[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 6th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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 361)
---------------------------------------
Vector Time (GMT): 2011/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1781829
97 A = 6765999
01 meter
Y = 5080504
90 meter E =
0001099
Z = 4097383
52 I = 51
96708
XDOT = -4634
544315 Wp = 342
08457
YDOT = -4742
432783 meter/sec RA = 72
79298 deg
ZDOT = 3866
194327 TA = 68
16834
MA = 68
15665
Ha = 211
414 n
mi
Hp = 208
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5845898
84 X = -1858412
69
Y = 16668323
15 feet Y = 5060150
69 meter
Z = 13442859
31 Z = 4088542
16
XDOT = -15205
197885 XDOT = -4599
949975
YDOT = -15559
162673 feet/sec YDOT = -4794
066123 meter/sec
ZDOT = 12684
364591 ZDOT = 3843
763589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17509915
58 X = 5337022
27
Y = 2526294
99 feet Y = 770014
71 meter
Z = 13406665
74 Z = 4086351
72
XDOT = -12058
675929 XDOT = -3675
484423
YDOT = 16770
135296 feet/sec YDOT = 5111
537238 meter/sec
ZDOT = 12593
520112 ZDOT = 3838
504930
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 11185
55510996
00016717 00000-0 10270-3 0 9003
2 25544 51
6410 73
2004 0011198 288
1459 71
8477 15
59717909 3620
Satellite: ISS
Catalog Number: 25544
Epoch time: 11185
55510996 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 73
2004 deg
Eccentricity:
0011198
Arg of perigee: 288
1459 deg
Mean anomaly: 71
8477 deg
Mean motion: 15
59717909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 362
Checksum: 317
Coasting Arc #2 (Orbit 376)
---------------------------------------
Vector Time (GMT): 2011/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3810951
01 A = 6760995
73 meter
Y = -1695408
81 meter E =
0006189
Z = -5324843
39 I = 51
94058
XDOT = 2984
366085 Wp = 44
86316
YDOT = 7069
989801 meter/sec RA = 67
76325 deg
ZDOT = -110
969866 TA = 224
05996
MA = 224
10930
Ha = 211
637 n
mi
Hp = 208
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12503120
11 X = 3855492
85
Y = -5562364
87 feet Y = -1652542
85 meter
Z = -17469958
62 Z = -5306222
08
XDOT = 9791
227313 XDOT = 2905
625349
YDOT = 23195
504595 feet/sec YDOT = 7102
922546 meter/sec
ZDOT = -364
074362 ZDOT = -96
662595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8130773
59 X = -2478259
79
Y = -11126488
35 feet Y = -3391353
65 meter
Z = -17394227
42 Z = -5301760
52
XDOT = 19753
182192 XDOT = 6020
769932
YDOT = -13934
242159 feet/sec YDOT = -4247
157010 meter/sec
ZDOT = -306
358199 ZDOT = -93
377979
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 11186
51617048
00016717 00000-0 10270-3 0 9017
2 25544 51
6409 68
3683 0011346 291
6859 68
3088 15
59762541 3771
Satellite: ISS
Catalog Number: 25544
Epoch time: 11186
51617048 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 68
3683 deg
Eccentricity:
0011346
Arg of perigee: 291
6859 deg
Mean anomaly: 68
3088 deg
Mean motion: 15
59762541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 377
Checksum: 332
Coasting Arc #3 (Orbit 392)
---------------------------------------
Vector Time (GMT): 2011/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4831386
42 A = 6765469
08 meter
Y = -2177559
04 meter E =
0007663
Z = 4211138
98 I = 51
94348
XDOT = -203
622052 Wp = 356
61303
YDOT = -6717
536871 meter/sec RA = 62
73149 deg
ZDOT = -3700
103714 TA = 131
19151
MA = 131
12541
Ha = 211
879 n
mi
Hp = 208
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15851005
31 X = -4827134
14
Y = -7144222
57 feet Y = -2231563
15 meter
Z = 13816072
77 Z = 4187678
54
XDOT = -668
051353 XDOT = -110
515924
YDOT = -22039
162964 feet/sec YDOT = -6719
292978 meter/sec
ZDOT = -12139
447882 ZDOT = -3700
867352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3276227
90 X = -998594
26
Y = 17151712
12 feet Y = 5227841
85 meter
Z = 13720905
74 Z = 4182132
07
XDOT = -20057
651357 XDOT = -6113
572133
YDOT = 5900
901236 feet/sec YDOT = 1798
594697 meter/sec
ZDOT = -12142
166386 ZDOT = -3700
932315
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 11187
54129565
00016717 00000-0 10270-3 0 9024
2 25544 51
6410 63
2142 0011472 295
8898 64
1074 15
59787708 3935
Satellite: ISS
Catalog Number: 25544
Epoch time: 11187
54129565 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 63
2142 deg
Eccentricity:
0011472
Arg of perigee: 295
8898 deg
Mean anomaly: 64
1074 deg
Mean motion: 15
59787708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 393
Checksum: 323
Coasting Arc #4 (Orbit 407)
---------------------------------------
Vector Time (GMT): 2011/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4329029
67 A = 6772376
18 meter
Y = 5047380
65 meter E =
0013611
Z = -1234661
68 I = 51
95144
XDOT = -2943
352520 Wp = 340
83456
YDOT = 3965
328607 meter/sec RA = 57
73680 deg
ZDOT = 5884
667393 TA = 5
76118
MA = 5
74554
Ha = 212
193 n
mi
Hp = 207
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14202853
25 X = 4278264
85
Y = 16559647
81 feet Y = 5095506
77 meter
Z = -4050727
29 Z = -1213754
28
XDOT = -9656
668372 XDOT = -3016
061236
YDOT = 13009
608291 feet/sec YDOT = 3932
007177 meter/sec
ZDOT = 19306
651552 ZDOT = 5870
192461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12526218
86 X = 3817991
51
Y = -17880583
08 feet Y = -5450001
72 meter
Z = -3966101
00 Z = -1208867
59
XDOT = 13719
498343 XDOT = 4181
703095
YDOT = 5337
583112 feet/sec YDOT = 1626
895332 meter/sec
ZDOT = 19247
627118 ZDOT = 5866
676746
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 11188
50234552
00016717 00000-0 10270-3 0 9035
2 25544 51
6409 58
3813 0011507 299
2798 60
7207 15
59763723 4087
Satellite: ISS
Catalog Number: 25544
Epoch time: 11188
50234552 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 58
3813 deg
Eccentricity:
0011507
Arg of perigee: 299
2798 deg
Mean anomaly: 60
7207 deg
Mean motion: 15
59763723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 408
Checksum: 316
Coasting Arc #5 (Orbit 423)
---------------------------------------
Vector Time (GMT): 2011/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2275092
90 A = 6770788
30 meter
Y = -5952593
65 meter E =
0006022
Z = -2286493
45 I = 51
92879
XDOT = 5396
221812 Wp = 289
09172
YDOT = 38
163817 meter/sec RA = 52
76035 deg
ZDOT = -5455
072101 TA = 276
31192
MA = 276
38051
Ha = 212
362 n
mi
Hp = 207
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7464215
55 X = -2197253
44
Y = -19529506
73 feet Y = -5977599
66 meter
Z = -7501618
93 Z = -2297357
35
XDOT = 17704
139803 XDOT = 5421
893617
YDOT = 125
209373 feet/sec YDOT = 98
651762 meter/sec
ZDOT = -17897
218180 ZDOT = -5428
795021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16878898
52 X = -5144688
27
Y = 12310983
90 feet Y = 3752387
89 meter
Z = -7545388
90 Z = -2299834
54
XDOT = -3683
846540 XDOT = -1122
836425
YDOT = -15981
673668 feet/sec YDOT = -4871
214134 meter/sec
ZDOT = -17790
490998 ZDOT = -5422
541656
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 11189
52745872
00016717 00000-0 10270-3 0 9041
2 25544 51
6406 53
2276 0011560 302
3626 57
6410 15
59746931 4247
Satellite: ISS
Catalog Number: 25544
Epoch time: 11189
52745872 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 53
2276 deg
Eccentricity:
0011560
Arg of perigee: 302
3626 deg
Mean anomaly: 57
6410 deg
Mean motion: 15
59746931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 424
Checksum: 302
Coasting Arc #6 (Orbit 439)
---------------------------------------
Vector Time (GMT): 2011/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -824223
21 A = 6763213
35 meter
Y = 4693598
31 meter E =
0004373
Z = 4800167
11 I = 51
88429
XDOT = -6170
021687 Wp = 320
27974
YDOT = -3747
646499 meter/sec RA = 47
74975 deg
ZDOT = 2609
594367 TA = 104
14384
MA = 104
09525
Ha = 212
697 n
mi
Hp = 207
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2704144
39 X = -899964
95
Y = 15398944
59 feet Y = 4683957
24 meter
Z = 15748579
77 Z = 4795979
67
XDOT = -20242
853304 XDOT = -6140
333104
YDOT = -12295
428147 feet/sec YDOT = -3816
477771 meter/sec
ZDOT = 8561
661308 ZDOT = 2579
692126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15566511
81 X = 4744672
80
Y = -1633431
43 feet Y = -497869
90 meter
Z = 15731283
10 Z = 4794895
09
XDOT = -6227
771202 XDOT = -1898
224662
YDOT = 21792
933200 feet/sec YDOT = 6642
486040 meter/sec
ZDOT = 8440
438248 ZDOT = 2572
645578
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 11190
55256599
00016717 00000-0 10270-3 0 9050
2 25544 51
6406 48
0724 0011531 307
3806 52
6299 15
59750484 4406
Satellite: ISS
Catalog Number: 25544
Epoch time: 11190
55256599 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 48
0724 deg
Eccentricity:
0011531
Arg of perigee: 307
3806 deg
Mean anomaly: 52
6299 deg
Mean motion: 15
59750484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 440
Checksum: 310
Coasting Arc #7 (Orbit 454)
---------------------------------------
Vector Time (GMT): 2011/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3895012
20 A = 6761529
11 meter
Y = -1939327
85 meter E =
0006881
Z = -5178637
92 I = 51
85692
XDOT = 4752
688701 Wp = 43
95514
YDOT = 5865
704340 meter/sec RA = 42
70670 deg
ZDOT = 1383
949061 TA = 239
26494
MA = 239
33273
Ha = 212
839 n
mi
Hp = 207
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12778911
41 X = 3941565
43
Y = -6362624
17 feet Y = -1895510
37 meter
Z = -16990281
89 Z = -5159603
24
XDOT = 15592
810698 XDOT = 4680
021080
YDOT = 19244
436810 feet/sec YDOT = 5918
445278 meter/sec
ZDOT = 4540
515293 ZDOT = 1406
861922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9901729
32 X = -3018047
10
Y = -10409834
51 feet Y = -3172917
56 meter
Z = -16912845
53 Z = -5155035
32
XDOT = 12994
714658 XDOT = 3960
789028
YDOT = -19856
253613 feet/sec YDOT = -6052
186101 meter/sec
ZDOT = 4633
210529 ZDOT = 1412
202569
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 11191
51359589
00016717 00000-0 10270-3 0 9061
2 25544 51
6396 43
2396 0011611 310
3768 49
6373 15
59803730 4554
Satellite: ISS
Catalog Number: 25544
Epoch time: 11191
51359589 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 43
2396 deg
Eccentricity:
0011611
Arg of perigee: 310
3768 deg
Mean anomaly: 49
6373 deg
Mean motion: 15
59803730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 455
Checksum: 319
Coasting Arc #8 (Orbit 470)
---------------------------------------
Vector Time (GMT): 2011/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5803848
11 A = 6768349
08 meter
Y = -1254927
20 meter E =
0008666
Z = 3252990
35 I = 51
85778
XDOT = -1421
255510 Wp = 29
40856
YDOT = -5834
601170 meter/sec RA = 37
68142 deg
ZDOT = -4773
848002 TA = 112
93726
MA = 112
84578
Ha = 212
986 n
mi
Hp = 207
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19041496
42 X = -5805186
24
Y = -4117215
22 feet Y = -1319837
40 meter
Z = 10672540
51 Z = 3224791
98
XDOT = -4662
911779 XDOT = -1332
715915
YDOT = -19142
392291 feet/sec YDOT = -5849
998647 meter/sec
ZDOT = -15662
230977 ZDOT = -4780
538349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2077555
79 X = 633239
01
Y = 19433059
01 feet Y = 5923196
39 meter
Z = 10558084
46 Z = 3218104
14
XDOT = -15330
257492 XDOT = -4672
662484
YDOT = 10185
834693 feet/sec YDOT = 3104
642414 meter/sec
ZDOT = -15689
028584 ZDOT = -4782
015912
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 11192
53868842
00016717 00000-0 10270-3 0 9072
2 25544 51
6402 38
0857 0011846 314
2723 45
7460 15
59844126 4716
Satellite: ISS
Catalog Number: 25544
Epoch time: 11192
53868842 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 38
0857 deg
Eccentricity:
0011846
Arg of perigee: 314
2723 deg
Mean anomaly: 45
7460 deg
Mean motion: 15
59844126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 471
Checksum: 312
Coasting Arc #9 (Orbit 486)
---------------------------------------
Vector Time (GMT): 2011/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5638134
43 A = 6772893
72 meter
Y = 3729846
53 meter E =
0017202
Z = 119268
49 I = 51
84656
XDOT = -2709
069645 Wp = 3
68168
YDOT = 3900
915674 meter/sec RA = 32
69203 deg
ZDOT = 6041
422892 TA = 357
60372
MA = 357
61195
Ha = 213
205 n
mi
Hp = 206
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18497816
38 X = 5595428
15
Y = 12237029
31 feet Y = 3792656
78 meter
Z = 391300
81 Z = 146555
16
XDOT = -8888
023771 XDOT = -2781
836886
YDOT = 12798
279769 feet/sec YDOT = 3870
213265 meter/sec
ZDOT = 19820
941248 ZDOT = 6028
086332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5456079
98 X = 1663013
18
Y = -21495267
10 feet Y = -6551757
41 meter
Z = 501893
30 Z = 152977
08
XDOT = 13485
540723 XDOT = 4110
392812
YDOT = 3886
391589 feet/sec YDOT = 1184
572156 meter/sec
ZDOT = 19766
511609 ZDOT = 6024
832738
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 11193
56377729
00016717 00000-0 10270-3 0 9086
2 25544 51
6386 32
9302 0011699 317
9813 42
0444 15
59799469 4879
Satellite: ISS
Catalog Number: 25544
Epoch time: 11193
56377729 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 32
9302 deg
Eccentricity:
0011699
Arg of perigee: 317
9813 deg
Mean anomaly: 42
0444 deg
Mean motion: 15
59799469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 487
Checksum: 349
Coasting Arc #10 (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 = -3315585
79 A = 6767715
67 meter
Y = -4798280
66 meter E =
0009643
Z = -3440510
23 I = 51
80280
XDOT = 6075
443918 Wp = 346
16833
YDOT = -894
429963 meter/sec RA = 27
70001 deg
ZDOT = -4595
635458 TA = 234
11067
MA = 234
20023
Ha = 213
344 n
mi
Hp = 206
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10877906
12 X = -3244970
97
Y = -15742390
62 feet Y = -4834962
12 meter
Z = -11287763
21 Z = -3456446
40
XDOT = 19932
558787 XDOT = 6107
318454
YDOT = -2934
481507 feet/sec YDOT = -826
311626 meter/sec
ZDOT = -15077
544154 ZDOT = -4566
044177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11032988
58 X = -3362854
92
Y = 15587382
56 feet Y = 4751034
21 meter
Z = -11352179
09 Z = -3460144
19
XDOT = -8542
212193 XDOT = -2603
666276
YDOT = -16967
625129 feet/sec YDOT = -5171
732139 meter/sec
ZDOT = -14957
281090 ZDOT = -4558
979276
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
52479021
00016717 00000-0 10270-3 0 9092
2 25544 51
6378 28
0981 0011677 321
8432 38
1896 15
59825206 5020
Satellite: ISS
Catalog Number: 25544
Epoch time: 11194
52479021 = yrday
fracday
Element set: 909
Inclination: 51
6378 deg
RA of node: 28
0981 deg
Eccentricity:
0011677
Arg of perigee: 321
8432 deg
Mean anomaly: 38
1896 deg
Mean motion: 15
59825206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 502
Checksum: 316
Coasting Arc #11 (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 = -453521
05 A = 6761299
69 meter
Y = 4271996
69 meter E =
0008319
Z = 5222859
95 I = 51
75343
XDOT = -7298
864919 Wp = 335
24150
YDOT = -2108
902902 meter/sec RA = 22
66424 deg
ZDOT = 1099
186403 TA = 104
29962
MA = 104
20722
Ha = 213
629 n
mi
Hp = 206
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1487929
95 X = -526628
80
Y = 14015737
19 feet Y = 4266515
52 meter
Z = 17135367
30 Z = 5220479
92
XDOT = -23946
407216 XDOT = -7280
079826
YDOT = -6918
972776 feet/sec YDOT = -2190
418397 meter/sec
ZDOT = 3606
254603 ZDOT = 1063
774544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13642139
13 X = 4158124
01
Y = -3589966
90 feet Y = -1094221
91 meter
Z = 17125414
29 Z = 5219826
27
XDOT = 1963
131308 XDOT = 598
362423
YDOT = 23852
095038 feet/sec YDOT = 7270
118568 meter/sec
ZDOT = 3462
543436 ZDOT = 1055
383239
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
54986612
00016717 00000-0 10270-3 0 9106
2 25544 51
6377 22
9421 0011619 325
8895 34
1513 15
59782611 5185
Satellite: ISS
Catalog Number: 25544
Epoch time: 11195
54986612 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 22
9421 deg
Eccentricity:
0011619
Arg of perigee: 325
8895 deg
Mean anomaly: 34
1513 deg
Mean motion: 15
59782611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 518
Checksum: 315
Coasting Arc #12 (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 = 4187256
35 A = 6763561
50 meter
Y = -2534368
89 meter E =
0007492
Z = -4668370
20 I = 51
73264
XDOT = 5742
661073 Wp = 31
90453
YDOT = 4204
020092 meter/sec RA = 17
61249 deg
ZDOT = 2876
868879 TA = 266
56365
MA = 266
64935
Ha = 213
708 n
mi
Hp = 206
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13737717
70 X = 4237962
50
Y = -8314858
56 feet Y = -2487260
25 meter
Z = -15316175
19 Z = -4647906
20
XDOT = 18840
751553 XDOT = 5681
249129
YDOT = 13792
716836 feet/sec YDOT = 4267
894230 meter/sec
ZDOT = 9438
546190 ZDOT = 2904
617506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12925313
97 X = -3939635
70
Y = -9661404
81 feet Y = -2944796
19 meter
Z = -15232875
59 Z = -4642980
48
XDOT = 4967
188707 XDOT = 1513
999118
YDOT = -21660
776447 feet/sec YDOT = -6602
204661 meter/sec
ZDOT = 9550
990293 ZDOT = 2911
141841
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
51086592
00016717 00000-0 10270-3 0 9113
2 25544 51
6372 18
1086 0011521 329
1198 30
9279 15
59840444 5338
Satellite: ISS
Catalog Number: 25544
Epoch time: 11196
51086592 = yrday
fracday
Element set: 911
Inclination: 51
6372 deg
RA of node: 18
1086 deg
Eccentricity:
0011521
Arg of perigee: 329
1198 deg
Mean anomaly: 30
9279 deg
Mean motion: 15
59840444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 533
Checksum: 305
Coasting Arc #13 (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 = -6466050
77 A = 6770992
77 meter
Y = 176976
15 meter E =
0009124
Z = 2006001
54 I = 51
72921
XDOT = -1871
623782 Wp = 54
77669
YDOT = -4925
138627 meter/sec RA = 12
59402 deg
ZDOT = -5575
367447 TA = 103
05772
MA = 102
95585
Ha = 213
812 n
mi
Hp = 205
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21214077
32 X = -6477293
72
Y = 580630
42 feet Y = 104605
72 meter
Z = 6581369
89 Z = 1974562
97
XDOT = -6140
497974 XDOT = -1789
327385
YDOT = -16158
591296 feet/sec YDOT = -4945
607427 meter/sec
ZDOT = -18291
887948 ZDOT = -5584
260285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8903188
23 X = 2713691
77
Y = 19307313
20 feet Y = 5884869
06 meter
Z = 6453645
01 Z = 1967071
00
XDOT = -11071
288999 XDOT = -3374
528887
YDOT = 11257
253093 feet/sec YDOT = 3431
210743 meter/sec
ZDOT = -18327
688076 ZDOT = -5586
279325
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
53592553
00016717 00000-0 10270-3 0 9126
2 25544 51
6375 12
9537 0011822 332
5754 27
4776 15
59885697 5493
Satellite: ISS
Catalog Number: 25544
Epoch time: 11197
53592553 = yrday
fracday
Element set: 912
Inclination: 51
6375 deg
RA of node: 12
9537 deg
Eccentricity:
0011822
Arg of perigee: 332
5754 deg
Mean anomaly: 27
4776 deg
Mean motion: 15
59885697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 549
Checksum: 343
Coasting Arc #14 (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 = 6247495
19 A = 6771673
87 meter
Y = 2065236
47 meter E =
0018693
Z = 1545754
80 I = 51
70150
XDOT = -2824
693680 Wp = 24
45978
YDOT = 4220
102359 meter/sec RA = 7
60111 deg
ZDOT = 5770
040715 TA = 352
48224
MA = 352
51023
Ha = 213
899 n
mi
Hp = 205
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20497031
48 X = 6216428
18
Y = 6775710
21 feet Y = 2134925
90 meter
Z = 5071374
03 Z = 1576029
14
XDOT = -9267
367718 XDOT = -2899
702866
YDOT = 13845
480181 feet/sec YDOT = 4188
094929 meter/sec
ZDOT = 18930
579774 ZDOT = 5756
136927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2199964
53 X = -670549
19
Y = -21446156
17 feet Y = -6536788
40 meter
Z = 5194220
27 Z = 1583198
34
XDOT = 14909
993740 XDOT = 4544
566092
YDOT = 3048
091743 feet/sec YDOT = 929
058363 meter/sec
ZDOT = 18873
822818 ZDOT = 5752
741195
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
56098210
00016717 00000-0 10270-3 0 9132
2 25544 51
6374 7
7981 0011526 336
9416 23
1221 15
59853832 5653
Satellite: ISS
Catalog Number: 25544
Epoch time: 11198
56098210 = yrday
fracday
Element set: 913
Inclination: 51
6374 deg
RA of node: 7
7981 deg
Eccentricity:
0011526
Arg of perigee: 336
9416 deg
Mean anomaly: 23
1221 deg
Mean motion: 15
59853832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 565
Checksum: 309
Coasting Arc #15 (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 = -3613689
57 A = 6764286
87 meter
Y = -3655545
80 meter E =
0015013
Z = -4409428
16 I = 51
64790
XDOT = 6482
563164 Wp = 18
80451
YDOT = -2358
250591 meter/sec RA = 2
58457 deg
ZDOT = -3346
910089 TA = 217
31988
MA = 217
42427
Ha = 214
078 n
mi
Hp = 205
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11855936
90 X = -3551124
25
Y = -11993260
49 feet Y = -3695606
09 meter
Z = -14466627
83 Z = -4426831
40
XDOT = 21268
251852 XDOT = 6524
710097
YDOT = -7737
042621 feet/sec YDOT = -2285
522691 meter/sec
ZDOT = -10980
676146 ZDOT = -3315
316329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5852229
36 X = -1783759
51
Y = 15751490
52 feet Y = 4801054
31 meter
Z = -14537084
15 Z = -4430903
25
XDOT = -14925
274548 XDOT = -4549
223682
YDOT = -15593
101853 feet/sec YDOT = -4752
777445 meter/sec
ZDOT = -10852
185719 ZDOT = -3307
746207
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
52196459
00016717 00000-0 10270-3 0 9144
2 25544 51
6382 2
9662 0011535 341
3681 18
7051 15
59884532 5808
Satellite: ISS
Catalog Number: 25544
Epoch time: 11199
52196459 = yrday
fracday
Element set: 914
Inclination: 51
6382 deg
RA of node: 2
9662 deg
Eccentricity:
0011535
Arg of perigee: 341
3681 deg
Mean anomaly: 18
7051 deg
Mean motion: 15
59884532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 580
Checksum: 316
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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