[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 8th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 568 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 2621)
---------------------------------------
Vector Time (GMT): 2015/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1738378
17 A = 6779592
83 meter
Y = 5289213
50 meter E =
0008380
Z = -3873234
84 I = 51
86101
XDOT = -6376
891572 Wp = 72
01895
YDOT = 934
691253 meter/sec RA = 141
30378 deg
ZDOT = 4148
341536 TA = 241
42160
MA = 241
50595
Ha = 220
313 n
mi
Hp = 212
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5703340
45 X = -1778579
45
Y = 17353062
65 feet Y = 5269549
52 meter
Z = -12707463
38 Z = -3881776
55
XDOT = -20921
560275 XDOT = -6407
020704
YDOT = 3066
572353 feet/sec YDOT = 863
211703 meter/sec
ZDOT = 13610
044408 ZDOT = 4117
290687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14905848
24 X = 4543302
54
Y = 10512593
82 feet Y = 3204238
59 meter
Z = -12745099
48 Z = -3884706
32
XDOT = -2529
720955 XDOT = -771
058947
YDOT = 19886
090437 feet/sec YDOT = 6061
280365 meter/sec
ZDOT = 13476
449728 ZDOT = 4107
621877
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 15156
50838088
00016717 00000-0 10270-3 0 9005
2 25544 51
6393 142
3529 0004705 22
0910 338
0445 15
55274795 26224
Satellite: ISS
Catalog Number: 25544
Epoch time: 15156
50838088 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 142
3529 deg
Eccentricity:
0004705
Arg of perigee: 22
0910 deg
Mean anomaly: 338
0445 deg
Mean motion: 15
55274795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2622
Checksum: 303
Coasting Arc #2 (Orbit 2637)
---------------------------------------
Vector Time (GMT): 2015/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3343805
24 A = 6783882
11 meter
Y = -5499812
18 meter E =
0015051
Z = 2129153
84 I = 51
90020
XDOT = 5215
752498 Wp = 91
52214
YDOT = 1016
919381 meter/sec RA = 136
33180 deg
ZDOT = -5531
179614 TA = 64
95682
MA = 64
80064
Ha = 220
284 n
mi
Hp = 211
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10970489
64 X = 3394714
31
Y = -18044003
21 feet Y = -5462135
15 meter
Z = 6985412
85 Z = 2145520
42
XDOT = 17112
048877 XDOT = 5230
861798
YDOT = 3336
349674 feet/sec YDOT = 1075
330443 meter/sec
ZDOT = -18146
914745 ZDOT = -5505
805696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14263824
99 X = -4347613
86
Y = -15539614
85 feet Y = -4736474
61 meter
Z = 7056724
03 Z = 2150889
49
XDOT = 6890
233924 XDOT = 2100
143300
YDOT = -14564
926918 feet/sec YDOT = -4439
389725 meter/sec
ZDOT = -18038
044833 ZDOT = -5497
996065
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 15157
53643460
00016717 00000-0 10270-3 0 9018
2 25544 51
6395 137
2178 0004777 24
1539 335
9838 15
55328481 26389
Satellite: ISS
Catalog Number: 25544
Epoch time: 15157
53643460 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 137
2178 deg
Eccentricity:
0004777
Arg of perigee: 24
1539 deg
Mean anomaly: 335
9838 deg
Mean motion: 15
55328481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2638
Checksum: 331
Coasting Arc #3 (Orbit 2652)
---------------------------------------
Vector Time (GMT): 2015/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4427162
05 A = 6785774
68 meter
Y = 5130923
10 meter E =
0016417
Z = -88297
82 I = 51
92898
XDOT = -3628
830590 Wp = 40
82080
YDOT = -3038
221221 meter/sec RA = 131
37366 deg
ZDOT = 6040
330525 TA = 318
23097
MA = 318
35617
Ha = 220
311 n
mi
Hp = 211
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14524809
88 X = -4483779
31
Y = 16833737
21 feet Y = 5081099
12 meter
Z = -289691
00 Z = -109941
10
XDOT = -11905
612172 XDOT = -3623
928379
YDOT = -9967
917391 feet/sec YDOT = -3078
774352 meter/sec
ZDOT = 19817
357366 ZDOT = 6022
714013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12414835
32 X = 3784041
81
Y = 18443248
74 feet Y = 5621502
22 meter
Z = -383629
00 Z = -116930
12
XDOT = -11437
883147 XDOT = -3486
266783
YDOT = 8076
757566 feet/sec YDOT = 2461
795706 meter/sec
ZDOT = 19742
177685 ZDOT = 6017
415758
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 15158
50022777
00016717 00000-0 10270-3 0 9029
2 25544 51
6395 132
4050 0004633 30
1378 330
0041 15
55350729 26533
Satellite: ISS
Catalog Number: 25544
Epoch time: 15158
50022777 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 132
4050 deg
Eccentricity:
0004633
Arg of perigee: 30
1378 deg
Mean anomaly: 330
0041 deg
Mean motion: 15
55350729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2653
Checksum: 276
Coasting Arc #4 (Orbit 2668)
---------------------------------------
Vector Time (GMT): 2015/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4999867
89 A = 6784127
17 meter
Y = -4120781
53 meter E =
0006950
Z = -2014694
27 I = 51
94446
XDOT = 1809
239993 Wp = 99
35445
YDOT = 4920
039289 meter/sec RA = 126
41654 deg
ZDOT = -5590
770773 TA = 102
79913
MA = 102
72146
Ha = 220
416 n
mi
Hp = 211
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16403766
04 X = 5055362
47
Y = -13519624
46 feet Y = -4064559
29 meter
Z = -6609889
32 Z = -1990271
43
XDOT = 5935
826749 XDOT = 1781
246312
YDOT = 16141
861185 feet/sec YDOT = 4940
115315 meter/sec
ZDOT = -18342
423795 ZDOT = -5582
049448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9044813
50 X = -2756859
16
Y = -19272818
69 feet Y = -5874355
14 meter
Z = -6504170
28 Z = -1982471
10
XDOT = 15729
051612 XDOT = 4794
214931
YDOT = -1223
568874 feet/sec YDOT = -372
943793 meter/sec
ZDOT = -18305
812336 ZDOT = -5579
611600
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 15159
52826453
00016717 00000-0 10270-3 0 9036
2 25544 51
6403 127
2699 0004821 31
3803 328
7638 15
55343092 26697
Satellite: ISS
Catalog Number: 25544
Epoch time: 15159
52826453 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 127
2699 deg
Eccentricity:
0004821
Arg of perigee: 31
3803 deg
Mean anomaly: 328
7638 deg
Mean motion: 15
55343092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2669
Checksum: 317
Coasting Arc #5 (Orbit 2684)
---------------------------------------
Vector Time (GMT): 2015/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5016169
45 A = 6779753
70 meter
Y = 2552940
51 meter E =
0014432
Z = 3765223
02 I = 51
94844
XDOT = -25
380256 Wp = 79
90828
YDOT = -6374
791341 meter/sec RA = 121
45108 deg
ZDOT = 4277
085166 TA = 325
00996
MA = 325
10471
Ha = 220
444 n
mi
Hp = 211
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16457248
87 X = -5062634
30
Y = 8375789
08 feet Y = 2496586
37 meter
Z = 12353093
91 Z = 3740742
71
XDOT = -83
268556 XDOT = 25
129560
YDOT = -20914
669753 feet/sec YDOT = -6374
793030 meter/sec
ZDOT = 14032
431647 ZDOT = 4277
084129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4348898
64 X = 1325544
30
Y = 18018939
07 feet Y = 5492172
63 meter
Z = 12247396
76 Z = 3733006
53
XDOT = -19078
324646 XDOT = -5815
073352
YDOT = -4959
646636 feet/sec YDOT = -1511
700295 meter/sec
ZDOT = 14033
572074 ZDOT = 4277
432768
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 15160
55629076
00016717 00000-0 10270-3 0 9044
2 25544 51
6404 122
1361 0004614 34
6547 325
4907 15
55384453 26856
Satellite: ISS
Catalog Number: 25544
Epoch time: 15160
55629076 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 122
1361 deg
Eccentricity:
0004614
Arg of perigee: 34
6547 deg
Mean anomaly: 325
4907 deg
Mean motion: 15
55384453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2685
Checksum: 304
Coasting Arc #6 (Orbit 2699)
---------------------------------------
Vector Time (GMT): 2015/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4605599
72 A = 6775483
38 meter
Y = -550350
97 meter E =
0016322
Z = -4954020
48 I = 51
94983
XDOT = -1579
889893 Wp = 63
77400
YDOT = 7143
526567 meter/sec RA = 116
46959 deg
ZDOT = -2261
106820 TA = 184
19680
MA = 184
21050
Ha = 220
456 n
mi
Hp = 211
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15110235
30 X = 4635476
48
Y = -1805613
40 feet Y = -498680
76 meter
Z = -16253348
04 Z = -4931574
72
XDOT = -5183
365791 XDOT = -1648
669427
YDOT = 23436
766951 feet/sec YDOT = 7125
474783 meter/sec
ZDOT = -7418
329462 ZDOT = -2268
948253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1478552
59 X = 450662
83
Y = -15248740
36 feet Y = -4647816
06 meter
Z = -16156750
07 Z = -4924577
42
XDOT = 20689
846109 XDOT = 6306
265094
YDOT = 9907
678891 feet/sec YDOT = 3019
860526 meter/sec
ZDOT = -7453
334997 ZDOT = -2271
776507
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 15161
52005940
00016717 00000-0 10270-3 0 9051
2 25544 51
6405 117
3217 0004789 37
7162 322
4326 15
55361377 27003
Satellite: ISS
Catalog Number: 25544
Epoch time: 15161
52005940 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 117
3217 deg
Eccentricity:
0004789
Arg of perigee: 37
7162 deg
Mean anomaly: 322
4326 deg
Mean motion: 15
55361377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2700
Checksum: 288
Coasting Arc #7 (Orbit 2715)
---------------------------------------
Vector Time (GMT): 2015/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3836636
13 A = 6773683
69 meter
Y = -1641562
22 meter E =
0006705
Z = 5330890
08 I = 51
95787
XDOT = 2888
033329 Wp = 55
22541
YDOT = -7110
365552 meter/sec RA = 111
47946 deg
ZDOT = -107
186246 TA = 35
81309
MA = 35
76815
Ha = 220
583 n
mi
Hp = 211
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12587388
88 X = -3843890
33
Y = -5385702
81 feet Y = -1684506
95 meter
Z = 17489796
83 Z = 5312234
54
XDOT = 9475
174963 XDOT = 2967
849166
YDOT = -23327
970970 feet/sec YDOT = -7077
623389 meter/sec
ZDOT = -351
660912 ZDOT = -92
963280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7773226
24 X = -2369279
36
Y = 11393588
32 feet Y = 3472765
72 meter
Z = 17409889
31 Z = 5306534
26
XDOT = -20181
435495 XDOT = -6151
301539
YDOT = -13307
522945 feet/sec YDOT = -4056
132994 meter/sec
ZDOT = -289
209017 ZDOT = -88
150908
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 15162
54806852
00016717 00000-0 10270-3 0 9066
2 25544 51
6409 112
1875 0004790 40
3284 319
8224 15
55386820 27161
Satellite: ISS
Catalog Number: 25544
Epoch time: 15162
54806852 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 112
1875 deg
Eccentricity:
0004790
Arg of perigee: 40
3284 deg
Mean anomaly: 319
8224 deg
Mean motion: 15
55386820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2716
Checksum: 311
Coasting Arc #8 (Orbit 2730)
---------------------------------------
Vector Time (GMT): 2015/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2878516
02 A = 6775647
49 meter
Y = 3728550
16 meter E =
0014578
Z = -4883048
61 I = 51
97536
XDOT = -3827
540742 Wp = 90
38300
YDOT = 6163
491789 meter/sec RA = 106
48951 deg
ZDOT = 2456
176010 TA = 203
60387
MA = 203
67082
Ha = 220
516 n
mi
Hp = 211
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9443950
20 X = 2860328
82
Y = 12232776
10 feet Y = 3760638
36 meter
Z = -16020500
70 Z = -4869109
02
XDOT = -12557
548367 XDOT = -3908
109220
YDOT = 20221
429753 feet/sec YDOT = 6120
239015 meter/sec
ZDOT = 8058
320243 ZDOT = 2437
387224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13746132
11 X = 4189821
07
Y = -7194971
34 feet Y = -2193027
26 meter
Z = -15961255
86 Z = -4864990
78
XDOT = 17105
678931 XDOT = 5213
810938
YDOT = 15031
420385 feet/sec YDOT = 4581
576933 meter/sec
ZDOT = 7976
392870 ZDOT = 2431
204547
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 15163
51181870
00016717 00000-0 10270-3 0 9071
2 25544 51
6410 107
3732 0004800 43
5201 316
6331 15
55386494 27315
Satellite: ISS
Catalog Number: 25544
Epoch time: 15163
51181870 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 107
3732 deg
Eccentricity:
0004800
Arg of perigee: 43
5201 deg
Mean anomaly: 316
6331 deg
Mean motion: 15
55386494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2731
Checksum: 280
Coasting Arc #9 (Orbit 2746)
---------------------------------------
Vector Time (GMT): 2015/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1775780
06 A = 6780067
59 meter
Y = -5445667
60 meter E =
0015991
Z = 3618176
25 I = 51
99938
XDOT = 4438
922743 Wp = 75
44421
YDOT = -4411
163164 meter/sec RA = 101
51231 deg
ZDOT = -4440
333723 TA = 61
88943
MA = 61
72790
Ha = 220
534 n
mi
Hp = 211
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5826050
07 X = -1732329
26
Y = -17866363
52 feet Y = -5465282
99 meter
Z = 11870656
99 Z = 3609654
70
XDOT = 14563
394827 XDOT = 4509
489227
YDOT = -14472
320091 feet/sec YDOT = -4361
129175 meter/sec
ZDOT = -14568
024027 ZDOT = -4418
599143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18586960
31 X = -5665305
50
Y = 2918751
72 feet Y = 889635
52 meter
Z = 11835036
84 Z = 3607319
23
XDOT = -11685
868880 XDOT = -3561
852835
YDOT = -15458
287051 feet/sec YDOT = -4711
685893 meter/sec
ZDOT = -14473
738751 ZDOT = -4411
595571
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 15164
53980953
00016717 00000-0 10270-3 0 9084
2 25544 51
6419 102
2386 0004819 47
0074 313
1482 15
55413925 27476
Satellite: ISS
Catalog Number: 25544
Epoch time: 15164
53980953 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 102
2386 deg
Eccentricity:
0004819
Arg of perigee: 47
0074 deg
Mean anomaly: 313
1482 deg
Mean motion: 15
55413925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2747
Checksum: 314
Coasting Arc #10 (Orbit 2761)
---------------------------------------
Vector Time (GMT): 2015/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 674142
91 A = 6784225
46 meter
Y = 6500193
40 meter E =
0012115
Z = -1807665
61 I = 52
01878
XDOT = -4709
356882 Wp = 43
02500
YDOT = 2062
435129 meter/sec RA = 96
55115 deg
ZDOT = 5691
011681 TA = 297
20576
MA = 297
32918
Ha = 220
558 n
mi
Hp = 211
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2211754
96 X = 610187
13
Y = 21326093
83 feet Y = 6507374
74 meter
Z = -5930661
44 Z = -1804545
23
XDOT = -15450
645937 XDOT = -4759
714573
YDOT = 6766
519453 feet/sec YDOT = 2009
489728 meter/sec
ZDOT = 18671
298165 ZDOT = 5668
012268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21425832
03 X = 6530593
60
Y = 878756
58 feet Y = 267845
01 meter
Z = -5918478
85 Z = -1803952
35
XDOT = 4493
954740 XDOT = 1369
757405
YDOT = 14826
091532 feet/sec YDOT = 4518
992699 meter/sec
ZDOT = 18572
002989 ZDOT = 5660
746511
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 15165
50354243
00016717 00000-0 10270-3 0 9090
2 25544 51
6419 97
4250 0004818 49
7250 310
4324 15
55407983 27624
Satellite: ISS
Catalog Number: 25544
Epoch time: 15165
50354243 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 97
4250 deg
Eccentricity:
0004818
Arg of perigee: 49
7250 deg
Mean anomaly: 310
4324 deg
Mean motion: 15
55407983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2762
Checksum: 308
Coasting Arc #11 (Orbit 2777)
---------------------------------------
Vector Time (GMT): 2015/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 460510
30 A = 6785512
68 meter
Y = -6757624
60 meter E =
0012893
Z = -347984
98 I = 52
02729
XDOT = 4692
914702 Wp = 115
69704
YDOT = 621
250946 meter/sec RA = 91
60032 deg
ZDOT = -6032
440897 TA = 68
03481
MA = 67
89785
Ha = 220
557 n
mi
Hp = 211
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1510860
56 X = 537731
84
Y = -22170684
37 feet Y = -6752043
05 meter
Z = -1141683
01 Z = -345561
28
XDOT = 15396
701779 XDOT = 4714
922457
YDOT = 2038
224889 feet/sec YDOT = 673
854087 meter/sec
ZDOT = -19791
472760 ZDOT = -6009
589937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21791802
02 X = -6642141
26
Y = -4354990
42 feet Y = -1327401
08 meter
Z = -1129959
44 Z = -344411
64
XDOT = 3696
902804 XDOT = 1126
815975
YDOT = -13542
748017 feet/sec YDOT = -4127
829595 meter/sec
ZDOT = -19693
320245 ZDOT = -6002
524011
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 15166
53151528
00016717 00000-0 10270-3 0 9107
2 25544 51
6433 92
2900 0004791 54
4176 305
7423 15
55423899 27783
Satellite: ISS
Catalog Number: 25544
Epoch time: 15166
53151528 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 92
2900 deg
Eccentricity:
0004791
Arg of perigee: 54
4176 deg
Mean anomaly: 305
7423 deg
Mean motion: 15
55423899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2778
Checksum: 314
Coasting Arc #12 (Orbit 2793)
---------------------------------------
Vector Time (GMT): 2015/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1518672
40 A = 6783092
92 meter
Y = 6148793
98 meter E =
0018479
Z = 2402352
15 I = 52
01928
XDOT = -4411
304788 Wp = 69
44402
YDOT = -3209
935312 meter/sec RA = 86
64774 deg
ZDOT = 5400
051294 TA = 317
29574
MA = 317
43921
Ha = 220
606 n
mi
Hp = 211
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4982521
01 X = -1598986
57
Y = 20173208
58 feet Y = 6131361
77 meter
Z = 7881732
77 Z = 2394780
54
XDOT = -14472
784737 XDOT = -4401
314155
YDOT = -10531
283831 feet/sec YDOT = -3259
210343 meter/sec
ZDOT = 17716
703721 ZDOT = 5378
645765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19487410
81 X = 5939762
81
Y = 7249532
52 feet Y = 2209657
51 meter
Z = 7847972
34 Z = 2392061
97
XDOT = -11560
855091 XDOT = -3523
748632
YDOT = 11899
806019 feet/sec YDOT = 3627
060875 meter/sec
ZDOT = 17625
265291 ZDOT = 5372
180861
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 15167
55947854
00016717 00000-0 10270-3 0 9116
2 25544 51
6433 87
1557 0004843 57
1977 302
9642 15
55440164 27945
Satellite: ISS
Catalog Number: 25544
Epoch time: 15167
55947854 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 87
1557 deg
Eccentricity:
0004843
Arg of perigee: 57
1977 deg
Mean anomaly: 302
9642 deg
Mean motion: 15
55440164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2794
Checksum: 335
Coasting Arc #13 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2015/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2550570
37 A = 6778304
17 meter
Y = -4758372
08 meter E =
0012184
Z = -4111599
66 I = 52
00187
XDOT = 3836
453835 Wp = 66
82565
YDOT = 5388
971710 meter/sec RA = 81
68202 deg
ZDOT = -3861
191783 TA = 163
42479
MA = 163
38492
Ha = 220
545 n
mi
Hp = 211
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8368013
04 X = 2623562
65
Y = -15611456
94 feet Y = -4729441
20 meter
Z = -13489500
21 Z = -4099032
91
XDOT = 12586
790796 XDOT = 3794
664126
YDOT = 17680
353379 feet/sec YDOT = 5431
640358 meter/sec
ZDOT = -12667
952044 ZDOT = -3842
655761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14745612
25 X = -4494462
61
Y = -9888811
05 feet Y = -3014109
61 meter
Z = -13434514
56 Z = -4094840
04
XDOT = 18074
188052 XDOT = 5509
012518
YDOT = -9867
592590 feet/sec YDOT = -3007
642222 meter/sec
ZDOT = -12589
283002 ZDOT = -3837
213459
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 15168
52318479
00016717 00000-0 10270-3 0 9120
2 25544 51
6442 82
3419 0004856 60
4830 299
6807 15
55477723 28091
Satellite: ISS
Catalog Number: 25544
Epoch time: 15168
52318479 = yrday
fracday
Element set: 912
Inclination: 51
6442 deg
RA of node: 82
3419 deg
Eccentricity:
0004856
Arg of perigee: 60
4830 deg
Mean anomaly: 299
6807 deg
Mean motion: 15
55477723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2809
Checksum: 335
Coasting Arc #14 (Orbit 2824)
---------------------------------------
Vector Time (GMT): 2015/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3449579
77 A = 6774312
21 meter
Y = 2786528
78 meter E =
0008525
Z = 5114161
30 I = 51
98283
XDOT = -2996
282312 Wp = 95
94670
YDOT = -6857
412082 meter/sec RA = 76
70028 deg
ZDOT = 1712
027937 TA = 337
59087
MA = 337
62809
Ha = 220
627 n
mi
Hp = 210
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11317518
94 X = -3505325
58
Y = 9142154
80 feet Y = 2747640
91 meter
Z = 16778744
41 Z = 5097268
97
XDOT = -9830
322546 XDOT = -2927
694750
YDOT = -22498
071135 feet/sec YDOT = -6890
535217 meter/sec
ZDOT = 5616
889557 ZDOT = 1697
638269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8234535
51 X = 2509886
42
Y = 12095829
95 feet Y = 3686808
97 meter
Z = 16705532
49 Z = 5091846
30
XDOT = -22309
988678 XDOT = -6800
084549
YDOT = 7499
194358 feet/sec YDOT = 2285
754440 meter/sec
ZDOT = 5556
349743 ZDOT = 1693
575402
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 15169
55112892
00016717 00000-0 10270-3 0 9136
2 25544 51
6439 77
2072 0004727 64
3671 295
7971 15
55496131 28259
Satellite: ISS
Catalog Number: 25544
Epoch time: 15169
55112892 = yrday
fracday
Element set: 913
Inclination: 51
6439 deg
RA of node: 77
2072 deg
Eccentricity:
0004727
Arg of perigee: 64
3671 deg
Mean anomaly: 295
7971 deg
Mean motion: 15
55496131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2825
Checksum: 329
Coasting Arc #15 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2015/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4197899
81 A = 6773551
19 meter
Y = -522746
58 meter E =
0018926
Z = -5306349
57 I = 51
97262
XDOT = 1842
162526 Wp = 88
59123
YDOT = 7395
814192 meter/sec RA = 71
70896 deg
ZDOT = 731
463265 TA = 188
35873
MA = 188
39031
Ha = 220
526 n
mi
Hp = 211
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13772637
16 X = 4229209
36
Y = -1715047
83 feet Y = -475627
18 meter
Z = -17409283
38 Z = -5285881
15
XDOT = 6043
840307 XDOT = 1755
770698
YDOT = 24264
482256 feet/sec YDOT = 7415
931320 meter/sec
ZDOT = 2399
813860 ZDOT = 740
203179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -880093
72 X = -268252
57
Y = -13961155
75 feet Y = -4255360
27 meter
Z = -17321132
65 Z = -5279481
23
XDOT = 23564
804148 XDOT = 7182
552304
YDOT = -4496
637875 feet/sec YDOT = -1370
575224 meter/sec
ZDOT = 2435
937303 ZDOT = 742
473690
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 15170
51481915
00016717 00000-0 10270-3 0 9140
2 25544 51
6444 72
3932 0004776 66
8861 293
2795 15
55499647 28407
Satellite: ISS
Catalog Number: 25544
Epoch time: 15170
51481915 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 72
3932 deg
Eccentricity:
0004776
Arg of perigee: 66
8861 deg
Mean anomaly: 293
2795 deg
Mean motion: 15
55499647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 341
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