[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 23rd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 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 1594)
---------------------------------------
Vector Time (GMT): 2011/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 165888
25 A = 6758059
61 meter
Y = -4629003
61 meter E =
0007232
Z = -4923284
25 I = 51
82598
XDOT = 6834
504443 Wp = 137
89177
YDOT = 2657
667170 meter/sec RA = 35
37067 deg
ZDOT = -2275
689601 TA = 109
99798
MA = 109
92010
Ha = 210
896 n
mi
Hp = 204
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 544252
79 X = 241554
71
Y = -15187019
71 feet Y = -4626725
69 meter
Z = -16152507
39 Z = -4922294
37
XDOT = 22422
914838 XDOT = 6815
332791
YDOT = 8719
380478 feet/sec YDOT = 2733
987484 meter/sec
ZDOT = -7466
173230 ZDOT = -2242
534349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -846701
18 X = -258074
52
Y = 15177744
65 feet Y = 4626176
57 meter
Z = -16148202
31 Z = -4921972
07
XDOT = -21240
931453 XDOT = -6474
235907
YDOT = -8959
944426 feet/sec YDOT = -2730
991061 meter/sec
ZDOT = -7331
266565 ZDOT = -2234
570049
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
51989137
00016717 00000-0 10270-3 0 9004
2 25544 51
6389 35
8221 0011319 218
5385 141
4964 15
61345705 15958
Satellite: ISS
Catalog Number: 25544
Epoch time: 11264
51989137 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 35
8221 deg
Eccentricity:
0011319
Arg of perigee: 218
5385 deg
Mean anomaly: 141
4964 deg
Mean motion: 15
61345705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 316
Coasting Arc #2 (Orbit 1610)
---------------------------------------
Vector Time (GMT): 2011/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4168465
01 A = 6758217
32 meter
Y = 2040723
88 meter E =
0005153
Z = 4912260
15 I = 51
80118
XDOT = -5219
206500 Wp = 199
26918
YDOT = -5144
555070 meter/sec RA = 30
30770 deg
ZDOT = -2297
144161 TA = 273
07240
MA = 273
13136
Ha = 210
772 n
mi
Hp = 204
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13676066
30 X = -4214837
72
Y = 6695288
32 feet Y = 1993850
55 meter
Z = 16116339
09 Z = 4891897
10
XDOT = -17123
380906 XDOT = -5150
132116
YDOT = -16878
461515 feet/sec YDOT = -5202
533345 meter/sec
ZDOT = -7536
562209 ZDOT = -2322
330863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13748151
12 X = 4190436
46
Y = -6746908
85 feet Y = -2056457
82 meter
Z = 16033266
12 Z = 4886939
51
XDOT = 16647
893855 XDOT = 5074
278047
YDOT = 15813
072899 feet/sec YDOT = 4819
824620 meter/sec
ZDOT = -7638
859360 ZDOT = -2328
324333
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
54395616
00016717 00000-0 10270-3 0 9012
2 25544 51
6392 30
6605 0011215 221
8898 138
1402 15
61340256 16117
Satellite: ISS
Catalog Number: 25544
Epoch time: 11265
54395616 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 30
6605 deg
Eccentricity:
0011215
Arg of perigee: 221
8898 deg
Mean anomaly: 138
1402 deg
Mean motion: 15
61340256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1611
Checksum: 283
Coasting Arc #3 (Orbit 1625)
---------------------------------------
Vector Time (GMT): 2011/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6333345
16 A = 6766533
82 meter
Y = 1196868
55 meter E =
0004594
Z = -2061716
16 I = 51
80355
XDOT = 825
479885 Wp = 235
57834
YDOT = 5226
606728 meter/sec RA = 25
27857 deg
ZDOT = 5558
592576 TA = 101
61230
MA = 101
56073
Ha = 210
341 n
mi
Hp = 204
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20778691
47 X = 6329506
21
Y = 3926734
08 feet Y = 1267670
27 meter
Z = -6764160
63 Z = -2030958
39
XDOT = 2708
267339 XDOT = 739
971123
YDOT = 17147
659870 feet/sec YDOT = 5235
360069 meter/sec
ZDOT = 18236
852282 ZDOT = 5562
394631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20896600
38 X = -6369283
80
Y = -3490521
57 feet Y = -1063910
97 meter
Z = -6638936
71 Z = -2023547
91
XDOT = -3210
558452 XDOT = -978
578216
YDOT = -15566
691179 feet/sec YDOT = -4744
727471 meter/sec
ZDOT = 18252
030403 ZDOT = 5563
218867
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
50399501
00016717 00000-0 10270-3 0 9027
2 25544 51
6399 25
8215 0011165 226
6389 133
3838 15
61395120 16265
Satellite: ISS
Catalog Number: 25544
Epoch time: 11266
50399501 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 25
8215 deg
Eccentricity:
0011165
Arg of perigee: 226
6389 deg
Mean anomaly: 133
3838 deg
Mean motion: 15
61395120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1626
Checksum: 306
Coasting Arc #4 (Orbit 1641)
---------------------------------------
Vector Time (GMT): 2011/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5332077
97 A = 6766410
78 meter
Y = -3642754
75 meter E =
0012942
Z = -1991315
75 I = 51
77610
XDOT = 4231
566624 Wp = 198
90890
YDOT = -3135
474231 meter/sec RA = 20
28404 deg
ZDOT = -5596
769194 TA = 3
12136
MA = 3
11329
Ha = 210
022 n
mi
Hp = 204
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17493694
12 X = -5281274
28
Y = -11951295
12 feet Y = -3702097
45 meter
Z = -6533188
16 Z = -2017095
06
XDOT = 13883
092598 XDOT = 4293
501551
YDOT = -10286
988948 feet/sec YDOT = -3087
808528 meter/sec
ZDOT = -18362
103656 ZDOT = -5576
061611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17896559
05 X = 5454871
20
Y = 11278106
18 feet Y = 3437566
76 meter
Z = -6637984
00 Z = -2023257
52
XDOT = -12769
122854 XDOT = -3892
028646
YDOT = 9508
379324 feet/sec YDOT = 2898
154018 meter/sec
ZDOT = -18277
566354 ZDOT = -5571
002225
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
52801787
00016717 00000-0 10270-3 0 9035
2 25544 51
6402 20
6602 0011158 230
4410 129
5761 15
61438887 16421
Satellite: ISS
Catalog Number: 25544
Epoch time: 11267
52801787 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 20
6602 deg
Eccentricity:
0011158
Arg of perigee: 230
4410 deg
Mean anomaly: 129
5761 deg
Mean motion: 15
61438887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1642
Checksum: 290
Coasting Arc #5 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2011/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1545854
70 A = 6757763
05 meter
Y = 4415698
70 meter E =
0010501
Z = 4882876
80 I = 51
71973
XDOT = -7302
956795 Wp = 198
13808
YDOT = -61
414446 meter/sec RA = 15
25146 deg
ZDOT = 2359
159511 TA = 228
76348
MA = 228
85401
Ha = 209
708 n
mi
Hp = 205
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5071701
77 X = 1472642
53
Y = 14487200
48 feet Y = 4432576
64 meter
Z = 16019936
99 Z = 4890208
17
XDOT = -23959
832005 XDOT = -7313
187612
YDOT = -201
490964 feet/sec YDOT = -143
137497 meter/sec
ZDOT = 7740
024641 ZDOT = 2323
657009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5768209
13 X = -1758150
14
Y = -14190827
34 feet Y = -4325364
17 meter
Z = 16049538
95 Z = 4891899
47
XDOT = 22945
674439 XDOT = 6993
841569
YDOT = -705
459294 feet/sec YDOT = -215
023993 meter/sec
ZDOT = 7595
417087 ZDOT = 2315
083128
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
55201841
00016717 00000-0 10270-3 0 9045
2 25544 51
6411 15
4986 0011121 234
7986 125
2130 15
61497789 16589
Satellite: ISS
Catalog Number: 25544
Epoch time: 11268
55201841 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 15
4986 deg
Eccentricity:
0011121
Arg of perigee: 234
7986 deg
Mean anomaly: 125
2130 deg
Mean motion: 15
61497789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 308
Coasting Arc #6 (Orbit 1672)
---------------------------------------
Vector Time (GMT): 2011/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3193728
05 A = 6757654
33 meter
Y = -3371227
37 meter E =
0009515
Z = -4914531
65 I = 51
69005
XDOT = 6684
074912 Wp = 165
51001
YDOT = 3018
425134 meter/sec RA = 10
18070 deg
ZDOT = 2265
051255 TA = 126
62413
MA = 126
53659
Ha = 209
460 n
mi
Hp = 205
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10478110
41 X = 3255062
38
Y = -11060457
26 feet Y = -3335170
86 meter
Z = -16123791
49 Z = -4898867
05
XDOT = 21929
379632 XDOT = 6638
822274
YDOT = 9902
969600 feet/sec YDOT = 3092
917834 meter/sec
ZDOT = 7431
270523 ZDOT = 2297
412238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9746080
16 X = -2970605
23
Y = 11798229
66 feet Y = 3596100
40 meter
Z = -16059790
26 Z = -4895024
07
XDOT = -21683
737886 XDOT = -6609
203308
YDOT = -7581
311574 feet/sec YDOT = -2310
783768 meter/sec
ZDOT = 7562
898266 ZDOT = 2305
171391
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
51200178
00016717 00000-0 10270-3 0 9055
2 25544 51
6413 10
6605 0010953 238
5448 121
4638 15
61528920 16733
Satellite: ISS
Catalog Number: 25544
Epoch time: 11269
51200178 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 10
6605 deg
Eccentricity:
0010953
Arg of perigee: 238
5448 deg
Mean anomaly: 121
4638 deg
Mean motion: 15
61528920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 292
Coasting Arc #7 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2011/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6352935
36 A = 6766209
79 meter
Y = 1055665
79 meter E =
0010740
Z = 2051667
74 I = 51
68835
XDOT = -2566
110135 Wp = 161
30919
YDOT = -4641
346091 meter/sec RA = 5
14376 deg
ZDOT = -5559
659594 TA = 355
93172
MA = 355
94044
Ha = 209
272 n
mi
Hp = 205
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20842963
79 X = -6374234
57
Y = 3463470
44 feet Y = 984504
55 meter
Z = 6731193
37 Z = 2020753
06
XDOT = -8418
996507 XDOT = -2487
010926
YDOT = -15227
513421 feet/sec YDOT = -4669
600355 meter/sec
ZDOT = -18240
352998 ZDOT = -5571
933124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20488897
41 X = 6245015
93
Y = -5320698
34 feet Y = -1621748
85 meter
Z = 6605223
96 Z = 2013272
26
XDOT = 9251
705059 XDOT = 2819
919702
YDOT = 12928
720301 feet/sec YDOT = 3940
673948 meter/sec
ZDOT = -18290
062895 ZDOT = -5574
811170
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 11270
53596335
00016717 00000-0 10270-3 0 9063
2 25544 51
6411 5
4993 0010912 242
4211 117
5838 15
61514484 16895
Satellite: ISS
Catalog Number: 25544
Epoch time: 11270
53596335 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 5
4993 deg
Eccentricity:
0010912
Arg of perigee: 242
4211 deg
Mean anomaly: 117
5838 deg
Mean motion: 15
61514484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 302
Coasting Arc #8 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2011/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6242437
36 A = 6765945
40 meter
Y = 1626223
79 meter E =
0003191
Z = 2036776
36 I = 51
65836
XDOT = -2959
611486 Wp = 77
16839
YDOT = 4389
767020 meter/sec RA =
14011 deg
ZDOT = 5559
246234 TA = 305
40601
MA = 305
43581
Ha = 208
800 n
mi
Hp = 205
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20480437
53 X = 6213894
23
Y = 5335379
88 feet Y = 1695871
18 meter
Z = 6682337
15 Z = 2067033
00
XDOT = -9710
011436 XDOT = -3035
484922
YDOT = 14402
122769 feet/sec YDOT = 4356
247214 meter/sec
ZDOT = 18238
996831 ZDOT = 5544
683474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20892420
77 X = -6368009
85
Y = -3124217
08 feet Y = -952261
37 meter
Z = 6805457
50 Z = 2074303
45
XDOT = 7999
059618 XDOT = 2438
113372
YDOT = -13845
084704 feet/sec YDOT = -4219
981818 meter/sec
ZDOT = 18179
425678 ZDOT = 5541
088947
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 11271
55990197
00016717 00000-0 10270-3 0 9071
2 25544 51
6416
3370 0010836 247
1468 112
8545 15
61569218 17051
Satellite: ISS
Catalog Number: 25544
Epoch time: 11271
55990197 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node:
3370 deg
Eccentricity:
0010836
Arg of perigee: 247
1468 deg
Mean anomaly: 112
8545 deg
Mean motion: 15
61569218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 306
Coasting Arc #9 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2011/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2849871
31 A = 6757352
88 meter
Y = -3663593
62 meter E =
0001608
Z = -4912389
87 I = 51
59857
XDOT = 6943
856519 Wp = 91
83640
YDOT = -2385
499525 meter/sec RA = 355
09819 deg
ZDOT = -2250
017657 TA = 156
21225
MA = 156
20482
Ha = 208
441 n
mi
Hp = 205
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9349971
47 X = -2784828
60
Y = -12019664
11 feet Y = -3695099
36 meter
Z = -16116764
65 Z = -4926076
45
XDOT = 22781
681493 XDOT = 6980
945901
YDOT = -7826
442012 feet/sec YDOT = -2307
641880 meter/sec
ZDOT = -7381
947692 ZDOT = -2216
193602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10669484
11 X = 3252058
76
Y = 10782579
53 feet Y = 3286530
24 meter
Z = -16172275
11 Z = -4929309
45
XDOT = -20895
034240 XDOT = -6368
806436
YDOT = 9814
212717 feet/sec YDOT = 2991
372036 meter/sec
ZDOT = -7244
061300 ZDOT = -2207
989884
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 11272
51982637
00016717 00000-0 10270-3 0 9089
2 25544 51
6409 355
4986 0010896 251
2488 108
7486 15
61578586 17207
Satellite: ISS
Catalog Number: 25544
Epoch time: 11272
51982637 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 355
4986 deg
Eccentricity:
0010896
Arg of perigee: 251
2488 deg
Mean anomaly: 108
7486 deg
Mean motion: 15
61578586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 350
Coasting Arc #10 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2011/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1993037
27 A = 6757498
69 meter
Y = 4261967
86 meter E =
0004512
Z = 4854635
50 I = 51
56966
XDOT = -7261
012464 Wp = 281
24187
YDOT = -658
541672 meter/sec RA = 350
01680 deg
ZDOT = -2403
842848 TA = 192
31339
MA = 192
32442
Ha = 207
987 n
mi
Hp = 205
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6538836
19 X = -2064130
59
Y = 13982834
20 feet Y = 4239283
27 meter
Z = 15927281
84 Z = 4844780
26
XDOT = -23822
219369 XDOT = -7241
431256
YDOT = -2160
569789 feet/sec YDOT = -739
629411 meter/sec
ZDOT = -7886
623516 ZDOT = -2439
069753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4599135
66 X = 1401816
55
Y = -14778673
50 feet Y = -4504539
68 meter
Z = 15886884
48 Z = 4842322
39
XDOT = 22763
922390 XDOT = 6938
443544
YDOT = -1544
390276 feet/sec YDOT = -470
730156 meter/sec
ZDOT = -8030
031407 ZDOT = -2447
553573
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 11273
54372384
00016717 00000-0 10270-3 0 9096
2 25544 51
6411 350
3362 0010815 255
9602 104
0352 15
61657204 17365
Satellite: ISS
Catalog Number: 25544
Epoch time: 11273
54372384 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 350
3362 deg
Eccentricity:
0010815
Arg of perigee: 255
9602 deg
Mean anomaly: 104
0352 deg
Mean motion: 15
61657204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1736
Checksum: 285
Coasting Arc #11 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2011/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5723806
38 A = 6766172
93 meter
Y = -3075502
30 meter E =
0007196
Z = -1872962
37 I = 51
56788
XDOT = 3783
122896 Wp = 302
02653
YDOT = 3606
979735 meter/sec RA = 344
97215 deg
ZDOT = 5626
366970 TA = 37
26733
MA = 37
21742
Ha = 207
564 n
mi
Hp = 205
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18778892
34 X = 5766870
46
Y = -10090230
64 feet Y = -3011254
48 meter
Z = -6144889
66 Z = -1845051
07
XDOT = 12411
820526 XDOT = 3715
175576
YDOT = 11833
923014 feet/sec YDOT = 3648
905233 meter/sec
ZDOT = 18459
209219 ZDOT = 5644
580407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16986903
26 X = -5177608
11
Y = 12934098
93 feet Y = 3942313
35 meter
Z = -6031038
31 Z = -1838260
48
XDOT = -13071
044292 XDOT = -3984
054300
YDOT = -8506
120670 feet/sec YDOT = -2592
665580 meter/sec
ZDOT = 18533
149332 ZDOT = 5648
903916
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 11274
50361018
00016717 00000-0 10270-3 0 9107
2 25544 51
6403 345
4967 0010748 260
3506 99
6436 15
61626725 17513
Satellite: ISS
Catalog Number: 25544
Epoch time: 11274
50361018 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 345
4967 deg
Eccentricity:
0010748
Arg of perigee: 260
3506 deg
Mean anomaly: 99
6436 deg
Mean motion: 15
61626725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 304
Coasting Arc #12 (Orbit 1766)
---------------------------------------
Vector Time (GMT): 2011/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6364075
21 A = 6765233
20 meter
Y = 427892
93 meter E =
0008379
Z = -2239198
11 I = 51
53577
XDOT = 1571
747493 Wp = 229
43543
YDOT = -5181
231469 meter/sec RA = 339
95975 deg
ZDOT = -5449
167173 TA = 335
59123
MA = 335
63089
Ha = 207
000 n
mi
Hp = 205
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20879511
86 X = -6357509
30
Y = 1403848
19 feet Y = 356762
59 meter
Z = -7346450
49 Z = -2270099
09
XDOT = 5156
651880 XDOT = 1656
039498
YDOT = -16998
790909 feet/sec YDOT = -5163
184094 meter/sec
ZDOT = -17877
845056 ZDOT = -5441
326658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20268649
55 X = 6177884
38
Y = -5024098
48 feet Y = -1531345
22 meter
Z = -7472310
21 Z = -2277560
15
XDOT = -2577
893878 XDOT = -785
742054
YDOT = 16180
166967 feet/sec YDOT = 4931
714892 meter/sec
ZDOT = -17845
590412 ZDOT = -5439
335957
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 11275
52746820
00016717 00000-0 10270-3 0 9119
2 25544 51
6396 340
3342 0010572 263
8308 96
1645 15
61684592 17675
Satellite: ISS
Catalog Number: 25544
Epoch time: 11275
52746820 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 340
3342 deg
Eccentricity:
0010572
Arg of perigee: 263
8308 deg
Mean anomaly: 96
1645 deg
Mean motion: 15
61684592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1767
Checksum: 318
Coasting Arc #13 (Orbit 1782)
---------------------------------------
Vector Time (GMT): 2011/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3685923
33 A = 6756527
75 meter
Y = 2668959
33 meter E =
0006893
Z = 5000267
94 I = 51
47926
XDOT = -5909
762202 Wp = 238
14981
YDOT = 4489
394586 meter/sec RA = 334
90375 deg
ZDOT = 1958
491799 TA = 192
80754
MA = 192
82506
Ha = 206
690 n
mi
Hp = 205
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12092924
32 X = 3631514
06
Y = 8756428
24 feet Y = 2709873
53 meter
Z = 16405078
53 Z = 5018041
97
XDOT = -19388
983604 XDOT = -5969
038301
YDOT = 14728
984863 feet/sec YDOT = 4422
976643 meter/sec
ZDOT = 6425
498027 ZDOT = 1929
637931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13450238
96 X = -4099632
83
Y = -6295272
69 feet Y = -1918799
11 meter
Z = 16477289
51 Z = 5022277
84
XDOT = 15783
950915 XDOT = 4810
948239
YDOT = -17199
953162 feet/sec YDOT = -5242
545724 meter/sec
ZDOT = 6307
718478 ZDOT = 1922
592592
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 11276
55130336
00016717 00000-0 10270-3 0 9123
2 25544 51
6400 335
1711 0010619 268
1753 91
8187 15
61732106 17833
Satellite: ISS
Catalog Number: 25544
Epoch time: 11276
55130336 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 335
1711 deg
Eccentricity:
0010619
Arg of perigee: 268
1753 deg
Mean anomaly: 91
8187 deg
Mean motion: 15
61732106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1783
Checksum: 290
Coasting Arc #14 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2011/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 765754
02 A = 6757768
82 meter
Y = -4786473
24 meter E =
0003116
Z = -4709904
86 I = 51
45593
XDOT = 7006
733427 Wp = 181
00488
YDOT = -1563
894908 meter/sec RA = 329
81319 deg
ZDOT = 2725
413118 TA = 115
99767
MA = 115
96557
Ha = 206
626 n
mi
Hp = 205
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2512316
33 X = 842100
27
Y = -15703652
36 feet Y = -4777483
44 meter
Z = -15452443
76 Z = -4705999
16
XDOT = 22987
970560 XDOT = 7010
460872
YDOT = -5130
888806 feet/sec YDOT = -1485
520363 meter/sec
ZDOT = 8941
644089 ZDOT = 2759
460975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 727436
38 X = 221722
61
Y = 15902443
97 feet Y = 4847064
92 meter
Z = -15436241
80 Z = -4704966
50
XDOT = -20199
479930 XDOT = -6156
801483
YDOT = 9748
025216 feet/sec YDOT = 2971
198086 meter/sec
ZDOT = 9080
389812 ZDOT = 2767
702815
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 11277
51113118
00016717 00000-0 10270-3 0 9130
2 25544 51
6395 330
3308 0010441 272
6650 87
3311 15
61755454 17980
Satellite: ISS
Catalog Number: 25544
Epoch time: 11277
51113118 = yrday
fracday
Element set: 913
Inclination: 51
6395 deg
RA of node: 330
3308 deg
Eccentricity:
0010441
Arg of perigee: 272
6650 deg
Mean anomaly: 87
3311 deg
Mean motion: 15
61755454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1798
Checksum: 294
Coasting Arc #15 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2011/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4579944
54 A = 6766113
76 meter
Y = 4732429
55 meter E =
0005624
Z = 1535299
49 I = 51
45929
XDOT = -4462
738713 Wp = 159
35168
YDOT = -2453
733967 meter/sec RA = 324
76424 deg
ZDOT = -5748
097446 TA = 3
77433
MA = 3
77008
Ha = 206
981 n
mi
Hp = 205
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15026064
76 X = -4639981
30
Y = 15526343
67 feet Y = 4680878
22 meter
Z = 5037071
82 Z = 1512904
03
XDOT = -14641
531209 XDOT = -4407
045704
YDOT = -8050
308290 feet/sec YDOT = -2503
327992 meter/sec
ZDOT = -18858
587420 ZDOT = -5769
641979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11169584
34 X = 3404489
31
Y = -18520357
33 feet Y = -5645004
91 meter
Z = 4945585
15 Z = 1507414
35
XDOT = 14617
748487 XDOT = 4455
489739
YDOT = 3755
521210 feet/sec YDOT = 1144
682865 meter/sec
ZDOT = -18946
169845 ZDOT = -5774
792569
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 11278
53492565
00016717 00000-0 10270-3 0 9140
2 25544 51
6401 325
1679 0010436 277
2815 82
7155 15
61811638 18140
Satellite: ISS
Catalog Number: 25544
Epoch time: 11278
53492565 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 325
1679 deg
Eccentricity:
0010436
Arg of perigee: 277
2815 deg
Mean anomaly: 82
7155 deg
Mean motion: 15
61811638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 314
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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