[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 10th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 ET - UTC (sec) : 67 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
348/14:31:56
272 -1
0 1
4 1
4
N/A 0
9 0
1 230
4
000/00:07:48
544 -0
4 0
3 213
2
Coasting Arc #1 (Orbit 493)
---------------------------------------
Vector Time (GMT): 2012/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5658399
78 A = 6794556
55 meter
Y = 3409686
23 meter E =
0018859
Z = 1601325
70 I = 51
54614
XDOT = -3727
172719 Wp = 58
53806
YDOT = -3473
635353 meter/sec RA = 340
02543 deg
ZDOT = -5714
350180 TA = 103
95535
MA = 103
74555
Ha = 229
370 n
mi
Hp = 214
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18564303
75 X = -5703886
02
Y = 11186634
63 feet Y = 3346156
09 meter
Z = 5253693
24 Z = 1573726
78
XDOT = -12228
256951 XDOT = -3660
293475
YDOT = -11396
441448 feet/sec YDOT = -3514
940823 meter/sec
ZDOT = -18747
868045 ZDOT = -5732
294455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6302377
39 X = -1920964
63
Y = -20766513
16 feet Y = -6329633
21 meter
Z = 5138816
12 Z = 1566311
15
XDOT = 12498
407779 XDOT = 3809
514691
YDOT = -8500
083373 feet/sec YDOT = -2590
825412 meter/sec
ZDOT = -18821
788163 ZDOT = -5736
881032
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 12342
53531506
00016717 00000-0 10270-3 0 9007
2 25544 51
6467 340
4075 0016560 13
4811 346
6780 15
51975226 4944
Satellite: ISS
Catalog Number: 25544
Epoch time: 12342
53531506 = yrday
fracday
Element set: 900
Inclination: 51
6467 deg
RA of node: 340
4075 deg
Eccentricity:
0016560
Arg of perigee: 13
4811 deg
Mean anomaly: 346
6780 deg
Mean motion: 15
51975226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 494
Checksum: 295
Coasting Arc #2 (Orbit 508)
---------------------------------------
Vector Time (GMT): 2012/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5881619
26 A = 6795329
10 meter
Y = -3309058
32 meter E =
0026560
Z = -654284
45 I = 51
52066
XDOT = 2847
095817 Wp = 26
17005
YDOT = 3904
096648 meter/sec RA = 335
05714 deg
ZDOT = 5964
185981 TA = 326
74914
MA = 326
91575
Ha = 229
348 n
mi
Hp = 214
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19296651
12 X = 5921363
12
Y = -10856490
54 feet Y = -3243064
13 meter
Z = -2146602
54 Z = -625615
00
XDOT = 9340
865542 XDOT = 2774
254720
YDOT = 12808
716037 feet/sec YDOT = 3935
527169 meter/sec
ZDOT = 19567
539308 ZDOT = 5977
840438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6174558
43 X = 1882005
41
Y = 21274324
72 feet Y = 6484414
18 meter
Z = -2027306
00 Z = -617922
87
XDOT = -13021
809152 XDOT = -3969
047430
YDOT = 5611
129137 feet/sec YDOT = 1710
272161 meter/sec
ZDOT = 19623
614974 ZDOT = 5981
277844
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 12343
50119315
00016717 00000-0 10270-3 0 9016
2 25544 51
6466 335
6093 0016364 17
3286 342
8421 15
52013976 5093
Satellite: ISS
Catalog Number: 25544
Epoch time: 12343
50119315 = yrday
fracday
Element set: 901
Inclination: 51
6466 deg
RA of node: 335
6093 deg
Eccentricity:
0016364
Arg of perigee: 17
3286 deg
Mean anomaly: 342
8421 deg
Mean motion: 15
52013976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 509
Checksum: 293
Coasting Arc #3 (Orbit 524)
---------------------------------------
Vector Time (GMT): 2012/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6030947
59 A = 6795430
16 meter
Y = 3120423
41 meter E =
0015229
Z = -380715
79 I = 51
49307
XDOT = -1904
135150 Wp = 61
12172
YDOT = -4387
674936 meter/sec RA = 330
08613 deg
ZDOT = -5973
504495 TA = 122
98047
MA = 122
83399
Ha = 229
551 n
mi
Hp = 213
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19786573
47 X = -6063543
12
Y = 10237609
61 feet Y = 3052799
35 meter
Z = -1249067
55 Z = -410093
35
XDOT = -6247
162567 XDOT = -1825
911320
YDOT = -14395
258978 feet/sec YDOT = -4408
530484 meter/sec
ZDOT = -19598
111860 ZDOT = -5982
565068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5835461
58 X = -1778648
69
Y = -21492889
86 feet Y = -6551032
83 meter
Z = -1371270
83 Z = -417963
35
XDOT = 13797
746962 XDOT = 4205
553274
YDOT = -2526
764900 feet/sec YDOT = -770
157942 meter/sec
ZDOT = -19635
076431 ZDOT = -5984
771296
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 12344
53145085
00016717 00000-0 10270-3 0 9024
2 25544 51
6459 330
4888 0016635 20
7303 339
4520 15
52001941 5258
Satellite: ISS
Catalog Number: 25544
Epoch time: 12344
53145085 = yrday
fracday
Element set: 902
Inclination: 51
6459 deg
RA of node: 330
4888 deg
Eccentricity:
0016635
Arg of perigee: 20
7303 deg
Mean anomaly: 339
4520 deg
Mean motion: 15
52001941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 525
Checksum: 286
Coasting Arc #4 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2012/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5990756
45 A = 6794567
80 meter
Y = -2866263
71 meter E =
0028728
Z = 1350020
31 I = 51
46439
XDOT = 1033
432492 Wp = 40
39198
YDOT = 4917
523486 meter/sec RA = 325
11390 deg
ZDOT = 5806
843439 TA = 334
36199
MA = 334
50415
Ha = 229
413 n
mi
Hp = 213
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19654712
75 X = 6015804
15
Y = -9403752
33 feet Y = -2799131
38 meter
Z = 4429200
48 Z = 1379184
25
XDOT = 3390
526547 XDOT = 950
158087
YDOT = 16133
607238 feet/sec YDOT = 4928
613914 meter/sec
ZDOT = 19051
323619 ZDOT = 5811
661997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5415459
07 X = 1650631
92
Y = 21078947
17 feet Y = 6424863
10 meter
Z = 4550483
17 Z = 1386987
27
XDOT = -14926
391208 XDOT = -4549
564040
YDOT = -315
092150 feet/sec YDOT = -96
040087 meter/sec
ZDOT = 19070
630192 ZDOT = 5812
728083
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 12345
56169403
00016717 00000-0 10270-3 0 9039
2 25544 51
6456 325
3700 0016390 24
5086 335
6841 15
52053183 5416
Satellite: ISS
Catalog Number: 25544
Epoch time: 12345
56169403 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 325
3700 deg
Eccentricity:
0016390
Arg of perigee: 24
5086 deg
Mean anomaly: 335
6841 deg
Mean motion: 15
52053183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 289
Coasting Arc #5 (Orbit 555)
---------------------------------------
Vector Time (GMT): 2012/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5885055
95 A = 6793045
37 meter
Y = 2494697
07 meter E =
0016055
Z = -2329418
36 I = 51
43491
XDOT = -180
560233 Wp = 47
26789
YDOT = -5435
586115 meter/sec RA = 320
13649 deg
ZDOT = -5378
133056 TA = 158
70257
MA = 158
63567
Ha = 229
700 n
mi
Hp = 213
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19307926
36 X = -5901198
82
Y = 8184701
68 feet Y = 2428796
68 meter
Z = -7642448
70 Z = -2358047
09
XDOT = -592
389215 XDOT = -93
638791
YDOT = -17833
287778 feet/sec YDOT = -5437
118682 meter/sec
ZDOT = -17644
793492 ZDOT = -5378
799662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4642187
51 X = -1414938
75
Y = -20405934
23 feet Y = -6219728
75 meter
Z = -7761464
25 Z = -2365694
30
XDOT = 16150
136624 XDOT = 4922
561643
YDOT = 3021
968225 feet/sec YDOT = 921
095915 meter/sec
ZDOT = -17646
817530 ZDOT = -5378
749983
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 12346
52753887
00016717 00000-0 10270-3 0 9042
2 25544 51
6457 320
5694 0016703 27
8841 332
3203 15
52037072 5560
Satellite: ISS
Catalog Number: 25544
Epoch time: 12346
52753887 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 320
5694 deg
Eccentricity:
0016703
Arg of perigee: 27
8841 deg
Mean anomaly: 332
3203 deg
Mean motion: 15
52037072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 556
Checksum: 306
Coasting Arc #6 (Orbit 571)
---------------------------------------
Vector Time (GMT): 2012/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5630237
93 A = 6790906
78 meter
Y = -2022317
71 meter E =
0025949
Z = 3177982
80 I = 51
40558
XDOT = -571
509681 Wp = 54
81573
YDOT = 5969
658561 meter/sec RA = 315
15598 deg
ZDOT = 4798
271500 TA = 342
07122
MA = 342
16259
Ha = 229
507 n
mi
Hp = 213
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18471909
23 X = 5636995
37
Y = -6634900
61 feet Y = -1959319
49 meter
Z = 10426452
76 Z = 3205350
70
XDOT = -1875
031763 XDOT = -661
530350
YDOT = 19585
493965 feet/sec YDOT = 5962
763635 meter/sec
ZDOT = 15742
360564 ZDOT = 4795
277204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3599213
21 X = 1097040
19
Y = 19232641
41 feet Y = 5862109
10 meter
Z = 10540181
33 Z = 3212647
27
XDOT = -17615
233705 XDOT = -5369
123233
YDOT = -5346
806404 feet/sec YDOT = -1629
706592 meter/sec
ZDOT = 15729
136264 ZDOT = 4794
240733
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 12347
55775767
00016717 00000-0 10270-3 0 9058
2 25544 51
6459 315
4504 0016469 31
4322 328
7810 15
52082491 5725
Satellite: ISS
Catalog Number: 25544
Epoch time: 12347
55775767 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 315
4504 deg
Eccentricity:
0016469
Arg of perigee: 31
4322 deg
Mean anomaly: 328
7810 deg
Mean motion: 15
52082491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 572
Checksum: 317
Coasting Arc #7 (Orbit 586)
---------------------------------------
Vector Time (GMT): 2012/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5346318
15 A = 6788616
82 meter
Y = 1432517
11 meter E =
0022490
Z = -3956939
74 I = 51
37738
XDOT = 1236
666549 Wp = 45
33518
YDOT = -6404
581191 meter/sec RA = 310
16880 deg
ZDOT = -3988
085877 TA = 182
77151
MA = 182
78400
Ha = 229
809 n
mi
Hp = 212
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17540413
89 X = -5342717
51
Y = 4699859
29 feet Y = 1372751
92 meter
Z = -12982085
77 Z = -3982903
09
XDOT = 4057
304951 XDOT = 1327
565311
YDOT = -21012
405481 feet/sec YDOT = -6390
243219 meter/sec
ZDOT = -13084
271251 ZDOT = -3981
858271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2149881
14 X = -655283
77
Y = -17953312
98 feet Y = -5472169
80 meter
Z = -13089916
42 Z = -3989806
53
XDOT = 18894
988284 XDOT = 5759
192429
YDOT = 7261
153401 feet/sec YDOT = 2213
199557 meter/sec
ZDOT = -13057
586270 ZDOT = -3979
952295
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 12348
52357904
00016717 00000-0 10270-3 0 9066
2 25544 51
6464 310
6499 0016711 34
9911 325
2335 15
52071071 5875
Satellite: ISS
Catalog Number: 25544
Epoch time: 12348
52357904 = yrday
fracday
Element set: 906
Inclination: 51
6464 deg
RA of node: 310
6499 deg
Eccentricity:
0016711
Arg of perigee: 34
9911 deg
Mean anomaly: 325
2335 deg
Mean motion: 15
52071071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 587
Checksum: 305
Coasting Arc #8 (Orbit 588)
---------------------------------------
Vector Time (GMT): 2012/348/14:35:50
544
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1275353
87 A = 6786025
83 meter
Y = 4552975
60 meter E =
0023733
Z = 4859653
92 I = 51
36564
XDOT = -5949
310043 Wp = 44
16266
YDOT = 4221
916839 meter/sec RA = 309
58580 deg
ZDOT = -2370
429406 TA = 69
26838
MA = 69
01420
Ha = 230
417 n
mi
Hp = 213
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4184231
86 X = 1200739
57
Y = 14937584
00 feet Y = 4566819
55 meter
Z = 15943746
47 Z = 4865668
95
XDOT = -19518
733737 XDOT = -5984
563184
YDOT = 13851
433199 feet/sec YDOT = 4155
191152 meter/sec
ZDOT = -7776
999364 ZDOT = -2399
416041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10732966
94 X = -3271408
32
Y = 11165415
85 feet Y = 3403218
75 meter
Z = 15968067
29 Z = 4867066
91
XDOT = -21058
516287 XDOT = -6418
635764
YDOT = -8836
854554 feet/sec YDOT = -2693
473268 meter/sec
ZDOT = -7897
741646 ZDOT = -2407
231654
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 12348
65236414
00016717 00000-0 10270-3 0 9073
2 25544 51
6481 310
0109 0017128 38
5888 321
6484 15
51815204 5892
Satellite: ISS
Catalog Number: 25544
Epoch time: 12348
65236414 = yrday
fracday
Element set: 907
Inclination: 51
6481 deg
RA of node: 310
0109 deg
Eccentricity:
0017128
Arg of perigee: 38
5888 deg
Mean anomaly: 321
6484 deg
Mean motion: 15
51815204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 589
Checksum: 309
Coasting Arc #9 (Orbit 603)
---------------------------------------
Vector Time (GMT): 2012/349/14:35:50
544
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -806720
51 A = 6787678
28 meter
Y = -5081827
66 meter E =
0022222
Z = -4438760
39 I = 51
35322
XDOT = 5793
598748 Wp = 64
43875
YDOT = -3771
073428 meter/sec RA = 304
59428 deg
ZDOT = 3286
755795 TA = 238
80512
MA = 239
02314
Ha = 230
454 n
mi
Hp = 212
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2646720
83 X = -728272
05
Y = -16672662
93 feet Y = -5090409
70 meter
Z = -14562862
19 Z = -4442489
51
XDOT = 19007
869908 XDOT = 5819
370817
YDOT = -12372
288151 feet/sec YDOT = -3706
142118 meter/sec
ZDOT = 10783
319537 ZDOT = 3314
962866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12819711
68 X = 3907448
12
Y = -10963901
82 feet Y = -3341797
28 meter
Z = -14577641
26 Z = -4443265
06
XDOT = 19699
321767 XDOT = 6004
353275
YDOT = 8637
219062 feet/sec YDOT = 2632
624370 meter/sec
ZDOT = 10900
771404 ZDOT = 3322
555124
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 12349
61833162
00016717 00000-0 10270-3 0 9084
2 25544 51
6487 305
2125 0017141 42
0948 318
1517 15
51832150 6049
Satellite: ISS
Catalog Number: 25544
Epoch time: 12349
61833162 = yrday
fracday
Element set: 908
Inclination: 51
6487 deg
RA of node: 305
2125 deg
Eccentricity:
0017141
Arg of perigee: 42
0948 deg
Mean anomaly: 318
1517 deg
Mean motion: 15
51832150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 604
Checksum: 287
Coasting Arc #10 (Orbit 619)
---------------------------------------
Vector Time (GMT): 2012/350/14:35:50
544
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 312299
49 A = 6789862
16 meter
Y = 5609410
52 meter E =
0027180
Z = 3803773
87 I = 51
34392
XDOT = -5617
434428 Wp = 60
31482
YDOT = 3155
806168 meter/sec RA = 299
60422 deg
ZDOT = -4156
979110 TA = 73
80089
MA = 73
50196
Ha = 230
526 n
mi
Hp = 212
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1024604
61 X = 231072
93
Y = 18403577
84 feet Y = 5612448
26 meter
Z = 12479573
07 Z = 3805094
34
XDOT = -18429
902979 XDOT = -5632
112298
YDOT = 10353
694776 feet/sec YDOT = 3092
906905 meter/sec
ZDOT = -13638
382907 ZDOT = -4184
303453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14955843
51 X = -4558541
10
Y = 10767828
53 feet Y = 3282034
14 meter
Z = 12484304
13 Z = 3805215
90
XDOT = -17855
763404 XDOT = -5442
436685
YDOT = -8720
627391 feet/sec YDOT = -2658
047229 meter/sec
ZDOT = -13752
093258 ZDOT = -4191
638025
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 12350
64868504
00016717 00000-0 10270-3 0 9098
2 25544 51
6486 300
0941 0017136 46
0256 314
2306 15
51842603 6202
Satellite: ISS
Catalog Number: 25544
Epoch time: 12350
64868504 = yrday
fracday
Element set: 909
Inclination: 51
6486 deg
RA of node: 300
0941 deg
Eccentricity:
0017136
Arg of perigee: 46
0256 deg
Mean anomaly: 314
2306 deg
Mean motion: 15
51842603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 620
Checksum: 284
Coasting Arc #11 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2012/351/14:35:50
544
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 21281
04 A = 6791769
27 meter
Y = -6034182
62 meter E =
0021282
Z = -3117332
62 I = 51
33703
XDOT = 5395
600420 Wp = 54
54229
YDOT = -2466
501701 meter/sec RA = 294
61651 deg
ZDOT = 4846
731309 TA = 269
45620
MA = 269
70006
Ha = 230
504 n
mi
Hp = 212
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 69819
69 X = 103898
12
Y = -19797187
07 feet Y = -6033482
42 meter
Z = -10227469
24 Z = -3117029
11
XDOT = 17702
101115 XDOT = 5399
236237
YDOT = -8092
197182 feet/sec YDOT = -2406
144830 meter/sec
ZDOT = 15901
349439 ZDOT = 4872
951265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16527437
40 X = 5037562
92
Y = -10900421
40 feet Y = -3322448
44 meter
Z = -10225421
46 Z = -3116708
46
XDOT = 15719
986561 XDOT = 4791
451904
YDOT = 8925
341528 feet/sec YDOT = 2720
444098 meter/sec
ZDOT = 16010
389023 ZDOT = 4879
966574
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 12351
61462925
00016717 00000-0 10270-3 0 9105
2 25544 51
6492 295
2958 0017121 49
4277 310
8361 15
51876100 6354
Satellite: ISS
Catalog Number: 25544
Epoch time: 12351
61462925 = yrday
fracday
Element set: 910
Inclination: 51
6492 deg
RA of node: 295
2958 deg
Eccentricity:
0017121
Arg of perigee: 49
4277 deg
Mean anomaly: 310
8361 deg
Mean motion: 15
51876100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 303
Coasting Arc #12 (Orbit 650)
---------------------------------------
Vector Time (GMT): 2012/352/14:35:50
544
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -382297
91 A = 6793801
09 meter
Y = 6399345
47 meter E =
0027482
Z = 2236581
19 I = 51
33148
XDOT = -5176
842892 Wp = 77
57048
YDOT = 1606
369138 meter/sec RA = 289
63070 deg
ZDOT = -5418
664358 TA = 77
47497
MA = 77
16769
Ha = 230
586 n
mi
Hp = 212
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1254258
22 X = -464693
03
Y = 20995227
92 feet Y = 6394609
52 meter
Z = 7337864
80 Z = 2234524
33
XDOT = -16984
392691 XDOT = -5168
098476
YDOT = 5270
239955 feet/sec YDOT = 1548
527708 meter/sec
ZDOT = -17777
770203 ZDOT = -5443
791661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17986804
11 X = -5482377
89
Y = 10908016
63 feet Y = 3324763
47 meter
Z = 7328510
75 Z = 2233730
08
XDOT = -13157
282674 XDOT = -4010
339759
YDOT = -9543
988812 feet/sec YDOT = -2909
007790 meter/sec
ZDOT = -17882
166343 ZDOT = -5450
484301
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 12352
64495842
00016717 00000-0 10270-3 0 9114
2 25544 51
6488 290
1769 0017113 53
3975 306
8748 15
51869621 6515
Satellite: ISS
Catalog Number: 25544
Epoch time: 12352
64495842 = yrday
fracday
Element set: 911
Inclination: 51
6488 deg
RA of node: 290
1769 deg
Eccentricity:
0017113
Arg of perigee: 53
3975 deg
Mean anomaly: 306
8748 deg
Mean motion: 15
51869621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 651
Checksum: 333
Coasting Arc #13 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2012/353/14:35:50
544
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 598678
42 A = 6794988
81 meter
Y = -6621332
41 meter E =
0025465
Z = -1368128
54 I = 51
32696
XDOT = 4977
232818 Wp = 50
08704
YDOT = -727
516131 meter/sec RA = 284
64659 deg
ZDOT = 5786
677765 TA = 294
95132
MA = 295
21569
Ha = 230
528 n
mi
Hp = 212
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1964168
06 X = 679321
08
Y = -21723531
53 feet Y = -6614186
64 meter
Z = -4488610
71 Z = -1365024
69
XDOT = 16329
503996 XDOT = 4956
887952
YDOT = -2386
863946 feet/sec YDOT = -671
971666 meter/sec
ZDOT = 18985
163272 ZDOT = 5810
807320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18791972
55 X = 5727793
23
Y = -11079461
29 feet Y = -3377019
80 meter
Z = -4474897
74 Z = -1363948
83
XDOT = 10602
585023 XDOT = 3231
667915
YDOT = 10391
361019 feet/sec YDOT = 3167
286839 meter/sec
ZDOT = 19085
309251 ZDOT = 5817
202260
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 12353
61087941
00016717 00000-0 10270-3 0 9120
2 25544 51
6491 285
3785 0017082 56
5198 303
7584 15
51912033 6666
Satellite: ISS
Catalog Number: 25544
Epoch time: 12353
61087941 = yrday
fracday
Element set: 912
Inclination: 51
6491 deg
RA of node: 285
3785 deg
Eccentricity:
0017082
Arg of perigee: 56
5198 deg
Mean anomaly: 303
7584 deg
Mean motion: 15
51912033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 666
Checksum: 320
Coasting Arc #14 (Orbit 681)
---------------------------------------
Vector Time (GMT): 2012/354/14:35:50
544
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -861677
17 A = 6795781
98 meter
Y = 6730710
90 meter E =
0024388
Z = 350252
26 I = 51
32244
XDOT = -4795
947640 Wp = 89
89789
YDOT = -284
719896 meter/sec RA = 279
66353 deg
ZDOT = -5965
821385 TA = 86
31612
MA = 86
03726
Ha = 230
598 n
mi
Hp = 212
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2827024
83 X = -938578
79
Y = 22082384
86 feet Y = 6720645
09 meter
Z = 1149121
58 Z = 345879
81
XDOT = -15734
736351 XDOT = -4763
426900
YDOT = -934
120393 feet/sec YDOT = -338
169067 meter/sec
ZDOT = -19572
904808 ZDOT = -5989
040811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19389908
52 X = -5910044
12
Y = 10940680
63 feet Y = 3334719
46 meter
Z = 1130144
07 Z = 344467
91
XDOT = -7794
249084 XDOT = -2375
687121
YDOT = -11657
187619 feet/sec YDOT = -3553
110786 meter/sec
ZDOT = -19669
149727 ZDOT = -5995
156837
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 12354
64118449
00016717 00000-0 10270-3 0 9133
2 25544 51
6489 280
2592 0017017 60
6793 299
6057 15
51892664 6821
Satellite: ISS
Catalog Number: 25544
Epoch time: 12354
64118449 = yrday
fracday
Element set: 913
Inclination: 51
6489 deg
RA of node: 280
2592 deg
Eccentricity:
0017017
Arg of perigee: 60
6793 deg
Mean anomaly: 299
6057 deg
Mean motion: 15
51892664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 682
Checksum: 338
Coasting Arc #15 (Orbit 697)
---------------------------------------
Vector Time (GMT): 2012/355/14:35:50
544
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1018274
99 A = 6795551
48 meter
Y = -6680348
56 meter E =
0029951
Z = 586793
29 I = 51
31797
XDOT = 4678
048531 Wp = 58
20617
YDOT = 1254
131078 meter/sec RA = 274
68015 deg
ZDOT = 5951
240104 TA = 308
15650
MA = 308
42600
Ha = 230
531 n
mi
Hp = 212
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3340797
20 X = 1090049
86
Y = -21917154
07 feet Y = -6668560
29 meter
Z = 1925174
82 Z = 591914
03
XDOT = 15347
928251 XDOT = 4634
767145
YDOT = 4114
603274 feet/sec YDOT = 1306
201654 meter/sec
ZDOT = 19525
065957 ZDOT = 5973
860757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19370844
17 X = 5904233
30
Y = -10779958
93 feet Y = -3285731
48 meter
Z = 1947241
12 Z = 593519
09
XDOT = 5277
638930 XDOT = 1608
624346
YDOT = 13149
548364 feet/sec YDOT = 4007
982341 meter/sec
ZDOT = 19618
709139 ZDOT = 5979
782546
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 12355
67147563
00016717 00000-0 10270-3 0 9147
2 25544 51
6490 275
1404 0017041 63
7242 296
5658 15
51942988 6983
Satellite: ISS
Catalog Number: 25544
Epoch time: 12355
67147563 = yrday
fracday
Element set: 914
Inclination: 51
6490 deg
RA of node: 275
1404 deg
Eccentricity:
0017041
Arg of perigee: 63
7242 deg
Mean anomaly: 296
5658 deg
Mean motion: 15
51942988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 698
Checksum: 334
Coasting Arc #16 (Orbit 712)
---------------------------------------
Vector Time (GMT): 2012/356/14:35:50
544
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1251730
48 A = 6794620
96 meter
Y = 6486835
29 meter E =
0020474
Z = -1606107
57 I = 51
31323
XDOT = -4575
074493 Wp = 89
46218
YDOT = -2278
045113 meter/sec RA = 269
69604 deg
ZDOT = -5698
157419 TA = 108
15378
MA = 107
93074
Ha = 230
553 n
mi
Hp = 212
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4106727
29 X = -1316372
49
Y = 21282268
00 feet Y = 6472476
31 meter
Z = -5269381
78 Z = -1612345
07
XDOT = -15010
086918 XDOT = -4521
580491
YDOT = -7473
901288 feet/sec YDOT = -2328
907033 meter/sec
ZDOT = -18694
742189 ZDOT = -5720
253143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19153221
25 X = -5837901
84
Y = 10132744
21 feet Y = 3088460
44 meter
Z = -5296049
00 Z = -1614235
73
XDOT = -2745
315236 XDOT = -836
772084
YDOT = -14900
520563 feet/sec YDOT = -4541
678668 meter/sec
ZDOT = -18786
085756 ZDOT = -5725
998938
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 12356
63736384
00016717 00000-0 10270-3 0 9150
2 25544 51
6489 270
3410 0016882 67
6267 292
6672 15
51927815 7130
Satellite: ISS
Catalog Number: 25544
Epoch time: 12356
63736384 = yrday
fracday
Element set: 915
Inclination: 51
6489 deg
RA of node: 270
3410 deg
Eccentricity:
0016882
Arg of perigee: 67
6267 deg
Mean anomaly: 292
6672 deg
Mean motion: 15
51927815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 713
Checksum: 334
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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