT = -5805
522630
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 09231
53458279
00010596 00000-0 82463-4 0 9075
2 25544 51
6423 341
6465 0008054 351
1438 8
9582 15
73655693 15934
Satellite: ISS
Catalog Number: 25544
Epoch time: 09231
53458279 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 341
6465 deg
Eccentricity:
0008054
Arg of perigee: 351
1438 deg
Mean anomaly: 8
9582 deg
Mean motion: 15
73655693 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1593
Checksum: 329
Coasting Arc #9 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2009/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3435557
81 A = 6721929
66 meter
Y = 2850619
89 meter E =
0006195
Z = 5021071
93 I = 51
49153
XDOT = -6155
601751 Wp = 34
70005
YDOT = 4273
445695 meter/sec RA = 336
18425 deg
ZDOT = 1789
600318 TA = 38
05365
MA = 38
00991
Ha = 191
996 n
mi
Hp = 183
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11271515
13 X = 3379035
40
Y = 9352427
46 feet Y = 2888722
33 meter
Z = 16473333
10 Z = 5037624
20
XDOT = -20195
543803 XDOT = -6211
624034
YDOT = 14020
491125 feet/sec YDOT = 4204
296922 meter/sec
ZDOT = 5871
392120 ZDOT = 1759
560905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4566879
20 X = -1391984
78
Y = -13838537
02 feet Y = -4217986
08 meter
Z = 16538565
94 Z = 5040954
90
XDOT = 23572
157041 XDOT = 7184
793466
YDOT = -918
486713 feet/sec YDOT = -279
954750 meter/sec
ZDOT = 5753
420727 ZDOT = 1753
642638
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 09232
55062824
00010596 00000-0 82463-4 0 9086
2 25544 51
6430 336
4312 0008171 354
8085 5
2992 15
73709960 16093
Satellite: ISS
Catalog Number: 25544
Epoch time: 09232
55062824 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 336
4312 deg
Eccentricity:
0008171
Arg of perigee: 354
8085 deg
Mean anomaly: 5
2992 deg
Mean motion: 15
73709960 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1609
Checksum: 309
Coasting Arc #10 (Orbit 1623)
---------------------------------------
Vector Time (GMT): 2009/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4945319
20 A = 6732004
42 meter
Y = -4244221
08 meter E =
0015440
Z = -1654152
13 I = 51
49798
XDOT = 4320
187021 Wp = 17
08219
YDOT = 2813
299944 meter/sec RA = 331
01190 deg
ZDOT = 5725
420556 TA = 324
59481
MA = 324
69722
Ha = 192
378 n
mi
Hp = 183
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16224800
53 X = 5000446
71
Y = -13924609
86 feet Y = -4188611
44 meter
Z = -5427008
29 Z = -1629994
12
XDOT = 14173
841931 XDOT = 4260
594514
YDOT = 9229
986694 feet/sec YDOT = 2861
277792 meter/sec
ZDOT = 18784
188177 ZDOT = 5746
262855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21094987
09 X = -6429752
07
Y = 3627771
18 feet Y = 1105744
65 meter
Z = -5332178
44 Z = -1625247
99
XDOT = -7083
160889 XDOT = -2158
947439
YDOT = -13594
818282 feet/sec YDOT = -4143
700612 meter/sec
ZDOT = 18866
294405 ZDOT = 5750
446535
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 09233
50316610
00010596 00000-0 82463-4 0 9098
2 25544 51
6430 331
5430 0008425 358
6363 1
4776 15
73656199 16243
Satellite: ISS
Catalog Number: 25544
Epoch time: 09233
50316610 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 331
5430 deg
Eccentricity:
0008425
Arg of perigee: 358
6363 deg
Mean anomaly: 1
4776 deg
Mean motion: 15
73656199 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1624
Checksum: 301
Coasting Arc #11 (Orbit 1639)
---------------------------------------
Vector Time (GMT): 2009/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4050194
79 A = 6722256
02 meter
Y = -2046271
49 meter E =
0017367
Z = -4974137
75 I = 51
43952
XDOT = 5137
149445 Wp = 47
93715
YDOT = -5371
208886 meter/sec RA = 325
89860 deg
ZDOT = -1966
254276 TA = 202
93286
MA = 203
01050
Ha = 192
353 n
mi
Hp = 183
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13288040
64 X = -4002848
79
Y = -6713489
14 feet Y = -2091298
61 meter
Z = -16319349
56 Z = -4993698
31
XDOT = 16854
164847 XDOT = 5206
381034
YDOT = -17622
076399 feet/sec YDOT = -5313
375244 meter/sec
ZDOT = -6450
965472 ZDOT = -1941
129889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8103174
01 X = 2469847
44
Y = 12387957
32 feet Y = 3775849
39 meter
Z = -16396378
11 Z = -4997616
05
XDOT = -22516
959187 XDOT = -6863
169160
YDOT = 6290
377924 feet/sec YDOT = 1917
307191 meter/sec
ZDOT = -6352
394171 ZDOT = -1936
209743
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 09234
51919760
00010596 00000-0 82463-4 0 9107
2 25544 51
6426 326
3283 0008293 2
1540 357
9657 15
73683036 16402
Satellite: ISS
Catalog Number: 25544
Epoch time: 09234
51919760 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 326
3283 deg
Eccentricity:
0008293
Arg of perigee: 2
1540 deg
Mean anomaly: 357
9657 deg
Mean motion: 15
73683036 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1640
Checksum: 309
Coasting Arc #12 (Orbit 1655)
---------------------------------------
Vector Time (GMT): 2009/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4006846
39 A = 6731678
18 meter
Y = 5106962
71 meter E =
0014048
Z = 1777064
15 I = 51
44658
XDOT = -4876
663958 Wp = 79
97808
YDOT = -1841
631785 meter/sec RA = 320
71931 deg
ZDOT = -5662
818045 TA = 80
28841
MA = 80
12977
Ha = 192
512 n
mi
Hp = 183
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13145821
49 X = -4072288
14
Y = 16755127
02 feet Y = 5061789
96 meter
Z = 5830262
95 Z = 1757439
86
XDOT = -15999
553667 XDOT = -4828
199255
YDOT = -6042
099032 feet/sec YDOT = -1895
894713 meter/sec
ZDOT = -18578
799361 ZDOT = -5686
390981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19629015
22 X = 5982923
84
Y = -8315044
64 feet Y = -2534425
61 meter
Z = 5753317
67 Z = 1753611
23
XDOT = 10396
023291 XDOT = 3168
707899
YDOT = 11529
489244 feet/sec YDOT = 3514
188322 meter/sec
ZDOT = -18671
596761 ZDOT = -5691
102693
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 09235
53522150
00010596 00000-0 82463-4 0 9114
2 25544 51
6418 321
1132 0008378 7
2791 352
8492 15
73705852 16566
Satellite: ISS
Catalog Number: 25544
Epoch time: 09235
53522150 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 321
1132 deg
Eccentricity:
0008378
Arg of perigee: 7
2791 deg
Mean anomaly: 352
8492 deg
Mean motion: 15
73705852 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1656
Checksum: 300
Coasting Arc #13 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2009/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4433401
44 A = 6722260
17 meter
Y = 1149703
03 meter E =
0008210
Z = 4913318
17 I = 51
39332
XDOT = -3969
387160 Wp = 53
17566
YDOT = 6256
033162 meter/sec RA = 315
60318 deg
ZDOT = 2120
190514 TA = 16
22387
MA = 16
19761
Ha = 192
413 n
mi
Hp = 182
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14545280
33 X = 4396347
79
Y = 3771991
57 feet Y = 1199072
85 meter
Z = 16119810
28 Z = 4934765
58
XDOT = -13022
923754 XDOT = -4049
347672
YDOT = 20525
043183 feet/sec YDOT = 6211
198102 meter/sec
ZDOT = 6956
005623 ZDOT = 2100
712912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11011896
84 X = -3356426
16
Y = -10089745
45 feet Y = -3075354
41 meter
Z = 16204213
91 Z = 4939044
40
XDOT = 20406
683939 XDOT = 6219
957265
YDOT = -11235
563153 feet/sec YDOT = -3424
599649 meter/sec
ZDOT = 6879
693813 ZDOT = 2096
930674
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 09236
55123548
00010596 00000-0 82463-4 0 9126
2 25544 51
6420 315
8971 0008418 10
2632 349
8701 15
73747053 16729
Satellite: ISS
Catalog Number: 25544
Epoch time: 09236
55123548 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 315
8971 deg
Eccentricity:
0008418
Arg of perigee: 10
2632 deg
Mean anomaly: 349
8701 deg
Mean motion: 15
73747053 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1672
Checksum: 305
Coasting Arc #14 (Orbit 1686)
---------------------------------------
Vector Time (GMT): 2009/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2885774
35 A = 6731434
01 meter
Y = -5760013
12 meter E =
0015318
Z = -1926249
26 I = 51
40252
XDOT = 5231
087144 Wp = 24
59517
YDOT = 756
641828 meter/sec RA = 310
41845 deg
ZDOT = 5603
937548 TA = 313
90296
MA = 314
02933
Ha = 192
766 n
mi
Hp = 182
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9467763
61 X = 2959326
70
Y = -18897680
85 feet Y = -5727331
45 meter
Z = -6319715
40 Z = -1912051
49
XDOT = 17162
359397 XDOT = 5195
014542
YDOT = 2482
420697 feet/sec YDOT = 814
937242 meter/sec
ZDOT = 18385
621878 ZDOT = 5629
262546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17022170
56 X = -5188357
59
Y = 12558099
73 feet Y = 3827708
80 meter
Z = -6264146
60 Z = -1909311
88
XDOT = -13173
601240 XDOT = -4015
313658
YDOT = -8684
726474 feet/sec YDOT = -2647
104629 meter/sec
ZDOT = 18485
256413 ZDOT = 5634
306155
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 09237
50374356
00010596 00000-0 82463-4 0 9138
2 25544 51
6413 311
0083 0008660 13
4632 346
6760 15
73702419 16870
Satellite: ISS
Catalog Number: 25544
Epoch time: 09237
50374356 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 311
0083 deg
Eccentricity:
0008660
Arg of perigee: 13
4632 deg
Mean anomaly: 346
6760 deg
Mean motion: 15
73702419 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1687
Checksum: 298
Coasting Arc #15 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2009/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4643667
65 A = 6722546
30 meter
Y = -186059
54 meter E =
0018656
Z = -4873991
04 I = 51
35370
XDOT = 2646
258367 Wp = 50
97891
YDOT = -6855
651176 meter/sec RA = 305
30179 deg
ZDOT = -2253
716897 TA = 196
93989
MA = 197
00226
Ha = 192
798 n
mi
Hp = 182
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15235130
08 X = -4617565
01
Y = -610431
55 feet Y = -237841
74 meter
Z = -15990784
25 Z = -4896486
57
XDOT = 8681
950023 XDOT = 2733
670905
YDOT = -22492
293884 feet/sec YDOT = -6825
570381 meter/sec
ZDOT = -7394
084308 ZDOT = -2240
649147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13354492
41 X = 4070449
29
Y = 7162524
53 feet Y = 2183137
48 meter
Z = -16079265
26 Z = -4900960
05
XDOT = -17150
035884 XDOT = -5227
330937
YDOT = 15449
352713 feet/sec YDOT = 4708
962707 meter/sec
ZDOT = -7343
011571 ZDOT = -2238
149927
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 09238
51974407
00010596 00000-0 82463-4 0 9144
2 25544 51
6406 305
7925 0008592 17
9331 342
2133 15
73728413 17033
Satellite: ISS
Catalog Number: 25544
Epoch time: 09238
51974407 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 305
7925 deg
Eccentricity:
0008592
Arg of perigee: 17
9331 deg
Mean anomaly: 342
2133 deg
Mean motion: 15
73728413 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1703
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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