[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 11th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
There are no maneuvers
Coasting Arc #1 (Orbit 298)
---------------------------------------
Vector Time (GMT): 2013/221/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3985982
98 A = 6796330
83 meter
Y = 4455063
88 meter E =
0001238
Z = -3235101
93 I = 51
51102
XDOT = -5755
362842 Wp = 35
02607
YDOT = 1694
051295 meter/sec RA = 202
69417 deg
ZDOT = -4758
242380 TA = 182
42354
MA = 182
42414
Ha = 225
997 n
mi
Hp = 222
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13077371
98 X = 3951584
24
Y = 14616351
31 feet Y = 4499445
23 meter
Z = -10613851
48 Z = -3215822
38
XDOT = -18882
424022 XDOT = -5750
764447
YDOT = 5557
911073 feet/sec YDOT = 1629
716748 meter/sec
ZDOT = -15611
031431 ZDOT = -4786
189860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10210285
55 X = -3112095
04
Y = -16795882
94 feet Y = -5119385
12 meter
Z = -10533641
92 Z = -3210654
06
XDOT = 18264
394282 XDOT = 5566
987377
YDOT = -1238
721897 feet/sec YDOT = -377
562434 meter/sec
ZDOT = -15728
303786 ZDOT = -4793
986994
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 13221
61427669
00016717 00000-0 10270-3 0 9007
2 25544 51
6476 203
6162 0004204 295
6312 64
4404 15
50232304 2996
Satellite: ISS
Catalog Number: 25544
Epoch time: 13221
61427669 = yrday
fracday
Element set: 900
Inclination: 51
6476 deg
RA of node: 203
6162 deg
Eccentricity:
0004204
Arg of perigee: 295
6312 deg
Mean anomaly: 64
4404 deg
Mean motion: 15
50232304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 299
Checksum: 277
Coasting Arc #2 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2013/222/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3952551
42 A = 6795360
22 meter
Y = -4227038
60 meter E =
0008553
Z = 3553077
79 I = 51
53722
XDOT = 5960
366733 Wp = 80
17700
YDOT = -1815
868954 meter/sec RA = 197
73121 deg
ZDOT = 4462
432275 TA = 321
75237
MA = 321
81301
Ha = 226
076 n
mi
Hp = 222
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12967688
37 X = -3922249
67
Y = -13868236
87 feet Y = -4271068
98 meter
Z = 11657079
35 Z = 3533950
63
XDOT = 19555
008966 XDOT = 5958
552159
YDOT = -5957
575308 feet/sec YDOT = -1749
226341 meter/sec
ZDOT = 14640
525836 ZDOT = 4491
382508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10521780
82 X = 3207038
79
Y = 15862872
88 feet Y = 4835003
65 meter
Z = 11577470
65 Z = 3528813
06
XDOT = -19031
587114 XDOT = -5800
827752
YDOT = 1830
872280 feet/sec YDOT = 558
049871 meter/sec
ZDOT = 14762
021311 ZDOT = 4499
464096
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 13222
64569771
00016717 00000-0 10270-3 0 9013
2 25544 51
6481 198
5053 0004203 297
8579 62
2146 15
50253503 3153
Satellite: ISS
Catalog Number: 25544
Epoch time: 13222
64569771 = yrday
fracday
Element set: 901
Inclination: 51
6481 deg
RA of node: 198
5053 deg
Eccentricity:
0004203
Arg of perigee: 297
8579 deg
Mean anomaly: 62
2146 deg
Mean motion: 15
50253503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 300
Coasting Arc #3 (Orbit 329)
---------------------------------------
Vector Time (GMT): 2013/223/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3879935
03 A = 6794366
05 meter
Y = 4025341
08 meter E =
0004597
Z = -3866181
09 I = 51
56401
XDOT = -6145
416405 Wp = 32
70216
YDOT = 1962
197440 meter/sec RA = 192
76889 deg
ZDOT = -4122
820158 TA = 193
86010
MA = 193
87273
Ha = 226
159 n
mi
Hp = 222
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12729445
63 X = 3853415
13
Y = 13206499
61 feet Y = 4068580
56 meter
Z = -12684321
15 Z = -3847397
42
XDOT = -20162
127314 XDOT = -6146
874006
YDOT = 6437
655642 feet/sec YDOT = 1893
467208 meter/sec
ZDOT = -13526
312853 ZDOT = -4152
677392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10663955
43 X = -3250373
61
Y = -14990271
61 feet Y = -4569034
79 meter
Z = -12606118
86 Z = -3842345
03
XDOT = 19727
100198 XDOT = 6012
820140
YDOT = -2549
191597 feet/sec YDOT = -776
993599 meter/sec
ZDOT = -13651
634902 ZDOT = -4161
018318
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 13223
61264739
00016717 00000-0 10270-3 0 9028
2 25544 51
6485 193
7133 0004255 303
5140 56
5604 15
50263052 3301
Satellite: ISS
Catalog Number: 25544
Epoch time: 13223
61264739 = yrday
fracday
Element set: 902
Inclination: 51
6485 deg
RA of node: 193
7133 deg
Eccentricity:
0004255
Arg of perigee: 303
5140 deg
Mean anomaly: 56
5604 deg
Mean motion: 15
50263052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 330
Checksum: 273
Coasting Arc #4 (Orbit 345)
---------------------------------------
Vector Time (GMT): 2013/224/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3772408
88 A = 6793376
14 meter
Y = -3833680
80 meter E =
0006741
Z = 4144079
61 I = 51
59116
XDOT = 6321
565634 Wp = 90
11332
YDOT = -2145
593516 meter/sec RA = 187
80858 deg
ZDOT = 3764
398920 TA = 321
04590
MA = 321
09445
Ha = 226
276 n
mi
Hp = 221
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12376669
55 X = -3749390
16
Y = -12577692
92 feet Y = -3875737
46 meter
Z = 13596061
71 Z = 4125809
69
XDOT = 20740
044730 XDOT = 6326
801961
YDOT = -7039
348805 feet/sec YDOT = -2074
872393 meter/sec
ZDOT = 12350
390158 ZDOT = 3795
121121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10660637
45 X = 3249362
30
Y = 14134854
46 feet Y = 4308303
64 meter
Z = 13519981
54 Z = 4120890
37
XDOT = -20389
824913 XDOT = -6214
818634
YDOT = 3424
898361 feet/sec YDOT = 1043
909020 meter/sec
ZDOT = 12479
369520 ZDOT = 3803
711830
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 13224
64405011
00016717 00000-0 10270-3 0 9033
2 25544 51
6487 188
6024 0004246 305
9608 54
1149 15
50277158 3467
Satellite: ISS
Catalog Number: 25544
Epoch time: 13224
64405011 = yrday
fracday
Element set: 903
Inclination: 51
6487 deg
RA of node: 188
6024 deg
Eccentricity:
0004246
Arg of perigee: 305
9608 deg
Mean anomaly: 54
1149 deg
Mean motion: 15
50277158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 346
Checksum: 294
Coasting Arc #5 (Orbit 360)
---------------------------------------
Vector Time (GMT): 2013/225/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3636154
24 A = 6792383
80 meter
Y = 3678612
72 meter E =
0007813
Z = -4410486
62 I = 51
61892
XDOT = -6461
419006 Wp = 41
06706
YDOT = 2348
013962 meter/sec RA = 182
84895 deg
ZDOT = -3366
270681 TA = 194
79683
MA = 194
81971
Ha = 226
338 n
mi
Hp = 221
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11929639
89 X = 3616173
81
Y = 12068939
39 feet Y = 3719162
75 meter
Z = -14470100
45 Z = -4392871
14
XDOT = -21198
881253 XDOT = -6470
842412
YDOT = 7703
457879 feet/sec YDOT = 2275
705561 meter/sec
ZDOT = -11044
195147 ZDOT = -3397
682460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10523229
25 X = -3207480
28
Y = -13392349
53 feet Y = -4081988
14 meter
Z = -14396736
89 Z = -4388125
40
XDOT = 20910
016630 XDOT = 6373
373069
YDOT = -4407
714620 feet/sec YDOT = -1343
471416 meter/sec
ZDOT = -11176
102264 ZDOT = -3406
475970
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 13225
61098203
00016717 00000-0 10270-3 0 9043
2 25544 51
6490 183
8104 0004282 311
3361 48
7421 15
50294928 3617
Satellite: ISS
Catalog Number: 25544
Epoch time: 13225
61098203 = yrday
fracday
Element set: 904
Inclination: 51
6490 deg
RA of node: 183
8104 deg
Eccentricity:
0004282
Arg of perigee: 311
3361 deg
Mean anomaly: 48
7421 deg
Mean motion: 15
50294928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 361
Checksum: 284
Coasting Arc #6 (Orbit 376)
---------------------------------------
Vector Time (GMT): 2013/226/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3467102
82 A = 6791462
75 meter
Y = -3544363
14 meter E =
0004578
Z = 4637535
15 I = 51
64641
XDOT = 6586
433255 Wp = 97
14836
YDOT = -2578
617679 meter/sec RA = 177
89101 deg
ZDOT = 2950
295474 TA = 323
43622
MA = 323
46746
Ha = 226
462 n
mi
Hp = 221
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11375009
26 X = -3449739
09
Y = -11628487
99 feet Y = -3583037
44 meter
Z = 15215010
32 Z = 4620734
49
XDOT = 21609
032988 XDOT = 6600
446726
YDOT = -8460
031756 feet/sec YDOT = -2504
885683 meter/sec
ZDOT = 9679
447094 ZDOT = 2982
325649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10248856
74 X = 3123851
53
Y = 12716047
67 feet Y = 3875851
33 meter
Z = 15145037
97 Z = 4616207
57
XDOT = -21359
261403 XDOT = -6510
302876
YDOT = 5514
454713 feet/sec YDOT = 1680
805796 meter/sec
ZDOT = 9813
990318 ZDOT = 2991
304249
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 13226
64236563
00016717 00000-0 10270-3 0 9051
2 25544 51
6487 178
6991 0004281 313
7560 46
3236 15
50305622 3774
Satellite: ISS
Catalog Number: 25544
Epoch time: 13226
64236563 = yrday
fracday
Element set: 905
Inclination: 51
6487 deg
RA of node: 178
6991 deg
Eccentricity:
0004281
Arg of perigee: 313
7560 deg
Mean anomaly: 46
3236 deg
Mean motion: 15
50305622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 377
Checksum: 309
Coasting Arc #7 (Orbit 391)
---------------------------------------
Vector Time (GMT): 2013/227/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3283687
48 A = 6790588
72 meter
Y = 3453797
83 meter E =
0010568
Z = -4847156
55 I = 51
67493
XDOT = -6661
632474 Wp = 50
30160
YDOT = 2818
386987 meter/sec RA = 172
93407 deg
ZDOT = -2501
730797 TA = 195
05930
MA = 195
09079
Ha = 226
515 n
mi
Hp = 221
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10773252
89 X = 3268368
32
Y = 11331357
72 feet Y = 3490432
57 meter
Z = -15902744
60 Z = -4831241
93
XDOT = -21855
749585 XDOT = -6680
500536
YDOT = 9246
676465 feet/sec YDOT = 2743
786954 meter/sec
ZDOT = -8207
778204 ZDOT = -2534
137947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9895287
14 X = -3016083
52
Y = -12192191
65 feet Y = -3716180
01 meter
Z = -15836466
99 Z = -4826955
14
XDOT = 21606
618393 XDOT = 6585
697286
YDOT = -6685
515897 feet/sec YDOT = -2037
745245 meter/sec
ZDOT = -8343
949694 ZDOT = -2543
235867
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 13227
60927931
00016717 00000-0 10270-3 0 9065
2 25544 51
6492 173
9069 0004321 318
9276 41
1549 15
50327511 3928
Satellite: ISS
Catalog Number: 25544
Epoch time: 13227
60927931 = yrday
fracday
Element set: 906
Inclination: 51
6492 deg
RA of node: 173
9069 deg
Eccentricity:
0004321
Arg of perigee: 318
9276 deg
Mean anomaly: 41
1549 deg
Mean motion: 15
50327511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 392
Checksum: 307
Coasting Arc #8 (Orbit 407)
---------------------------------------
Vector Time (GMT): 2013/228/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3072362
14 A = 6789833
45 meter
Y = -3393053
75 meter E =
0002374
Z = 5012879
71 I = 51
70272
XDOT = 6718
292273 Wp = 89
51872
YDOT = -3074
356562 meter/sec RA = 167
97855 deg
ZDOT = 2035
853312 TA = 340
69180
MA = 340
70079
Ha = 226
629 n
mi
Hp = 221
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10079928
27 X = -3058542
87
Y = -11132066
12 feet Y = -3427333
73 meter
Z = 16446455
75 Z = 4997988
08
XDOT = 22041
641315 XDOT = 6742
281564
YDOT = -10086
471661 feet/sec YDOT = -2999
094291 meter/sec
ZDOT = 6679
308765 ZDOT = 2068
547989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9428207
08 X = 2873717
52
Y = 11775926
82 feet Y = 3589302
50 meter
Z = 16384450
42 Z = 4993980
49
XDOT = -21756
382866 XDOT = -6631
345498
YDOT = 7930
692269 feet/sec YDOT = 2417
275003 meter/sec
ZDOT = 6816
737224 ZDOT = 2077
741506
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 13228
64064332
00016717 00000-0 10270-3 0 9078
2 25544 51
6490 168
7951 0004332 321
2528 38
8312 15
50337715 4083
Satellite: ISS
Catalog Number: 25544
Epoch time: 13228
64064332 = yrday
fracday
Element set: 907
Inclination: 51
6490 deg
RA of node: 168
7951 deg
Eccentricity:
0004332
Arg of perigee: 321
2528 deg
Mean anomaly: 38
8312 deg
Mean motion: 15
50337715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 408
Checksum: 295
Coasting Arc #9 (Orbit 422)
---------------------------------------
Vector Time (GMT): 2013/229/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2864001
39 A = 6789188
28 meter
Y = 3378601
60 meter E =
0012559
Z = -5156277
62 I = 51
73155
XDOT = -6716
315173 Wp = 59
46397
YDOT = 3326
535498 meter/sec RA = 163
02458 deg
ZDOT = -1547
417647 TA = 195
59275
MA = 195
63147
Ha = 226
679 n
mi
Hp = 221
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9396330
03 X = 2851055
68
Y = 11084650
91 feet Y = 3410556
41 meter
Z = -16916921
32 Z = -5142396
14
XDOT = -22035
154766 XDOT = -6745
497229
YDOT = 10913
830374 feet/sec YDOT = 3251
266277 meter/sec
ZDOT = -5076
829551 ZDOT = -1580
115191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8951821
73 X = -2728515
26
Y = -11531565
52 feet Y = -3514821
17 meter
Z = -16859140
40 Z = -5138666
00
XDOT = 21666
237615 XDOT = 6603
869225
YDOT = -9179
504967 feet/sec YDOT = -2797
913114 meter/sec
ZDOT = -5214
321197 ZDOT = -1589
325101
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 13229
60753836
00016717 00000-0 10270-3 0 9080
2 25544 51
6499 164
0029 0004398 325
9517 34
1341 15
50359887 4230
Satellite: ISS
Catalog Number: 25544
Epoch time: 13229
60753836 = yrday
fracday
Element set: 908
Inclination: 51
6499 deg
RA of node: 164
0029 deg
Eccentricity:
0004398
Arg of perigee: 325
9517 deg
Mean anomaly: 34
1341 deg
Mean motion: 15
50359887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 423
Checksum: 324
Coasting Arc #10 (Orbit 438)
---------------------------------------
Vector Time (GMT): 2013/230/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2634631
97 A = 6788690
76 meter
Y = -3400264
76 meter E =
0001886
Z = 5250986
76 I = 51
75939
XDOT = 6694
983463 Wp = 26
66139
YDOT = -3580
475689 meter/sec RA = 158
07200 deg
ZDOT = 1042
114041 TA = 53
37703
MA = 53
35968
Ha = 226
776 n
mi
Hp = 221
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8643805
68 X = -2621921
02
Y = -11155724
29 feet Y = -3429655
85 meter
Z = 17227646
85 Z = 5238219
06
XDOT = 21965
168841 XDOT = 6729
461330
YDOT = -11746
967485 feet/sec YDOT = -3505
415372 meter/sec
ZDOT = 3419
009321 ZDOT = 1074
720744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8396421
65 X = 2559229
32
Y = 11423353
02 feet Y = 3481838
00 meter
Z = 17174530
16 Z = 5234796
79
XDOT = -21468
135132 XDOT = -6543
487588
YDOT = 10440
431528 feet/sec YDOT = 3182
243530 meter/sec
ZDOT = 3556
169712 ZDOT = 1083
920528
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 13230
63888291
00016717 00000-0 10270-3 0 9090
2 25544 51
6501 158
8910 0004417 328
3197 31
7687 15
50372320 4397
Satellite: ISS
Catalog Number: 25544
Epoch time: 13230
63888291 = yrday
fracday
Element set: 909
Inclination: 51
6501 deg
RA of node: 158
8910 deg
Eccentricity:
0004417
Arg of perigee: 328
3197 deg
Mean anomaly: 31
7687 deg
Mean motion: 15
50372320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 439
Checksum: 311
Coasting Arc #11 (Orbit 453)
---------------------------------------
Vector Time (GMT): 2013/231/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2427013
08 A = 6788366
92 meter
Y = 3465419
39 meter E =
0013549
Z = -5319965
49 I = 51
78739
XDOT = -6612
348627 Wp = 68
19367
YDOT = 3816
470083 meter/sec RA = 153
12126 deg
ZDOT = -526
740154 TA = 196
75835
MA = 196
80316
Ha = 226
833 n
mi
Hp = 221
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7962641
33 X = 2413924
00
Y = 11369486
19 feet Y = 3492486
51 meter
Z = -17453955
01 Z = -5308207
39
XDOT = -21694
057175 XDOT = -6651
975080
YDOT = 12521
227305 feet/sec YDOT = 3742
305035 meter/sec
ZDOT = -1728
150111 ZDOT = -558
957956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7908975
55 X = -2410655
75
Y = -11481331
32 feet Y = -3499509
79 meter
Z = -17405072
70 Z = -5305066
16
XDOT = 21020
868703 XDOT = 6407
160781
YDOT = -11635
955343 feet/sec YDOT = -3546
639189 meter/sec
ZDOT = -1863
724304 ZDOT = -568
063168
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 13231
60575977
00016717 00000-0 10270-3 0 9104
2 25544 51
6509 154
0988 0004508 332
3797 27
7113 15
50390675 4549
Satellite: ISS
Catalog Number: 25544
Epoch time: 13231
60575977 = yrday
fracday
Element set: 910
Inclination: 51
6509 deg
RA of node: 154
0988 deg
Eccentricity:
0004508
Arg of perigee: 332
3797 deg
Mean anomaly: 27
7113 deg
Mean motion: 15
50390675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 454
Checksum: 317
Coasting Arc #12 (Orbit 469)
---------------------------------------
Vector Time (GMT): 2013/232/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2206176
77 A = 6788199
59 meter
Y = -3569598
35 meter E =
0004058
Z = 5335330
27 I = 51
81434
XDOT = 6512
936547 Wp = 7
19770
YDOT = -4038
218646 meter/sec RA = 148
17207 deg
ZDOT = -4
720615 TA = 82
87027
MA = 82
82413
Ha = 226
912 n
mi
Hp = 221
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7238112
77 X = -2192013
81
Y = -11711280
68 feet Y = -3594189
80 meter
Z = 17504364
39 Z = 5324647
65
XDOT = 21367
902056 XDOT = 6557
631665
YDOT = -13248
748838 feet/sec YDOT = -3965
136955 meter/sec
ZDOT = -15
487583 ZDOT = 27
026691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7382142
94 X = 2250077
17
Y = 11687579
76 feet Y = 3562374
31 meter
Z = 17459999
69 Z = 5321807
91
XDOT = -20474
985293 XDOT = -6240
775517
YDOT = 12775
249009 feet/sec YDOT = 3893
895898 meter/sec
ZDOT = 118
153364 ZDOT = 36
013145
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 13232
63708447
00016717 00000-0 10270-3 0 9119
2 25544 51
6512 148
9871 0004529 334
9943 25
0988 15
50407725 4704
Satellite: ISS
Catalog Number: 25544
Epoch time: 13232
63708447 = yrday
fracday
Element set: 911
Inclination: 51
6512 deg
RA of node: 148
9871 deg
Eccentricity:
0004529
Arg of perigee: 334
9943 deg
Mean anomaly: 25
0988 deg
Mean motion: 15
50407725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 470
Checksum: 317
Coasting Arc #13 (Orbit 484)
---------------------------------------
Vector Time (GMT): 2013/233/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2025329
08 A = 6788255
21 meter
Y = 3708771
22 meter E =
0013414
Z = -5323571
38 I = 51
84012
XDOT = -6356
385663 Wp = 76
04566
YDOT = 4228
899159 meter/sec RA = 143
22440 deg
ZDOT = 532
160797 TA = 199
00283
MA = 199
05293
Ha = 226
981 n
mi
Hp = 221
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6644780
46 X = 2009566
25
Y = 12167884
58 feet Y = 3731331
26 meter
Z = -17465785
36 Z = -5313771
22
XDOT = -20854
283671 XDOT = -6405
786761
YDOT = 13874
341073 feet/sec YDOT = 4157
541840 meter/sec
ZDOT = 1745
934372 ZDOT = 501
162370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6997896
71 X = -2132958
92
Y = -12027396
58 feet Y = -3665950
48 meter
Z = -17425135
69 Z = -5311181
36
XDOT = 19702
611104 XDOT = 6005
355865
YDOT = -13783
576002 feet/sec YDOT = -4201
233965 meter/sec
ZDOT = 1615
400229 ZDOT = 492
373990
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 13233
60394298
00016717 00000-0 10270-3 0 9123
2 25544 51
6511 144
1947 0004618 338
5005 21
5951 15
50418877 4850
Satellite: ISS
Catalog Number: 25544
Epoch time: 13233
60394298 = yrday
fracday
Element set: 912
Inclination: 51
6511 deg
RA of node: 144
1947 deg
Eccentricity:
0004618
Arg of perigee: 338
5005 deg
Mean anomaly: 21
5951 deg
Mean motion: 15
50418877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 485
Checksum: 307
Coasting Arc #14 (Orbit 500)
---------------------------------------
Vector Time (GMT): 2013/234/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1838759
52 A = 6788458
08 meter
Y = -3886047
37 meter E =
0006577
Z = 5253220
11 I = 51
86513
XDOT = 6189
222021 Wp = 14
46413
YDOT = -4389
008323 meter/sec RA = 138
27856 deg
ZDOT = -1073
871543 TA = 85
83620
MA = 85
76104
Ha = 227
041 n
mi
Hp = 220
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6032675
58 X = -1820686
58
Y = -12749499
24 feet Y = -3906508
09 meter
Z = 17234974
13 Z = 5244331
91
XDOT = 20305
846525 XDOT = 6243
057376
YDOT = -14399
633607 feet/sec YDOT = -4319
495589 meter/sec
ZDOT = -3523
200601 ZDOT = -1043
674198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6612425
80 X = 2015467
38
Y = 12509436
13 feet Y = 3812876
13 meter
Z = 17198170
58 Z = 5242002
39
XDOT = -18861
855369 XDOT = -5749
093516
YDOT = 14668
511832 feet/sec YDOT = 4470
962406 meter/sec
ZDOT = -3395
996720 ZDOT = -1035
099800
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 13234
63524782
00016717 00000-0 10270-3 0 9131
2 25544 51
6511 139
0830 0004646 341
3202 18
7778 15
50441732 5016
Satellite: ISS
Catalog Number: 25544
Epoch time: 13234
63524782 = yrday
fracday
Element set: 913
Inclination: 51
6511 deg
RA of node: 139
0830 deg
Eccentricity:
0004646
Arg of perigee: 341
3202 deg
Mean anomaly: 18
7778 deg
Mean motion: 15
50441732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 501
Checksum: 281
Coasting Arc #15 (Orbit 515)
---------------------------------------
Vector Time (GMT): 2013/235/14:07:40
198
Vector Time (MET): N/A
Weight (LBS) : 974011
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1707739
51 A = 6788901
63 meter
Y = 4084567
22 meter E =
0012178
Z = -5156768
22 I = 51
88794
XDOT = -5975
586769 Wp = 82
05066
YDOT = 4508
294507 meter/sec RA = 133
33367 deg
ZDOT = 1596
885937 TA = 203
29872
MA = 203
35396
Ha = 227
124 n
mi
Hp = 220
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5602819
92 X = 1686988
00
Y = 13400811
10 feet Y = 4103547
80 meter
Z = -16918530
91 Z = -5148523
00
XDOT = -19604
943469 XDOT = -6033
312547
YDOT = 14790
992478 feet/sec YDOT = 4441
149072 meter/sec
ZDOT = 5239
127090 ZDOT = 1567
716789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6431033
44 X = -1960178
99
Y = -13067790
83 feet Y = -3983062
64 meter
Z = -16884450
52 Z = -5146380
52
XDOT = 17847
011622 XDOT = 5439
769142
YDOT = -15372
845274 feet/sec YDOT = -4685
643239 meter/sec
ZDOT = 5116
210511 ZDOT = 1559
420964
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 13235
60208789
00016717 00000-0 10270-3 0 9146
2 25544 51
6500 134
2899 0004699 344
5814 15
5193 15
50444656 5168
Satellite: ISS
Catalog Number: 25544
Epoch time: 13235
60208789 = yrday
fracday
Element set: 914
Inclination: 51
6500 deg
RA of node: 134
2899 deg
Eccentricity:
0004699
Arg of perigee: 344
5814 deg
Mean anomaly: 15
5193 deg
Mean motion: 15
50444656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 516
Checksum: 318
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