[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 27th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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 3432)
---------------------------------------
Vector Time (GMT): 2015/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1473751
27 A = 6778452
31 meter
Y = -4855695
66 meter E =
0008727
Z = 4488230
62 I = 51
30936
XDOT = 5312
891620 Wp = 106
27858
YDOT = 4543
193526 meter/sec RA = 241
78141 deg
ZDOT = 3163
092754 TA = 311
80304
MA = 311
87755
Ha = 219
772 n
mi
Hp = 213
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4835141
96 X = 1506137
35
Y = -15930760
02 feet Y = -4839034
48 meter
Z = 14725166
07 Z = 4495468
03
XDOT = 17430
746786 XDOT = 5246
328692
YDOT = 14905
490570 feet/sec YDOT = 4602
233338 meter/sec
ZDOT = 10377
600899 ZDOT = 3188
740207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15856312
10 X = -4833003
93
Y = 4980126
33 feet Y = 1517942
51 meter
Z = 14757165
61 Z = 4497984
08
XDOT = 3006
695662 XDOT = 916
440838
YDOT = -21575
469816 feet/sec YDOT = -6576
203200 meter/sec
ZDOT = 10487
102516 ZDOT = 3196
468847
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
55394984
00016717 00000-0 10270-3 0 9000
2 25544 51
6426 242
4627 0000940 5
7131 354
4033 15
54912432 34334
Satellite: ISS
Catalog Number: 25544
Epoch time: 15208
55394984 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 242
4627 deg
Eccentricity:
0000940
Arg of perigee: 5
7131 deg
Mean anomaly: 354
4033 deg
Mean motion: 15
54912432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3433
Checksum: 288
Coasting Arc #2 (Orbit 3447)
---------------------------------------
Vector Time (GMT): 2015/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2816712
50 A = 6775489
17 meter
Y = 3311609
42 meter E =
0014448
Z = -5209541
51 I = 51
31620
XDOT = -4852
717665 Wp = 77
98911
YDOT = -5826
314636 meter/sec RA = 236
75459 deg
ZDOT = -1079
492335 TA = 181
60633
MA = 181
61098
Ha = 219
813 n
mi
Hp = 213
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9241182
74 X = -2828228
69
Y = 10864860
29 feet Y = 3280047
14 meter
Z = -17091671
61 Z = -5223252
07
XDOT = -15920
989716 XDOT = -4781
962046
YDOT = -19115
205499 feet/sec YDOT = -5880
185199 meter/sec
ZDOT = -3541
641518 ZDOT = -1102
894235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14136530
47 X = 4308814
49
Y = 1250366
23 feet Y = 381111
63 meter
Z = -17151238
34 Z = -5227697
45
XDOT = -6449
846118 XDOT = -1965
913097
YDOT = 22955
984719 feet/sec YDOT = 6996
984142 meter/sec
ZDOT = -3641
274701 ZDOT = -1109
860529
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
51799080
00016717 00000-0 10270-3 0 9014
2 25544 51
6435 237
6512 0000956 1
9523 358
1634 15
54910317 34487
Satellite: ISS
Catalog Number: 25544
Epoch time: 15209
51799080 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 237
6512 deg
Eccentricity:
0000956
Arg of perigee: 1
9523 deg
Mean anomaly: 358
1634 deg
Mean motion: 15
54910317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3448
Checksum: 305
Coasting Arc #3 (Orbit 3463)
---------------------------------------
Vector Time (GMT): 2015/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4069541
17 A = 6775390
19 meter
Y = -1546171
16 meter E =
0004694
Z = 5189261
94 I = 51
33283
XDOT = 3938
848531 Wp = 47
65436
YDOT = 6482
116012 meter/sec RA = 231
72359 deg
ZDOT = -1153
776419 TA = 53
47203
MA = 53
42882
Ha = 219
694 n
mi
Hp = 213
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13351513
03 X = 4061321
30
Y = -5072740
01 feet Y = -1500709
25 meter
Z = 17025137
59 Z = 5209010
56
XDOT = 12922
731402 XDOT = 3871
675727
YDOT = 21266
784815 feet/sec YDOT = 6525
787305 meter/sec
ZDOT = -3785
355704 ZDOT = -1134
805217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11884172
07 X = -3622295
65
Y = -7736441
22 feet Y = -2358067
29 meter
Z = 17110372
08 Z = 5215241
41
XDOT = 9037
915648 XDOT = 2754
756690
YDOT = -22104
597431 feet/sec YDOT = -6737
481297 meter/sec
ZDOT = -3704
877322 ZDOT = -1129
246608
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
54629280
00016717 00000-0 10270-3 0 9024
2 25544 51
6418 232
5185 0001061 12
3047 347
8132 15
54945656 34643
Satellite: ISS
Catalog Number: 25544
Epoch time: 15210
54629280 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 232
5185 deg
Eccentricity:
0001061
Arg of perigee: 12
3047 deg
Mean anomaly: 347
8132 deg
Mean motion: 15
54945656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3464
Checksum: 291
Coasting Arc #4 (Orbit 3478)
---------------------------------------
Vector Time (GMT): 2015/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5103077
37 A = 6778423
22 meter
Y = -210307
42 meter E =
0009421
Z = -4465805
93 I = 51
36397
XDOT = -2551
673307 Wp = 103
86313
YDOT = -6464
962738 meter/sec RA = 226
69935 deg
ZDOT = 3223
772314 TA = 198
71287
MA = 198
74753
Ha = 219
827 n
mi
Hp = 213
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16742379
81 X = -5078653
62
Y = -689984
96 feet Y = -267236
53 meter
Z = -14651594
27 Z = -4490535
88
XDOT = -8371
631584 XDOT = -2494
850448
YDOT = -21210
507672 feet/sec YDOT = -6493
179715 meter/sec
ZDOT = 10576
680820 ZDOT = 3211
514633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9459653
65 X = 2883302
43
Y = 13717508
08 feet Y = 4181096
46 meter
Z = -14757963
96 Z = -4498227
42
XDOT = -10870
556526 XDOT = -3313
345629
YDOT = 18807
419771 feet/sec YDOT = 5732
501546 meter/sec
ZDOT = 10525
063121 ZDOT = 3208
039239
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
51031902
00016717 00000-0 10270-3 0 9031
2 25544 51
6425 227
7068 0001152 9
9610 350
1566 15
54930739 34796
Satellite: ISS
Catalog Number: 25544
Epoch time: 15211
51031902 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 227
7068 deg
Eccentricity:
0001152
Arg of perigee: 9
9610 deg
Mean anomaly: 350
1566 deg
Mean motion: 15
54930739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3479
Checksum: 291
Coasting Arc #5 (Orbit 3494)
---------------------------------------
Vector Time (GMT): 2015/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5751311
17 A = 6782699
13 meter
Y = 1818967
74 meter E =
0013254
Z = 3089934
80 I = 51
39972
XDOT = 763
758520 Wp = 89
92140
YDOT = 5881
909868 meter/sec RA = 221
68805 deg
ZDOT = -4866
002561 TA = 54
39069
MA = 54
26728
Ha = 219
757 n
mi
Hp = 213
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18869131
13 X = 5715534
19
Y = 5967741
94 feet Y = 1883082
51 meter
Z = 10137581
36 Z = 3117786
09
XDOT = 2505
769423 XDOT = 721
565496
YDOT = 19297
604553 feet/sec YDOT = 5890
215011 meter/sec
ZDOT = -15964
575331 ZDOT = -4862
394683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6858675
64 X = -2090524
33
Y = -18498072
19 feet Y = -5638212
40 meter
Z = 10257119
62 Z = 3126370
06
XDOT = 12262
545694 XDOT = 3737
623928
YDOT = -13423
513883 feet/sec YDOT = -4091
487031 meter/sec
ZDOT = -15950
059750 ZDOT = -4861
578212
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
53860523
00016717 00000-0 10270-3 0 9044
2 25544 51
6409 222
5733 0001238 16
4726 343
6467 15
54982690 34954
Satellite: ISS
Catalog Number: 25544
Epoch time: 15212
53860523 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 222
5733 deg
Eccentricity:
0001238
Arg of perigee: 16
4726 deg
Mean anomaly: 343
6467 deg
Mean motion: 15
54982690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3495
Checksum: 312
Coasting Arc #6 (Orbit 3509)
---------------------------------------
Vector Time (GMT): 2015/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5892821
94 A = 6785990
52 meter
Y = -3091842
55 meter E =
0009829
Z = -1306802
05 I = 51
43579
XDOT = 1258
117540 Wp = 36
65919
YDOT = -4841
793774 meter/sec RA = 216
69247 deg
ZDOT = 5812
557489 TA = 309
07393
MA = 309
16133
Ha = 219
767 n
mi
Hp = 213
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19333405
31 X = -5851462
44
Y = -10143840
38 feet Y = -3157508
67 meter
Z = -4287408
31 Z = -1335327
18
XDOT = 4127
682219 XDOT = 1283
931572
YDOT = -15885
150178 feet/sec YDOT = -4827
580458 meter/sec
ZDOT = 19070
070502 ZDOT = 5818
731640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4243289
64 X = 1293354
68
Y = 21391807
60 feet Y = 6520222
96 meter
Z = -4409647
25 Z = -1344060
48
XDOT = -13312
130445 XDOT = -4057
537360
YDOT = 6557
341964 feet/sec YDOT = 1998
677831 meter/sec
ZDOT = 19097
463350 ZDOT = 5820
906829
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
50261682
00016717 00000-0 10270-3 0 9054
2 25544 51
6414 217
7617 0001093 25
2433 334
8773 15
55012405 35108
Satellite: ISS
Catalog Number: 25544
Epoch time: 15213
50261682 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 217
7617 deg
Eccentricity:
0001093
Arg of perigee: 25
2433 deg
Mean anomaly: 334
8773 deg
Mean motion: 15
55012405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3510
Checksum: 276
Coasting Arc #7 (Orbit 3525)
---------------------------------------
Vector Time (GMT): 2015/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5426563
15 A = 6786667
37 meter
Y = 4008143
43 meter E =
0010139
Z = -700805
38 I = 51
46285
XDOT = -3345
486304 Wp = 133
57512
YDOT = 3500
363372 meter/sec RA = 211
70409 deg
ZDOT = -5946
274126 TA = 54
01543
MA = 53
92146
Ha = 219
905 n
mi
Hp = 213
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17803684
88 X = 5384743
99
Y = 13150076
88 feet Y = 4068593
00 meter
Z = -2299230
26 Z = -674546
33
XDOT = -10976
004936 XDOT = -3355
495415
YDOT = 11484
131799 feet/sec YDOT = 3462
895979 meter/sec
ZDOT = -19508
773380 ZDOT = -5962
549815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1350878
20 X = -411747
67
Y = -22103729
48 feet Y = -6737216
75 meter
Z = -2186880
89 Z = -666561
29
XDOT = 14158
059387 XDOT = 4315
376501
YDOT = 1051
088907 feet/sec YDOT = 320
371899 meter/sec
ZDOT = -19579
412724 ZDOT = -5967
804998
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
53088788
00016717 00000-0 10270-3 0 9063
2 25544 51
6406 212
6277 0001262 23
6254 336
4957 15
54978886 35268
Satellite: ISS
Catalog Number: 25544
Epoch time: 15214
53088788 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 212
6277 deg
Eccentricity:
0001262
Arg of perigee: 23
6254 deg
Mean anomaly: 336
4957 deg
Mean motion: 15
54978886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3526
Checksum: 335
Coasting Arc #8 (Orbit 3541)
---------------------------------------
Vector Time (GMT): 2015/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4366771
98 A = 6783968
21 meter
Y = -4495423
35 meter E =
0014336
Z = 2578583
33 I = 51
48178
XDOT = 5215
235460 Wp = 72
69451
YDOT = -2047
173676 meter/sec RA = 206
71521 deg
ZDOT = 5242
986987 TA = 316
40392
MA = 316
51711
Ha = 219
806 n
mi
Hp = 213
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14326679
72 X = -4328704
09
Y = -14748764
27 feet Y = -4544042
57 meter
Z = 8459919
07 Z = 2557463
31
XDOT = 17110
352560 XDOT = 5212
271833
YDOT = -6716
449068 feet/sec YDOT = -1988
869983 meter/sec
ZDOT = 17201
400877 ZDOT = 5268
313966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1728114
62 X = -526729
34
Y = 20525857
83 feet Y = 6256281
47 meter
Z = 8369755
66 Z = 2551101
53
XDOT = -14711
065863 XDOT = -4483
932875
YDOT = -8324
232009 feet/sec YDOT = -2537
225916 meter/sec
ZDOT = 17310
760661 ZDOT = 5276
319850
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
55914882
00016717 00000-0 10270-3 0 9070
2 25544 51
6406 207
4952 0001156 19
7714 340
3483 15
55023742 35428
Satellite: ISS
Catalog Number: 25544
Epoch time: 15215
55914882 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 207
4952 deg
Eccentricity:
0001156
Arg of perigee: 19
7714 deg
Mean anomaly: 340
3483 deg
Mean motion: 15
55023742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3542
Checksum: 302
Coasting Arc #9 (Orbit 3556)
---------------------------------------
Vector Time (GMT): 2015/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2754279
40 A = 6779655
23 meter
Y = 4629642
59 meter E =
0008448
Z = -4125461
50 I = 51
49575
XDOT = -6640
497962 Wp = 65
06596
YDOT = 588
505664 meter/sec RA = 201
71510 deg
ZDOT = -3775
556174 TA = 165
91579
MA = 165
89221
Ha = 219
902 n
mi
Hp = 213
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9036349
74 X = 2722344
59
Y = 15189116
10 feet Y = 4660264
11 meter
Z = -13534978
66 Z = -4112159
58
XDOT = -21786
410635 XDOT = -6628
245256
YDOT = 1930
792861 feet/sec YDOT = 514
315695 meter/sec
ZDOT = -12386
995321 ZDOT = -3807
784225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5213335
04 X = 1589024
52
Y = -16932578
22 feet Y = -5161049
84 meter
Z = -13478480
80 Z = -4108240
95
XDOT = 14697
182355 XDOT = 4479
701182
YDOT = 14488
954834 feet/sec YDOT = 4416
233433 meter/sec
ZDOT = -12525
829580 ZDOT = -3817
872856
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 15216
52313869
00016717 00000-0 10270-3 0 9087
2 25544 51
6404 202
6821 0001334 26
4243 333
6978 15
54996184 35576
Satellite: ISS
Catalog Number: 25544
Epoch time: 15216
52313869 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 202
6821 deg
Eccentricity:
0001334
Arg of perigee: 26
4243 deg
Mean anomaly: 333
6978 deg
Mean motion: 15
54996184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3557
Checksum: 317
Coasting Arc #10 (Orbit 3572)
---------------------------------------
Vector Time (GMT): 2015/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -772766
17 A = 6775867
95 meter
Y = -4433519
18 meter E =
0005376
Z = 5061630
43 I = 51
51317
XDOT = 7425
226460 Wp = 110
46376
YDOT = 746
988514 meter/sec RA = 196
70452 deg
ZDOT = 1784
533295 TA = 322
23276
MA = 322
27048
Ha = 219
856 n
mi
Hp = 213
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2535322
07 X = -747719
30
Y = -14545666
60 feet Y = -4442020
65 meter
Z = 16606399
06 Z = 5057937
42
XDOT = 24360
979199 XDOT = 7407
653093
YDOT = 2450
749719 feet/sec YDOT = 829
924037 meter/sec
ZDOT = 5854
768029 ZDOT = 1820
560532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8860061
49 X = -2700546
74
Y = 11832462
52 feet Y = 3606534
58 meter
Z = 16591229
78 Z = 5057006
84
XDOT = -13892
599701 XDOT = -4234
464389
YDOT = -18844
983147 feet/sec YDOT = -5743
950863 meter/sec
ZDOT = 6009
751430 ZDOT = 1831
772236
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 15217
55138444
00016717 00000-0 10270-3 0 9096
2 25544 51
6404 197
5494 0001377 22
6885 337
4329 15
55018257 35738
Satellite: ISS
Catalog Number: 25544
Epoch time: 15217
55138444 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 197
5494 deg
Eccentricity:
0001377
Arg of perigee: 22
6885 deg
Mean anomaly: 337
4329 deg
Mean motion: 15
55018257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3573
Checksum: 328
Coasting Arc #11 (Orbit 3587)
---------------------------------------
Vector Time (GMT): 2015/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1377090
72 A = 6774830
75 meter
Y = 4011169
01 meter E =
0015452
Z = -5296580
88 I = 51
54061
XDOT = -7399
972103 Wp = 89
01648
YDOT = -1915
711284 meter/sec RA = 191
68723 deg
ZDOT = 474
630558 TA = 185
51434
MA = 185
53137
Ha = 219
899 n
mi
Hp = 212
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4518014
16 X = -1396113
64
Y = 13160003
32 feet Y = 3995663
11 meter
Z = -17377233
86 Z = -5303316
67
XDOT = -24278
123696 XDOT = -7380
305734
YDOT = -6285
142007 feet/sec YDOT = -1998
352669 meter/sec
ZDOT = 1557
186871 ZDOT = 438
731002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12540581
55 X = 3822369
26
Y = -5941395
69 feet Y = -1810937
41 meter
Z = -17406895
98 Z = -5305621
89
XDOT = 11866
712567 XDOT = 3616
973991
YDOT = 20950
973026 feet/sec YDOT = 6385
856578 meter/sec
ZDOT = 1402
929008 ZDOT = 427
612762
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 15218
51535711
00016717 00000-0 10270-3 0 9103
2 25544 51
6405 192
7370 0001418 28
8314 331
2918 15
55017524 35888
Satellite: ISS
Catalog Number: 25544
Epoch time: 15218
51535711 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 192
7370 deg
Eccentricity:
0001418
Arg of perigee: 28
8314 deg
Mean anomaly: 331
2918 deg
Mean motion: 15
55017524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3588
Checksum: 295
Coasting Arc #12 (Orbit 3603)
---------------------------------------
Vector Time (GMT): 2015/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3439165
34 A = 6776976
33 meter
Y = -3390783
97 meter E =
0008735
Z = 4749931
04 I = 51
57941
XDOT = 6576
100094 Wp = 56
59987
YDOT = 2907
708088 meter/sec RA = 186
67444 deg
ZDOT = -2677
434750 TA = 59
89264
MA = 59
80609
Ha = 219
753 n
mi
Hp = 212
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11283350
85 X = 3453753
10
Y = -11124619
31 feet Y = -3352243
46 meter
Z = 15583763
26 Z = 4766673
09
XDOT = 21575
131541 XDOT = 6556
102520
YDOT = 9539
724698 feet/sec YDOT = 2981
134580 meter/sec
ZDOT = -8784
234744 ZDOT = -2645
538125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15773222
34 X = -4807678
17
Y = -83266
02 feet Y = -25379
48 meter
Z = 15656416
02 Z = 4772075
60
XDOT = -8499
717919 XDOT = -2590
714022
YDOT = -20911
905886 feet/sec YDOT = -6373
948914 meter/sec
ZDOT = -8647
359192 ZDOT = -2635
715082
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 15219
54358556
00016717 00000-0 10270-3 0 9118
2 25544 51
6403 187
6040 0001443 26
9634 333
1594 15
55048122 36043
Satellite: ISS
Catalog Number: 25544
Epoch time: 15219
54358556 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 187
6040 deg
Eccentricity:
0001443
Arg of perigee: 26
9634 deg
Mean anomaly: 333
1594 deg
Mean motion: 15
55048122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3604
Checksum: 295
Coasting Arc #13 (Orbit 3618)
---------------------------------------
Vector Time (GMT): 2015/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5141860
83 A = 6781263
68 meter
Y = 2654310
86 meter E =
0006064
Z = -3540326
41 I = 51
62545
XDOT = -4993
183422 Wp = 83
89403
YDOT = -3699
485791 meter/sec RA = 181
67494 deg
ZDOT = 4485
547664 TA = 234
36970
MA = 234
42620
Ha = 219
868 n
mi
Hp = 212
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16869622
15 X = -5153962
41
Y = 8708368
97 feet Y = 2596743
62 meter
Z = -11615244
12 Z = -3565333
66
XDOT = -16381
835375 XDOT = -4973
232675
YDOT = -12137
420574 feet/sec YDOT = -3755
211408 meter/sec
ZDOT = 14716
363726 ZDOT = 4461
340347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18114776
21 X = 5521383
79
Y = 5454441
86 feet Y = 1662513
88 meter
Z = -11723381
96 Z = -3573286
82
XDOT = 3761
888858 XDOT = 1146
623724
YDOT = 18863
298612 feet/sec YDOT = 5749
533417 meter/sec
ZDOT = 14612
716880 ZDOT = 4453
956105
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 15220
50754169
00016717 00000-0 10270-3 0 9127
2 25544 51
6403 182
7917 0001519 30
9145 329
2097 15
55039505 36193
Satellite: ISS
Catalog Number: 25544
Epoch time: 15220
50754169 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 182
7917 deg
Eccentricity:
0001519
Arg of perigee: 30
9145 deg
Mean anomaly: 329
2097 deg
Mean motion: 15
55039505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3619
Checksum: 304
Coasting Arc #14 (Orbit 3634)
---------------------------------------
Vector Time (GMT): 2015/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6295177
89 A = 6785180
74 meter
Y = -1775310
66 meter E =
0014267
Z = 1782301
15 I = 51
67107
XDOT = 2833
392742 Wp = 108
49129
YDOT = 4324
320342 meter/sec RA = 176
69145 deg
ZDOT = -5667
584196 TA = 51
92749
MA = 51
79887
Ha = 219
840 n
mi
Hp = 212
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20653470
76 X = 6305904
33
Y = -5824510
05 feet Y = -1704853
93 meter
Z = 5847444
72 Z = 1812907
52
XDOT = 9295
907947 XDOT = 2812
357220
YDOT = 14187
402698 feet/sec YDOT = 4355
887758 meter/sec
ZDOT = -18594
436338 ZDOT = -5653
871256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19019208
56 X = -5797054
77
Y = -9858895
53 feet Y = -3004991
36 meter
Z = 5979570
75 Z = 1822573
17
XDOT = 2121
997598 XDOT = 646
784868
YDOT = -15399
765527 feet/sec YDOT = -4693
848533 meter/sec
ZDOT = -18536
081354 ZDOT = -5649
797597
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 15221
53575270
00016717 00000-0 10270-3 0 9136
2 25544 51
6408 177
6581 0001518 32
7458 327
3789 15
55072081 36355
Satellite: ISS
Catalog Number: 25544
Epoch time: 15221
53575270 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 177
6581 deg
Eccentricity:
0001518
Arg of perigee: 32
7458 deg
Mean anomaly: 327
3789 deg
Mean motion: 15
55072081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3635
Checksum: 315
Coasting Arc #15 (Orbit 3650)
---------------------------------------
Vector Time (GMT): 2015/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6727394
90 A = 6786513
27 meter
Y = 815722
71 meter E =
0013863
Z = 204751
95 I = 51
70738
XDOT = -384
678099 Wp = 46
40049
YDOT = -4744
189724 meter/sec RA = 171
71947 deg
ZDOT = 6016
302645 TA = 315
80474
MA = 315
91540
Ha = 219
828 n
mi
Hp = 212
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22071505
57 X = -6737011
11
Y = 2676255
62 feet Y = 740438
79 meter
Z = 671758
38 Z = 172048
76
XDOT = -1262
067253 XDOT = -360
823312
YDOT = -15564
926915 feet/sec YDOT = -4748
358243 meter/sec
ZDOT = 19738
525737 ZDOT = 6014
491784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18153474
36 X = 5533178
99
Y = 12842688
47 feet Y = 3914451
45 meter
Z = 530738
29 Z = 161769
03
XDOT = -8487
215027 XDOT = -2586
903140
YDOT = 11139
388501 feet/sec YDOT = 3395
285615 meter/sec
ZDOT = 19731
505582 ZDOT = 6014
162901
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 15222
56395378
00016717 00000-0 10270-3 0 9140
2 25544 51
6409 172
5249 0001466 36
7380 323
3874 15
55094932 36519
Satellite: ISS
Catalog Number: 25544
Epoch time: 15222
56395378 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 172
5249 deg
Eccentricity:
0001466
Arg of perigee: 36
7380 deg
Mean anomaly: 323
3874 deg
Mean motion: 15
55094932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3651
Checksum: 323
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