[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 14th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
228/16:15:37
620 -4
5 9
4 9
4
N/A -5
5 0
2 225
2
000/00:31:11
240 6
2 -0
1 217
2
Coasting Arc #1 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2012/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5058466
79 A = 6778357
92 meter
Y = -1098965
46 meter E =
0010615
Z = 4370635
06 I = 51
45085
XDOT = 4132
439665 Wp = 63
77041
YDOT = 5505
896660 meter/sec RA = 210
02574 deg
ZDOT = -3387
367936 TA = 60
65174
MA = 60
54575
Ha = 219
730 n
mi
Hp = 212
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16596019
66 X = 5049148
32
Y = -3605529
72 feet Y = -1042450
80 meter
Z = 14339353
87 Z = 4395185
98
XDOT = 13557
872918 XDOT = 4087
019389
YDOT = 18063
965420 feet/sec YDOT = 5551
854330 meter/sec
ZDOT = -11113
411862 ZDOT = -3367
403029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14761539
70 X = -4499317
30
Y = -8222258
75 feet Y = -2506144
47 meter
Z = 14440782
16 Z = 4401550
40
XDOT = 1139
160306 XDOT = 347
216061
YDOT = -21482
695522 feet/sec YDOT = -6547
925595 meter/sec
ZDOT = -11031
473458 ZDOT = -3362
393110
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 12223
54215855
00016717 00000-0 10270-3 0 9002
2 25544 51
6375 210
8803 0001717 22
9917 337
1313 15
55070907 26476
Satellite: ISS
Catalog Number: 25544
Epoch time: 12223
54215855 = yrday
fracday
Element set: 900
Inclination: 51
6375 deg
RA of node: 210
8803 deg
Eccentricity:
0001717
Arg of perigee: 22
9917 deg
Mean anomaly: 337
1313 deg
Mean motion: 15
55070907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 292
Coasting Arc #2 (Orbit 2661)
---------------------------------------
Vector Time (GMT): 2012/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6103115
60 A = 6782805
74 meter
Y = -259953
93 meter E =
0006049
Z = -2948352
77 I = 51
49240
XDOT = -2175
632767 Wp = 58
27473
YDOT = -5397
162314 meter/sec RA = 205
02209 deg
ZDOT = 4990
103835 TA = 267
98201
MA = 268
05129
Ha = 219
870 n
mi
Hp = 212
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20023345
13 X = -6085432
85
Y = -852867
23 feet Y = -328103
77 meter
Z = -9673073
40 Z = -2977958
19
XDOT = -7137
902778 XDOT = -2139
359436
YDOT = -17707
225439 feet/sec YDOT = -5421
288990 meter/sec
ZDOT = 16371
731742 ZDOT = 4979
622692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14638214
76 X = 4461727
86
Y = 13601675
41 feet Y = 4145790
66 meter
Z = -9795262
96 Z = -2985596
15
XDOT = -4987
784060 XDOT = -1520
276582
YDOT = 17102
302941 feet/sec YDOT = 5212
781936 meter/sec
ZDOT = 16328
921380 ZDOT = 4977
055237
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 12224
50610178
00016717 00000-0 10270-3 0 9017
2 25544 51
6372 206
0680 0001810 29
6470 330
4786 15
55070456 26621
Satellite: ISS
Catalog Number: 25544
Epoch time: 12224
50610178 = yrday
fracday
Element set: 901
Inclination: 51
6372 deg
RA of node: 206
0680 deg
Eccentricity:
0001810
Arg of perigee: 29
6470 deg
Mean anomaly: 330
4786 deg
Mean motion: 15
55070456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2662
Checksum: 282
Coasting Arc #3 (Orbit 2677)
---------------------------------------
Vector Time (GMT): 2012/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6530191
96 A = 6785938
64 meter
Y = 1489470
07 meter E =
0013615
Z = 1054170
92 I = 51
53136
XDOT = -162
983044 Wp = 115
67319
YDOT = 4917
306379 meter/sec RA = 200
03251 deg
ZDOT = -5884
683106 TA = 52
87315
MA = 52
74884
Ha = 219
835 n
mi
Hp = 212
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21424514
31 X = 6507930
20
Y = 4886712
83 feet Y = 1562370
22 meter
Z = 3458566
00 Z = 1085839
89
XDOT = -534
721273 XDOT = -189
371167
YDOT = 16132
894943 feet/sec YDOT = 4915
336528 meter/sec
ZDOT = -19306
703103 ZDOT = -5885
538729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13417414
10 X = -4089627
82
Y = -17376483
83 feet Y = -5296352
27 meter
Z = 3589186
95 Z = 1093984
18
XDOT = 9307
788307 XDOT = 2837
013876
YDOT = -11210
734754 feet/sec YDOT = -3417
031953 meter/sec
ZDOT = -19310
648325 ZDOT = -5885
885610
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 12225
53429266
00016717 00000-0 10270-3 0 9028
2 25544 51
6372 200
9335 0001864 28
4207 331
7048 15
55121316 26789
Satellite: ISS
Catalog Number: 25544
Epoch time: 12225
53429266 = yrday
fracday
Element set: 902
Inclination: 51
6372 deg
RA of node: 200
9335 deg
Eccentricity:
0001864
Arg of perigee: 28
4207 deg
Mean anomaly: 331
7048 deg
Mean motion: 15
55121316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2678
Checksum: 291
Coasting Arc #4 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2012/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6237456
86 A = 6785955
06 meter
Y = -2471475
13 meter E =
0015067
Z = 966217
26 I = 51
56047
XDOT = 2573
648859 Wp = 53
46907
YDOT = -4163
931375 meter/sec RA = 195
05148 deg
ZDOT = 5908
199599 TA = 317
01631
MA = 317
13393
Ha = 219
783 n
mi
Hp = 212
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20464097
30 X = -6214050
32
Y = -8108514
22 feet Y = -2541095
42 meter
Z = 3170004
13 Z = 935973
19
XDOT = 8443
729851 XDOT = 2591
319269
YDOT = -13661
192174 feet/sec YDOT = -4135
052690 meter/sec
ZDOT = 19383
856953 ZDOT = 5920
744814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10989804
16 X = 3349692
31
Y = 19092573
74 feet Y = 5819416
48 meter
Z = 3045330
76 Z = 928216
82
XDOT = -13624
457072 XDOT = -4152
734516
YDOT = 4712
126558 feet/sec YDOT = 1436
256175 meter/sec
ZDOT = 19436
003572 ZDOT = 5924
093889
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 12226
56246733
00016717 00000-0 10270-3 0 9039
2 25544 51
6370 195
8000 0001649 36
9333 323
1934 15
55165613 26948
Satellite: ISS
Catalog Number: 25544
Epoch time: 12226
56246733 = yrday
fracday
Element set: 903
Inclination: 51
6370 deg
RA of node: 195
8000 deg
Eccentricity:
0001649
Arg of perigee: 36
9333 deg
Mean anomaly: 323
1934 deg
Mean motion: 15
55165613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2694
Checksum: 301
Coasting Arc #5 (Orbit 2708)
---------------------------------------
Vector Time (GMT): 2012/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5207528
89 A = 6782868
98 meter
Y = 3250948
85 meter E =
0005213
Z = -2888114
52 I = 51
58055
XDOT = -4796
231921 Wp = 97
03343
YDOT = 3210
572560 meter/sec RA = 190
06635 deg
ZDOT = -5042
564775 TA = 115
87797
MA = 115
82421
Ha = 219
854 n
mi
Hp = 212
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17085068
54 X = 5184818
62
Y = 10665842
69 feet Y = 3309055
79 meter
Z = -9475441
34 Z = -2862872
10
XDOT = -15735
669033 XDOT = -4807
281552
YDOT = 10533
374541 feet/sec YDOT = 3156
876498 meter/sec
ZDOT = -16543
847687 ZDOT = -5065
890955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7109917
00 X = -2167102
70
Y = -18896253
70 feet Y = -5759578
13 meter
Z = -9371469
05 Z = -2856423
77
XDOT = 17437
316810 XDOT = 5314
894164
YDOT = 1677
840619 feet/sec YDOT = 511
405821 meter/sec
ZDOT = -16640
439888 ZDOT = -5072
006078
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 12227
52636940
00016717 00000-0 10270-3 0 9040
2 25544 51
6377 190
9864 0001870 34
5287 325
5987 15
55159515 27092
Satellite: ISS
Catalog Number: 25544
Epoch time: 12227
52636940 = yrday
fracday
Element set: 904
Inclination: 51
6377 deg
RA of node: 190
9864 deg
Eccentricity:
0001870
Arg of perigee: 34
5287 deg
Mean anomaly: 325
5987 deg
Mean motion: 15
55159515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2709
Checksum: 336
Coasting Arc #6 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2012/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3555311
65 A = 6778205
77 meter
Y = -3779791
83 meter E =
0010286
Z = 4353147
07 I = 51
59617
XDOT = 6513
166268 Wp = 99
87476
YDOT = -2157
566543 meter/sec RA = 185
07110 deg
ZDOT = 3437
410283 TA = 315
22308
MA = 315
30606
Ha = 219
781 n
mi
Hp = 212
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11664408
31 X = -3533927
17
Y = -12400891
83 feet Y = -3819430
03 meter
Z = 14281978
57 Z = 4335927
77
XDOT = 21368
655736 XDOT = 6520
110731
YDOT = -7078
630390 feet/sec YDOT = -2084
693491 meter/sec
ZDOT = 11277
592791 ZDOT = 3469
067134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2068555
14 X = 630495
61
Y = 16958159
66 feet Y = 5168847
07 meter
Z = 14211169
96 Z = 4331564
60
XDOT = -20094
161003 XDOT = -6124
700274
YDOT = -7133
292605 feet/sec YDOT = -2174
227586 meter/sec
ZDOT = 11408
514451 ZDOT = 3477
315205
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 12228
55451362
00016717 00000-0 10270-3 0 9058
2 25544 51
6382 185
8530 0001653 35
9610 324
1654 15
55211114 27253
Satellite: ISS
Catalog Number: 25544
Epoch time: 12228
55451362 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 185
8530 deg
Eccentricity:
0001653
Arg of perigee: 35
9610 deg
Mean anomaly: 324
1654 deg
Mean motion: 15
55211114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2725
Checksum: 285
Coasting Arc #7 (Orbit 2727)
---------------------------------------
Vector Time (GMT): 2012/228/16:31:13
240
Vector Time (MET): N/A
Weight (LBS) : 953367
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5689465
78 A = 6790998
66 meter
Y = -2536784
58 meter E =
0015698
Z = 2677479
47 I = 51
62103
XDOT = 4152
818573 Wp = 37
66974
YDOT = -3825
871529 meter/sec RA = 184
12901 deg
ZDOT = 5195
697105 TA = 352
57725
MA = 352
60046
Ha = 225
186 n
mi
Hp = 217
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18666226
30 X = -5673682
39
Y = -8322784
07 feet Y = -2600319
51 meter
Z = 8784381
46 Z = 2649879
18
XDOT = 13624
732852 XDOT = 4170
052615
YDOT = -12552
071946 feet/sec YDOT = -3779
335826 meter/sec
ZDOT = 17046
250344 ZDOT = 5215
912707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20310213
82 X = 6190553
17
Y = -2679199
48 feet Y = -816620
00 meter
Z = 8670594
05 Z = 2642797
07
XDOT = -5170
551160 XDOT = -1575
983993
YDOT = 16283
281379 feet/sec YDOT = 4963
144164 meter/sec
ZDOT = 17130
056019 ZDOT = 5221
241075
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 12228
74739941
00016717 00000-0 10270-3 0 9062
2 25544 51
6406 184
8918 0010271 338
8416 21
2310 15
52538308 27285
Satellite: ISS
Catalog Number: 25544
Epoch time: 12228
74739941 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 184
8918 deg
Eccentricity:
0010271
Arg of perigee: 338
8416 deg
Mean anomaly: 21
2310 deg
Mean motion: 15
52538308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 311
Coasting Arc #8 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2012/229/16:31:13
240
Vector Time (MET): N/A
Weight (LBS) : 953367
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4998986
25 A = 6788364
80 meter
Y = 2810356
14 meter E =
0010632
Z = -3643763
99 I = 51
64337
XDOT = -5187
461932 Wp = 11
12104
YDOT = 3540
959523 meter/sec RA = 179
15789 deg
ZDOT = -4377
708456 TA = 212
02746
MA = 212
09212
Ha = 225
177 n
mi
Hp = 217
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16400873
51 X = 4984888
94
Y = 9220328
53 feet Y = 2866179
04 meter
Z = -11954606
27 Z = -3619513
94
XDOT = -17019
232059 XDOT = -5205
406661
YDOT = 11617
321271 feet/sec YDOT = 3482
849709 meter/sec
ZDOT = -14362
560551 ZDOT = -4402
952005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18848013
09 X = -5744874
39
Y = 1065386
74 feet Y = 324729
88 meter
Z = -11854664
69 Z = -3613301
80
XDOT = 8125
954023 XDOT = 2476
790786
YDOT = -17515
459398 feet/sec YDOT = -5338
712025 meter/sec
ZDOT = -14467
117672 ZDOT = -4409
577467
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 12229
71290233
00016717 00000-0 10270-3 0 9077
2 25544 51
6411 180
0898 0010277 341
0187 19
0580 15
52565154 27433
Satellite: ISS
Catalog Number: 25544
Epoch time: 12229
71290233 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 180
0898 deg
Eccentricity:
0010277
Arg of perigee: 341
0187 deg
Mean anomaly: 19
0580 deg
Mean motion: 15
52565154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 294
Coasting Arc #9 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2012/230/16:31:13
240
Vector Time (MET): N/A
Weight (LBS) : 953367
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4101655
24 A = 6785628
71 meter
Y = -3096481
03 meter E =
0009296
Z = 4421496
47 I = 51
66516
XDOT = 6076
503465 Wp = 43
18905
YDOT = -3277
221568 meter/sec RA = 174
18285 deg
ZDOT = 3344
293368 TA = 13
05878
MA = 13
03473
Ha = 225
410 n
mi
Hp = 216
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13456874
13 X = -4088203
11
Y = -10159058
51 feet Y = -3142272
93 meter
Z = 14506222
00 Z = 4401603
99
XDOT = 19936
034990 XDOT = 6096
452915
YDOT = -10752
039264 feet/sec YDOT = -3209
158665 meter/sec
ZDOT = 10972
091103 ZDOT = 3373
860729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16901130
68 X = 5151464
63
Y = 1007951
64 feet Y = 307223
66 meter
Z = 14424292
81 Z = 4396524
45
XDOT = -10576
340183 XDOT = -3223
668488
YDOT = 18690
693827 feet/sec YDOT = 5696
923478 meter/sec
ZDOT = 11094
496345 ZDOT = 3381
602486
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 12230
74276005
00016717 00000-0 10270-3 0 9084
2 25544 51
6415 174
9668 0010300 345
8859 14
2004 15
52582075 27595
Satellite: ISS
Catalog Number: 25544
Epoch time: 12230
74276005 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 174
9668 deg
Eccentricity:
0010300
Arg of perigee: 345
8859 deg
Mean anomaly: 14
2004 deg
Mean motion: 15
52582075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 303
Coasting Arc #10 (Orbit 2773)
---------------------------------------
Vector Time (GMT): 2012/231/16:31:13
240
Vector Time (MET): N/A
Weight (LBS) : 953367
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3106782
43 A = 6783288
04 meter
Y = 3415308
77 meter E =
0016751
Z = -4982574
60 I = 51
68771
XDOT = -6716
928187 Wp = 36
32821
YDOT = 2992
091683 meter/sec RA = 169
20549 deg
ZDOT = -2127
770566 TA = 212
87192
MA = 212
97622
Ha = 225
394 n
mi
Hp = 216
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10192855
74 X = 3092564
65
Y = 11205081
26 feet Y = 3449970
99 meter
Z = -16347029
54 Z = -4967516
96
XDOT = -22037
165969 XDOT = -6739
551103
YDOT = 9816
573762 feet/sec YDOT = 2916
852208 meter/sec
ZDOT = -6980
874562 ZDOT = -2160
455652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14824922
59 X = -4518636
40
Y = -3419207
60 feet Y = -1042174
48 meter
Z = -16285091
91 Z = -4963696
01
XDOT = 12338
070240 XDOT = 3760
643809
YDOT = -19453
120313 feet/sec YDOT = -5929
311071 meter/sec
ZDOT = -7116
146216 ZDOT = -2169
001367
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 12231
70823648
00016717 00000-0 10270-3 0 9093
2 25544 51
6412 170
1644 0010382 348
3668 11
7243 15
52631688 27749
Satellite: ISS
Catalog Number: 25544
Epoch time: 12231
70823648 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 170
1644 deg
Eccentricity:
0010382
Arg of perigee: 348
3668 deg
Mean anomaly: 11
7243 deg
Mean motion: 15
52631688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2774
Checksum: 306
Coasting Arc #11 (Orbit 2789)
---------------------------------------
Vector Time (GMT): 2012/232/16:31:13
240
Vector Time (MET): N/A
Weight (LBS) : 953367
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1978342
36 A = 6781920
44 meter
Y = -3769656
81 meter E =
0008724
Z = 5276936
49 I = 51
71325
XDOT = 7148
042992 Wp = 10
08128
YDOT = -2663
386680 meter/sec RA = 164
22625 deg
ZDOT = 785
392285 TA = 72
46886
MA = 72
37355
Ha = 225
513 n
mi
Hp = 216
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6490624
55 X = -1961676
09
Y = -12367640
47 feet Y = -3791686
36 meter
Z = 17312783
74 Z = 5267366
62
XDOT = 23451
584621 XDOT = 7173
479064
YDOT = -8738
145277 feet/sec YDOT = -2583
310545 meter/sec
ZDOT = 2576
746341 ZDOT = 820
178655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12543429
86 X = 3823237
42
Y = 6253502
42 feet Y = 1906067
54 meter
Z = 17273543
17 Z = 5264975
96
XDOT = -13575
751110 XDOT = -4137
888938
YDOT = 19789
886147 feet/sec YDOT = 6031
957297 meter/sec
ZDOT = 2720
683360 ZDOT = 829
264288
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 12232
73806570
00016717 00000-0 10270-3 0 9104
2 25544 51
6415 165
0417 0010305 352
4491 7
6504 15
52635214 27909
Satellite: ISS
Catalog Number: 25544
Epoch time: 12232
73806570 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 165
0417 deg
Eccentricity:
0010305
Arg of perigee: 352
4491 deg
Mean anomaly: 7
6504 deg
Mean motion: 15
52635214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2790
Checksum: 277
Coasting Arc #12 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2012/233/16:31:13
240
Vector Time (MET): N/A
Weight (LBS) : 953367
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 867689
58 A = 6781677
64 meter
Y = 4146598
35 meter E =
0016641
Z = -5306891
81 I = 51
74072
XDOT = -7289
959170 Wp = 56
66576
YDOT = 2265
840880 meter/sec RA = 159
24700 deg
ZDOT = 588
763926 TA = 218
89425
MA = 219
01410
Ha = 225
553 n
mi
Hp = 216
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2846750
57 X = 847036
44
Y = 13604325
29 feet Y = 4156185
59 meter
Z = -17411062
38 Z = -5302727
07
XDOT = -23917
188879 XDOT = -7317
614523
YDOT = 7433
861155 feet/sec YDOT = 2184
165425 meter/sec
ZDOT = 1931
640176 ZDOT = 553
282618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10451247
78 X = -3185540
32
Y = -9194591
84 feet Y = -2802511
59 meter
Z = -17394184
36 Z = -5301747
39
XDOT = 14173
979435 XDOT = 4320
228932
YDOT = -19424
060640 feet/sec YDOT = -5920
453683 meter/sec
ZDOT = 1784
852405 ZDOT = 544
023013
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 12233
70351598
00016717 00000-0 10270-3 0 9118
2 25544 51
6403 160
2384 0010354 355
4112 4
6944 15
52678190 28055
Satellite: ISS
Catalog Number: 25544
Epoch time: 12233
70351598 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 160
2384 deg
Eccentricity:
0010354
Arg of perigee: 355
4112 deg
Mean anomaly: 4
6944 deg
Mean motion: 15
52678190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 287
Coasting Arc #13 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2012/234/16:31:13
240
Vector Time (MET): N/A
Weight (LBS) : 953367
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 282557
44 A = 6782747
14 meter
Y = -4537503
66 meter E =
0014248
Z = 5033654
80 I = 51
77272
XDOT = 7199
716194 Wp = 18
71245
YDOT = -1749
796692 meter/sec RA = 154
27091 deg
ZDOT = -1966
753629 TA = 90
43130
MA = 90
26804
Ha = 225
578 n
mi
Hp = 215
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 927025
73 X = 308823
50
Y = -14886823
04 feet Y = -4534196
80 meter
Z = 16514615
48 Z = 5035091
48
XDOT = 23621
116123 XDOT = 7228
301684
YDOT = -5740
802794 feet/sec YDOT = -1669
125256 meter/sec
ZDOT = -6452
603771 ZDOT = -1931
708369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8384438
64 X = 2555576
90
Y = 12327605
91 feet Y = 3757454
28 meter
Z = 16520917
72 Z = 5035575
72
XDOT = -14410
928814 XDOT = -4392
451102
YDOT = 18319
298307 feet/sec YDOT = 5583
722124 meter/sec
ZDOT = -6307
646823 ZDOT = -1922
570752
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 12234
73331534
00016717 00000-0 10270-3 0 9121
2 25544 51
6404 155
1156 0010329 358
6521 1
4601 15
52700134 28214
Satellite: ISS
Catalog Number: 25544
Epoch time: 12234
73331534 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 155
1156 deg
Eccentricity:
0010329
Arg of perigee: 358
6521 deg
Mean anomaly: 1
4601 deg
Mean motion: 15
52700134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 259
Coasting Arc #14 (Orbit 2835)
---------------------------------------
Vector Time (GMT): 2012/235/16:31:13
240
Vector Time (MET): N/A
Weight (LBS) : 953367
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1300533
06 A = 6784802
88 meter
Y = 4901147
55 meter E =
0011732
Z = -4512349
64 I = 51
80514
XDOT = -6860
766304 Wp = 54
24767
YDOT = 1129
953046 meter/sec RA = 149
29887 deg
ZDOT = 3217
238892 TA = 247
98761
MA = 248
11229
Ha = 225
677 n
mi
Hp = 215
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4266840
76 X = -1333322
12
Y = 16079880
42 feet Y = 4886420
69 meter
Z = -14804296
72 Z = -4518747
37
XDOT = -22509
075800 XDOT = -6888
520348
YDOT = 3707
195033 feet/sec YDOT = 1053
076618 meter/sec
ZDOT = 10555
245709 ZDOT = 3183
842222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6709927
65 X = -2045185
95
Y = -15197037
30 feet Y = -4632056
97 meter
Z = -14831136
63 Z = -4520530
45
XDOT = 14284
293768 XDOT = 4353
852740
YDOT = -16433
169126 feet/sec YDOT = -5008
829949 meter/sec
ZDOT = 10417
138259 ZDOT = 3175
143741
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 12235
69873959
00016717 00000-0 10270-3 0 9130
2 25544 51
6388 150
3117 0010296 2
3081 357
8117 15
52711679 28368
Satellite: ISS
Catalog Number: 25544
Epoch time: 12235
69873959 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 150
3117 deg
Eccentricity:
0010296
Arg of perigee: 2
3081 deg
Mean anomaly: 357
8117 deg
Mean motion: 15
52711679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2836
Checksum: 322
Coasting Arc #15 (Orbit 2851)
---------------------------------------
Vector Time (GMT): 2012/236/16:31:13
240
Vector Time (MET): N/A
Weight (LBS) : 953367
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2269480
19 A = 6787449
54 meter
Y = -5213275
85 meter E =
0016997
Z = 3706099
49 I = 51
84034
XDOT = 6314
774265 Wp = 47
93498
YDOT = -345
211070 meter/sec RA = 144
33413 deg
ZDOT = -4328
696368 TA = 88
08015
MA = 87
88549
Ha = 225
690 n
mi
Hp = 215
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7445801
14 X = 2309604
08
Y = -17103923
39 feet Y = -5187672
71 meter
Z = 12159119
05 Z = 3717222
03
XDOT = 20717
763337 XDOT = 6339
192941
YDOT = -1132
582251 feet/sec YDOT = -274
458864 meter/sec
ZDOT = -14201
759737 ZDOT = -4297
960229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5149935
14 X = 1569700
23
Y = 17897813
58 feet Y = 5455253
58 meter
Z = 12205521
82 Z = 3720243
05
XDOT = -14059
352583 XDOT = -4285
290667
YDOT = 13696
916195 feet/sec YDOT = 4174
820056 meter/sec
ZDOT = -14074
698551 ZDOT = -4289
968118
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 12236
72850912
00016717 00000-0 10270-3 0 9140
2 25544 51
6391 145
1884 0010373 5
1648 354
9609 15
52763275 28522
Satellite: ISS
Catalog Number: 25544
Epoch time: 12236
72850912 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 145
1884 deg
Eccentricity:
0010373
Arg of perigee: 5
1648 deg
Mean anomaly: 354
9609 deg
Mean motion: 15
52763275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2852
Checksum: 316
Coasting Arc #16 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2012/237/16:31:13
240
Vector Time (MET): N/A
Weight (LBS) : 953367
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3029226
82 A = 6790138
88 meter
Y = 5422328
45 meter E =
0013861
Z = -2730530
73 I = 51
87190
XDOT = -5622
062807 Wp = 24
81713
YDOT = -540
199125 meter/sec RA = 139
37540 deg
ZDOT = 5186
102694 TA = 304
41185
MA = 304
54282
Ha = 225
781 n
mi
Hp = 215
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9938408
19 X = -3076371
03
Y = 17789791
49 feet Y = 5388190
16 meter
Z = -8958434
14 Z = -2745361
00
XDOT = -18445
087948 XDOT = -5640
797149
YDOT = -1772
306840 feet/sec YDOT = -603
173300 meter/sec
ZDOT = 17014
772617 ZDOT = 5158
745578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3986876
74 X = -1215200
03
Y = -19956029
75 feet Y = -6082597
87 meter
Z = -9020192
43 Z = -2749354
65
XDOT = 13826
978322 XDOT = 4214
462993
YDOT = -10369
974459 feet/sec YDOT = -3160
768215 meter/sec
ZDOT = 16901
738820 ZDOT = 5151
649992
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 12237
69390707
00016717 00000-0 10270-3 0 9159
2 25544 51
6377 140
3842 0010210 9
4491 350
6851 15
52747865 28675
Satellite: ISS
Catalog Number: 25544
Epoch time: 12237
69390707 = yrday
fracday
Element set: 915
Inclination: 51
6377 deg
RA of node: 140
3842 deg
Eccentricity:
0010210
Arg of perigee: 9
4491 deg
Mean anomaly: 350
6851 deg
Mean motion: 15
52747865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 318
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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