[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 6th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10494 81 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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 3748)
---------------------------------------
Vector Time (GMT): 2012/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2984041
49 A = 6776056
96 meter
Y = 6055296
30 meter E =
0031779
Z = 274415
38 I = 51
96907
XDOT = -4367
366738 Wp = 25
87687
YDOT = 1867
440426 meter/sec RA = 61
94397 deg
ZDOT = 6050
552461 TA = 337
07891
MA = 337
22042
Ha = 220
217 n
mi
Hp = 202
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9790162
36 X = 2914775
16
Y = 19866457
69 feet Y = 6088278
40 meter
Z = 900312
93 Z = 288743
08
XDOT = -14328
631030 XDOT = -4417
315635
YDOT = 6126
773050 feet/sec YDOT = 1818
322550 meter/sec
ZDOT = 19850
893900 ZDOT = 6029
215267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7040933
36 X = -2146076
49
Y = 20996198
94 feet Y = 6399641
44 meter
Z = 958577
63 Z = 292174
46
XDOT = -13043
440210 XDOT = -3975
640576
YDOT = -5309
195515 feet/sec YDOT = -1618
242793 meter/sec
ZDOT = 19763
242165 ZDOT = 6023
836212
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 12037
56355562
00016717 00000-0 10270-3 0 9007
2 25544 51
6409 62
2910 0020603 12
8885 347
2793 15
58699571 37494
Satellite: ISS
Catalog Number: 25544
Epoch time: 12037
56355562 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 62
2910 deg
Eccentricity:
0020603
Arg of perigee: 12
8885 deg
Mean anomaly: 347
2793 deg
Mean motion: 15
58699571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3749
Checksum: 325
Coasting Arc #2 (Orbit 3763)
---------------------------------------
Vector Time (GMT): 2012/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -740031
31 A = 6771328
82 meter
Y = -5881766
55 meter E =
0021950
Z = -3302506
74 I = 51
93808
XDOT = 5690
498137 Wp = 28
26123
YDOT = 1947
107631 meter/sec RA = 56
96611 deg
ZDOT = -4736
976557 TA = 189
91713
MA = 189
96052
Ha = 220
246 n
mi
Hp = 202
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2427924
24 X = -658162
84
Y = -19297134
35 feet Y = -5889584
36 meter
Z = -10834995
86 Z = -3305902
68
XDOT = 18669
613310 XDOT = 5691
312762
YDOT = 6388
148396 feet/sec YDOT = 2010
746729 meter/sec
ZDOT = -15541
261671 ZDOT = -4709
331239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11644782
05 X = 3549329
57
Y = -15568611
29 feet Y = -4745312
72 meter
Z = -10848444
09 Z = -3306605
76
XDOT = 7994
660364 XDOT = 2436
772479
YDOT = 16743
835614 feet/sec YDOT = 5103
521095 meter/sec
ZDOT = -15428
049453 ZDOT = -4702
469473
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 12038
52524298
00016717 00000-0 10270-3 0 9019
2 25544 51
6405 57
4626 0020537 16
5385 343
6436 15
58734358 37646
Satellite: ISS
Catalog Number: 25544
Epoch time: 12038
52524298 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 57
4626 deg
Eccentricity:
0020537
Arg of perigee: 16
5385 deg
Mean anomaly: 343
6436 deg
Mean motion: 15
58734358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3764
Checksum: 319
Coasting Arc #3 (Orbit 3779)
---------------------------------------
Vector Time (GMT): 2012/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1968227
37 A = 6764839
28 meter
Y = 3970583
54 meter E =
0019903
Z = 5097275
01 I = 51
89790
XDOT = -5605
302539 Wp = 34
42936
YDOT = -4972
121843 meter/sec RA = 51
95345 deg
ZDOT = 1721
471175 TA = 39
11039
MA = 38
96669
Ha = 220
447 n
mi
Hp = 202
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6457438
86 X = -2037241
68
Y = 13026848
88 feet Y = 3948187
97 meter
Z = 16723343
20 Z = 5087545
89
XDOT = -18390
100192 XDOT = -5557
648969
YDOT = -16312
735705 feet/sec YDOT = -5034
537262 meter/sec
ZDOT = 5647
871309 ZDOT = 1694
357600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13662945
44 X = -4164465
77
Y = 5105377
93 feet Y = 1556119
19 meter
Z = 16683121
84 Z = 5085015
54
XDOT = -2067
697746 XDOT = -630
234273
YDOT = -23490
141875 feet/sec YDOT = -7159
795244 meter/sec
ZDOT = 5537
087500 ZDOT = 1687
704270
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 12039
55102962
00016717 00000-0 10270-3 0 9024
2 25544 51
6394 52
3119 0020593 20
4942 339
7035 15
58751098 37808
Satellite: ISS
Catalog Number: 25544
Epoch time: 12039
55102962 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 52
3119 deg
Eccentricity:
0020593
Arg of perigee: 20
4942 deg
Mean anomaly: 339
7035 deg
Mean motion: 15
58751098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3780
Checksum: 306
Coasting Arc #4 (Orbit 3794)
---------------------------------------
Vector Time (GMT): 2012/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4358646
89 A = 6765151
27 meter
Y = -1149495
45 meter E =
0026059
Z = -5057919
79 I = 51
87979
XDOT = 3866
666804 Wp = 52
78496
YDOT = 6334
873846 meter/sec RA = 46
92298 deg
ZDOT = 1914
492512 TA = 235
60339
MA = 235
85006
Ha = 220
497 n
mi
Hp = 202
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14300022
61 X = 4395746
49
Y = -3771310
54 feet Y = -1100547
27 meter
Z = -16594225
04 Z = -5036656
00
XDOT = 12685
914710 XDOT = 3786
241644
YDOT = 20783
706845 feet/sec YDOT = 6377
663742 meter/sec
ZDOT = 6281
143413 ZDOT = 1933
080391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13249207
76 X = 4038358
53
Y = 6786853
15 feet Y = 2068632
84 meter
Z = -16506933
46 Z = -5031313
32
XDOT = -3930
953729 XDOT = -1198
154697
YDOT = 22957
688028 feet/sec YDOT = 6997
503311 meter/sec
ZDOT = 6356
849244 ZDOT = 1937
567650
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 12040
51269074
00016717 00000-0 10270-3 0 9031
2 25544 51
6400 47
4847 0020604 23
6687 336
5412 15
58751826 37952
Satellite: ISS
Catalog Number: 25544
Epoch time: 12040
51269074 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 47
4847 deg
Eccentricity:
0020604
Arg of perigee: 23
6687 deg
Mean anomaly: 336
5412 deg
Mean motion: 15
58751826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3795
Checksum: 307
Coasting Arc #5 (Orbit 3810)
---------------------------------------
Vector Time (GMT): 2012/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5722341
80 A = 6771687
31 meter
Y = -1857799
81 meter E =
0028274
Z = 3109194
49 I = 51
88002
XDOT = -781
284515 Wp = 52
37763
YDOT = -5858
259960 meter/sec RA = 41
90924 deg
ZDOT = -4891
113989 TA = 91
92031
MA = 91
59647
Ha = 220
512 n
mi
Hp = 201
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18774087
28 X = -5716245
69
Y = -6095143
74 feet Y = -1921756
25 meter
Z = 10200769
34 Z = 3081411
10
XDOT = -2563
269407 XDOT = -691
958739
YDOT = -19220
012992 feet/sec YDOT = -5866
497677 meter/sec
ZDOT = -16046
961905 ZDOT = -4894
691963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10271161
07 X = -3130649
89
Y = -16924202
25 feet Y = -5158496
84 meter
Z = 10086994
30 Z = 3074515
86
XDOT = 9463
348985 XDOT = 2884
428771
YDOT = -15409
219424 feet/sec YDOT = -4696
730081 meter/sec
ZDOT = -16061
150736 ZDOT = -4895
438744
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 12041
53844747
00016717 00000-0 10270-3 0 9041
2 25544 51
6392 42
3334 0020720 27
4046 332
8197 15
58826544 38115
Satellite: ISS
Catalog Number: 25544
Epoch time: 12041
53844747 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 42
3334 deg
Eccentricity:
0020720
Arg of perigee: 27
4046 deg
Mean anomaly: 332
8197 deg
Mean motion: 15
58826544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3811
Checksum: 300
Coasting Arc #6 (Orbit 3825)
---------------------------------------
Vector Time (GMT): 2012/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5436669
17 A = 6775615
50 meter
Y = 4013555
28 meter E =
0032384
Z = -73994
74 I = 51
87052
XDOT = -2778
896938 Wp = 36
20674
YDOT = 3850
569800 meter/sec RA = 36
92860 deg
ZDOT = 6048
558173 TA = 322
99572
MA = 323
21863
Ha = 220
457 n
mi
Hp = 201
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17836841
12 X = 5391744
17
Y = 13167832
27 feet Y = 4074100
27 meter
Z = -242764
89 Z = -47693
44
XDOT = -9117
115938 XDOT = -2851
130347
YDOT = 12633
103020 feet/sec YDOT = 3819
091005 meter/sec
ZDOT = 19844
350962 ZDOT = 6034
882898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5264004
57 X = 1604468
59
Y = 21537771
59 feet Y = 6564712
78 meter
Z = -135253
47 Z = -41225
26
XDOT = -13615
709710 XDOT = -4150
068319
YDOT = 3401
562184 feet/sec YDOT = 1036
796154 meter/sec
ZDOT = 19787
955909 ZDOT = 6031
368961
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 12042
50008200
00016717 00000-0 10270-3 0 9056
2 25544 51
6395 37
5064 0020526 31
5183 328
7197 15
58862410 38268
Satellite: ISS
Catalog Number: 25544
Epoch time: 12042
50008200 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 37
5064 deg
Eccentricity:
0020526
Arg of perigee: 31
5183 deg
Mean anomaly: 328
7197 deg
Mean motion: 15
58862410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3826
Checksum: 288
Coasting Arc #7 (Orbit 3841)
---------------------------------------
Vector Time (GMT): 2012/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3443914
52 A = 6771630
11 meter
Y = -4982816
19 meter E =
0022574
Z = -3061001
50 I = 51
83187
XDOT = 5775
182720 Wp = 45
51565
YDOT = -966
652534 meter/sec RA = 31
94493 deg
ZDOT = -4931
072248 TA = 169
49200
MA = 169
44475
Ha = 220
629 n
mi
Hp = 201
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11298932
17 X = -3373070
23
Y = -16347822
15 feet Y = -5020932
22 meter
Z = -10042655
83 Z = -3077559
33
XDOT = 18947
449869 XDOT = 5809
516561
YDOT = -3171
432197 feet/sec YDOT = -901
879183 meter/sec
ZDOT = -16178
058555 ZDOT = -4902
933545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1501714
35 X = 457722
53
Y = -19781362
48 feet Y = -6029359
28 meter
Z = -10110125
90 Z = -3081566
37
XDOT = 15380
467160 XDOT = 4687
966390
YDOT = 9365
444842 feet/sec YDOT = 2854
587588 meter/sec
ZDOT = -16062
601527 ZDOT = -4895
880945
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 12043
52581012
00016717 00000-0 10270-3 0 9067
2 25544 51
6392 32
3551 0020735 35
0625 325
1891 15
58839468 38428
Satellite: ISS
Catalog Number: 25544
Epoch time: 12043
52581012 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 32
3551 deg
Eccentricity:
0020735
Arg of perigee: 35
0625 deg
Mean anomaly: 325
1891 deg
Mean motion: 15
58839468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3842
Checksum: 299
Coasting Arc #8 (Orbit 3857)
---------------------------------------
Vector Time (GMT): 2012/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 212081
97 A = 6764834
62 meter
Y = 4526723
30 meter E =
0021864
Z = 5003610
14 I = 51
78289
XDOT = -7184
518763 Wp = 53
11009
YDOT = -1875
703037 meter/sec RA = 26
92800 deg
ZDOT = 2008
270040 TA = 17
51890
MA = 17
44360
Ha = 220
664 n
mi
Hp = 200
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 695806
98 X = 137141
32
Y = 14851454
41 feet Y = 4528676
09 meter
Z = 16416043
76 Z = 5004458
23
XDOT = -23571
255784 XDOT = -7172
765929
YDOT = -6153
881356 feet/sec YDOT = -1955
978971 meter/sec
ZDOT = 6588
812466 ZDOT = 1973
396942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8644745
39 X = -2634918
40
Y = 12092013
44 feet Y = 3685645
70 meter
Z = 16419132
94 Z = 5004551
72
XDOT = -13982
610393 XDOT = -4261
899648
YDOT = -18718
682701 feet/sec YDOT = -5705
454487 meter/sec
ZDOT = 6445
989410 ZDOT = 1964
737572
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 12044
55152172
00016717 00000-0 10270-3 0 9073
2 25544 51
6391 27
2052 0020674 38
3649 321
8972 15
58868107 38582
Satellite: ISS
Catalog Number: 25544
Epoch time: 12044
55152172 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 27
2052 deg
Eccentricity:
0020674
Arg of perigee: 38
3649 deg
Mean anomaly: 321
8972 deg
Mean motion: 15
58868107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3858
Checksum: 319
Coasting Arc #9 (Orbit 3872)
---------------------------------------
Vector Time (GMT): 2012/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3237277
26 A = 6764556
30 meter
Y = -3047231
10 meter E =
0029675
Z = -5118396
60 I = 51
75431
XDOT = 6337
813193 Wp = 64
83263
YDOT = 3963
628183 meter/sec RA = 21
88767 deg
ZDOT = 1668
650175 TA = 221
16059
MA = 221
38477
Ha = 220
745 n
mi
Hp = 200
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10620988
39 X = 3295975
14
Y = -9997477
36 feet Y = -3010701
74 meter
Z = -16792639
76 Z = -5102527
62
XDOT = 20793
350371 XDOT = 6284
914233
YDOT = 13004
029471 feet/sec YDOT = 4034
205764 meter/sec
ZDOT = 5474
574065 ZDOT = 1699
310092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14577340
20 X = 4443173
29
Y = -1563941
61 feet Y = -476689
40 meter
Z = -16727311
12 Z = -5098484
43
XDOT = 8689
312574 XDOT = 2648
502472
YDOT = 21797
029204 feet/sec YDOT = 6643
734501 meter/sec
ZDOT = 5599
937214 ZDOT = 1706
860863
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 12045
51311243
00016717 00000-0 10270-3 0 9087
2 25544 51
6393 22
3771 0020727 42
0422 318
2319 15
58864690 38733
Satellite: ISS
Catalog Number: 25544
Epoch time: 12045
51311243 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 22
3771 deg
Eccentricity:
0020727
Arg of perigee: 42
0422 deg
Mean anomaly: 318
2319 deg
Mean motion: 15
58864690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3873
Checksum: 294
Coasting Arc #10 (Orbit 3888)
---------------------------------------
Vector Time (GMT): 2012/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5869052
12 A = 6771037
83 meter
Y = 896200
56 meter E =
0030844
Z = 3247307
30 I = 51
74778
XDOT = -3418
196247 Wp = 62
96398
YDOT = -4958
345009 meter/sec RA = 16
86289 deg
ZDOT = -4761
022185 TA = 79
36945
MA = 79
02222
Ha = 220
762 n
mi
Hp = 200
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19255420
34 X = -5894411
87
Y = 2940290
54 feet Y = 830427
40 meter
Z = 10653895
34 Z = 3218734
53
XDOT = -11214
554615 XDOT = -3339
369360
YDOT = -16267
536118 feet/sec YDOT = -4996
128632 meter/sec
ZDOT = -15620
151527 ZDOT = -4777
435926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17375973
28 X = -5296196
65
Y = -8942942
36 feet Y = -2725808
83 meter
Z = 10536666
52 Z = 3211575
96
XDOT = -123
897987 XDOT = -37
764106
YDOT = -18431
316772 feet/sec YDOT = -5617
865352 meter/sec
ZDOT = -15687
013566 ZDOT = -4781
401735
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 12046
53879267
00016717 00000-0 10270-3 0 9096
2 25544 51
6392 17
2261 0020740 45
5461 314
7387 15
58922764 38895
Satellite: ISS
Catalog Number: 25544
Epoch time: 12046
53879267 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 17
2261 deg
Eccentricity:
0020740
Arg of perigee: 45
5461 deg
Mean anomaly: 314
7387 deg
Mean motion: 15
58922764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3889
Checksum: 335
Coasting Arc #11 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2012/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6646760
26 A = 6775347
32 meter
Y = 1217517
98 meter E =
0032460
Z = -222896
44 I = 51
73324
XDOT = -681
150152 Wp = 47
09993
YDOT = 4717
401696 meter/sec RA = 11
87104 deg
ZDOT = 6030
127622 TA = 310
49352
MA = 310
77594
Ha = 220
733 n
mi
Hp = 200
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21806956
25 X = 6633734
49
Y = 3994481
56 feet Y = 1291773
32 meter
Z = -731287
54 Z = -190639
04
XDOT = -2234
744592 XDOT = -763
142891
YDOT = 15477
039685 feet/sec YDOT = 4709
326175 meter/sec
ZDOT = 19783
883275 ZDOT = 6026
619561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15602023
26 X = 4755496
69
Y = 15756011
89 feet Y = 4802432
42 meter
Z = -599136
59 Z = -182616
83
XDOT = -9638
742679 XDOT = -2937
888769
YDOT = 10208
822806 feet/sec YDOT = 3111
649191 meter/sec
ZDOT = 19769
083511 ZDOT = 6025
616654
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 12047
50035354
00016717 00000-0 10270-3 0 9107
2 25544 51
6393 12
3983 0020711 49
5775 310
7183 15
58948940 39045
Satellite: ISS
Catalog Number: 25544
Epoch time: 12047
50035354 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 12
3983 deg
Eccentricity:
0020711
Arg of perigee: 49
5775 deg
Mean anomaly: 310
7183 deg
Mean motion: 15
58948940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 306
Coasting Arc #12 (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 = -5304433
97 A = 6771429
60 meter
Y = -3008078
23 meter E =
0023512
Z = -2976179
95 I = 51
69150
XDOT = 4713
591638 Wp = 61
71191
YDOT = -3398
360938 meter/sec RA = 6
87832 deg
ZDOT = -4985
367833 TA = 152
27206
MA = 152
14651
Ha = 220
736 n
mi
Hp = 200
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17402998
58 X = -5255945
53
Y = -9869023
05 feet Y = -3067124
57 meter
Z = -9764369
92 Z = -3001830
25
XDOT = 15464
539496 XDOT = 4775
459678
YDOT = -11149
478143 feet/sec YDOT = -3345
304738 meter/sec
ZDOT = -16356
193678 ZDOT = -4962
319689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8885028
32 X = -2708156
63
Y = -17867809
01 feet Y = -5446108
19 meter
Z = -9869273
95 Z = -3008154
70
XDOT = 17834
240293 XDOT = 5435
876441
YDOT = 79
326650 feet/sec YDOT = 24
178763 meter/sec
ZDOT = -16261
393468 ZDOT = -4956
472729
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
52600190
00016717 00000-0 10270-3 0 9117
2 25544 51
6402 7
2467 0020762 52
9217 307
3832 15
58972896 39209
Satellite: ISS
Catalog Number: 25544
Epoch time: 12048
52600190 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 7
2467 deg
Eccentricity:
0020762
Arg of perigee: 52
9217 deg
Mean anomaly: 307
3832 deg
Mean motion: 15
58972896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3920
Checksum: 300
Coasting Arc #13 (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 = 2190247
08 A = 6764468
30 meter
Y = 4006220
12 meter E =
0023484
Z = 4969545
83 I = 51
63874
XDOT = -7275
200294 Wp = 69
56063
YDOT = 1406
290118 meter/sec RA = 1
85196 deg
ZDOT = 2072
887892 TA =
34518
MA =
34356
Ha = 220
592 n
mi
Hp = 200
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7185850
00 X = 2121145
67
Y = 13143766
80 feet Y = 4030326
54 meter
Z = 16304284
23 Z = 4980017
74
XDOT = -23868
767370 XDOT = -7300
454349
YDOT = 4613
812723 feet/sec YDOT = 1324
793179 meter/sec
ZDOT = 6800
813294 ZDOT = 2037
484909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1198010
22 X = -365153
51
Y = 14885206
93 feet Y = 4537011
07 meter
Z = 16346868
70 Z = 4982525
58
XDOT = -21490
747719 XDOT = -6550
379905
YDOT = -9038
192936 feet/sec YDOT = -2754
841207 meter/sec
ZDOT = 6655
533130 ZDOT = 2028
606498
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
55163226
00016717 00000-0 10270-3 0 9126
2 25544 51
6407 2
0969 0020527 56
6661 303
6456 15
59024869 39364
Satellite: ISS
Catalog Number: 25544
Epoch time: 12049
55163226 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 2
0969 deg
Eccentricity:
0020527
Arg of perigee: 56
6661 deg
Mean anomaly: 303
6456 deg
Mean motion: 15
59024869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 314
Coasting Arc #14 (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 = 1622704
49 A = 6764149
17 meter
Y = -4149548
00 meter E =
0031849
Z = -5114224
55 I = 51
60694
XDOT = 7422
527745 Wp = 76
23003
YDOT = 892
217175 meter/sec RA = 356
79939 deg
ZDOT = 1647
213404 TA = 209
61397
MA = 209
79469
Ha = 220
744 n
mi
Hp = 199
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5323833
62 X = 1693827
98
Y = -13614002
63 feet Y = -4131004
45 meter
Z = -16778951
93 Z = -5106168
84
XDOT = 24352
125147 XDOT = 7403
997581
YDOT = 2927
221704 feet/sec YDOT = 975
116915 meter/sec
ZDOT = 5404
243453 ZDOT = 1683
225604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11807873
00 X = 3599039
69
Y = -8682038
41 feet Y = -2646285
31 meter
Z = -16745561
92 Z = -5104047
27
XDOT = 18453
473291 XDOT = 5624
618659
YDOT = 14490
840352 feet/sec YDOT = 4416
808139 meter/sec
ZDOT = 5551
818421 ZDOT = 1692
194255
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
51314791
00016717 00000-0 10270-3 0 9130
2 25544 51
6409 357
2676 0020643 60
1038 300
2164 15
59002087 39517
Satellite: ISS
Catalog Number: 25544
Epoch time: 12050
51314791 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 357
2676 deg
Eccentricity:
0020643
Arg of perigee: 60
1038 deg
Mean anomaly: 300
2164 deg
Mean motion: 15
59002087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 281
Coasting Arc #15 (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 = -4951127
82 A = 6770734
91 meter
Y = 3294616
64 meter E =
0032453
Z = 3218989
23 I = 51
59969
XDOT = -5177
937394 Wp = 74
71733
YDOT = -3071
918160 meter/sec RA = 351
76382 deg
ZDOT = -4771
635423 TA = 67
88098
MA = 67
53678
Ha = 220
775 n
mi
Hp = 199
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16243857
68 X = -5003237
58
Y = 10809109
70 feet Y = 3238958
91 meter
Z = 10560988
30 Z = 3194810
81
XDOT = -16987
983577 XDOT = -5120
022901
YDOT = -10078
471655 feet/sec YDOT = -3129
497526 meter/sec
ZDOT = -15654
971859 ZDOT = -4796
648015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19545211
27 X = -5957380
40
Y = 880009
00 feet Y = 268226
74 meter
Z = 10461574
42 Z = 3188687
88
XDOT = -9236
246307 XDOT = -2815
207874
YDOT = -15908
418138 feet/sec YDOT = -4848
885848 meter/sec
ZDOT = -15757
258004 ZDOT = -4802
812240
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
53874666
00016717 00000-0 10270-3 0 9146
2 25544 51
6416 352
1166 0020661 63
8897 296
4381 15
59047410 39679
Satellite: ISS
Catalog Number: 25544
Epoch time: 12051
53874666 = yrday
fracday
Element set: 914
Inclination: 51
6416 deg
RA of node: 352
1166 deg
Eccentricity:
0020661
Arg of perigee: 63
8897 deg
Mean anomaly: 296
4381 deg
Mean motion: 15
59047410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 329
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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