[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 21st 2015
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) : 124 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 730 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 3322)
---------------------------------------
Vector Time (GMT): 2015/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4278527
40 A = 6774392
59 meter
Y = -382464
23 meter E =
0001609
Z = 5237773
61 I = 51
26267
XDOT = -284
173301 Wp = 148
25978
YDOT = 7625
364973 meter/sec RA = 276
88314 deg
ZDOT = 787
480935 TA = 294
16949
MA = 294
18631
Ha = 218
424 n
mi
Hp = 213
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14037163
40 X = 4257043
49
Y = -1254803
89 feet Y = -334739
24 meter
Z = 17184296
61 Z = 5258505
34
XDOT = -932
327104 XDOT = -373
246072
YDOT = 25017
601618 feet/sec YDOT = 7621
689097 meter/sec
ZDOT = 2583
598869 ZDOT = 785
884435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7462656
54 X = -2274617
71
Y = -11825864
85 feet Y = -3604523
61 meter
Z = 17273512
01 Z = 5264966
46
XDOT = 21838
826266 XDOT = 6656
474246
YDOT = -10012
749193 feet/sec YDOT = -3051
885954 meter/sec
ZDOT = 2575
281647 ZDOT = 784
945846
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 15201
54954766
00016717 00000-0 10270-3 0 9002
2 25544 51
6440 277
4299 0001968 275
1496 84
9433 15
55213438 33239
Satellite: ISS
Catalog Number: 25544
Epoch time: 15201
54954766 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 277
4299 deg
Eccentricity:
0001968
Arg of perigee: 275
1496 deg
Mean anomaly: 84
9433 deg
Mean motion: 15
55213438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3323
Checksum: 325
Coasting Arc #2 (Orbit 3337)
---------------------------------------
Vector Time (GMT): 2015/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4043915
20 A = 6775029
62 meter
Y = -1873859
11 meter E =
0011750
Z = -5113133
71 I = 51
26061
XDOT = 1469
891940 Wp = 101
22494
YDOT = -7360
500236 meter/sec RA = 271
84560 deg
ZDOT = 1535
717067 TA = 183
66214
MA = 183
67075
Ha = 218
647 n
mi
Hp = 213
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13267438
32 X = -3997823
34
Y = -6147831
72 feet Y = -1918822
95 meter
Z = -16775373
06 Z = -5132666
11
XDOT = 4822
480119 XDOT = 1544
629740
YDOT = -24148
622821 feet/sec YDOT = -7343
645103 meter/sec
ZDOT = 5038
441821 ZDOT = 1543
038726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 773516
32 X = 235767
77
Y = 14505497
69 feet Y = 4421275
70 meter
Z = -16859006
64 Z = -5138625
22
XDOT = -22500
538856 XDOT = -6858
164243
YDOT = 7091
088327 feet/sec YDOT = 2161
363722 meter/sec
ZDOT = 5071
310691 ZDOT = 1545
735498
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 15202
51341663
00016717 00000-0 10270-3 0 9017
2 25544 51
6428 272
6175 0001898 284
6484 75
4458 15
55199087 33380
Satellite: ISS
Catalog Number: 25544
Epoch time: 15202
51341663 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 272
6175 deg
Eccentricity:
0001898
Arg of perigee: 284
6484 deg
Mean anomaly: 75
4458 deg
Mean motion: 15
55199087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3338
Checksum: 331
Coasting Arc #3 (Orbit 3353)
---------------------------------------
Vector Time (GMT): 2015/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3587334
41 A = 6778514
35 meter
Y = 3930683
15 meter E =
0008586
Z = 4194134
33 I = 51
27314
XDOT = -2575
279483 Wp = 66
45645
YDOT = 6243
216128 meter/sec RA = 266
81445 deg
ZDOT = -3639
054480 TA = 61
03477
MA = 60
94872
Ha = 218
489 n
mi
Hp = 213
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11769469
83 X = 3522740
62
Y = 12895942
10 feet Y = 3970437
79 meter
Z = 13760283
25 Z = 4211403
95
XDOT = -8449
079669 XDOT = -2627
224249
YDOT = 20482
992547 feet/sec YDOT = 6214
127329 meter/sec
ZDOT = -11939
155117 ZDOT = -3651
690545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5592885
86 X = 1704711
61
Y = -16477758
07 feet Y = -5022420
66 meter
Z = 13833808
40 Z = 4216544
80
XDOT = 20767
691572 XDOT = 6329
992391
YDOT = -3046
564683 feet/sec YDOT = -928
592915 meter/sec
ZDOT = -11994
653833 ZDOT = -3655
970488
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 15203
54153173
00016717 00000-0 10270-3 0 9029
2 25544 51
6433 267
4834 0001999 290
4249 69
6689 15
55250807 33543
Satellite: ISS
Catalog Number: 25544
Epoch time: 15203
54153173 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 267
4834 deg
Eccentricity:
0001999
Arg of perigee: 290
4249 deg
Mean anomaly: 69
6689 deg
Mean motion: 15
55250807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3354
Checksum: 326
Coasting Arc #4 (Orbit 3368)
---------------------------------------
Vector Time (GMT): 2015/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2940266
11 A = 6783084
58 meter
Y = -5506235
77 meter E =
0004337
Z = -2651089
63 I = 51
29013
XDOT = 3560
734497 Wp = 32
88536
YDOT = -4391
375566 meter/sec RA = 261
79821 deg
ZDOT = 5179
200248 TA = 297
05068
MA = 297
09493
Ha = 218
639 n
mi
Hp = 213
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9646542
35 X = -2865597
63
Y = -18065077
97 feet Y = -5538698
17 meter
Z = -8697800
63 Z = -2665191
57
XDOT = 11682
199793 XDOT = 3584
416860
YDOT = -14407
400150 feet/sec YDOT = -4351
424846 meter/sec
ZDOT = 16992
126798 ZDOT = 5196
554850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10829191
92 X = -3300737
70
Y = 17351965
79 feet Y = 5288879
17 meter
Z = -8757422
15 Z = -2669262
27
XDOT = -17000
697266 XDOT = -5181
812527
YDOT = -2008
539461 feet/sec YDOT = -612
202828 meter/sec
ZDOT = 17067
564171 ZDOT = 5202
193559
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 15204
50538256
00016717 00000-0 10270-3 0 9036
2 25544 51
6424 262
6705 0001871 295
3576 64
7383 15
55235614 33695
Satellite: ISS
Catalog Number: 25544
Epoch time: 15204
50538256 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 262
6705 deg
Eccentricity:
0001871
Arg of perigee: 295
3576 deg
Mean anomaly: 64
7383 deg
Mean motion: 15
55235614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3369
Checksum: 315
Coasting Arc #5 (Orbit 3384)
---------------------------------------
Vector Time (GMT): 2015/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2059989
49 A = 6785820
75 meter
Y = 6424829
81 meter E =
0011340
Z = 671505
13 I = 51
30558
XDOT = -4406
571024 Wp = 128
15793
YDOT = 2039
902386 meter/sec RA = 256
79508 deg
ZDOT = -5937
696677 TA = 44
55211
MA = 44
46100
Ha = 218
697 n
mi
Hp = 213
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6758495
69 X = 1984730
49
Y = 21078837
97 feet Y = 6447445
14 meter
Z = 2203100
81 Z = 681329
56
XDOT = -14457
254016 XDOT = -4400
211272
YDOT = 6692
593130 feet/sec YDOT = 1990
661016 meter/sec
ZDOT = -19480
632141 ZDOT = -5959
087283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14578842
74 X = 4443631
27
Y = -16651407
46 feet Y = -5075348
99 meter
Z = 2244170
56 Z = 684023
19
XDOT = 11911
229834 XDOT = 3630
542853
YDOT = 7764
017351 feet/sec YDOT = 2366
472489 meter/sec
ZDOT = -19572
990707 ZDOT = -5965
847568
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 15205
53347916
00016717 00000-0 10270-3 0 9042
2 25544 51
6430 257
5363 0001875 305
5223 54
5755 15
55268106 33852
Satellite: ISS
Catalog Number: 25544
Epoch time: 15205
53347916 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 257
5363 deg
Eccentricity:
0001875
Arg of perigee: 305
5223 deg
Mean anomaly: 54
5755 deg
Mean motion: 15
55268106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3385
Checksum: 308
Coasting Arc #6 (Orbit 3400)
---------------------------------------
Vector Time (GMT): 2015/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -986500
64 A = 6785338
31 meter
Y = -6560494
21 meter E =
0013471
Z = 1388986
20 I = 51
31104
XDOT = 5026
468558 Wp = 52
83548
YDOT = 473
901359 meter/sec RA = 251
79628 deg
ZDOT = 5777
543862 TA = 322
38512
MA = 322
47926
Ha = 218
855 n
mi
Hp = 213
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3236550
64 X = -919813
43
Y = -21523931
15 feet Y = -6571153
11 meter
Z = 4557041
34 Z = 1384355
63
XDOT = 16491
038575 XDOT = 4992
730718
YDOT = 1554
794485 feet/sec YDOT = 529
921683 meter/sec
ZDOT = 18955
196396 ZDOT = 5801
879412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16512566
51 X = -5033030
27
Y = 14186623
57 feet Y = 4324082
86 meter
Z = 4538320
92 Z = 1383280
22
XDOT = -6330
486203 XDOT = -1929
532195
YDOT = -13498
043492 feet/sec YDOT = -4114
203656 meter/sec
ZDOT = 19059
764958 ZDOT = 5809
416359
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 15206
56156793
00016717 00000-0 10270-3 0 9058
2 25544 51
6424 252
4023 0001863 315
3179 44
7824 15
55224040 34014
Satellite: ISS
Catalog Number: 25544
Epoch time: 15206
56156793 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 252
4023 deg
Eccentricity:
0001863
Arg of perigee: 315
3179 deg
Mean anomaly: 44
7824 deg
Mean motion: 15
55224040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3401
Checksum: 286
Coasting Arc #7 (Orbit 3415)
---------------------------------------
Vector Time (GMT): 2015/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -299044
15 A = 6781431
65 meter
Y = 5938090
51 meter E =
0003447
Z = -3265273
97 I = 51
31029
XDOT = -5329
251474 Wp = 77
34170
YDOT = -2856
551486 meter/sec RA = 246
79045 deg
ZDOT = -4710
209806 TA = 140
73506
MA = 140
71005
Ha = 218
799 n
mi
Hp = 213
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -981115
98 X = -349561
71
Y = 19481924
25 feet Y = 5934464
16 meter
Z = -10712841
10 Z = -3266848
96
XDOT = -17484
420846 XDOT = -5274
032465
YDOT = -9371
888078 feet/sec YDOT = -2915
837606 meter/sec
ZDOT = -15453
444246 ZDOT = -4735
964178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16830808
59 X = 5130030
46
Y = -9852090
15 feet Y = -3002917
08 meter
Z = -10720686
89 Z = -3267665
36
XDOT = 898
151932 XDOT = 273
756709
YDOT = 18457
807502 feet/sec YDOT = 5625
939727 meter/sec
ZDOT = -15563
693420 ZDOT = -4743
813754
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 15207
52538899
00016717 00000-0 10270-3 0 9067
2 25544 51
6433 247
5891 0001807 316
8655 43
2356 15
55286885 34160
Satellite: ISS
Catalog Number: 25544
Epoch time: 15207
52538899 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 247
5891 deg
Eccentricity:
0001807
Arg of perigee: 316
8655 deg
Mean anomaly: 43
2356 deg
Mean motion: 15
55286885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3416
Checksum: 341
Coasting Arc #8 (Orbit 3431)
---------------------------------------
Vector Time (GMT): 2015/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1691581
41 A = 6776849
44 meter
Y = -4661936
99 meter E =
0006795
Z = 4613918
86 I = 51
30715
XDOT = 5229
746837 Wp = 108
07386
YDOT = 4794
506199 meter/sec RA = 241
77053 deg
ZDOT = 2921
421616 TA = 312
70002
MA = 312
75722
Ha = 218
790 n
mi
Hp = 213
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5549807
79 X = 1721174
11
Y = -15295068
86 feet Y = -4642855
52 meter
Z = 15137529
07 Z = 4622207
67
XDOT = 17157
962063 XDOT = 5161
553787
YDOT = 15730
007216 feet/sec YDOT = 4852
607136 meter/sec
ZDOT = 9584
716589 ZDOT = 2946
661233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15727614
25 X = -4793776
82
Y = 4034311
23 feet Y = 1229658
06 meter
Z = 15174016
19 Z = 4625040
13
XDOT = 3770
882505 XDOT = 1149
364988
YDOT = -21824
088117 feet/sec YDOT = -6651
982058 meter/sec
ZDOT = 9692
419018 ZDOT = 2954
249317
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 15208
55345661
00016717 00000-0 10270-3 0 9075
2 25544 51
6420 242
4549 0001792 323
2184 36
8846 15
55293429 34324
Satellite: ISS
Catalog Number: 25544
Epoch time: 15208
55345661 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 242
4549 deg
Eccentricity:
0001792
Arg of perigee: 323
2184 deg
Mean anomaly: 36
8846 deg
Mean motion: 15
55293429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3432
Checksum: 313
Coasting Arc #9 (Orbit 3446)
---------------------------------------
Vector Time (GMT): 2015/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3110761
43 A = 6774129
46 meter
Y = 2940244
41 meter E =
0013786
Z = -5262411
72 I = 51
31481
XDOT = -4619
077719 Wp = 78
09699
YDOT = -6074
997357 meter/sec RA = 236
73848 deg
ZDOT = -662
473740 TA = 185
53455
MA = 185
54981
Ha = 218
867 n
mi
Hp = 213
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10205910
22 X = -3117846
26
Y = 9646471
16 feet Y = 2905418
66 meter
Z = -17265130
32 Z = -5277539
97
XDOT = -15154
454460 XDOT = -4547
584329
YDOT = -19931
093690 feet/sec YDOT = -6126
251114 meter/sec
ZDOT = -2173
470276 ZDOT = -684
738906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13691092
34 X = 4173044
95
Y = 2738528
47 feet Y = 834703
48 meter
Z = -17330729
54 Z = -5282406
36
XDOT = -7444
207087 XDOT = -2268
994320
YDOT = 22835
557315 feet/sec YDOT = 6960
277870 meter/sec
ZDOT = -2268
169457 ZDOT = -691
338051
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 15209
51726127
00016717 00000-0 10270-3 0 9083
2 25544 51
6429 237
6419 0001888 324
4890 35
6138 15
55291809 34475
Satellite: ISS
Catalog Number: 25544
Epoch time: 15209
51726127 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 237
6419 deg
Eccentricity:
0001888
Arg of perigee: 324
4890 deg
Mean anomaly: 35
6138 deg
Mean motion: 15
55291809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3447
Checksum: 332
Coasting Arc #10 (Orbit 3462)
---------------------------------------
Vector Time (GMT): 2015/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4380745
20 A = 6774781
00 meter
Y = -997231
12 meter E =
0005706
Z = 5068998
90 I = 51
33404
XDOT = 3486
513013 Wp = 36
07383
YDOT = 6617
640346 meter/sec RA = 231
70366 deg
ZDOT = -1705
713767 TA = 70
50079
MA = 70
43916
Ha = 218
762 n
mi
Hp = 213
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14372523
62 X = 4366948
01
Y = -3271755
63 feet Y = -948320
30 meter
Z = 16630573
83 Z = 5090245
77
XDOT = 11438
690989 XDOT = 3420
539422
YDOT = 21711
418457 feet/sec YDOT = 6656
260076 meter/sec
ZDOT = -5596
173777 ZDOT = -1688
936963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11028202
75 X = -3361396
20
Y = -9622785
29 feet Y = -2933024
96 meter
Z = 16722157
56 Z = 5096913
62
XDOT = 10125
152822 XDOT = 3086
146580
YDOT = -21236
642648 feet/sec YDOT = -6472
928679 meter/sec
ZDOT = -5525
159923 ZDOT = -1684
068744
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 15210
54530922
00016717 00000-0 10270-3 0 9095
2 25544 51
6412 232
5074 0001896 332
7414 27
3640 15
55333894 34636
Satellite: ISS
Catalog Number: 25544
Epoch time: 15210
54530922 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 232
5074 deg
Eccentricity:
0001896
Arg of perigee: 332
7414 deg
Mean anomaly: 27
3640 deg
Mean motion: 15
55333894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3463
Checksum: 295
Coasting Arc #11 (Orbit 3477)
---------------------------------------
Vector Time (GMT): 2015/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5333844
40 A = 6778622
14 meter
Y = -886733
53 meter E =
0006364
Z = -4094191
41 I = 51
36796
XDOT = -1851
937561 Wp = 96
08118
YDOT = -6392
087099 meter/sec RA = 226
67886 deg
ZDOT = 3801
533261 TA = 213
31566
MA = 213
35573
Ha = 218
912 n
mi
Hp = 212
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17499489
50 X = -5303644
67
Y = -2909230
76 feet Y = -946210
96 meter
Z = -13432386
52 Z = -4120028
37
XDOT = -6075
910632 XDOT = -1798
788109
YDOT = -20971
414368 feet/sec YDOT = -6412
499748 meter/sec
ZDOT = 12472
221984 ZDOT = 3792
665773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8146603
90 X = 2483084
87
Y = 15663137
47 feet Y = 4774124
30 meter
Z = -13543401
83 Z = -4128028
88
XDOT = -11910
796560 XDOT = -3630
410791
YDOT = 16934
760041 feet/sec YDOT = 5161
714860 meter/sec
ZDOT = 12435
178650 ZDOT = 3790
242453
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 15211
50909569
00016717 00000-0 10270-3 0 9101
2 25544 51
6419 227
6941 0002014 336
4970 23
6091 15
55325149 34781
Satellite: ISS
Catalog Number: 25544
Epoch time: 15211
50909569 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 227
6941 deg
Eccentricity:
0002014
Arg of perigee: 336
4970 deg
Mean anomaly: 23
6091 deg
Mean motion: 15
55325149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3478
Checksum: 306
Coasting Arc #12 (Orbit 3493)
---------------------------------------
Vector Time (GMT): 2015/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5789051
50 A = 6783121
71 meter
Y = 2542444
75 meter E =
0012752
Z = 2442591
15 I = 51
40434
XDOT = -174
230743 Wp = 97
52145
YDOT = 5526
674614 meter/sec RA = 221
66976 deg
ZDOT = -5317
444569 TA = 55
02198
MA = 54
90231
Ha = 218
930 n
mi
Hp = 212
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18992951
11 X = 5748326
10
Y = 8341354
16 feet Y = 2606953
90 meter
Z = 8013750
50 Z = 2470613
79
XDOT = -571
623174 XDOT = -210
188843
YDOT = 18132
134561 feet/sec YDOT = 5524
525427 meter/sec
ZDOT = -17445
684281 ZDOT = -5318
378028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5071699
99 X = -1545854
16
Y = -20066092
72 feet Y = -6116145
06 meter
Z = 8133901
89 Z = 2479213
30
XDOT = 13115
945255 XDOT = 3997
740114
YDOT = -10417
892618 feet/sec YDOT = -3175
373670 meter/sec
ZDOT = -17450
650095 ZDOT = -5318
958149
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 15212
53712443
00016717 00000-0 10270-3 0 9119
2 25544 51
6403 222
5588 0002038 342
6589 17
4495 15
55367684 34943
Satellite: ISS
Catalog Number: 25544
Epoch time: 15212
53712443 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 222
5588 deg
Eccentricity:
0002038
Arg of perigee: 342
6589 deg
Mean anomaly: 17
4495 deg
Mean motion: 15
55367684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3494
Checksum: 316
Coasting Arc #13 (Orbit 3508)
---------------------------------------
Vector Time (GMT): 2015/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5622429
83 A = 6785516
80 meter
Y = -3763320
86 meter E =
0012222
Z = -426401
10 I = 51
43746
XDOT = 2357
111528 Wp = 34
67643
YDOT = -4188
373413 meter/sec RA = 216
67599 deg
ZDOT = 5979
608374 TA = 320
70963
MA = 320
79826
Ha = 218
875 n
mi
Hp = 212
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18446292
10 X = -5577858
35
Y = -12346853
23 feet Y = -3825945
34 meter
Z = -1398953
73 Z = -453604
95
XDOT = 7733
305539 XDOT = 2374
725725
YDOT = -13741
382588 feet/sec YDOT = -4161
916275 meter/sec
ZDOT = 19618
137711 ZDOT = 5991
101197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1984006
25 X = 604725
10
Y = 22100562
28 feet Y = 6736251
38 meter
Z = -1515392
48 Z = -461891
63
XDOT = -13856
848343 XDOT = -4223
567375
YDOT = 2572
985957 feet/sec YDOT = 784
246120 meter/sec
ZDOT = 19668
309649 ZDOT = 5994
900781
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 15213
50089237
00016717 00000-0 10270-3 0 9126
2 25544 51
6407 217
7455 0001872 343
5883 16
5209 15
55409475 35093
Satellite: ISS
Catalog Number: 25544
Epoch time: 15213
50089237 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 217
7455 deg
Eccentricity:
0001872
Arg of perigee: 343
5883 deg
Mean anomaly: 16
5209 deg
Mean motion: 15
55409475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3509
Checksum: 313
Coasting Arc #14 (Orbit 3524)
---------------------------------------
Vector Time (GMT): 2015/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4759511
17 A = 6784535
11 meter
Y = 4525282
33 meter E =
0006014
Z = -1695719
59 I = 51
45898
XDOT = -4459
897481 Wp = 133
52916
YDOT = 2567
386452 meter/sec RA = 211
68532 deg
ZDOT = -5683
219186 TA = 65
11137
MA = 65
04887
Ha = 219
066 n
mi
Hp = 212
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15615194
12 X = 4716791
63
Y = 14846726
81 feet Y = 4578267
45 meter
Z = -5563384
49 Z = -1672703
07
XDOT = -14632
209583 XDOT = -4460
668789
YDOT = 8423
183897 feet/sec YDOT = 2517
508632 meter/sec
ZDOT = -18645
732239 ZDOT = -5704
885914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1341181
01 X = 408791
97
Y = -21530094
92 feet Y = -6562372
93 meter
Z = -5465077
99 Z = -1665755
77
XDOT = 14202
536300 XDOT = 4328
933064
YDOT = 5627
251650 feet/sec YDOT = 1715
186303 meter/sec
ZDOT = -18739
418711 ZDOT = -5711
774823
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 15214
52890185
00016717 00000-0 10270-3 0 9132
2 25544 51
6399 212
6097 0002063 349
1417 10
9692 15
55371904 35254
Satellite: ISS
Catalog Number: 25544
Epoch time: 15214
52890185 = yrday
fracday
Element set: 913
Inclination: 51
6399 deg
RA of node: 212
6097 deg
Eccentricity:
0002063
Arg of perigee: 349
1417 deg
Mean anomaly: 10
9692 deg
Mean motion: 15
55371904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3525
Checksum: 310
Coasting Arc #15 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2015/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3264336
05 A = 6780390
51 meter
Y = -4778740
20 meter E =
0011905
Z = 3521091
32 I = 51
47299
XDOT = 6163
026715 Wp = 82
04542
YDOT = -897
713659 meter/sec RA = 206
68809 deg
ZDOT = 4483
884950 TA = 319
59155
MA = 319
67992
Ha = 219
022 n
mi
Hp = 212
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10709763
96 X = -3227760
26
Y = -15678281
49 feet Y = -4815039
59 meter
Z = 11552136
89 Z = 3505323
00
XDOT = 20219
903919 XDOT = 6150
826474
YDOT = -2945
254787 feet/sec YDOT = -828
862798 meter/sec
ZDOT = 14710
908629 ZDOT = 4513
793581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4786055
96 X = -1458789
86
Y = 18415932
20 feet Y = 5613176
13 meter
Z = 11485056
85 Z = 3500645
33
XDOT = -14061
830257 XDOT = -4286
045862
YDOT = -12932
719013 feet/sec YDOT = -3941
892755 meter/sec
ZDOT = 14839
799030 ZDOT = 4523
170744
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 15215
55689959
00016717 00000-0 10270-3 0 9142
2 25544 51
6399 207
4751 0002134 348
2360 11
8743 15
55412806 35411
Satellite: ISS
Catalog Number: 25544
Epoch time: 15215
55689959 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 207
4751 deg
Eccentricity:
0002134
Arg of perigee: 348
2360 deg
Mean anomaly: 11
8743 deg
Mean motion: 15
55412806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 317
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