[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 16th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17760 45 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 356)
---------------------------------------
Vector Time (GMT): 2012/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5589312
61 A = 6771503
14 meter
Y = 2741823
92 meter E =
0026205
Z = 2619545
63 I = 51
39576
XDOT = -317
820877 Wp = 136
55018
YDOT = 5643
621934 meter/sec RA = 225
76032 deg
ZDOT = -5216
655379 TA = 13
69513
MA = 13
62417
Ha = 218
008 n
mi
Hp = 202
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18337639
79 X = 5545512
60
Y = 8995485
30 feet Y = 2804082
33 meter
Z = 8594309
82 Z = 2646591
29
XDOT = -1042
719412 XDOT = -355
564422
YDOT = 18515
819992 feet/sec YDOT = 5639
856501 meter/sec
ZDOT = -17115
011087 ZDOT = -5218
291346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17183575
01 X = 5237553
66
Y = 10954295
83 feet Y = 3338869
37 meter
Z = 8705061
91 Z = 2653302
87
XDOT = -2172
511821 XDOT = -662
181603
YDOT = 17045
934658 feet/sec YDOT = 5195
600884 meter/sec
ZDOT = -17122
063813 ZDOT = -5218
805050
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 12076
53743703
00016717 00000-0 10270-3 0 9005
2 25544 51
6378 226
5823 0016763 163
3686 196
8022 15
59240406 3575
Satellite: ISS
Catalog Number: 25544
Epoch time: 12076
53743703 = yrday
fracday
Element set: 900
Inclination: 51
6378 deg
RA of node: 226
5823 deg
Eccentricity:
0016763
Arg of perigee: 163
3686 deg
Mean anomaly: 196
8022 deg
Mean motion: 15
59240406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 357
Checksum: 314
Coasting Arc #2 (Orbit 372)
---------------------------------------
Vector Time (GMT): 2012/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4747622
49 A = 6774067
84 meter
Y = -4791915
11 meter E =
0016355
Z = 666318
49 I = 51
42855
XDOT = 3833
379075 Wp = 120
17920
YDOT = -2954
976515 meter/sec RA = 220
74794 deg
ZDOT = 5944
804473 TA = 247
04379
MA = 247
21645
Ha = 217
866 n
mi
Hp = 202
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15576189
27 X = -4696922
25
Y = -15721506
26 feet Y = -4844722
42 meter
Z = 2186084
27 Z = 643378
68
XDOT = 12576
703003 XDOT = 3837
259288
YDOT = -9694
804839 feet/sec YDOT = -2912
087123 meter/sec
ZDOT = 19503
951683 ZDOT = 5963
436200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14059928
82 X = -4285466
30
Y = -17102723
83 feet Y = -5212910
22 meter
Z = 2092279
87 Z = 637726
91
XDOT = 12058
143584 XDOT = 3675
322164
YDOT = -7468
153535 feet/sec YDOT = -2276
293197 meter/sec
ZDOT = 19580
546623 ZDOT = 5968
150611
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 12077
56285940
00016717 00000-0 10270-3 0 9014
2 25544 51
6391 221
4304 0016737 167
0423 193
1166 15
59330852 3731
Satellite: ISS
Catalog Number: 25544
Epoch time: 12077
56285940 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 221
4304 deg
Eccentricity:
0016737
Arg of perigee: 167
0423 deg
Mean anomaly: 193
1166 deg
Mean motion: 15
59330852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 373
Checksum: 299
Coasting Arc #3 (Orbit 387)
---------------------------------------
Vector Time (GMT): 2012/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2143543
43 A = 6768230
51 meter
Y = 5214305
28 meter E =
0017248
Z = -3739075
60 I = 51
43309
XDOT = -6379
024405 Wp = 151
24874
YDOT = -411
015460 meter/sec RA = 215
72725 deg
ZDOT = -4253
146301 TA = 73
73473
MA = 73
54506
Ha = 217
622 n
mi
Hp = 203
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7032622
79 X = 2103239
98
Y = 17107300
77 feet Y = 5238049
97 meter
Z = -12267308
41 Z = -3728760
97
XDOT = -20928
557759 XDOT = -6353
293770
YDOT = -1348
475919 feet/sec YDOT = -482
206217 meter/sec
ZDOT = -13953
892065 ZDOT = -4284
072240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5789259
92 X = 1764566
42
Y = 17596330
87 feet Y = 5363361
65 meter
Z = -12225301
14 Z = -3726271
79
XDOT = -19397
895044 XDOT = -5912
478410
YDOT = -3348
219233 feet/sec YDOT = -1020
537222 meter/sec
ZDOT = -14080
724062 ZDOT = -4291
804694
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 12078
52416276
00016717 00000-0 10270-3 0 9020
2 25544 51
6393 216
5999 0016501 170
7312 189
4151 15
59358407 3889
Satellite: ISS
Catalog Number: 25544
Epoch time: 12078
52416276 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 216
5999 deg
Eccentricity:
0016501
Arg of perigee: 170
7312 deg
Mean anomaly: 189
4151 deg
Mean motion: 15
59358407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 388
Checksum: 323
Coasting Arc #4 (Orbit 403)
---------------------------------------
Vector Time (GMT): 2012/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1333219
96 A = 6762185
80 meter
Y = -4062914
43 meter E =
0018489
Z = 5236944
87 I = 51
43974
XDOT = 6874
168485 Wp = 166
52720
YDOT = 3324
891079 meter/sec RA = 210
67023 deg
ZDOT = 811
247288 TA = 275
60278
MA = 275
81360
Ha = 217
295 n
mi
Hp = 203
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4374081
24 X = 1353113
69
Y = -13329771
74 feet Y = -4047893
68 meter
Z = 17181577
67 Z = 5243470
30
XDOT = 22553
046211 XDOT = 6832
537182
YDOT = 10908
435297 feet/sec YDOT = 3401
529602 meter/sec
ZDOT = 2661
572468 ZDOT = 844
539658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5044292
15 X = 1537500
25
Y = -13055343
87 feet Y = -3979268
81 meter
Z = 17208577
09 Z = 5245174
30
XDOT = 20905
577936 XDOT = 6372
020155
YDOT = 11844
251799 feet/sec YDOT = 3610
127948 meter/sec
ZDOT = 2797
956797 ZDOT = 852
817232
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 12079
54951810
00016717 00000-0 10270-3 0 9032
2 25544 51
6400 211
4474 0016345 174
7679 185
3650 15
59435360 4048
Satellite: ISS
Catalog Number: 25544
Epoch time: 12079
54951810 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 211
4474 deg
Eccentricity:
0016345
Arg of perigee: 174
7679 deg
Mean anomaly: 185
3650 deg
Mean motion: 15
59435360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 404
Checksum: 304
Coasting Arc #5 (Orbit 418)
---------------------------------------
Vector Time (GMT): 2012/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4651352
51 A = 6764820
78 meter
Y = 1816434
38 meter E =
0022244
Z = -4582490
09 I = 51
47637
XDOT = -4940
251105 Wp = 153
11974
YDOT = -5024
053905 meter/sec RA = 205
60439 deg
ZDOT = 3009
303184 TA = 147
08433
MA = 146
94563
Ha = 217
093 n
mi
Hp = 203
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15260342
87 X = -4649058
10
Y = 5959430
39 feet Y = 1764432
30 meter
Z = -15034416
29 Z = -4605080
54
XDOT = -16208
172916 XDOT = -4898
322293
YDOT = -16483
116485 feet/sec YDOT = -5079
064010 meter/sec
ZDOT = 9873
041941 ZDOT = 2985
406466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15402883
96 X = -4694799
03
Y = 5324066
92 feet Y = 1622775
60 meter
Z = -15127194
90 Z = -4610769
00
XDOT = -15181
706823 XDOT = -4627
384240
YDOT = -16020
187318 feet/sec YDOT = -4882
953094 meter/sec
ZDOT = 9775
285636 ZDOT = 2979
507062
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 12080
51075787
00016717 00000-0 10270-3 0 9042
2 25544 51
6405 206
6173 0016270 178
1635 181
9583 15
59466679 4192
Satellite: ISS
Catalog Number: 25544
Epoch time: 12080
51075787 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 206
6173 deg
Eccentricity:
0016270
Arg of perigee: 178
1635 deg
Mean anomaly: 181
9583 deg
Mean motion: 15
59466679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 419
Checksum: 328
Coasting Arc #6 (Orbit 434)
---------------------------------------
Vector Time (GMT): 2012/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6418029
12 A = 6772023
26 meter
Y = 730425
02 meter E =
0024745
Z = 1977682
80 I = 51
52929
XDOT = 1135
559122 Wp = 149
97951
YDOT = 5165
349789 meter/sec RA = 200
57313 deg
ZDOT = -5583
789697 TA = 8
06270
MA = 8
02300
Ha = 216
824 n
mi
Hp = 203
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21056525
99 X = 6399777
30
Y = 2396407
54 feet Y = 802093
61 meter
Z = 6488460
63 Z = 2008816
61
XDOT = 3725
587671 XDOT = 1104
839321
YDOT = 16946
685660 feet/sec YDOT = 5177
875771 meter/sec
ZDOT = -18319
520004 ZDOT = -5578
348583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20952262
74 X = 6386249
68
Y = 2906778
77 feet Y = 885986
17 meter
Z = 6616154
50 Z = 2016603
89
XDOT = 3635
881155 XDOT = 1108
216576
YDOT = 15506
043322 feet/sec YDOT = 4726
242004 meter/sec
ZDOT = -18297
480847 ZDOT = -5577
072162
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 12081
53604623
00016717 00000-0 10270-3 0 9053
2 25544 51
6411 201
4643 0016238 181
8265 178
2834 15
59501844 4358
Satellite: ISS
Catalog Number: 25544
Epoch time: 12081
53604623 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 201
4643 deg
Eccentricity:
0016238
Arg of perigee: 181
8265 deg
Mean anomaly: 178
2834 deg
Mean motion: 15
59501844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 435
Checksum: 295
Coasting Arc #7 (Orbit 450)
---------------------------------------
Vector Time (GMT): 2012/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5963215
07 A = 6772654
66 meter
Y = -2867415
91 meter E =
0014066
Z = 1463406
28 I = 51
56186
XDOT = 3274
661445 Wp = 131
15635
YDOT = -3841
979624 meter/sec RA = 195
57091 deg
ZDOT = 5770
620405 TA = 244
84713
MA = 244
99310
Ha = 216
583 n
mi
Hp = 203
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19564353
90 X = -5937816
72
Y = -9407532
52 feet Y = -2933958
06 meter
Z = 4801201
71 Z = 1434499
45
XDOT = 10743
639910 XDOT = 3289
347582
YDOT = -12604
920027 feet/sec YDOT = -3805
277418 meter/sec
ZDOT = 18932
481645 ZDOT = 5786
564708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19525876
15 X = -5951487
05
Y = -9546157
42 feet Y = -2909668
78 meter
Z = 4682754
42 Z = 1427303
55
XDOT = 10021
510810 XDOT = 3054
556495
YDOT = -11104
234905 feet/sec YDOT = -3384
570799 meter/sec
ZDOT = 18998
111263 ZDOT = 5790
624313
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 12082
56129804
00016717 00000-0 10270-3 0 9061
2 25544 51
6419 196
3113 0016010 185
5561 174
5419 15
59580535 4518
Satellite: ISS
Catalog Number: 25544
Epoch time: 12082
56129804 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 196
3113 deg
Eccentricity:
0016010
Arg of perigee: 185
5561 deg
Mean anomaly: 174
5419 deg
Mean motion: 15
59580535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 451
Checksum: 303
Coasting Arc #8 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2012/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3222579
57 A = 6765534
06 meter
Y = 4086647
18 meter E =
0013825
Z = -4319508
15 I = 51
56809
XDOT = -6655
138206 Wp = 157
60026
YDOT = 1576
922451 meter/sec RA = 190
55019 deg
ZDOT = -3489
360412 TA = 77
01604
MA = 76
86171
Ha = 216
377 n
mi
Hp = 204
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10572767
61 X = 3197625
55
Y = 13407635
10 feet Y = 4122543
96 meter
Z = -14171614
67 Z = -4303914
16
XDOT = -21834
442934 XDOT = -6655
326513
YDOT = 5173
630089 feet/sec YDOT = 1502
499067 meter/sec
ZDOT = -11448
032847 ZDOT = -3521
691442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10793568
65 X = 3289879
72
Y = 13298500
70 feet Y = 4053383
01 meter
Z = -14107852
82 Z = -4300073
54
XDOT = -20741
370763 XDOT = -6321
969809
YDOT = 4605
497570 feet/sec YDOT = 1403
755659 meter/sec
ZDOT = -11580
781447 ZDOT = -3529
822185
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 12083
52244081
00016717 00000-0 10270-3 0 9074
2 25544 51
6421 191
4807 0015946 189
6085 170
4768 15
59609927 4665
Satellite: ISS
Catalog Number: 25544
Epoch time: 12083
52244081 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 191
4807 deg
Eccentricity:
0015946
Arg of perigee: 189
6085 deg
Mean anomaly: 170
4768 deg
Mean motion: 15
59609927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 333
Coasting Arc #9 (Orbit 481)
---------------------------------------
Vector Time (GMT): 2012/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 725489
60 A = 6761163
69 meter
Y = -4146033
16 meter E =
0014855
Z = 5291740
08 I = 51
58495
XDOT = 7610
439092 Wp = 184
99608
YDOT = 969
592267 meter/sec RA = 185
49374 deg
ZDOT = -298
274910 TA = 267
76089
MA = 267
93099
Ha = 215
954 n
mi
Hp = 204
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2380215
21 X = 746091
29
Y = -13602471
01 feet Y = -4137804
46 meter
Z = 17361351
96 Z = 5295315
02
XDOT = 24968
632191 XDOT = 7600
480244
YDOT = 3181
076990 feet/sec YDOT = 1054
641182 meter/sec
ZDOT = -978
592223 ZDOT = -261
327928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1902502
76 X = 579882
84
Y = -13658534
77 feet Y = -4163121
40 meter
Z = 17376250
89 Z = 5296281
27
XDOT = 24055
656410 XDOT = 7332
164074
YDOT = 2359
308888 feet/sec YDOT = 719
117349 meter/sec
ZDOT = -827
032464 ZDOT = -252
079495
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 12084
54762432
00016717 00000-0 10270-3 0 9083
2 25544 51
6423 186
3276 0015725 193
4690 166
6048 15
59709350 4827
Satellite: ISS
Catalog Number: 25544
Epoch time: 12084
54762432 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 186
3276 deg
Eccentricity:
0015725
Arg of perigee: 193
4690 deg
Mean anomaly: 166
6048 deg
Mean motion: 15
59709350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 482
Checksum: 324
Coasting Arc #10 (Orbit 496)
---------------------------------------
Vector Time (GMT): 2012/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4531943
06 A = 6766282
97 meter
Y = 3104339
34 meter E =
0017182
Z = -3965389
70 I = 51
63262
XDOT = -5703
642441 Wp = 173
55393
YDOT = -3205
876033 meter/sec RA = 180
44259 deg
ZDOT = 3993
769525 TA = 138
15666
MA = 138
02519
Ha = 215
701 n
mi
Hp = 204
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14868579
60 X = -4547056
51
Y = 10184840
34 feet Y = 3053575
43 meter
Z = -13009808
72 Z = -3987442
82
XDOT = -18712
737668 XDOT = -5686
770714
YDOT = -10517
965987 feet/sec YDOT = -3269
562934 meter/sec
ZDOT = 13102
918390 ZDOT = 3966
102662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14321502
51 X = -4365193
97
Y = 10832017
60 feet Y = 3301598
97 meter
Z = -13100485
32 Z = -3993027
93
XDOT = -18451
445727 XDOT = -5624
000658
YDOT = -8626
405208 feet/sec YDOT = -2629
328307 meter/sec
ZDOT = 12989
556170 ZDOT = 3959
216721
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 12085
50870403
00016717 00000-0 10270-3 0 9099
2 25544 51
6419 181
4968 0015638 196
9329 163
1306 15
59738805 4978
Satellite: ISS
Catalog Number: 25544
Epoch time: 12085
50870403 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 181
4968 deg
Eccentricity:
0015638
Arg of perigee: 196
9329 deg
Mean anomaly: 163
1306 deg
Mean motion: 15
59738805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 497
Checksum: 341
Coasting Arc #11 (Orbit 512)
---------------------------------------
Vector Time (GMT): 2012/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6587360
00 A = 6772657
58 meter
Y = -1222203
71 meter E =
0023073
Z = 878035
31 I = 51
68373
XDOT = 1645
050459 Wp = 166
25063
YDOT = 4585
007770 meter/sec RA = 175
43325 deg
ZDOT = -5949
570027 TA = 4
21629
MA = 4
19688
Ha = 215
455 n
mi
Hp = 204
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21612073
48 X = 6596272
01
Y = -4009854
68 feet Y = -1148489
87 meter
Z = 2880693
27 Z = 910058
35
XDOT = 5397
147175 XDOT = 1622
559555
YDOT = 15042
676411 feet/sec YDOT = 4603
277459 meter/sec
ZDOT = -19519
586704 ZDOT = -5941
633437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21305795
06 X = 6494006
33
Y = -5333745
21 feet Y = -1625725
54 meter
Z = 3012193
10 Z = 918116
46
XDOT = 6043
819286 XDOT = 1842
156118
YDOT = 13119
167032 feet/sec YDOT = 3998
722111 meter/sec
ZDOT = -19487
272521 ZDOT = -5939
720664
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 12086
53382187
00016717 00000-0 10270-3 0 9102
2 25544 51
6411 176
3435 0015555 200
4424 159
6111 15
59760696 5133
Satellite: ISS
Catalog Number: 25544
Epoch time: 12086
53382187 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 176
3435 deg
Eccentricity:
0015555
Arg of perigee: 200
4424 deg
Mean anomaly: 159
6111 deg
Mean motion: 15
59760696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 513
Checksum: 299
Coasting Arc #12 (Orbit 528)
---------------------------------------
Vector Time (GMT): 2012/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6162808
21 A = 6769952
58 meter
Y = -1050508
60 meter E =
0012851
Z = 2608504
89 I = 51
70584
XDOT = 3030
231099 Wp = 147
71858
YDOT = -4706
993335 meter/sec RA = 170
43805 deg
ZDOT = 5241
010026 TA = 241
66393
MA = 241
79361
Ha = 215
135 n
mi
Hp = 204
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20219187
04 X = -6163274
77
Y = -3446550
52 feet Y = -1119427
34 meter
Z = 8558086
90 Z = 2578565
03
XDOT = 9941
703081 XDOT = 3057
180651
YDOT = -15442
891519 feet/sec YDOT = -4672
956343 meter/sec
ZDOT = 17194
914785 ZDOT = 5255
796642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20479389
91 X = -6242118
04
Y = -1837434
99 feet Y = -560050
18 meter
Z = 8435253
88 Z = 2571065
38
XDOT = 8455
166833 XDOT = 2577
134851
YDOT = -14675
926635 feet/sec YDOT = -4473
222438 meter/sec
ZDOT = 17255
879433 ZDOT = 5259
592051
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 12087
55890316
00016717 00000-0 10270-3 0 9114
2 25544 51
6413 171
1889 0015396 204
6281 155
4141 15
59842586 5294
Satellite: ISS
Catalog Number: 25544
Epoch time: 12087
55890316 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 171
1889 deg
Eccentricity:
0015396
Arg of perigee: 204
6281 deg
Mean anomaly: 155
4141 deg
Mean motion: 15
59842586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 529
Checksum: 322
Coasting Arc #13 (Orbit 543)
---------------------------------------
Vector Time (GMT): 2012/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3345837
17 A = 6762318
85 meter
Y = 3167589
00 meter E =
0010996
Z = -4950368
67 I = 51
70943
XDOT = -6492
538490 Wp = 155
68634
YDOT = 3468
543863 meter/sec RA = 165
41046 deg
ZDOT = -2180
254106 TA = 93
16370
MA = 93
03788
Ha = 214
906 n
mi
Hp = 205
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10977156
08 X = 3334215
75
Y = 10392352
35 feet Y = 3204938
92 meter
Z = -16241367
04 Z = -4934143
12
XDOT = -21300
979299 XDOT = -6520
250683
YDOT = 11379
737083 feet/sec YDOT = 3395
785197 meter/sec
ZDOT = -7153
064653 ZDOT = -2211
862217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12021747
53 X = 3664228
65
Y = 9280610
65 feet Y = 2828730
13 meter
Z = -16174943
54 Z = -4930122
79
XDOT = -19390
243497 XDOT = -5910
146218
YDOT = 12490
099484 feet/sec YDOT = 3806
982323 meter/sec
ZDOT = -7283
022205 ZDOT = -2219
865168
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 12088
51988764
00016717 00000-0 10270-3 0 9127
2 25544 51
6403 166
3571 0015290 208
5456 151
4864 15
59863049 5449
Satellite: ISS
Catalog Number: 25544
Epoch time: 12088
51988764 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 166
3571 deg
Eccentricity:
0015290
Arg of perigee: 208
5456 deg
Mean anomaly: 151
4864 deg
Mean motion: 15
59863049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 544
Checksum: 330
Coasting Arc #14 (Orbit 559)
---------------------------------------
Vector Time (GMT): 2012/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 626129
16 A = 6761499
16 meter
Y = -4452675
79 meter E =
0010343
Z = 5050234
78 I = 51
73763
XDOT = 7370
315620 Wp = 201
28128
YDOT = -1068
074139 meter/sec RA = 160
35637 deg
ZDOT = -1866
084854 TA = 266
69199
MA = 266
81032
Ha = 214
450 n
mi
Hp = 205
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2054229
54 X = 651340
42
Y = -14608516
37 feet Y = -4445532
76 meter
Z = 16569011
74 Z = 5053337
99
XDOT = 24180
825524 XDOT = 7390
776291
YDOT = -3504
180247 feet/sec YDOT = -985
540424 meter/sec
ZDOT = -6122
325636 ZDOT = -1830
230388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 289253
22 X = 88164
38
Y = -14734784
48 feet Y = -4491162
31 meter
Z = 16582014
91 Z = 5054198
15
XDOT = 22591
531949 XDOT = 6885
898938
YDOT = -6241
474726 feet/sec YDOT = -1902
401497 meter/sec
ZDOT = -5975
058133 ZDOT = -1821
197719
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 12089
54490291
00016717 00000-0 10270-3 0 9135
2 25544 51
6408 161
2024 0015161 212
7576 147
2641 15
59963163 5600
Satellite: ISS
Catalog Number: 25544
Epoch time: 12089
54490291 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 161
2024 deg
Eccentricity:
0015161
Arg of perigee: 212
7576 deg
Mean anomaly: 147
2641 deg
Mean motion: 15
59963163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 560
Checksum: 299
Coasting Arc #15 (Orbit 574)
---------------------------------------
Vector Time (GMT): 2012/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4273041
54 A = 6768856
33 meter
Y = 4422037
31 meter E =
0011076
Z = -2838735
20 I = 51
79002
XDOT = -5396
945244 Wp = 205
37588
YDOT = -1933
881565 meter/sec RA = 155
32772 deg
ZDOT = 5094
192754 TA = 122
38736
MA = 122
28014
Ha = 214
164 n
mi
Hp = 205
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14019165
15 X = -4308382
15
Y = 14507996
42 feet Y = 4374055
75 meter
Z = -9313435
69 Z = -2859579
51
XDOT = -17706
513267 XDOT = -5399
665478
YDOT = -6344
755792 feet/sec YDOT = -1994
248450 meter/sec
ZDOT = 16713
230819 ZDOT = 5067
968186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11955451
06 X = -3644021
48
Y = 16201222
70 feet Y = 4938132
68 meter
Z = -9399287
69 Z = -2864902
89
XDOT = -17300
519811 XDOT = -5273
198438
YDOT = -3100
435861 feet/sec YDOT = -945
012851 meter/sec
ZDOT = 16605
665492 ZDOT = 5061
406842
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 12090
50582657
00016717 00000-0 10270-3 0 9142
2 25544 51
6399 156
3697 0014995 215
9688 144
0459 15
59985347 5759
Satellite: ISS
Catalog Number: 25544
Epoch time: 12090
50582657 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 156
3697 deg
Eccentricity:
0014995
Arg of perigee: 215
9688 deg
Mean anomaly: 144
0459 deg
Mean motion: 15
59985347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 575
Checksum: 365
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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