[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 14th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14800 38 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 1454)
---------------------------------------
Vector Time (GMT): 2011/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1253106
88 A = 6765946
96 meter
Y = 6010569
70 meter E =
0015541
Z = 2844923
33 I = 51
98500
XDOT = -4613
713121 Wp = 127
49042
YDOT = -3393
189409 meter/sec RA = 80
54060 deg
ZDOT = 5108
448287 TA = 264
76045
MA = 264
93781
Ha = 212
921 n
mi
Hp = 202
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4111243
05 X = -1334045
14
Y = 19719716
85 feet Y = 5996104
44 meter
Z = 9333737
97 Z = 2838638
54
XDOT = -15136
854070 XDOT = -4600
242646
YDOT = -11132
511184 feet/sec YDOT = -3444
706906 meter/sec
ZDOT = 16760
000941 ZDOT = 5086
068123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7412297
21 X = 2259268
19
Y = -18743261
66 feet Y = -5712946
15 meter
Z = 9307857
36 Z = 2837034
92
XDOT = 11790
534025 XDOT = 3593
754771
YDOT = 12986
676942 feet/sec YDOT = 3958
339132 meter/sec
ZDOT = 16668
983031 ZDOT = 5080
706028
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 11255
55826141
00016717 00000-0 10270-3 0 9003
2 25544 51
6352 80
9716 0011708 184
6837 175
4212 15
61016096 14551
Satellite: ISS
Catalog Number: 25544
Epoch time: 11255
55826141 = yrday
fracday
Element set: 900
Inclination: 51
6352 deg
RA of node: 80
9716 deg
Eccentricity:
0011708
Arg of perigee: 184
6837 deg
Mean anomaly: 175
4212 deg
Mean motion: 15
61016096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 298
Coasting Arc #2 (Orbit 1469)
---------------------------------------
Vector Time (GMT): 2011/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3502551
06 A = 6758046
15 meter
Y = -2607435
81 meter E =
0015019
Z = -5166464
52 I = 51
95228
XDOT = 2981
617242 Wp = 126
08634
YDOT = 6913
067666 meter/sec RA = 75
51451 deg
ZDOT = -1479
164702 TA = 129
80933
MA = 129
67703
Ha = 212
838 n
mi
Hp = 202
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11491309
24 X = 3556545
27
Y = -8554579
44 feet Y = -2567966
81 meter
Z = -16950342
91 Z = -5149317
74
XDOT = 9782
208798 XDOT = 2911
277857
YDOT = 22680
668194 feet/sec YDOT = 6946
016483 meter/sec
ZDOT = -4852
902566 ZDOT = -1464
851663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12749143
72 X = -3885939
01
Y = 6712503
47 feet Y = 2045971
06 meter
Z = -16880366
51 Z = -5145135
71
XDOT = -5795
442711 XDOT = -1766
450938
YDOT = -22969
343084 feet/sec YDOT = -7001
055772 meter/sec
ZDOT = -4794
921617 ZDOT = -1461
492109
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 11256
51853653
00016717 00000-0 10270-3 0 9019
2 25544 51
6350 76
1334 0011620 187
2611 172
8379 15
61025009 14700
Satellite: ISS
Catalog Number: 25544
Epoch time: 11256
51853653 = yrday
fracday
Element set: 901
Inclination: 51
6350 deg
RA of node: 76
1334 deg
Eccentricity:
0011620
Arg of perigee: 187
2611 deg
Mean anomaly: 172
8379 deg
Mean motion: 15
61025009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1470
Checksum: 283
Coasting Arc #3 (Orbit 1485)
---------------------------------------
Vector Time (GMT): 2011/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4526640
27 A = 6760193
79 meter
Y = -1882887
49 meter E =
0009414
Z = 4646286
17 I = 51
95093
XDOT = -69
409810 Wp = 146
33888
YDOT = -7096
765824 meter/sec RA = 70
46533 deg
ZDOT = -2948
361130 TA = 332
79165
MA = 332
84094
Ha = 212
743 n
mi
Hp = 203
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14851181
99 X = -4527819
86
Y = -6177452
39 feet Y = -1933513
26 meter
Z = 15243721
04 Z = 4624293
07
XDOT = -227
722473 XDOT = 24
275393
YDOT = -23283
352442 feet/sec YDOT = -7097
018495 meter/sec
ZDOT = -9673
100819 ZDOT = -2948
470015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13984264
56 X = 4262403
84
Y = 8116621
27 feet Y = 2473946
16 meter
Z = 15154219
21 Z = 4619006
01
XDOT = -2349
132908 XDOT = -716
015710
YDOT = 22078
194505 feet/sec YDOT = 6729
433685 meter/sec
ZDOT = -9673
197036 ZDOT = -2948
390457
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 11257
54281105
00016717 00000-0 10270-3 0 9021
2 25544 51
6351 70
9729 0011621 191
6563 168
4326 15
61029055 14862
Satellite: ISS
Catalog Number: 25544
Epoch time: 11257
54281105 = yrday
fracday
Element set: 902
Inclination: 51
6351 deg
RA of node: 70
9729 deg
Eccentricity:
0011621
Arg of perigee: 191
6563 deg
Mean anomaly: 168
4326 deg
Mean motion: 15
61029055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1486
Checksum: 297
Coasting Arc #4 (Orbit 1500)
---------------------------------------
Vector Time (GMT): 2011/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3813113
28 A = 6768147
69 meter
Y = 5367137
66 meter E =
0005212
Z = -1584099
53 I = 51
96755
XDOT = -3158
660093 Wp = 157
30391
YDOT = 3946
332304 meter/sec RA = 65
45578 deg
ZDOT = 5769
042667 TA = 185
41895
MA = 185
42459
Ha = 212
412 n
mi
Hp = 203
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12510214
16 X = 3760508
79
Y = 17608719
36 feet Y = 5409483
95 meter
Z = -5197176
95 Z = -1565703
65
XDOT = -10363
058048 XDOT = -3230
579072
YDOT = 12947
284462 feet/sec YDOT = 3910
608665 meter/sec
ZDOT = 18927
305337 ZDOT = 5753
522769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10405387
19 X = -3171562
01
Y = -18949166
49 feet Y = -5775705
95 meter
Z = -5122510
20 Z = -1561341
11
XDOT = 10531
756440 XDOT = 3210
079363
YDOT = -10881
212292 feet/sec YDOT = -3316
593507 meter/sec
ZDOT = 18863
882744 ZDOT = 5749
711461
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 11258
50305159
00016717 00000-0 10270-3 0 9035
2 25544 51
6357 66
1342 0011633 194
7131 165
3688 15
61079863 15011
Satellite: ISS
Catalog Number: 25544
Epoch time: 11258
50305159 = yrday
fracday
Element set: 903
Inclination: 51
6357 deg
RA of node: 66
1342 deg
Eccentricity:
0011633
Arg of perigee: 194
7131 deg
Mean anomaly: 165
3688 deg
Mean motion: 15
61079863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1501
Checksum: 300
Coasting Arc #5 (Orbit 1516)
---------------------------------------
Vector Time (GMT): 2011/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1364490
75 A = 6766637
25 meter
Y = -6178539
29 meter E =
0014693
Z = -2373352
68 I = 51
94992
XDOT = 5376
920117 Wp = 178
14736
YDOT = 888
061957 meter/sec RA = 60
47401 deg
ZDOT = -5418
435552 TA = 28
33876
MA = 28
25892
Ha = 212
125 n
mi
Hp = 203
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4476675
68 X = -1283770
31
Y = -20270798
19 feet Y = -6193346
72 meter
Z = -7786590
16 Z = -2379784
83
XDOT = 17640
814031 XDOT = 5392
911942
YDOT = 2913
589098 feet/sec YDOT = 948
278937 meter/sec
ZDOT = -17777
019528 ZDOT = -5392
275554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2393730
57 X = 729609
08
Y = 20610974
30 feet Y = 6282224
97 meter
Z = -7812468
45 Z = -2381240
38
XDOT = -15867
469713 XDOT = -4836
404769
YDOT = -4836
180692 feet/sec YDOT = -1474
067875 meter/sec
ZDOT = -17670
500662 ZDOT = -5385
968602
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 11259
52728960
00016717 00000-0 10270-3 0 9048
2 25544 51
6362 60
9740 0011403 198
7179 161
3560 15
61125455 15173
Satellite: ISS
Catalog Number: 25544
Epoch time: 11259
52728960 = yrday
fracday
Element set: 904
Inclination: 51
6362 deg
RA of node: 60
9740 deg
Eccentricity:
0011403
Arg of perigee: 198
7179 deg
Mean anomaly: 161
3560 deg
Mean motion: 15
61125455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1517
Checksum: 305
Coasting Arc #6 (Orbit 1532)
---------------------------------------
Vector Time (GMT): 2011/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1917006
46 A = 6758393
46 meter
Y = 4127631
17 meter E =
0013926
Z = 5000166
38 I = 51
90639
XDOT = -5422
156993 Wp = 177
46808
YDOT = -5029
003825 meter/sec RA = 55
45150 deg
ZDOT = 2058
849483 TA = 252
53104
MA = 252
68330
Ha = 211
979 n
mi
Hp = 203
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6289391
28 X = -1987310
03
Y = 13542097
01 feet Y = 4105801
28 meter
Z = 16404745
33 Z = 4990682
45
XDOT = -17789
228979 XDOT = -5375
520280
YDOT = -16499
356380 feet/sec YDOT = -5089
376802 meter/sec
ZDOT = 6754
755521 ZDOT = 2032
622099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7480063
23 X = 2279923
27
Y = -12971771
36 feet Y = -3953795
91 meter
Z = 16365888
48 Z = 4988322
81
XDOT = 15466
742236 XDOT = 4714
263033
YDOT = 17363
715203 feet/sec YDOT = 5292
460394 meter/sec
ZDOT = 6648
188688 ZDOT = 2026
367912
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 11260
55150928
00016717 00000-0 10270-3 0 9057
2 25544 51
6361 55
8131 0011490 202
9178 157
1467 15
61137172 15338
Satellite: ISS
Catalog Number: 25544
Epoch time: 11260
55150928 = yrday
fracday
Element set: 905
Inclination: 51
6361 deg
RA of node: 55
8131 deg
Eccentricity:
0011490
Arg of perigee: 202
9178 deg
Mean anomaly: 157
1467 deg
Mean motion: 15
61137172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1533
Checksum: 289
Coasting Arc #7 (Orbit 1547)
---------------------------------------
Vector Time (GMT): 2011/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4698146
83 A = 6758999
04 meter
Y = -301810
87 meter E =
0015203
Z = -4860457
93 I = 51
89170
XDOT = 2980
190045 Wp = 155
80848
YDOT = 6626
814807 meter/sec RA = 50
39705 deg
ZDOT = 2458
360050 TA = 138
28525
MA = 138
16923
Ha = 211
818 n
mi
Hp = 203
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15413867
54 X = 4724783
92
Y = -990193
13 feet Y = -249124
64 meter
Z = -15946384
29 Z = -4837569
49
XDOT = 9777
526395 XDOT = 2893
923871
YDOT = 21741
518396 feet/sec YDOT = 6659
658907 meter/sec
ZDOT = 8065
485727 ZDOT = 2472
627993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15541326
48 X = -4736996
31
Y = -20322
27 feet Y = -6194
23 meter
Z = -15853129
83 Z = -4832033
97
XDOT = -8294
907156 XDOT = -2528
287701
YDOT = -21195
564599 feet/sec YDOT = -6460
408090 meter/sec
ZDOT = 8123
237734 ZDOT = 2475
962861
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 11261
51169745
00016717 00000-0 10270-3 0 9062
2 25544 51
6374 50
9757 0011476 205
9073 154
1511 15
61160677 15482
Satellite: ISS
Catalog Number: 25544
Epoch time: 11261
51169745 = yrday
fracday
Element set: 906
Inclination: 51
6374 deg
RA of node: 50
9757 deg
Eccentricity:
0011476
Arg of perigee: 205
9073 deg
Mean anomaly: 154
1511 deg
Mean motion: 15
61160677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1548
Checksum: 308
Coasting Arc #8 (Orbit 1563)
---------------------------------------
Vector Time (GMT): 2011/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5512219
42 A = 6767260
52 meter
Y = -3358132
13 meter E =
0016827
Z = 1995125
87 I = 51
89891
XDOT = 1102
307367 Wp = 154
25955
YDOT = -5142
380324 meter/sec RA = 45
37730 deg
ZDOT = -5607
166997 TA = 3
69886
MA = 3
68644
Ha = 211
634 n
mi
Hp = 204
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18084709
37 X = -5483950
44
Y = -11017493
86 feet Y = -3419614
99 meter
Z = 6545688
54 Z = 1968416
23
XDOT = 3616
493987 XDOT = 1186
967248
YDOT = -16871
326522 feet/sec YDOT = -5129
580538 meter/sec
ZDOT = -18396
217181 ZDOT = -5601
606101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17575399
96 X = 5356981
91
Y = 11872543
49 feet Y = 3618751
26 meter
Z = 6437076
15 Z = 1962020
81
XDOT = -3665
349323 XDOT = -1117
198474
YDOT = 15392
717463 feet/sec YDOT = 4691
700283 meter/sec
ZDOT = -18373
270526 ZDOT = -5600
172856
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 11262
53587862
00016717 00000-0 10270-3 0 9070
2 25544 51
6369 45
8147 0011455 210
2094 149
8403 15
61181439 15649
Satellite: ISS
Catalog Number: 25544
Epoch time: 11262
53587862 = yrday
fracday
Element set: 907
Inclination: 51
6369 deg
RA of node: 45
8147 deg
Eccentricity:
0011455
Arg of perigee: 210
2094 deg
Mean anomaly: 149
8403 deg
Mean motion: 15
61181439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 313
Coasting Arc #9 (Orbit 1579)
---------------------------------------
Vector Time (GMT): 2011/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3768163
98 A = 6766964
71 meter
Y = 5257526
44 meter E =
0007991
Z = 1991323
54 I = 51
87817
XDOT = -5036
177001 Wp = 123
19679
YDOT = 1481
866477 meter/sec RA = 40
39053 deg
ZDOT = 5597
019973 TA = 258
76573
MA = 258
85555
Ha = 211
280 n
mi
Hp = 204
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12362742
72 X = 3699419
73
Y = 17249102
48 feet Y = 5299280
06 meter
Z = 6533213
72 Z = 2009462
10
XDOT = -16522
890424 XDOT = -5079
562551
YDOT = 4861
766656 feet/sec YDOT = 1425
306510 meter/sec
ZDOT = 18362
926422 ZDOT = 5572
448768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11787692
56 X = -3592888
69
Y = -17619658
21 feet Y = -5370471
82 meter
Z = 6606797
55 Z = 2013751
89
XDOT = 15489
911163 XDOT = 4721
324922
YDOT = -3490
069689 feet/sec YDOT = -1063
773241 meter/sec
ZDOT = 18262
746123 ZDOT = 5566
485018
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 11263
56003854
00016717 00000-0 10270-3 0 9089
2 25544 51
6384 40
6541 0011470 213
9261 146
1163 15
61252977 15807
Satellite: ISS
Catalog Number: 25544
Epoch time: 11263
56003854 = yrday
fracday
Element set: 908
Inclination: 51
6384 deg
RA of node: 40
6541 deg
Eccentricity:
0011470
Arg of perigee: 213
9261 deg
Mean anomaly: 146
1163 deg
Mean motion: 15
61252977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 290
Coasting Arc #10 (Orbit 1594)
---------------------------------------
Vector Time (GMT): 2011/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 497
23 A = 6758551
89 meter
Y = -4691639
41 meter E =
0006949
Z = -4866717
29 I = 51
82637
XDOT = 6837
154520 Wp = 139
43742
YDOT = 2512
138688 meter/sec RA = 35
36775 deg
ZDOT = -2428
159899 TA = 106
88028
MA = 106
80407
Ha = 211
031 n
mi
Hp = 204
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1631
33 X = 76601
60
Y = -15392517
74 feet Y = -4691208
54 meter
Z = -15966920
25 Z = -4866529
81
XDOT = 22431
609319 XDOT = 6820
350671
YDOT = 8241
924830 feet/sec YDOT = 2588
501870 meter/sec
ZDOT = -7966
403868 ZDOT = -2394
986015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -305795
67 X = -93206
52
Y = 15390558
98 feet Y = 4691042
38 meter
Z = -15965880
19 Z = -4866400
28
XDOT = -21243
570992 XDOT = -6475
040438
YDOT = -8522
109902 feet/sec YDOT = -2597
539098 meter/sec
ZDOT = -7831
412737 ZDOT = -2387
014602
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 11264
52017205
00016717 00000-0 10270-3 0 9092
2 25544 51
6386 35
8166 0011263 218
2721 141
7636 15
61255933 15954
Satellite: ISS
Catalog Number: 25544
Epoch time: 11264
52017205 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 35
8166 deg
Eccentricity:
0011263
Arg of perigee: 218
2721 deg
Mean anomaly: 141
7636 deg
Mean motion: 15
61255933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 300
Coasting Arc #11 (Orbit 1610)
---------------------------------------
Vector Time (GMT): 2011/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4014642
17 A = 6758196
38 meter
Y = 2189399
95 meter E =
0005384
Z = 4976395
59 I = 51
79991
XDOT = -5372
655793 Wp = 202
94917
YDOT = -5064
915735 meter/sec RA = 30
30568 deg
ZDOT = -2111
584856 TA = 267
50013
MA = 267
56177
Ha = 210
897 n
mi
Hp = 204
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13171398
19 X = -4063000
40
Y = 7183070
71 feet Y = 2144235
66 meter
Z = 16326757
19 Z = 4956774
98
XDOT = -17626
823468 XDOT = -5305
361956
YDOT = -16617
177609 feet/sec YDOT = -5124
619919 meter/sec
ZDOT = -6927
771836 ZDOT = -2137
521340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13242961
72 X = 4036454
73
Y = -7232837
91 feet Y = -2204569
00 meter
Z = 16246699
85 Z = 4951994
11
XDOT = 17118
594289 XDOT = 5217
747539
YDOT = 15586
726745 feet/sec YDOT = 4750
834312 meter/sec
ZDOT = -7033
128057 ZDOT = -2143
697432
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 11265
54429496
00016717 00000-0 10270-3 0 9106
2 25544 51
6389 30
6553 0011146 221
6569 138
3740 15
61253121 16112
Satellite: ISS
Catalog Number: 25544
Epoch time: 11265
54429496 = yrday
fracday
Element set: 910
Inclination: 51
6389 deg
RA of node: 30
6553 deg
Eccentricity:
0011146
Arg of perigee: 221
6569 deg
Mean anomaly: 138
3740 deg
Mean motion: 15
61253121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1611
Checksum: 292
Coasting Arc #12 (Orbit 1625)
---------------------------------------
Vector Time (GMT): 2011/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6300957
94 A = 6766455
29 meter
Y = 1018022
06 meter E =
0005025
Z = -2249016
81 I = 51
80201
XDOT = 1102
028087 Wp = 230
35432
YDOT = 5274
866843 meter/sec RA = 25
27464 deg
ZDOT = 5463
948340 TA = 104
62889
MA = 104
57317
Ha = 210
480 n
mi
Hp = 204
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20672434
17 X = 6300031
16
Y = 3339967
40 feet Y = 1088477
88 meter
Z = -7378664
07 Z = -2218409
28
XDOT = 3615
577713 XDOT = 1016
418879
YDOT = 17305
993580 feet/sec YDOT = 5286
712147 meter/sec
ZDOT = 17926
339698 ZDOT = 5469
093610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20781810
92 X = -6334295
97
Y = -2905996
48 feet Y = -885747
73 meter
Z = -7254041
60 Z = -2211031
88
XDOT = -4080
210116 XDOT = -1243
648043
YDOT = -15714
348297 feet/sec YDOT = -4789
733361 meter/sec
ZDOT = 17946
986678 ZDOT = 5470
241540
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 11266
50438841
00016717 00000-0 10270-3 0 9118
2 25544 51
6396 25
8167 0011104 226
3976 133
6259 15
61304946 16266
Satellite: ISS
Catalog Number: 25544
Epoch time: 11266
50438841 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 25
8167 deg
Eccentricity:
0011104
Arg of perigee: 226
3976 deg
Mean anomaly: 133
6259 deg
Mean motion: 15
61304946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1626
Checksum: 308
Coasting Arc #13 (Orbit 1641)
---------------------------------------
Vector Time (GMT): 2011/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5491725
33 A = 6767023
45 meter
Y = -3517152
32 meter E =
0013469
Z = -1772027
52 I = 51
77690
XDOT = 3959
308928 Wp = 196
59162
YDOT = -3315
632329 meter/sec RA = 20
28037 deg
ZDOT = -5691
443978 TA = 2
90635
MA = 2
89853
Ha = 210
162 n
mi
Hp = 205
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18017471
57 X = -5443379
55
Y = -11539213
66 feet Y = -3578294
02 meter
Z = -5813738
57 Z = -1798588
37
XDOT = 12989
858687 XDOT = 4023
738563
YDOT = -10878
058822 feet/sec YDOT = -3270
997239 meter/sec
ZDOT = -18672
716464 ZDOT = -5672
052937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18408584
18 X = 5610936
46
Y = 10846173
79 feet Y = 3305913
77 meter
Z = -5921725
44 Z = -1804941
92
XDOT = -11887
407236 XDOT = -3623
281726
YDOT = 10027
746020 feet/sec YDOT = 3056
456987 meter/sec
ZDOT = -18593
531405 ZDOT = -5667
308372
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 11267
52846954
00016717 00000-0 10270-3 0 9120
2 25544 51
6398 20
6557 0011094 230
1750 129
8431 15
61350901 16424
Satellite: ISS
Catalog Number: 25544
Epoch time: 11267
52846954 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 20
6557 deg
Eccentricity:
0011094
Arg of perigee: 230
1750 deg
Mean anomaly: 129
8431 deg
Mean motion: 15
61350901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1642
Checksum: 298
Coasting Arc #14 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2011/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1864053
35 A = 6758466
18 meter
Y = 4412981
61 meter E =
0010357
Z = 4773666
17 I = 51
72087
XDOT = -7206
822995 Wp = 193
53698
YDOT = 187
766037 meter/sec RA = 15
25178 deg
ZDOT = 2631
893388 TA = 230
51373
MA = 230
60537
Ha = 209
851 n
mi
Hp = 205
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6115660
60 X = 1791378
44
Y = 14478286
11 feet Y = 4433420
83 meter
Z = 15661634
42 Z = 4782544
65
XDOT = -23644
432399 XDOT = -7221
172230
YDOT = 616
030305 feet/sec YDOT = 107
095019 meter/sec
ZDOT = 8634
820826 ZDOT = 2596
847869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6812216
63 X = -2076363
63
Y = -14124087
97 feet Y = -4305022
01 meter
Z = 15697538
33 Z = 4784609
68
XDOT = 22595
826917 XDOT = 6887
208044
YDOT = -1428
508330 feet/sec YDOT = -435
409339 meter/sec
ZDOT = 8492
059973 ZDOT = 2588
379880
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 11268
55252848
00016717 00000-0 10270-3 0 9138
2 25544 51
6408 15
4944 0011058 234
4872 125
5254 15
61408403 16584
Satellite: ISS
Catalog Number: 25544
Epoch time: 11268
55252848 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 15
4944 deg
Eccentricity:
0011058
Arg of perigee: 234
4872 deg
Mean anomaly: 125
5254 deg
Mean motion: 15
61408403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 306
Coasting Arc #15 (Orbit 1672)
---------------------------------------
Vector Time (GMT): 2011/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2863230
53 A = 6757467
40 meter
Y = -3513459
81 meter E =
0009557
Z = -5017528
90 I = 51
68822
XDOT = 6873
939317 Wp = 160
11026
YDOT = 2802
117269 meter/sec RA = 10
18212 deg
ZDOT = 1952
732996 TA = 128
85123
MA = 128
76590
Ha = 209
599 n
mi
Hp = 205
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9393800
96 X = 2926680
23
Y = -11527099
12 feet Y = -3481087
31 meter
Z = -16461708
98 Z = -5003464
71
XDOT = 22552
294348 XDOT = 6832
608555
YDOT = 9193
298127 feet/sec YDOT = 2878
755036 meter/sec
ZDOT = 6406
604317 ZDOT = 1986
025896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8632866
40 X = -2631297
68
Y = 12185262
81 feet Y = 3714068
10 meter
Z = -16404217
78 Z = -5000005
58
XDOT = -22231
531737 XDOT = -6776
170873
YDOT = -6909
061953 feet/sec YDOT = -2105
882083 meter/sec
ZDOT = 6542
040557 ZDOT = 1994
013962
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 11269
51256662
00016717 00000-0 10270-3 0 9144
2 25544 51
6409 10
6567 0010880 238
3062 121
7034 15
61439941 16731
Satellite: ISS
Catalog Number: 25544
Epoch time: 11269
51256662 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 10
6567 deg
Eccentricity:
0010880
Arg of perigee: 238
3062 deg
Mean anomaly: 121
7034 deg
Mean motion: 15
61439941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 299
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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