[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 16th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 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 501)
---------------------------------------
Vector Time (GMT): 2011/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3254040
49 A = 6767424
05 meter
Y = -4806827
74 meter E =
0009428
Z = -3485974
38 I = 51
80226
XDOT = 6117
974573 Wp = 345
01813
YDOT = -832
469390 meter/sec RA = 27
70393 deg
ZDOT = -4551
388829 TA = 235
90992
MA = 235
99943
Ha = 213
098 n
mi
Hp = 206
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10675985
86 X = -3183113
82
Y = -15770432
21 feet Y = -4842819
21 meter
Z = -11436923
83 Z = -3501610
82
XDOT = 20072
095057 XDOT = 6148
938154
YDOT = -2731
198785 feet/sec YDOT = -763
880550 meter/sec
ZDOT = -14932
378047 ZDOT = -4521
593139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11129448
29 X = -3392255
84
Y = 15406784
78 feet Y = 4695988
00 meter
Z = -11500121
57 Z = -3505237
06
XDOT = -8412
591040 XDOT = -2564
157749
YDOT = -17161
002087 feet/sec YDOT = -5230
673436 meter/sec
ZDOT = -14811
288763 ZDOT = -4514
480815
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 11194
52467334
00016717 00000-0 10270-3 0 9007
2 25544 51
6376 28
1027 0011498 319
5903 40
4397 15
59879530 5029
Satellite: ISS
Catalog Number: 25544
Epoch time: 11194
52467334 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 28
1027 deg
Eccentricity:
0011498
Arg of perigee: 319
5903 deg
Mean anomaly: 40
4397 deg
Mean motion: 15
59879530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 502
Checksum: 310
Coasting Arc #2 (Orbit 517)
---------------------------------------
Vector Time (GMT): 2011/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -550020
65 A = 6761056
53 meter
Y = 4243709
53 meter E =
0008261
Z = 5236795
82 I = 51
75314
XDOT = -7290
038975 Wp = 332
03713
YDOT = -2181
707604 meter/sec RA = 22
66691 deg
ZDOT = 1010
077924 TA = 108
36245
MA = 108
27259
Ha = 213
372 n
mi
Hp = 206
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1804529
69 X = -622872
62
Y = 13922931
52 feet Y = 4237150
66 meter
Z = 17181088
65 Z = 5233947
62
XDOT = -23917
450706 XDOT = -7270
007558
YDOT = -7157
833348 feet/sec YDOT = -2263
117419 meter/sec
ZDOT = 3313
903951 ZDOT = 974
711956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13670312
18 X = 4166711
15
Y = -3260991
68 feet Y = -993950
26 meter
Z = 17169235
70 Z = 5233183
04
XDOT = 1753
323767 XDOT = 534
413084
YDOT = 23907
865448 feet/sec YDOT = 7287
117388 meter/sec
ZDOT = 3170
384051 ZDOT = 966
333059
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 11195
54971014
00016717 00000-0 10270-3 0 9016
2 25544 51
6375 22
9464 0011445 323
5894 36
4482 15
59846356 5188
Satellite: ISS
Catalog Number: 25544
Epoch time: 11195
54971014 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 22
9464 deg
Eccentricity:
0011445
Arg of perigee: 323
5894 deg
Mean anomaly: 36
4482 deg
Mean motion: 15
59846356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 518
Checksum: 318
Coasting Arc #3 (Orbit 532)
---------------------------------------
Vector Time (GMT): 2011/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284834
99 A = 6763549
97 meter
Y = -2461502
22 meter E =
0006886
Z = -4618019
11 I = 51
73320
XDOT = 5649
447227 Wp = 28
98262
YDOT = 4259
390319 meter/sec RA = 17
61481 deg
ZDOT = 2979
243142 TA = 270
60047
MA = 270
67937
Ha = 213
445 n
mi
Hp = 206
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14057857
58 X = 4334474
48
Y = -8075794
68 feet Y = -2413308
36 meter
Z = -15150981
35 Z = -4597083
67
XDOT = 18534
931846 XDOT = 5586
925746
YDOT = 13974
377687 feet/sec YDOT = 4322
215864 meter/sec
ZDOT = 9774
419757 ZDOT = 3006
536260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12824578
66 X = -3908931
58
Y = -10047226
90 feet Y = -3062394
76 meter
Z = -15065771
43 Z = -4592047
13
XDOT = 5223
593017 XDOT = 1592
151152
YDOT = -21451
775196 feet/sec YDOT = -6538
501080 meter/sec
ZDOT = 9885
009763 ZDOT = 3012
950976
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 11196
51066746
00016717 00000-0 10270-3 0 9022
2 25544 51
6370 18
1126 0011366 326
7781 33
2660 15
59913524 5339
Satellite: ISS
Catalog Number: 25544
Epoch time: 11196
51066746 = yrday
fracday
Element set: 902
Inclination: 51
6370 deg
RA of node: 18
1126 deg
Eccentricity:
0011366
Arg of perigee: 326
7781 deg
Mean anomaly: 33
2660 deg
Mean motion: 15
59913524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 533
Checksum: 295
Coasting Arc #4 (Orbit 548)
---------------------------------------
Vector Time (GMT): 2011/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6503657
27 A = 6770940
88 meter
Y = 71663
43 meter E =
0008330
Z = 1886598
90 I = 51
72974
XDOT = -1693
701219 Wp = 56
84207
YDOT = -4928
850357 meter/sec RA = 12
59719 deg
ZDOT = -5629
048563 TA = 102
37445
MA = 102
28120
Ha = 213
536 n
mi
Hp = 205
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21337458
25 X = -6513139
79
Y = 235116
23 feet Y = -1117
68 meter
Z = 6189628
94 Z = 1854981
90
XDOT = -5556
762528 XDOT = -1611
115773
YDOT = -16170
768888 feet/sec YDOT = -4947
327896 meter/sec
ZDOT = -18468
007095 ZDOT = -5637
076373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8633229
36 X = 2631408
31
Y = 19554623
06 feet Y = 5960249
11 meter
Z = 6061186
20 Z = 1847449
55
XDOT = -11294
734419 XDOT = -3442
635051
YDOT = 10744
202001 feet/sec YDOT = 3274
832770 meter/sec
ZDOT = -18500
292969 ZDOT = -5638
889297
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 11197
53567550
00016717 00000-0 10270-3 0 9035
2 25544 51
6374 12
9574 0011688 330
3203 29
7288 15
59970816 5499
Satellite: ISS
Catalog Number: 25544
Epoch time: 11197
53567550 = yrday
fracday
Element set: 903
Inclination: 51
6374 deg
RA of node: 12
9574 deg
Eccentricity:
0011688
Arg of perigee: 330
3203 deg
Mean anomaly: 29
7288 deg
Mean motion: 15
59970816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 549
Checksum: 328
Coasting Arc #5 (Orbit 564)
---------------------------------------
Vector Time (GMT): 2011/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6170395
83 A = 6771190
99 meter
Y = 2175535
38 meter E =
0017972
Z = 1696661
11 I = 51
70062
XDOT = -3035
510859 Wp = 25
04705
YDOT = 4147
927025 meter/sec RA = 7
60392 deg
ZDOT = 5714
732509 TA = 353
60727
MA = 353
63017
Ha = 213
606 n
mi
Hp = 205
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20244080
81 X = 6137368
11
Y = 7137583
27 feet Y = 2244351
66 meter
Z = 5566473
47 Z = 1726556
16
XDOT = -9959
025129 XDOT = -3109
428627
YDOT = 13608
684465 feet/sec YDOT = 4113
568216 meter/sec
ZDOT = 18749
122405 ZDOT = 5699
807240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1764997
82 X = -537971
34
Y = -21360888
68 feet Y = -6510798
87 meter
Z = 5687771
72 Z = 1733632
82
XDOT = 14982
982724 XDOT = 4566
813134
YDOT = 3743
341432 feet/sec YDOT = 1140
970468 meter/sec
ZDOT = 18688
220679 ZDOT = 5696
169663
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 11198
56067405
00016717 00000-0 10270-3 0 9044
2 25544 51
6372 7
8013 0011387 334
5673 25
4921 15
59946751 5657
Satellite: ISS
Catalog Number: 25544
Epoch time: 11198
56067405 = yrday
fracday
Element set: 904
Inclination: 51
6372 deg
RA of node: 7
8013 deg
Eccentricity:
0011387
Arg of perigee: 334
5673 deg
Mean anomaly: 25
4921 deg
Mean motion: 15
59946751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 565
Checksum: 315
Coasting Arc #6 (Orbit 579)
---------------------------------------
Vector Time (GMT): 2011/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3405842
54 A = 6763602
51 meter
Y = -3727618
07 meter E =
0014956
Z = -4512023
64 I = 51
64642
XDOT = 6625
400599 Wp = 19
58786
YDOT = -2208
485056 meter/sec RA = 2
58465 deg
ZDOT = -3165
805220 TA = 218
59030
MA = 218
69729
Ha = 213
776 n
mi
Hp = 205
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11174024
10 X = -3341988
37
Y = -12229718
06 feet Y = -3765346
87 meter
Z = -14803227
16 Z = -4528414
06
XDOT = 21736
878605 XDOT = 6664
982453
YDOT = -7245
685878 feet/sec YDOT = -2134
174217 meter/sec
ZDOT = -10386
500067 ZDOT = -3133
523789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6357048
44 X = -1937628
36
Y = 15233001
56 feet Y = 4643018
88 meter
Z = -14869564
60 Z = -4532243
29
XDOT = -14716
045228 XDOT = -4485
450585
YDOT = -16186
130264 feet/sec YDOT = -4933
532504 meter/sec
ZDOT = -10255
225982 ZDOT = -3125
792879
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 11199
52159625
00016717 00000-0 10270-3 0 9058
2 25544 51
6381 2
9691 0011395 338
9912 21
0774 15
59986739 5803
Satellite: ISS
Catalog Number: 25544
Epoch time: 11199
52159625 = yrday
fracday
Element set: 905
Inclination: 51
6381 deg
RA of node: 2
9691 deg
Eccentricity:
0011395
Arg of perigee: 338
9912 deg
Mean anomaly: 21
0774 deg
Mean motion: 15
59986739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 580
Checksum: 335
Coasting Arc #7 (Orbit 595)
---------------------------------------
Vector Time (GMT): 2011/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -769845
94 A = 6760732
61 meter
Y = 4195357
88 meter E =
0012572
Z = 5247361
03 I = 51
60553
XDOT = -7623
397299 Wp = 357
48927
YDOT = -335
195190 meter/sec RA = 357
52393 deg
ZDOT = -838
214396 TA = 100
58986
MA = 100
44823
Ha = 214
031 n
mi
Hp = 205
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2525741
29 X = -842192
26
Y = 13764297
51 feet Y = 4186344
12 meter
Z = 17215751
42 Z = 5243445
76
XDOT = -25011
145994 XDOT = -7615
010679
YDOT = -1099
721752 feet/sec YDOT = -420
397712 meter/sec
ZDOT = -2750
047232 ZDOT = -875
227790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13515146
85 X = 4119416
76
Y = -3705766
48 feet Y = -1129517
62 meter
Z = 17199577
10 Z = 5242431
10
XDOT = 9756
749875 XDOT = 2973
857362
YDOT = 21935
566273 feet/sec YDOT = 6685
960600 meter/sec
ZDOT = -2900
371546 ZDOT = -884
033247
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 11200
54656855
00016717 00000-0 10270-3 0 9061
2 25544 51
6377 357
8126 0011345 342
8876 17
1896 15
59944072 5963
Satellite: ISS
Catalog Number: 25544
Epoch time: 11200
54656855 = yrday
fracday
Element set: 906
Inclination: 51
6377 deg
RA of node: 357
8126 deg
Eccentricity:
0011345
Arg of perigee: 342
8876 deg
Mean anomaly: 17
1896 deg
Mean motion: 15
59944072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 596
Checksum: 338
Coasting Arc #8 (Orbit 610)
---------------------------------------
Vector Time (GMT): 2011/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4577700
02 A = 6766900
56 meter
Y = -3463447
51 meter E =
0010754
Z = -3575478
77 I = 51
59802
XDOT = 5592
973204 Wp = 12
89760
YDOT = 2815
825686 meter/sec RA = 352
47455 deg
ZDOT = 4445
948310 TA = 304
67570
MA = 304
77700
Ha = 214
093 n
mi
Hp = 204
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15018700
85 X = 4633457
49
Y = -11363016
77 feet Y = -3411944
90 meter
Z = -11730573
40 Z = -3553105
45
XDOT = 18349
649621 XDOT = 5539
473149
YDOT = 9238
273249 feet/sec YDOT = 2878
070301 meter/sec
ZDOT = 14586
444586 ZDOT = 4472
988767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16994404
78 X = -5179894
58
Y = -8246131
13 feet Y = -2513420
77 meter
Z = -11639476
17 Z = -3547712
34
XDOT = -707
247948 XDOT = -215
569175
YDOT = -19226
164815 feet/sec YDOT = -5860
135036 meter/sec
ZDOT = 14696
095080 ZDOT = 4479
369780
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 11201
50746496
00016717 00000-0 10270-3 0 9070
2 25544 51
6391 352
9800 0011356 346
1007 13
9835 15
60009721 6119
Satellite: ISS
Catalog Number: 25544
Epoch time: 11201
50746496 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 352
9800 deg
Eccentricity:
0011356
Arg of perigee: 346
1007 deg
Mean anomaly: 13
9835 deg
Mean motion: 15
60009721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 611
Checksum: 283
Coasting Arc #9 (Orbit 626)
---------------------------------------
Vector Time (GMT): 2011/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6568541
12 A = 6772134
43 meter
Y = 1640477
04 meter E =
0007632
Z = 221506
48 I = 51
58557
XDOT = -1351
288543 Wp = 67
38111
YDOT = -4577
203087 meter/sec RA = 347
46407 deg
ZDOT = -6004
263269 TA = 110
22703
MA = 110
14496
Ha = 214
158 n
mi
Hp = 204
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21550331
76 X = -6587473
09
Y = 5382142
51 feet Y = 1566917
74 meter
Z = 726727
31 Z = 189551
04
XDOT = -4433
361363 XDOT = -1270
837689
YDOT = -15017
070494 feet/sec YDOT = -4591
863795 meter/sec
ZDOT = -19699
026473 ZDOT = -6010
632636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14905317
31 X = 4543140
72
Y = 16473848
83 feet Y = 5021229
12 meter
Z = 596833
12 Z = 181914
74
XDOT = -10010
748773 XDOT = -3051
276226
YDOT = 9796
511975 feet/sec YDOT = 2985
976850 meter/sec
ZDOT = -19724
602588 ZDOT = -6012
058869
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 11202
53240861
00016717 00000-0 10270-3 0 9080
2 25544 51
6384 347
8243 0011564 349
6790 10
4127 15
60054932 6270
Satellite: ISS
Catalog Number: 25544
Epoch time: 11202
53240861 = yrday
fracday
Element set: 908
Inclination: 51
6384 deg
RA of node: 347
8243 deg
Eccentricity:
0011564
Arg of perigee: 349
6790 deg
Mean anomaly: 10
4127 deg
Mean motion: 15
60054932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 627
Checksum: 294
Coasting Arc #10 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2011/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5885422
05 A = 6767576
20 meter
Y = 818111
13 meter E =
0016454
Z = 3216019
10 I = 51
54262
XDOT = -3311
969235 Wp = 43
30011
YDOT = 5028
074890 meter/sec RA = 342
45509 deg
ZDOT = 4779
229360 TA = 354
13403
MA = 354
15328
Ha = 214
096 n
mi
Hp = 204
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19309127
44 X = 5860213
67
Y = 2684091
65 feet Y = 883784
32 meter
Z = 10551243
76 Z = 3244549
02
XDOT = -10866
040797 XDOT = -3391
164385
YDOT = 16496
308694 feet/sec YDOT = 4990
595271 meter/sec
ZDOT = 15679
886351 ZDOT = 4762
947988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7015129
36 X = -2138211
43
Y = -18121181
61 feet Y = -5523336
15 meter
Z = 10667062
99 Z = 3251320
80
XDOT = 18423
679654 XDOT = 5615
537559
YDOT = 2063
822348 feet/sec YDOT = 629
053052 meter/sec
ZDOT = 15613
438921 ZDOT = 4758
976183
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 11203
55733947
00016717 00000-0 10270-3 0 9096
2 25544 51
6396 342
6690 0011404 353
3416 6
7586 15
60074144 6434
Satellite: ISS
Catalog Number: 25544
Epoch time: 11203
55733947 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 342
6690 deg
Eccentricity:
0011404
Arg of perigee: 353
3416 deg
Mean anomaly: 6
7586 deg
Mean motion: 15
60074144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 304
Coasting Arc #11 (Orbit 657)
---------------------------------------
Vector Time (GMT): 2011/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2954754
50 A = 6760620
59 meter
Y = -3225254
75 meter E =
0019291
Z = -5169070
71 I = 51
49110
XDOT = 6504
990656 Wp = 43
26443
YDOT = -3838
414758 meter/sec RA = 337
40424 deg
ZDOT = -1312
546514 TA = 214
03520
MA = 214
15907
Ha = 214
361 n
mi
Hp = 203
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9694076
45 X = -2893359
28
Y = -10581544
46 feet Y = -3257952
89 meter
Z = -16958893
40 Z = -5183275
94
XDOT = 21341
832861 XDOT = 6553
805146
YDOT = -12593
224273 feet/sec YDOT = -3765
398940 meter/sec
ZDOT = -4306
254967 ZDOT = -1280
827300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4347443
58 X = -1325100
80
Y = 13604810
40 feet Y = 4146746
21 meter
Z = -17016378
43 Z = -5186592
15
XDOT = -20616
843890 XDOT = -6284
014018
YDOT = -11857
236503 feet/sec YDOT = -3614
085686 meter/sec
ZDOT = -4177
187959 ZDOT = -1273
206890
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 11204
51820056
00016717 00000-0 10270-3 0 9103
2 25544 51
6399 337
8371 0011576 357
3518 2
7574 15
60082549 6583
Satellite: ISS
Catalog Number: 25544
Epoch time: 11204
51820056 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 337
8371 deg
Eccentricity:
0011576
Arg of perigee: 357
3518 deg
Mean anomaly: 2
7574 deg
Mean motion: 15
60082549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 658
Checksum: 310
Coasting Arc #12 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2011/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1046420
71 A = 6762788
03 meter
Y = 4762376
29 meter E =
0016841
Z = 4686641
26 I = 51
47058
XDOT = -7055
105268 Wp = 25
86588
YDOT = 1201
718882 meter/sec RA = 332
33095 deg
ZDOT = -2777
734444 TA = 91
78101
MA = 91
58811
Ha = 214
574 n
mi
Hp = 203
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3433138
81 X = -1122363
42
Y = 15624594
12 feet Y = 4750249
48 meter
Z = 15376119
62 Z = 4681373
81
XDOT = -23146
670828 XDOT = -7054
525149
YDOT = 3942
647250 feet/sec YDOT = 1122
827922 meter/sec
ZDOT = -9113
301980 ZDOT = -2812
006336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15202748
88 X = 4633797
86
Y = -5045550
38 feet Y = -1537883
76 meter
Z = 15354422
36 Z = 4680027
93
XDOT = 14927
395184 XDOT = 4549
870052
YDOT = 16634
234772 feet/sec YDOT = 5070
114759 meter/sec
ZDOT = -9252
565289 ZDOT = -2820
181900
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 11205
54310633
00016717 00000-0 10270-3 0 9113
2 25544 51
6400 332
6806 0011535 1
5626 358
5564 15
60059505 6740
Satellite: ISS
Catalog Number: 25544
Epoch time: 11205
54310633 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 332
6806 deg
Eccentricity:
0011535
Arg of perigee: 1
5626 deg
Mean anomaly: 358
5564 deg
Mean motion: 15
60059505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 277
Coasting Arc #13 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2011/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4382384
19 A = 6770318
54 meter
Y = -4732614
40 meter E =
0017658
Z = -2027133
17 I = 51
47070
XDOT = 4861
011040 Wp = 16
92127
YDOT = 2134
496777 meter/sec RA = 327
29213 deg
ZDOT = 5554
288515 TA = 320
54269
MA = 320
67115
Ha = 214
675 n
mi
Hp = 203
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14377900
89 X = 4444826
85
Y = -15526950
13 feet Y = -4683258
54 meter
Z = -6650699
38 Z = -2005692
62
XDOT = 15948
198950 XDOT = 4809
799929
YDOT = 7002
942183 feet/sec YDOT = 2188
568587 meter/sec
ZDOT = 18222
731348 ZDOT = 5577
778941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20812282
74 X = -6343583
78
Y = -3976645
59 feet Y = -1212081
58 meter
Z = -6563321
83 Z = -2000500
49
XDOT = -2761
531509 XDOT = -841
714804
YDOT = -15622
842290 feet/sec YDOT = -4761
842330 meter/sec
ZDOT = 18317
995496 ZDOT = 5583
325027
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 11206
50394056
00016717 00000-0 10270-3 0 9122
2 25544 51
6408 327
8475 0011734 4
4700 355
6559 15
60098175 6896
Satellite: ISS
Catalog Number: 25544
Epoch time: 11206
50394056 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 327
8475 deg
Eccentricity:
0011734
Arg of perigee: 4
4700 deg
Mean anomaly: 355
6559 deg
Mean motion: 15
60098175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 312
Coasting Arc #14 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2011/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5893961
49 A = 6770712
43 meter
Y = 2919362
71 meter E =
0008461
Z = -1626976
50 I = 51
44779
XDOT = -922
919687 Wp = 49
64308
YDOT = -5036
063566 meter/sec RA = 322
28108 deg
ZDOT = -5707
272506 TA = 148
23830
MA = 148
18724
Ha = 214
695 n
mi
Hp = 203
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19337144
00 X = -5918264
86
Y = 9577961
63 feet Y = 2853317
16 meter
Z = -5337849
40 Z = -1655667
68
XDOT = -3027
951729 XDOT = -838
812297
YDOT = -16522
518261 feet/sec YDOT = -5045
913225 meter/sec
ZDOT = -18724
647330 ZDOT = -5711
552338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18555458
23 X = 5655703
67
Y = 10958917
98 feet Y = 3340278
20 meter
Z = -5454558
62 Z = -1662549
47
XDOT = -11461
594346 XDOT = -3493
493957
YDOT = 10101
053928 feet/sec YDOT = 3078
801237 meter/sec
ZDOT = -18741
709649 ZDOT = -5712
473101
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 11207
52881865
00016717 00000-0 10270-3 0 9135
2 25544 51
6408 322
6917 0011728 8
4284 351
7067 15
60143555 7057
Satellite: ISS
Catalog Number: 25544
Epoch time: 11207
52881865 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 322
6917 deg
Eccentricity:
0011728
Arg of perigee: 8
4284 deg
Mean anomaly: 351
7067 deg
Mean motion: 15
60143555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 306
Coasting Arc #15 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2011/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5047423
26 A = 6763050
59 meter
Y = 207272
95 meter E =
0013282
Z = 4483150
21 I = 51
40010
XDOT = -3074
350600 Wp = 52
22859
YDOT = 6291
312893 meter/sec RA = 317
24294 deg
ZDOT = 3172
015172 TA = 5
90972
MA = 5
89406
Ha = 214
608 n
mi
Hp = 203
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16559787
61 X = 5022952
38
Y = 680029
37 feet Y = 263578
90 meter
Z = 14708498
08 Z = 4507610
79
XDOT = -10086
452099 XDOT = -3159
881614
YDOT = 20640
790330 feet/sec YDOT = 6256
454988 meter/sec
ZDOT = 10406
873923 ZDOT = 3156
873286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8653883
85 X = -2637703
80
Y = -14030943
58 feet Y = -4276631
60 meter
Z = 14807830
29 Z = 4513426
67
XDOT = 21762
702775 XDOT = 6633
271806
YDOT = -2510
272470 feet/sec YDOT = -765
131049 meter/sec
ZDOT = 10344
981806 ZDOT = 3153
150454
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 11208
55368217
00016717 00000-0 10270-3 0 9141
2 25544 51
6416 317
5359 0011736 12
0037 348
1396 15
60183306 7216
Satellite: ISS
Catalog Number: 25544
Epoch time: 11208
55368217 = yrday
fracday
Element set: 914
Inclination: 51
6416 deg
RA of node: 317
5359 deg
Eccentricity:
0011736
Arg of perigee: 12
0037 deg
Mean anomaly: 348
1396 deg
Mean motion: 15
60183306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 291
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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