[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 20th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
060/10:21:47
800 3
0 4
9 4
9
N/A -3
8 -0
0 220
2
000/00:01:35
600 0
2 0
0 201
8
Coasting Arc #1 (Orbit 3919)
---------------------------------------
Vector Time (GMT): 2012/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5289502
04 A = 6771312
05 meter
Y = -3019047
65 meter E =
0023437
Z = -2991361
26 I = 51
69185
XDOT = 4734
806063 Wp = 61
49116
YDOT = -3385
970657 meter/sec RA = 6
88563 deg
ZDOT = -4973
768654 TA = 152
69048
MA = 152
56707
Ha = 220
652 n
mi
Hp = 200
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17354009
30 X = -5240818
30
Y = -9905011
98 feet Y = -3077925
92 meter
Z = -9814177
35 Z = -3016938
54
XDOT = 15534
140628 XDOT = 4796
477631
YDOT = -11108
827614 feet/sec YDOT = -3332
678323 meter/sec
ZDOT = -16318
138627 ZDOT = -4950
617931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8824041
49 X = -2689567
85
Y = -17870172
13 feet Y = -5446828
47 meter
Z = -9918781
07 Z = -3023244
47
XDOT = 17868
948815 XDOT = 5446
455599
YDOT = 147
322540 feet/sec YDOT = 44
903910 meter/sec
ZDOT = -16222
918914 ZDOT = -4944
745685
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 12048
52596559
00016717 00000-0 10270-3 0 9008
2 25544 51
6407 7
2544 0020654 52
7442 307
5593 15
59000183 39206
Satellite: ISS
Catalog Number: 25544
Epoch time: 12048
52596559 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 7
2544 deg
Eccentricity:
0020654
Arg of perigee: 52
7442 deg
Mean anomaly: 307
5593 deg
Mean motion: 15
59000183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3920
Checksum: 298
Coasting Arc #2 (Orbit 3935)
---------------------------------------
Vector Time (GMT): 2012/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2155300
65 A = 6764334
46 meter
Y = 4013041
60 meter E =
0023301
Z = 4979300
33 I = 51
63907
XDOT = -7288
621101 Wp = 69
35436
YDOT = 1380
822153 meter/sec RA = 1
85881 deg
ZDOT = 2042
392616 TA =
86063
MA =
85663
Ha = 220
499 n
mi
Hp = 200
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7071196
37 X = 2086078
18
Y = 13166146
99 feet Y = 4036756
55 meter
Z = 16336287
17 Z = 4989602
18
XDOT = -23912
798887 XDOT = -7313
441235
YDOT = 4530
256408 feet/sec YDOT = 1299
177560 meter/sec
ZDOT = 6700
763176 ZDOT = 2006
925492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1306569
93 X = -398242
52
Y = 14841557
25 feet Y = 4523706
65 meter
Z = 16378173
79 Z = 4992067
37
XDOT = -21484
948682 XDOT = -6548
612358
YDOT = -9124
018347 feet/sec YDOT = -2781
000792 meter/sec
ZDOT = 6555
222246 ZDOT = 1998
031741
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 12049
55157624
00016717 00000-0 10270-3 0 9019
2 25544 51
6412 2
1045 0020416 56
4929 303
8173 15
59056944 39365
Satellite: ISS
Catalog Number: 25544
Epoch time: 12049
55157624 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 2
1045 deg
Eccentricity:
0020416
Arg of perigee: 56
4929 deg
Mean anomaly: 303
8173 deg
Mean motion: 15
59056944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 298
Coasting Arc #3 (Orbit 3950)
---------------------------------------
Vector Time (GMT): 2012/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1672559
21 A = 6764089
51 meter
Y = -4143122
20 meter E =
0031620
Z = -5103000
29 I = 51
60755
XDOT = 7408
594291 Wp = 76
24641
YDOT = 928
311024 meter/sec RA = 356
80593 deg
ZDOT = 1690
691037 TA = 210
02861
MA = 210
21031
Ha = 220
641 n
mi
Hp = 199
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5487398
98 X = 1743552
62
Y = -13592920
61 feet Y = -4124021
87 meter
Z = -16742126
93 Z = -5094702
71
XDOT = 24306
411717 XDOT = 7389
450356
YDOT = 3045
639841 feet/sec YDOT = 1011
051520 meter/sec
ZDOT = 5546
886605 ZDOT = 1726
634058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11935316
87 X = 3637884
58
Y = -8577720
80 feet Y = -2614489
30 meter
Z = -16707745
80 Z = -5092520
92
XDOT = 18358
894005 XDOT = 5595
790893
YDOT = 14557
390731 feet/sec YDOT = 4437
092695 meter/sec
ZDOT = 5694
174809 ZDOT = 1735
584482
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 12050
51307033
00016717 00000-0 10270-3 0 9029
2 25544 51
6414 357
2752 0020525 59
9457 300
3731 15
59039443 39515
Satellite: ISS
Catalog Number: 25544
Epoch time: 12050
51307033 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 357
2752 deg
Eccentricity:
0020525
Arg of perigee: 59
9457 deg
Mean anomaly: 300
3731 deg
Mean motion: 15
59039443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 288
Coasting Arc #4 (Orbit 3966)
---------------------------------------
Vector Time (GMT): 2012/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4996990
89 A = 6770728
24 meter
Y = 3266625
61 meter E =
0032341
Z = 3176646
45 I = 51
60051
XDOT = -5120
848224 Wp = 74
98229
YDOT = -3109
928258 meter/sec RA = 351
77057 deg
ZDOT = -4808
234683 TA = 68
19142
MA = 67
84765
Ha = 220
662 n
mi
Hp = 199
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16394327
06 X = -5048578
55
Y = 10717275
62 feet Y = 3210457
93 meter
Z = 10422068
39 Z = 3152246
50
XDOT = -16800
683151 XDOT = -5062
335152
YDOT = -10203
176701 feet/sec YDOT = -3166
865873 meter/sec
ZDOT = -15775
048173 ZDOT = -4832
968490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19626267
87 X = -5982086
45
Y = 724278
91 feet Y = 220760
21 meter
Z = 10321748
67 Z = 3146068
99
XDOT = -9022
208290 XDOT = -2749
969087
YDOT = -15912
719785 feet/sec YDOT = -4850
196991 meter/sec
ZDOT = -15876
188050 ZDOT = -4839
062118
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 12051
53864280
00016717 00000-0 10270-3 0 9035
2 25544 51
6421 352
1240 0020539 63
7431 296
5832 15
59089651 39670
Satellite: ISS
Catalog Number: 25544
Epoch time: 12051
53864280 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 352
1240 deg
Eccentricity:
0020539
Arg of perigee: 63
7431 deg
Mean anomaly: 296
5832 deg
Mean motion: 15
59089651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 309
Coasting Arc #5 (Orbit 3981)
---------------------------------------
Vector Time (GMT): 2012/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6567100
62 A = 6774913
20 meter
Y = -1617286
91 meter E =
0031979
Z = -89806
56 I = 51
58473
XDOT = 1198
688545 Wp = 58
66830
YDOT = 4621
636191 meter/sec RA = 346
76836 deg
ZDOT = 6019
121372 TA = 300
36074
MA = 300
67656
Ha = 220
607 n
mi
Hp = 199
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21545605
72 X = 6585133
62
Y = -5306059
42 feet Y = -1543748
72 meter
Z = -294640
96 Z = -57860
82
XDOT = 3932
705199 XDOT = 1117
680652
YDOT = 15162
848396 feet/sec YDOT = 4634
588219 meter/sec
ZDOT = 19747
773531 ZDOT = 6024
747248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21315953
63 X = 6497102
67
Y = 6169082
86 feet Y = 1880336
46 meter
Z = -163533
04 Z = -49844
87
XDOT = -3823
676630 XDOT = -1165
456637
YDOT = 13486
198016 feet/sec YDOT = 4110
593155 meter/sec
ZDOT = 19770
445385 ZDOT = 6026
031753
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 12052
50009863
00016717 00000-0 10270-3 0 9042
2 25544 51
6420 347
2958 0020488 67
2930 293
0388 15
59102441 39824
Satellite: ISS
Catalog Number: 25544
Epoch time: 12052
50009863 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 347
2958 deg
Eccentricity:
0020488
Arg of perigee: 67
2930 deg
Mean anomaly: 293
0388 deg
Mean motion: 15
59102441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3982
Checksum: 310
Coasting Arc #6 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2012/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5980819
03 A = 6770484
91 meter
Y = -649852
58 meter E =
0024527
Z = -3133592
22 I = 51
54214
XDOT = 3076
967946 Wp = 76
05301
YDOT = -5067
792894 meter/sec RA = 341
76391 deg
ZDOT = -4847
904157 TA = 140
09986
MA = 139
91932
Ha = 220
540 n
mi
Hp = 199
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19622109
68 X = -5957885
82
Y = -2132062
27 feet Y = -716605
87 meter
Z = -10280814
37 Z = -3162590
30
XDOT = 10095
039193 XDOT = 3156
957798
YDOT = -16626
617106 feet/sec YDOT = -5032
937568 meter/sec
ZDOT = -15905
197366 ZDOT = -4832
761961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16075114
40 X = -4899694
87
Y = -11344876
76 feet Y = -3457918
44 meter
Z = -10399638
96 Z = -3169809
96
XDOT = 16145
757356 XDOT = 4921
226842
YDOT = -8432
703902 feet/sec YDOT = -2570
288149 meter/sec
ZDOT = -15842
695013 ZDOT = -4828
853440
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 12053
52563153
00016717 00000-0 10270-3 0 9053
2 25544 51
6429 342
1441 0020513 71
1324 289
2053 15
59151894 39983
Satellite: ISS
Catalog Number: 25544
Epoch time: 12053
52563153 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 342
1441 deg
Eccentricity:
0020513
Arg of perigee: 71
1324 deg
Mean anomaly: 289
2053 deg
Mean motion: 15
59151894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 300
Coasting Arc #7 (Orbit 4013)
---------------------------------------
Vector Time (GMT): 2012/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3435423
60 A = 6763611
85 meter
Y = 2887108
67 meter E =
0024058
Z = 5039201
23 I = 51
49068
XDOT = -6182
631142 Wp = 84
25819
YDOT = 4214
708152 meter/sec RA = 336
72335 deg
ZDOT = 1795
226745 TA = 348
36784
MA = 348
42333
Ha = 220
340 n
mi
Hp = 199
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11271074
81 X = 3378405
24
Y = 9472141
29 feet Y = 2925207
43 meter
Z = 16532812
45 Z = 5055751
22
XDOT = -20284
222906 XDOT = -6238
021981
YDOT = 13827
782651 feet/sec YDOT = 4145
260642 meter/sec
ZDOT = 5889
851524 ZDOT = 1765
057416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5414682
38 X = 1650395
19
Y = 13608816
70 feet Y = 4147967
33 meter
Z = 16600415
60 Z = 5059806
68
XDOT = -23440
864090 XDOT = -7144
775375
YDOT = 2273
469820 feet/sec YDOT = 692
953601 meter/sec
ZDOT = 5765
827173 ZDOT = 1757
424122
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 12054
55114267
00016717 00000-0 10270-3 0 9066
2 25544 51
6426 336
9937 0020306 75
1401 285
2001 15
59204643 40141
Satellite: ISS
Catalog Number: 25544
Epoch time: 12054
55114267 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 336
9937 deg
Eccentricity:
0020306
Arg of perigee: 75
1401 deg
Mean anomaly: 285
2001 deg
Mean motion: 15
59204643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4014
Checksum: 281
Coasting Arc #8 (Orbit 4028)
---------------------------------------
Vector Time (GMT): 2012/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 85388
11 A = 6764012
43 meter
Y = -4577050
71 meter E =
0032312
Z = -5007116
05 I = 51
46456
XDOT = 7105
470815 Wp = 88
19335
YDOT = -2031
450129 meter/sec RA = 331
65897 deg
ZDOT = 1990
269780 TA = 201
15701
MA = 201
29095
Ha = 220
480 n
mi
Hp = 199
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 280144
72 X = 160886
32
Y = -15016570
57 feet Y = -4575674
26 meter
Z = -16427546
08 Z = -5006517
36
XDOT = 23311
912123 XDOT = 7117
990679
YDOT = -6664
862628 feet/sec YDOT = -1951
922148 meter/sec
ZDOT = 6529
756495 ZDOT = 2024
817906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7160497
98 X = 2182519
78
Y = -13205914
81 feet Y = -4025162
83 meter
Z = -16424713
86 Z = -5006252
79
XDOT = 22796
501811 XDOT = 6948
373752
YDOT = 4112
548609 feet/sec YDOT = 1253
504816 meter/sec
ZDOT = 6671
539367 ZDOT = 2033
485199
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 12055
51254325
00016717 00000-0 10270-3 0 9074
2 25544 51
6431 332
1642 0020392 78
3999 281
9444 15
59196031 40291
Satellite: ISS
Catalog Number: 25544
Epoch time: 12055
51254325 = yrday
fracday
Element set: 907
Inclination: 51
6431 deg
RA of node: 332
1642 deg
Eccentricity:
0020392
Arg of perigee: 78
3999 deg
Mean anomaly: 281
9444 deg
Mean motion: 15
59196031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 309
Coasting Arc #9 (Orbit 4044)
---------------------------------------
Vector Time (GMT): 2012/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3448914
59 A = 6771039
08 meter
Y = 5038387
24 meter E =
0033414
Z = 2899164
84 I = 51
46153
XDOT = -5733
976144 Wp = 88
41421
YDOT = -1008
311818 meter/sec RA = 326
61575 deg
ZDOT = -5018
081885 TA = 58
33073
MA = 58
00528
Ha = 220
495 n
mi
Hp = 199
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11315336
60 X = -3519081
83
Y = 16530141
88 feet Y = 4999427
33 meter
Z = 9511695
66 Z = 2882239
42
XDOT = -18812
257691 XDOT = -5697
898435
YDOT = -3308
109639 feet/sec YDOT = -1072
231480 meter/sec
ZDOT = -16463
523246 ZDOT = -5045
849189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17474080
74 X = -5326099
81
Y = 9862133
58 feet Y = 3005978
31 meter
Z = 9441907
16 Z = 2877893
30
XDOT = -14642
062034 XDOT = -4462
900508
YDOT = -9911
465222 feet/sec YDOT = -3021
014600 meter/sec
ZDOT = -16577
254350 ZDOT = -5052
747126
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 12056
53801632
00016717 00000-0 10270-3 0 9087
2 25544 51
6426 327
0124 0020403 82
4358 277
9114 15
59220065 40453
Satellite: ISS
Catalog Number: 25544
Epoch time: 12056
53801632 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 327
0124 deg
Eccentricity:
0020403
Arg of perigee: 82
4358 deg
Mean anomaly: 277
9114 deg
Mean motion: 15
59220065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4045
Checksum: 284
Coasting Arc #10 (Orbit 4060)
---------------------------------------
Vector Time (GMT): 2012/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5439513
92 A = 6774439
75 meter
Y = -4013831
48 meter E =
0031434
Z = 291826
43 I = 51
44873
XDOT = 2618
132938 Wp = 71
17830
YDOT = 4021
693411 meter/sec RA = 321
60486 deg
ZDOT = 5995
823764 TA = 291
98306
MA = 292
31678
Ha = 220
390 n
mi
Hp = 199
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17846174
28 X = 5482575
50
Y = -13168738
46 feet Y = -3952762
68 meter
Z = 957435
78 Z = 318356
04
XDOT = 8589
674992 XDOT = 2543
840902
YDOT = 13194
532188 feet/sec YDOT = 4050
556158 meter/sec
ZDOT = 19671
337809 ZDOT = 6008
361579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21737493
40 X = 6625587
99
Y = -4377470
78 feet Y = -1334253
09 meter
Z = 1066500
05 Z = 325069
22
XDOT = 1767
794495 XDOT = 538
823762
YDOT = 13955
506755 feet/sec YDOT = 4253
638459 meter/sec
ZDOT = 19722
397521 ZDOT = 6011
386764
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 12057
56346850
00016717 00000-0 10270-3 0 9098
2 25544 51
6429 321
8611 0020316 85
8972 274
4505 15
59251358 40614
Satellite: ISS
Catalog Number: 25544
Epoch time: 12057
56346850 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 321
8611 deg
Eccentricity:
0020316
Arg of perigee: 85
8972 deg
Mean anomaly: 274
4505 deg
Mean motion: 15
59251358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4061
Checksum: 316
Coasting Arc #11 (Orbit 4075)
---------------------------------------
Vector Time (GMT): 2012/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5626301
11 A = 6769137
98 meter
Y = 1511285
78 meter E =
0025268
Z = -3469586
73 I = 51
40878
XDOT = 1148
722248 Wp = 88
46203
YDOT = -6067
315573 meter/sec RA = 316
58698 deg
ZDOT = -4533
550437 TA = 132
43148
MA = 132
21749
Ha = 220
255 n
mi
Hp = 199
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18458993
13 X = -5625928
12
Y = 4958286
67 feet Y = 1448370
82 meter
Z = -11383158
57 Z = -3496918
02
XDOT = 3768
773779 XDOT = 1238
505588
YDOT = -19905
890986 feet/sec YDOT = -6053
968207 meter/sec
ZDOT = -14873
853141 ZDOT = -4527
751482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18812957
35 X = -5734189
40
Y = -2970864
96 feet Y = -905519
64 meter
Z = -11495300
36 Z = -3503767
55
XDOT = 11423
371670 XDOT = 3481
843685
YDOT = -15231
734057 feet/sec YDOT = -4642
632541 meter/sec
ZDOT = -14849
592386 ZDOT = -4526
155759
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 12058
52481038
00016717 00000-0 10270-3 0 9105
2 25544 51
6434 317
0307 0020183 89
5988 270
7481 15
59289524 40763
Satellite: ISS
Catalog Number: 25544
Epoch time: 12058
52481038 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 317
0307 deg
Eccentricity:
0020183
Arg of perigee: 89
5988 deg
Mean anomaly: 270
7481 deg
Mean motion: 15
59289524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4076
Checksum: 322
Coasting Arc #12 (Orbit 4091)
---------------------------------------
Vector Time (GMT): 2012/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4024926
47 A = 6762707
06 meter
Y = 1667139
86 meter E =
0023771
Z = 5152766
47 I = 51
36596
XDOT = -4233
875072 Wp = 98
10388
YDOT = 6299
983865 meter/sec RA = 311
53061 deg
ZDOT = 1260
574283 TA = 339
74265
MA = 339
83680
Ha = 220
089 n
mi
Hp = 199
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13205139
35 X = 3980954
28
Y = 5469618
96 feet Y = 1711903
56 meter
Z = 16905401
82 Z = 5172212
30
XDOT = -13890
666246 XDOT = -4310
131620
YDOT = 20669
238401 feet/sec YDOT = 6252
211772 meter/sec
ZDOT = 4135
742398 ZDOT = 1239
820840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9909700
51 X = 3020476
71
Y = 10168275
06 feet Y = 3099290
24 meter
Z = 16984965
87 Z = 5177017
60
XDOT = -20162
012474 XDOT = -6145
381402
YDOT = 12838
802952 feet/sec YDOT = 3913
267140 meter/sec
ZDOT = 4050
175186 ZDOT = 1234
493397
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 12059
55022242
00016717 00000-0 10270-3 0 9118
2 25544 51
6431 311
8789 0020173 93
4662 266
8801 15
59339099 40921
Satellite: ISS
Catalog Number: 25544
Epoch time: 12059
55022242 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 311
8789 deg
Eccentricity:
0020173
Arg of perigee: 93
4662 deg
Mean anomaly: 266
8801 deg
Mean motion: 15
59339099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4092
Checksum: 313
Coasting Arc #13 (Orbit 4105)
---------------------------------------
Vector Time (GMT): 2012/060/10:22:35
600
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3001157
39 A = 6764941
71 meter
Y = -3033307
15 meter E =
0031021
Z = -5276447
98 I = 51
34599
XDOT = 4920
688660 Wp = 95
81254
YDOT = -5834
048815 meter/sec RA = 306
81259 deg
ZDOT = 554
792847 TA = 179
51589
MA = 179
51288
Ha = 220
178 n
mi
Hp = 201
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9846316
89 X = -2941383
73
Y = -9951795
12 feet Y = -3066534
04 meter
Z = -17311181
03 Z = -5290881
96
XDOT = 16143
991668 XDOT = 4982
865418
YDOT = -19140
580103 feet/sec YDOT = -5778
674957 meter/sec
ZDOT = 1820
186507 ZDOT = 578
848462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 516301
18 X = 157368
60
Y = -13916838
19 feet Y = -4241852
28 meter
Z = -17370095
54 Z = -5294405
12
XDOT = 23974
376475 XDOT = 7307
389949
YDOT = -1507
109012 feet/sec YDOT = -459
366827 meter/sec
ZDOT = 1919
246514 ZDOT = 584
986338
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 12060
44744373
00016717 00000-0 10270-3 0 9125
2 25544 51
6426 307
3703 0016300 97
5293 262
7714 15
58445425 41067
Satellite: ISS
Catalog Number: 25544
Epoch time: 12060
44744373 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 307
3703 deg
Eccentricity:
0016300
Arg of perigee: 97
5293 deg
Mean anomaly: 262
7714 deg
Mean motion: 15
58445425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4106
Checksum: 296
Coasting Arc #14 (Orbit 4121)
---------------------------------------
Vector Time (GMT): 2012/061/10:22:35
600
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 488550
58 A = 6769676
75 meter
Y = 5378698
07 meter E =
0026399
Z = 4058246
89 I = 51
34425
XDOT = -5721
540441 Wp = 91
46899
YDOT = 3424
508988 meter/sec RA = 301
75451 deg
ZDOT = -3829
098700 TA = 38
24397
MA = 38
05700
Ha = 220
102 n
mi
Hp = 201
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1602856
25 X = 408654
77
Y = 17646647
22 feet Y = 5383714
83 meter
Z = 13314458
29 Z = 4060425
88
XDOT = -18771
458141 XDOT = -5740
808070
YDOT = 11235
265710 feet/sec YDOT = 3360
419268 meter/sec
ZDOT = -12562
659777 ZDOT = -3856
940333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11525648
03 X = -3513017
52
Y = 13450138
18 feet Y = 4099602
12 meter
Z = 13322962
37 Z = 4060838
93
XDOT = -20133
436062 XDOT = -6136
671312
YDOT = -4627
709437 feet/sec YDOT = -1410
525836 meter/sec
ZDOT = -12677
042060 ZDOT = -3863
962420
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 12061
47341537
00016717 00000-0 10270-3 0 9135
2 25544 51
6421 302
2221 0016300 101
1990 259
0998 15
58471737 41223
Satellite: ISS
Catalog Number: 25544
Epoch time: 12061
47341537 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 302
2221 deg
Eccentricity:
0016300
Arg of perigee: 101
1990 deg
Mean anomaly: 259
0998 deg
Mean motion: 15
58471737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4122
Checksum: 282
Coasting Arc #15 (Orbit 4136)
---------------------------------------
Vector Time (GMT): 2012/062/10:22:35
600
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1858557
40 A = 6775670
11 meter
Y = -6344974
65 meter E =
0020886
Z = -1492512
34 I = 51
35036
XDOT = 5071
482251 Wp = 82
98962
YDOT = 150
187466 meter/sec RA = 296
72678 deg
ZDOT = 5748
587198 TA = 260
63344
MA = 260
86965
Ha = 220
006 n
mi
Hp = 201
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6097629
27 X = 1936620
24
Y = -20816845
96 feet Y = -6323754
71 meter
Z = -4896694
02 Z = -1483293
77
XDOT = 16638
721295 XDOT = 5041
500966
YDOT = 492
741031 feet/sec YDOT = 206
732553 meter/sec
ZDOT = 18860
194218 ZDOT = 5773
151040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18968063
24 X = 5781465
67
Y = -10540785
47 feet Y = -3212831
41 meter
Z = -4858414
28 Z = -1480844
67
XDOT = 10663
117076 XDOT = 3250
118085
YDOT = 10558
237870 feet/sec YDOT = 3218
150903 meter/sec
ZDOT = 18960
861273 ZDOT = 5779
270516
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 12062
43524558
00016717 00000-0 10270-3 0 9149
2 25544 51
6428 297
3956 0016181 104
8826 255
4122 15
58512229 41371
Satellite: ISS
Catalog Number: 25544
Epoch time: 12062
43524558 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 297
3956 deg
Eccentricity:
0016181
Arg of perigee: 104
8826 deg
Mean anomaly: 255
4122 deg
Mean motion: 15
58512229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4137
Checksum: 314
Coasting Arc #16 (Orbit 4152)
---------------------------------------
Vector Time (GMT): 2012/063/10:22:35
600
Vector Time (MET): N/A
Weight (LBS) : 886110
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3627091
27 A = 6775406
23 meter
Y = 5465789
65 meter E =
0022883
Z = -1683994
39 I = 51
33683
XDOT = -3326
947568 Wp = 119
31927
YDOT = -3937
618500 meter/sec RA = 291
71547 deg
ZDOT = -5684
006961 TA = 79
24968
MA = 78
99214
Ha = 219
917 n
mi
Hp = 202
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11899905
75 X = -3679760
94
Y = 17932380
76 feet Y = 5424934
70 meter
Z = -5524915
97 Z = -1701742
54
XDOT = -10915
182310 XDOT = -3255
057924
YDOT = -12918
695867 feet/sec YDOT = -3974
420824 meter/sec
ZDOT = -18648
316800 ZDOT = -5699
994011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20955377
55 X = -6387199
08
Y = 4820412
18 feet Y = 1469261
63 meter
Z = -5598081
01 Z = -1706295
09
XDOT = 1424
768330 XDOT = 434
269387
YDOT = -15278
012242 feet/sec YDOT = -4656
738131 meter/sec
ZDOT = -18713
542222 ZDOT = -5703
887669
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 12063
46117985
00016717 00000-0 10270-3 0 9156
2 25544 51
6430 292
2467 0016071 109
0946 251
1951 15
58499004 41539
Satellite: ISS
Catalog Number: 25544
Epoch time: 12063
46117985 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 292
2467 deg
Eccentricity:
0016071
Arg of perigee: 109
0946 deg
Mean anomaly: 251
1951 deg
Mean motion: 15
58499004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4153
Checksum: 309
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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