[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 1st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
126/05:21:57
922 -0
5 4
8 4
8
N/A -4
1 -0
0 216
7
000/00:13:55
845 -2
5 0
2 215
4
133/21:39:30
000 0
0 0
0 0
0
N/A 0
0 0
0 218
2
000/00:00:00
000 0
0 0
0 214
3
136/01:09:28
983 -5
1 7
1 7
1
N/A -0
4 -0
4 218
4
000/00:24:57
966 -4
9 0
1 217
6
Coasting Arc #1 (Orbit 2076)
---------------------------------------
Vector Time (GMT): 2015/121/11:10:07
131
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5289592
03 A = 6782895
00 meter
Y = 4177352
46 meter E =
0006262
Z = -723334
38 I = 51
41790
XDOT = -2482
675292 Wp = 168
61912
YDOT = -4169
702166 meter/sec RA = 316
78938 deg
ZDOT = -5940
118636 TA = 19
22624
MA = 19
20262
Ha = 216
112 n
mi
Hp = 213
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17354304
57 X = -5332397
30
Y = 13705224
62 feet Y = 4117961
41 meter
Z = -2373144
28 Z = -749134
82
XDOT = -8145
260143 XDOT = -2407
008809
YDOT = -13680
125215 feet/sec YDOT = -4197
042316 meter/sec
ZDOT = -19488
578202 ZDOT = -5951
995174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9660019
87 X = -2944374
06
Y = 19878331
85 feet Y = 6058915
55 meter
Z = -2484516
44 Z = -757280
61
XDOT = -11720
646654 XDOT = -3572
453100
YDOT = -8131
993817 feet/sec YDOT = -2478
631715 meter/sec
ZDOT = -19538
665811 ZDOT = -5955
385339
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 15121
49602152
00016717 00000-0 10270-3 0 9006
2 25544 51
6445 317
2527 0005767 288
7696 71
2831 15
56259898 20771
Satellite: ISS
Catalog Number: 25544
Epoch time: 15121
49602152 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 317
2527 deg
Eccentricity:
0005767
Arg of perigee: 288
7696 deg
Mean anomaly: 71
2831 deg
Mean motion: 15
56259898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2077
Checksum: 331
Coasting Arc #2 (Orbit 2092)
---------------------------------------
Vector Time (GMT): 2015/122/11:10:07
131
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5505267
40 A = 6779107
62 meter
Y = -2594651
71 meter E =
0008476
Z = 2974548
86 I = 51
38248
XDOT = 77
554897 Wp = 63
12198
YDOT = 5856
548208 meter/sec RA = 311
78552 deg
ZDOT = 4957
876794 TA = 331
07227
MA = 331
11923
Ha = 216
052 n
mi
Hp = 213
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18061900
90 X = 5519422
71
Y = -8512636
84 feet Y = -2533008
93 meter
Z = 9759018
56 Z = 3001327
40
XDOT = 254
445200 XDOT = -12
024168
YDOT = 19214
397008 feet/sec YDOT = 5856
914823 meter/sec
ZDOT = 16265
999980 ZDOT = 4958
035715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12243681
72 X = 3731874
19
Y = -15701170
68 feet Y = -4785716
82 meter
Z = 9874269
11 Z = 3009677
23
XDOT = 7637
370371 XDOT = 2327
870489
YDOT = 16199
376808 feet/sec YDOT = 4937
570051 meter/sec
ZDOT = 16265
550619 ZDOT = 4957
739829
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 15122
52342134
00016717 00000-0 10270-3 0 9013
2 25544 51
6436 312
1127 0005916 292
6070 67
4458 15
56322371 20934
Satellite: ISS
Catalog Number: 25544
Epoch time: 15122
52342134 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 312
1127 deg
Eccentricity:
0005916
Arg of perigee: 292
6070 deg
Mean anomaly: 67
4458 deg
Mean motion: 15
56322371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2093
Checksum: 281
Coasting Arc #3 (Orbit 2107)
---------------------------------------
Vector Time (GMT): 2015/123/11:10:07
131
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4943247
77 A = 6773747
35 meter
Y = 446455
89 meter E =
0007764
Z = -4616696
69 I = 51
34307
XDOT = 2126
390027 Wp = 37
01969
YDOT = -6758
212938 meter/sec RA = 306
76198 deg
ZDOT = -2926
831925 TA = 203
69142
MA = 203
72719
Ha = 216
352 n
mi
Hp = 213
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16218004
48 X = -4925446
08
Y = 1464750
30 feet Y = 391276
68 meter
Z = -15146642
67 Z = -4640667
31
XDOT = 6976
345232 XDOT = 2216
021694
YDOT = -22172
614625 feet/sec YDOT = -6733
933169 meter/sec
ZDOT = -9602
466945 ZDOT = -2916
284229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13589054
23 X = -4141943
73
Y = 8796706
46 feet Y = 2681236
13 meter
Z = -15249442
86 Z = -4648030
18
XDOT = -3446
987186 XDOT = -1050
641694
YDOT = -21910
371907 feet/sec YDOT = -6678
281357 meter/sec
ZDOT = -9555
969291 ZDOT = -2912
659440
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 15123
48659358
00016717 00000-0 10270-3 0 9029
2 25544 51
6424 307
2948 0005804 297
1164 62
9398 15
56335413 21088
Satellite: ISS
Catalog Number: 25544
Epoch time: 15123
48659358 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 307
2948 deg
Eccentricity:
0005804
Arg of perigee: 297
1164 deg
Mean anomaly: 62
9398 deg
Mean motion: 15
56335413 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2108
Checksum: 321
Coasting Arc #4 (Orbit 2123)
---------------------------------------
Vector Time (GMT): 2015/124/11:10:07
131
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3760370
70 A = 6770988
39 meter
Y = 1958947
25 meter E =
0003528
Z = 5281151
75 I = 51
31564
XDOT = -3840
502942 Wp = 314
16609
YDOT = 6634
359276 meter/sec RA = 301
71898 deg
ZDOT = 276
211963 TA = 133
20471
MA = 133
17523
Ha = 216
460 n
mi
Hp = 213
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12337174
20 X = 3712531
38
Y = 6426992
30 feet Y = 2000730
72 meter
Z = 17326613
36 Z = 5299303
10
XDOT = -12600
075269 XDOT = -3915
746254
YDOT = 21766
270590 feet/sec YDOT = 6590
991553 meter/sec
ZDOT = 906
207228 ZDOT = 257
372330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13811876
04 X = 4209859
82
Y = -236592
76 feet Y = -72113
47 meter
Z = 17404014
82 Z = 5304743
72
XDOT = -614
661695 XDOT = -187
348885
YDOT = 24138
744796 feet/sec YDOT = 7357
489414 meter/sec
ZDOT = 824
207274 ZDOT = 251
218377
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 15124
51395931
00016717 00000-0 10270-3 0 9039
2 25544 51
6427 302
1552 0005786 301
1037 58
9548 15
56322232 21245
Satellite: ISS
Catalog Number: 25544
Epoch time: 15124
51395931 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 302
1552 deg
Eccentricity:
0005786
Arg of perigee: 301
1037 deg
Mean anomaly: 58
9548 deg
Mean motion: 15
56322232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2124
Checksum: 288
Coasting Arc #5 (Orbit 2138)
---------------------------------------
Vector Time (GMT): 2015/125/11:10:07
131
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2220656
19 A = 6772779
24 meter
Y = -4201026
01 meter E =
0006435
Z = -4831727
56 I = 51
30583
XDOT = 4887
059940 Wp = 92
62395
YDOT = -5381
995028 meter/sec RA = 296
67225 deg
ZDOT = 2435
903012 TA = 201
38327
MA = 201
41017
Ha = 216
513 n
mi
Hp = 212
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7285617
43 X = -2150043
05
Y = -13782893
73 feet Y = -4225463
96 meter
Z = -15852124
53 Z = -4842343
84
XDOT = 16033
661219 XDOT = 4935
046513
YDOT = -17657
464002 feet/sec YDOT = -5327
076451 meter/sec
ZDOT = 7991
807781 ZDOT = 2459
760397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13070693
69 X = -3983947
44
Y = -8413476
93 feet Y = -2564427
77 meter
Z = -15896811
17 Z = -4845348
04
XDOT = 4520
823965 XDOT = 1377
947144
YDOT = -22302
874557 feet/sec YDOT = -6797
916165 meter/sec
ZDOT = 8095
064966 ZDOT = 2467
375802
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 15125
47709529
00016717 00000-0 10270-3 0 9048
2 25544 51
6421 297
3362 0005756 304
2933 55
7666 15
56392478 21390
Satellite: ISS
Catalog Number: 25544
Epoch time: 15125
47709529 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 297
3362 deg
Eccentricity:
0005756
Arg of perigee: 304
2933 deg
Mean anomaly: 55
7666 deg
Mean motion: 15
56392478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2139
Checksum: 332
Coasting Arc #6 (Orbit 2150)
---------------------------------------
Vector Time (GMT): 2015/126/05:28:55
845
Vector Time (MET): N/A
Weight (LBS) : 911172
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4520257
68 A = 6774577
26 meter
Y = 322035
09 meter E =
0006782
Z = -5041537
51 I = 51
29632
XDOT = 1502
926702 Wp = 52
71467
YDOT = -7295
439530 meter/sec RA = 292
87542 deg
ZDOT = -1811
182754 TA = 199
64875
MA = 199
67489
Ha = 216
716 n
mi
Hp = 215
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14830241
73 X = -4499032
41
Y = 1056545
58 feet Y = 271605
42 meter
Z = -16540477
40 Z = -5063444
92
XDOT = 4930
861884 XDOT = 1593
192563
YDOT = -23935
169062 feet/sec YDOT = -7278
128072 meter/sec
ZDOT = -5942
200635 ZDOT = -1803
662608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9341287
60 X = -2847224
46
Y = -11431379
00 feet Y = -3484284
32 meter
Z = -16634412
25 Z = -5070168
86
XDOT = 21596
792158 XDOT = 6582
702250
YDOT = -9039
011295 feet/sec YDOT = -2755
090643 meter/sec
ZDOT = -5908
585523 ZDOT = -1800
936867
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 15126
24760318
00016717 00000-0 10270-3 0 9058
2 25544 51
6461 293
4858 0007499 277
7902 82
2400 15
55450990 21515
Satellite: ISS
Catalog Number: 25544
Epoch time: 15126
24760318 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 293
4858 deg
Eccentricity:
0007499
Arg of perigee: 277
7902 deg
Mean anomaly: 82
2400 deg
Mean motion: 15
55450990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2151
Checksum: 317
Coasting Arc #7 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2015/127/05:28:55
845
Vector Time (MET): N/A
Weight (LBS) : 911172
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3806889
68 A = 6773509
35 meter
Y = 1938341
21 meter E =
0005614
Z = 5260999
02 I = 51
28158
XDOT = -2793
221356 Wp = 299
23430
YDOT = 7115
237607 meter/sec RA = 287
83698 deg
ZDOT = -598
107350 TA = 156
51661
MA = 156
49097
Ha = 217
086 n
mi
Hp = 215
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12489795
52 X = 3759375
35
Y = 6359387
16 feet Y = 1980646
48 meter
Z = 17260495
46 Z = 5279377
12
XDOT = -9164
112060 XDOT = -2869
672607
YDOT = 23343
955403 feet/sec YDOT = 7083
574537 meter/sec
ZDOT = -1962
294456 ZDOT = -611
861951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2164643
07 X = 659783
21
Y = 13749146
89 feet Y = 4190739
97 meter
Z = 17338880
62 Z = 5284890
81
XDOT = -23246
290349 XDOT = -7085
469298
YDOT = 6219
619582 feet/sec YDOT = 1895
740049 meter/sec
ZDOT = -2022
584547 ZDOT = -616
483770
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 15127
27556454
00016717 00000-0 10270-3 0 9067
2 25544 51
6461 288
3511 0007699 281
6459 78
3830 15
55491661 21677
Satellite: ISS
Catalog Number: 25544
Epoch time: 15127
27556454 = yrday
fracday
Element set: 906
Inclination: 51
6461 deg
RA of node: 288
3511 deg
Eccentricity:
0007699
Arg of perigee: 281
6459 deg
Mean anomaly: 78
3830 deg
Mean motion: 15
55491661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 338
Coasting Arc #8 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2015/128/05:28:55
845
Vector Time (MET): N/A
Weight (LBS) : 911172
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2878315
87 A = 6776251
00 meter
Y = -4041189
06 meter E =
0002772
Z = -4618130
00 I = 51
28237
XDOT = 3762
431590 Wp = 120
39977
YDOT = -6011
314922 meter/sec RA = 282
80079 deg
ZDOT = 2915
267135 TA = 178
76392
MA = 178
76323
Ha = 217
274 n
mi
Hp = 215
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9443293
55 X = -2810478
97
Y = -13258494
29 feet Y = -4072996
79 meter
Z = -15151345
15 Z = -4631947
87
XDOT = 12343
935664 XDOT = 3815
210452
YDOT = -19722
161818 feet/sec YDOT = -5968
945965 meter/sec
ZDOT = 9564
524721 ZDOT = 2933
672496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4930363
38 X = 1502774
76
Y = -15455752
48 feet Y = -4710913
36 meter
Z = -15209798
02 Z = -4635946
44
XDOT = 22010
487233 XDOT = 6708
796509
YDOT = -2469
954187 feet/sec YDOT = -752
842036 meter/sec
ZDOT = 9644
530059 ZDOT = 2939
652762
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 15128
23926369
00016717 00000-0 10270-3 0 9071
2 25544 51
6466 283
5373 0007709 285
9846 74
0458 15
55488476 21820
Satellite: ISS
Catalog Number: 25544
Epoch time: 15128
23926369 = yrday
fracday
Element set: 907
Inclination: 51
6466 deg
RA of node: 283
5373 deg
Eccentricity:
0007709
Arg of perigee: 285
9846 deg
Mean anomaly: 74
0458 deg
Mean motion: 15
55488476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2182
Checksum: 355
Coasting Arc #9 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2015/129/05:28:55
845
Vector Time (MET): N/A
Weight (LBS) : 911172
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1810744
53 A = 6780941
03 meter
Y = 5695696
78 meter E =
0005915
Z = 3200637
75 I = 51
29189
XDOT = -4409
931593 Wp = 71
31129
YDOT = 4083
420323 meter/sec RA = 277
77826 deg
ZDOT = -4762
649300 TA = 71
46107
MA = 71
39682
Ha = 217
609 n
mi
Hp = 215
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5940762
91 X = 1731371
67
Y = 18686669
22 feet Y = 5715501
79 meter
Z = 10500780
01 Z = 3209241
49
XDOT = -14468
279505 XDOT = -4432
130229
YDOT = 13397
048305 feet/sec YDOT = 4033
981640 meter/sec
ZDOT = -15625
489829 ZDOT = -4784
125866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11077840
76 X = -3376525
86
Y = 16155878
47 feet Y = 4924311
76 meter
Z = 10536587
97 Z = 3211552
01
XDOT = -18230
093332 XDOT = -5556
532448
YDOT = -2229
476704 feet/sec YDOT = -679
544499 meter/sec
ZDOT = -15718
290970 ZDOT = -4790
935088
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 15129
26719141
00016717 00000-0 10270-3 0 9084
2 25544 51
6463 278
4029 0007657 290
4040 69
6291 15
55508780 21980
Satellite: ISS
Catalog Number: 25544
Epoch time: 15129
26719141 = yrday
fracday
Element set: 908
Inclination: 51
6463 deg
RA of node: 278
4029 deg
Eccentricity:
0007657
Arg of perigee: 290
4040 deg
Mean anomaly: 69
6291 deg
Mean motion: 15
55508780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2198
Checksum: 328
Coasting Arc #10 (Orbit 2212)
---------------------------------------
Vector Time (GMT): 2015/130/05:28:55
845
Vector Time (MET): N/A
Weight (LBS) : 911172
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -679887
50 A = 6784534
56 meter
Y = -6626878
48 meter E =
0010474
Z = -1247438
04 I = 51
30110
XDOT = 4744
088163 Wp = 351
08090
YDOT = -1581
504227 meter/sec RA = 272
76998 deg
ZDOT = 5819
502635 TA = 355
27814
MA = 355
28802
Ha = 217
727 n
mi
Hp = 215
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2230602
02 X = -599674
00
Y = -21741727
28 feet Y = -6634032
89 meter
Z = -4092644
48 Z = -1250546
16
XDOT = 15564
593710 XDOT = 4733
151165
YDOT = -5188
662162 feet/sec YDOT = -1528
514037 meter/sec
ZDOT = 19092
856414 ZDOT = 5842
522051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15482881
70 X = 4719182
34
Y = -15422694
78 feet Y = -4700837
37 meter
Z = -4104739
86 Z = -1251124
71
XDOT = 12639
966836 XDOT = 3852
661892
YDOT = 7584
534323 feet/sec YDOT = 2311
766062 meter/sec
ZDOT = 19191
804066 ZDOT = 5849
661879
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 15130
23085560
00016717 00000-0 10270-3 0 9095
2 25544 51
6465 273
5884 0007841 294
1714 65
8620 15
55550280 22135
Satellite: ISS
Catalog Number: 25544
Epoch time: 15130
23085560 = yrday
fracday
Element set: 909
Inclination: 51
6465 deg
RA of node: 273
5884 deg
Eccentricity:
0007841
Arg of perigee: 294
1714 deg
Mean anomaly: 65
8620 deg
Mean motion: 15
55550280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2213
Checksum: 304
Coasting Arc #11 (Orbit 2228)
---------------------------------------
Vector Time (GMT): 2015/131/05:28:55
845
Vector Time (MET): N/A
Weight (LBS) : 911172
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -485496
45 A = 6784885
55 meter
Y = 6700243
44 meter E =
0004234
Z = -930983
75 I = 51
30107
XDOT = -4768
401097 Wp = 190
69490
YDOT = -1164
106322 meter/sec RA = 267
77010 deg
ZDOT = -5891
120125 TA = 359
43559
MA = 359
43607
Ha = 217
963 n
mi
Hp = 215
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1592836
12 X = -555861
69
Y = 21982425
97 feet Y = 6694420
87 meter
Z = -3054408
64 Z = -933513
05
XDOT = -15644
360555 XDOT = -4726
412346
YDOT = -3819
246462 feet/sec YDOT = -1217
194859 meter/sec
ZDOT = -19327
821932 ZDOT = -5914
182267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17831639
21 X = -5435083
63
Y = 12950790
25 feet Y = 3947400
87 meter
Z = -3066474
46 Z = -934661
42
XDOT = -6126
515134 XDOT = -1867
361813
YDOT = -13035
409896 feet/sec YDOT = -3973
192936 meter/sec
ZDOT = -19426
451751 ZDOT = -5921
182494
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 15131
25874791
00016717 00000-0 10270-3 0 9102
2 25544 51
6461 268
4538 0007873 297
0462 62
9887 15
55529676 22292
Satellite: ISS
Catalog Number: 25544
Epoch time: 15131
25874791 = yrday
fracday
Element set: 910
Inclination: 51
6461 deg
RA of node: 268
4538 deg
Eccentricity:
0007873
Arg of perigee: 297
0462 deg
Mean anomaly: 62
9887 deg
Mean motion: 15
55529676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2229
Checksum: 348
Coasting Arc #12 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2015/132/05:28:55
845
Vector Time (MET): N/A
Weight (LBS) : 911172
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1640460
64 A = 6781381
63 meter
Y = -5872957
91 meter E =
0008779
Z = 2953903
80 I = 51
29135
XDOT = 4487
847169 Wp = 46
31391
YDOT = 3752
701016 meter/sec RA = 262
76276 deg
ZDOT = 4965
485242 TA = 347
65118
MA = 347
67268
Ha = 218
128 n
mi
Hp = 214
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5382088
73 X = 1691662
47
Y = -19268234
60 feet Y = -5854326
91 meter
Z = 9691285
45 Z = 2961997
28
XDOT = 14723
908035 XDOT = 4421
429369
YDOT = 12312
011206 feet/sec YDOT = 3802
515705 meter/sec
ZDOT = 16290
962081 ZDOT = 4987
125171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18021229
93 X = 5492870
88
Y = -8647125
09 feet Y = -2635643
73 meter
Z = 9727037
41 Z = 2964801
00
XDOT = -308
705856 XDOT = -94
093545
YDOT = 17797
834545 feet/sec YDOT = 5424
779969 meter/sec
ZDOT = 16383
033906 ZDOT = 4993
548734
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 15132
28662106
00016717 00000-0 10270-3 0 9112
2 25544 51
6455 263
3175 0008032 303
0751 56
9631 15
55578671 22450
Satellite: ISS
Catalog Number: 25544
Epoch time: 15132
28662106 = yrday
fracday
Element set: 911
Inclination: 51
6455 deg
RA of node: 263
3175 deg
Eccentricity:
0008032
Arg of perigee: 303
0751 deg
Mean anomaly: 56
9631 deg
Mean motion: 15
55578671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 296
Coasting Arc #13 (Orbit 2259)
---------------------------------------
Vector Time (GMT): 2015/133/05:28:55
845
Vector Time (MET): N/A
Weight (LBS) : 911172
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2743718
08 A = 6776431
66 meter
Y = 4287519
66 meter E =
0008458
Z = -4479654
70 I = 51
27925
XDOT = -3868
706705 Wp = 16
28297
YDOT = -5803
308170 meter/sec RA = 257
74075 deg
ZDOT = -3178
362835 TA = 221
57814
MA = 221
64249
Ha = 218
293 n
mi
Hp = 214
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9001699
75 X = -2769697
51
Y = 14066665
54 feet Y = 4256692
30 meter
Z = -14697029
86 Z = -4493046
44
XDOT = -12692
607301 XDOT = -3788
085735
YDOT = -19039
724966 feet/sec YDOT = -5846
119832 meter/sec
ZDOT = -10427
699590 ZDOT = -3196
960583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16410580
50 X = -5001944
94
Y = 2807372
51 feet Y = 855687
14 meter
Z = -14755198
13 Z = -4497384
39
XDOT = 5884
758969 XDOT = 1793
674534
YDOT = -20932
567926 feet/sec YDOT = -6380
246704 meter/sec
ZDOT = -10506
374393 ZDOT = -3202
342915
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 15133
25023492
00016717 00000-0 10270-3 0 9120
2 25544 51
6446 258
5030 0008158 305
9138 54
1258 15
55614626 22608
Satellite: ISS
Catalog Number: 25544
Epoch time: 15133
25023492 = yrday
fracday
Element set: 912
Inclination: 51
6446 deg
RA of node: 258
5030 deg
Eccentricity:
0008158
Arg of perigee: 305
9138 deg
Mean anomaly: 54
1258 deg
Mean motion: 15
55614626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2260
Checksum: 292
Coasting Arc #14 (Orbit 2270)
---------------------------------------
Vector Time (GMT): 2015/133/21:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 893564
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2298903
70 A = 6776848
33 meter
Y = -4672487
82 meter E =
0003409
Z = 4333276
84 I = 51
28339
XDOT = 4342
025085 Wp = 57
34884
YDOT = 5315
495421 meter/sec RA = 254
35675 deg
ZDOT = 3427
887117 TA = 357
71508
MA = 357
71663
Ha = 218
211 n
mi
Hp = 214
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7542334
97 X = 2329931
99
Y = -15329684
44 feet Y = -4646606
44 meter
Z = 14216787
53 Z = 4344520
03
XDOT = 14245
489124 XDOT = 4265
611623
YDOT = 17439
289439 feet/sec YDOT = 5363
623568 meter/sec
ZDOT = 11246
348810 ZDOT = 3448
794456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3124856
56 X = -952456
28
Y = 16754849
24 feet Y = 5106878
05 meter
Z = 14265811
85 Z = 4348219
45
XDOT = -17065
825917 XDOT = -5201
663739
YDOT = -12834
439113 feet/sec YDOT = -3911
937041 meter/sec
ZDOT = 11335
017915 ZDOT = 3454
913461
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 15133
95687621
00016717 00000-0 10270-3 0 9138
2 25544 51
6421 254
9716 0007938 308
4200 51
6240 15
55657534 22715
Satellite: ISS
Catalog Number: 25544
Epoch time: 15133
95687621 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 254
9716 deg
Eccentricity:
0007938
Arg of perigee: 308
4200 deg
Mean anomaly: 51
6240 deg
Mean motion: 15
55657534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2271
Checksum: 307
Coasting Arc #15 (Orbit 2285)
---------------------------------------
Vector Time (GMT): 2015/134/21:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 893564
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3442244
95 A = 6773365
24 meter
Y = 2671873
06 meter E =
0011247
Z = -5194078
34 I = 51
28144
XDOT = -3504
596062 Wp = 47
50347
YDOT = -6721
498181 meter/sec RA = 249
32066 deg
ZDOT = -1129
108746 TA = 211
57843
MA = 211
64597
Ha = 218
490 n
mi
Hp = 213
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11293454
56 X = -3446635
31
Y = 8765987
72 feet Y = 2633355
06 meter
Z = -17040939
43 Z = -5210811
05
XDOT = -11498
018575 XDOT = -3423
689314
YDOT = -22052
159387 feet/sec YDOT = -6760
236493 meter/sec
ZDOT = -3704
425019 ZDOT = -1145
937152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8265897
02 X = 2519445
41
Y = -11558276
92 feet Y = -3522962
81 meter
Z = -17113136
89 Z = -5216084
13
XDOT = 16374
550493 XDOT = 4990
962990
YDOT = 17328
578917 feet/sec YDOT = 5281
750854 meter/sec
ZDOT = -3775
370947 ZDOT = -1150
733065
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 15134
92046496
00016717 00000-0 10270-3 0 9146
2 25544 51
6424 250
1562 0007920 313
4213 46
6280 15
55651013 22866
Satellite: ISS
Catalog Number: 25544
Epoch time: 15134
92046496 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 250
1562 deg
Eccentricity:
0007920
Arg of perigee: 313
4213 deg
Mean anomaly: 46
6280 deg
Mean motion: 15
55651013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2286
Checksum: 286
Coasting Arc #16 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2015/135/21:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 893564
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4395246
07 A = 6773466
22 meter
Y = -372885
78 meter E =
0008632
Z = 5143607
20 I = 51
29460
XDOT = 2239
124391 Wp = 347
88561
YDOT = 7202
527502 meter/sec RA = 244
27965 deg
ZDOT = -1383
327100 TA = 115
52469
MA = 115
43540
Ha = 218
607 n
mi
Hp = 213
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14420098
65 X = 4374102
88
Y = -1223378
54 feet Y = -323853
55 meter
Z = 16875351
69 Z = 5164907
52
XDOT = 7346
208632 XDOT = 2165
137413
YDOT = 23630
339573 feet/sec YDOT = 7227
153188 meter/sec
ZDOT = -4538
474738 ZDOT = -1372
629265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13298621
66 X = -4053419
88
Y = 5430494
51 feet Y = 1655214
73 meter
Z = 16966725
85 Z = 5171458
04
XDOT = -13684
050068 XDOT = -4170
898461
YDOT = -19389
884190 feet/sec YDOT = -5910
036701 meter/sec
ZDOT = -4493
884100 ZDOT = -1369
735874
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 15135
94827462
00016717 00000-0 10270-3 0 9150
2 25544 51
6428 245
0206 0008045 317
4406 42
6123 15
55678537 23026
Satellite: ISS
Catalog Number: 25544
Epoch time: 15135
94827462 = yrday
fracday
Element set: 915
Inclination: 51
6428 deg
RA of node: 245
0206 deg
Eccentricity:
0008045
Arg of perigee: 317
4406 deg
Mean anomaly: 42
6123 deg
Mean motion: 15
55678537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 300
Coasting Arc #17 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2015/136/01:21:57
966
Vector Time (MET): N/A
Weight (LBS) : 892643
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2466281
40 A = 6779306
94 meter
Y = 3933954
57 meter E =
0005451
Z = -4944530
36 I = 51
30187
XDOT = -4721
835202 Wp = 52
05652
YDOT = -5646
230954 meter/sec RA = 243
53388 deg
ZDOT = -2135
358388 TA = 197
01792
MA = 197
03620
Ha = 218
399 n
mi
Hp = 217
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8091474
42 X = -2486069
35
Y = 12906675
11 feet Y = 3906264
44 meter
Z = -16222212
46 Z = -4956559
32
XDOT = -15491
585308 XDOT = -4647
973779
YDOT = -18524
379770 feet/sec YDOT = -5698
620585 meter/sec
ZDOT = -7005
768991 ZDOT = -2158
117301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10026070
05 X = -3055946
15
Y = -11394470
00 feet Y = -3473034
46 meter
Z = -16274469
90 Z = -4960458
43
XDOT = 21384
166050 XDOT = 6517
893812
YDOT = -8664
120116 feet/sec YDOT = -2640
823811 meter/sec
ZDOT = -7102
337502 ZDOT = -2164
792471
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 15136
07677600
00016717 00000-0 10270-3 0 9163
2 25544 51
6449 244
3799 0007681 269
7883 90
2390 15
53989655 23042
Satellite: ISS
Catalog Number: 25544
Epoch time: 15136
07677600 = yrday
fracday
Element set: 916
Inclination: 51
6449 deg
RA of node: 244
3799 deg
Eccentricity:
0007681
Arg of perigee: 269
7883 deg
Mean anomaly: 90
2390 deg
Mean motion: 15
53989655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 349
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