[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 3rd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 819 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
247/07:42:03
000 0
0 0
0 0
0
N/A 0
0 0
0 219
2
000/00:00:00
000 0
0 0
0 212
8
250/04:14:38
538 1
3 1
6 1
6
N/A 0
9 0
0 219
1
000/00:09:17
076 -0
0 -0
1 213
8
257/01:31:24
281 1
6 3
6 3
6
N/A 1
8 -0
2 221
3
000/00:38:48
562 2
6 0
2 216
4
Coasting Arc #1 (Orbit 6)
---------------------------------------
Vector Time (GMT): 2015/245/10:57:49
539
Vector Time (MET): N/A
Weight (LBS) : 927021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4417420
07 A = 6775057
91 meter
Y = 510618
68 meter E =
0004874
Z = 5108181
48 I = 51
93509
XDOT = -2805
891544 Wp = 65
25470
YDOT = -6928
829573 meter/sec RA = 57
50906 deg
ZDOT = -1730
569913 TA = 41
41016
MA = 41
37323
Ha = 219
435 n
mi
Hp = 212
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14492847
98 X = -4447615
21
Y = 1675258
15 feet Y = 461051
86 meter
Z = 16759125
58 Z = 5086649
16
XDOT = -9205
680917 XDOT = -2719
796706
YDOT = -22732
380489 feet/sec YDOT = -6959
725684 meter/sec
ZDOT = -5677
722811 ZDOT = -1743
990570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12907850
65 X = 3934312
88
Y = 7024557
46 feet Y = 2141085
11 meter
Z = 16666145
53 Z = 5079841
16
XDOT = -5060
427813 XDOT = -1542
418397
YDOT = 22929
337986 feet/sec YDOT = 6988
862218 meter/sec
ZDOT = -5734
316120 ZDOT = -1747
819553
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 15245
50202171
00016717 00000-0 10270-3 0 9002
2 25544 51
6407 57
9872 0001003 174
7877 185
3287 15
55262501 71
Satellite: ISS
Catalog Number: 25544
Epoch time: 15245
50202171 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 57
9872 deg
Eccentricity:
0001003
Arg of perigee: 174
7877 deg
Mean anomaly: 185
3287 deg
Mean motion: 15
55262501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 7
Checksum: 287
Coasting Arc #2 (Orbit 21)
---------------------------------------
Vector Time (GMT): 2015/246/10:57:49
539
Vector Time (MET): N/A
Weight (LBS) : 927021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5183528
62 A = 6778823
18 meter
Y = 1441142
56 meter E =
0007925
Z = -4132471
97 I = 51
92961
XDOT = 1230
871580 Wp = 115
46510
YDOT = 6525
855367 meter/sec RA = 52
52355 deg
ZDOT = 3822
121285 TA = 193
84207
MA = 193
86381
Ha = 219
266 n
mi
Hp = 212
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17006327
49 X = 5187102
15
Y = 4728157
99 feet Y = 1499127
82 meter
Z = -13557978
90 Z = -4107282
85
XDOT = 4038
292585 XDOT = 1139
239979
YDOT = 21410
286637 feet/sec YDOT = 6539
107755 meter/sec
ZDOT = 12539
767997 ZDOT = 3827
877515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11498449
48 X = -3504727
40
Y = -13501239
52 feet Y = -4115177
81 meter
Z = -13449596
11 Z = -4099436
89
XDOT = 7749
415923 XDOT = 2362
021973
YDOT = -19107
300516 feet/sec YDOT = -5823
905197 meter/sec
ZDOT = 12563
361594 ZDOT = 3829
312614
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 15246
46583454
00016717 00000-0 10270-3 0 9015
2 25544 51
6403 53
1726 0001051 172
9748 187
1421 15
55291892 225
Satellite: ISS
Catalog Number: 25544
Epoch time: 15246
46583454 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 53
1726 deg
Eccentricity:
0001051
Arg of perigee: 172
9748 deg
Mean anomaly: 187
1421 deg
Mean motion: 15
55291892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 22
Checksum: 294
Coasting Arc #3 (Orbit 35)
---------------------------------------
Vector Time (GMT): 2015/247/07:42:03
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4494761
80 A = 6775319
45 meter
Y = 845678
27 meter E =
0005776
Z = 4995161
88 I = 51
90536
XDOT = -3559
727553 Wp = 62
07062
YDOT = -6463
468615 meter/sec RA = 48
23743 deg
ZDOT = -2104
374446 TA = 48
34864
MA = 48
29920
Ha = 219
221 n
mi
Hp = 212
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14746593
84 X = -4528148
92
Y = 2774535
01 feet Y = 795228
56 meter
Z = 16388326
37 Z = 4973246
07
XDOT = -11678
896171 XDOT = -3476
964661
YDOT = -21205
605693 feet/sec YDOT = -6502
813225 meter/sec
ZDOT = -6904
115638 ZDOT = -2121
465416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4762360
65 X = 1451567
53
Y = 14337881
58 feet Y = 4370186
31 meter
Z = 16293630
30 Z = 4966298
52
XDOT = -18388
965913 XDOT = -5604
956810
YDOT = 14053
012317 feet/sec YDOT = 4283
358154 meter/sec
ZDOT = -6976
603378 ZDOT = -2126
468710
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 15247
36538467
00016717 00000-0 10270-3 0 9020
2 25544 51
6445 48
6840 0000708 188
4475 171
6666 15
55339664 368
Satellite: ISS
Catalog Number: 25544
Epoch time: 15247
36538467 = yrday
fracday
Element set: 902
Inclination: 51
6445 deg
RA of node: 48
6840 deg
Eccentricity:
0000708
Arg of perigee: 188
4475 deg
Mean anomaly: 171
6666 deg
Mean motion: 15
55339664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 36
Checksum: 332
Coasting Arc #4 (Orbit 50)
---------------------------------------
Vector Time (GMT): 2015/248/07:42:03
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5471443
14 A = 6779535
08 meter
Y = 953910
39 meter E =
0006358
Z = -3894815
43 I = 51
89645
XDOT = 1855
268003 Wp = 110
94500
YDOT = 6186
343580 meter/sec RA = 43
25218 deg
ZDOT = 4124
638530 TA = 202
19807
MA = 202
22561
Ha = 219
091 n
mi
Hp = 212
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17950928
92 X = 5479289
13
Y = 3129627
27 feet Y = 1015139
30 meter
Z = -12778265
84 Z = -3868217
29
XDOT = 6086
837280 XDOT = 1765
917028
YDOT = 20296
402821 feet/sec YDOT = 6206
591071 meter/sec
ZDOT = 13532
278643 ZDOT = 4133
433632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 342001
71 X = 104242
12
Y = -18298298
85 feet Y = -5577321
49 meter
Z = -12663719
35 Z = -3859901
66
XDOT = 17810
828343 XDOT = 5428
740479
YDOT = -9050
485624 feet/sec YDOT = -2758
588018 meter/sec
ZDOT = 13569
024583 ZDOT = 4135
838693
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 15248
32918259
00016717 00000-0 10270-3 0 9039
2 25544 51
6436 43
8701 0000694 194
5467 165
5667 15
55324152 510
Satellite: ISS
Catalog Number: 25544
Epoch time: 15248
32918259 = yrday
fracday
Element set: 903
Inclination: 51
6436 deg
RA of node: 43
8701 deg
Eccentricity:
0000694
Arg of perigee: 194
5467 deg
Mean anomaly: 165
5667 deg
Mean motion: 15
55324152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 51
Checksum: 313
Coasting Arc #5 (Orbit 66)
---------------------------------------
Vector Time (GMT): 2015/249/07:42:03
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5913384
96 A = 6783873
10 meter
Y = -2512077
20 meter E =
0013967
Z = 2156396
24 I = 51
88754
XDOT = 241
034078 Wp = 111
96490
YDOT = -5325
133967 meter/sec RA = 38
28165 deg
ZDOT = -5519
047002 TA = 44
18095
MA = 44
06949
Ha = 219
083 n
mi
Hp = 212
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19400869
29 X = -5895329
72
Y = -8241723
08 feet Y = -2578103
48 meter
Z = 7074790
80 Z = 2127714
32
XDOT = 790
794220 XDOT = 327
372421
YDOT = -17470
911964 feet/sec YDOT = -5321
956146 meter/sec
ZDOT = -18107
109586 ZDOT = -5517
666089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4826288
90 X = -1471052
86
Y = 20561009
96 feet Y = 6266995
84 meter
Z = 6951560
85 Z = 2118835
75
XDOT = -15874
057656 XDOT = -4838
412774
YDOT = 2419
901329 feet/sec YDOT = 737
585925 meter/sec
ZDOT = -18100
121037 ZDOT = -5516
916892
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 15249
35722387
00016717 00000-0 10270-3 0 9049
2 25544 51
6438 38
7361 0000553 196
6343 163
4792 15
55351376 678
Satellite: ISS
Catalog Number: 25544
Epoch time: 15249
35722387 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 38
7361 deg
Eccentricity:
0000553
Arg of perigee: 196
6343 deg
Mean anomaly: 163
4792 deg
Mean motion: 15
55351376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 67
Checksum: 321
Coasting Arc #6 (Orbit 79)
---------------------------------------
Vector Time (GMT): 2015/250/04:19:17
076
Vector Time (MET): N/A
Weight (LBS) : 941127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4125652
15 A = 6776134
15 meter
Y = -1968453
45 meter E =
0011485
Z = -5012555
10 I = 51
83742
XDOT = 5063
003269 Wp = 109
58034
YDOT = 5367
935688 meter/sec RA = 34
00584 deg
ZDOT = 2059
246494 TA = 180
41011
MA = 180
41105
Ha = 219
075 n
mi
Hp = 213
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13535604
17 X = 4171706
17
Y = -6458180
62 feet Y = -1922060
51 meter
Z = -16445390
75 Z = -4992401
66
XDOT = 16610
903114 XDOT = 4992
598450
YDOT = 17611
337558 feet/sec YDOT = 5424
159994 meter/sec
ZDOT = 6756
058051 ZDOT = 2083
670043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3841622
41 X = 1170926
51
Y = -14595435
51 feet Y = -4448688
74 meter
Z = -16358079
15 Z = -4985942
52
XDOT = 23078
626012 XDOT = 7034
365208
YDOT = -1614
090495 feet/sec YDOT = -491
974783 meter/sec
ZDOT = 6860
360789 ZDOT = 2091
037968
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 15250
19250293
00016717 00000-0 10270-3 0 9056
2 25544 51
6444 34
5645 0001476 247
4390 112
6608 15
55045224 805
Satellite: ISS
Catalog Number: 25544
Epoch time: 15250
19250293 = yrday
fracday
Element set: 905
Inclination: 51
6444 deg
RA of node: 34
5645 deg
Eccentricity:
0001476
Arg of perigee: 247
4390 deg
Mean anomaly: 112
6608 deg
Mean motion: 15
55045224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 80
Checksum: 285
Coasting Arc #7 (Orbit 95)
---------------------------------------
Vector Time (GMT): 2015/251/04:19:17
076
Vector Time (MET): N/A
Weight (LBS) : 941127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5471330
39 A = 6780069
54 meter
Y = 527498
56 meter E =
0009699
Z = 3962273
47 I = 51
82348
XDOT = -3457
853181 Wp = 80
83095
YDOT = -5539
380147 meter/sec RA = 29
01845 deg
ZDOT = -4027
441037 TA = 51
10772
MA = 51
02125
Ha = 219
163 n
mi
Hp = 213
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17950559
04 X = -5496069
41
Y = 1730638
34 feet Y = 466176
51 meter
Z = 12999584
89 Z = 3935634
96
XDOT = -11344
662667 XDOT = -3376
089898
YDOT = -18173
819380 feet/sec YDOT = -5577
591260 meter/sec
ZDOT = -13213
389230 ZDOT = -4044
039451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10029519
54 X = -3056997
56
Y = 15086521
13 feet Y = 4598371
64 meter
Z = 12884583
97 Z = 3927221
19
XDOT = -20105
922587 XDOT = -6128
285204
YDOT = -1993
372003 feet/sec YDOT = -607
579787 meter/sec
ZDOT = -13283
901249 ZDOT = -4048
933101
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 15251
22072702
00016717 00000-0 10270-3 0 9069
2 25544 51
6441 29
4315 0001414 253
9128 106
1870 15
55060354 969
Satellite: ISS
Catalog Number: 25544
Epoch time: 15251
22072702 = yrday
fracday
Element set: 906
Inclination: 51
6441 deg
RA of node: 29
4315 deg
Eccentricity:
0001414
Arg of perigee: 253
9128 deg
Mean anomaly: 106
1870 deg
Mean motion: 15
55060354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 96
Checksum: 272
Coasting Arc #8 (Orbit 110)
---------------------------------------
Vector Time (GMT): 2015/252/04:19:17
076
Vector Time (MET): N/A
Weight (LBS) : 941127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6310806
29 A = 6784278
16 meter
Y = 783356
44 meter E =
0004648
Z = -2359045
61 I = 51
81019
XDOT = 1363
674617 Wp = 33
72710
YDOT = 5263
907840 meter/sec RA = 24
04241 deg
ZDOT = 5404
867059 TA = 300
00834
MA = 300
05446
Ha = 219
000 n
mi
Hp = 213
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20704745
04 X = 6313036
80
Y = 2570067
07 feet Y = 853940
30 meter
Z = -7739650
94 Z = -2328383
95
XDOT = 4473
998086 XDOT = 1278
456461
YDOT = 17270
038844 feet/sec YDOT = 5278
681324 meter/sec
ZDOT = 17732
503475 ZDOT = 5411
284015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14831816
09 X = 4520737
55
Y = -14742326
82 feet Y = -4493461
21 meter
Z = -7607558
08 Z = -2318783
70
XDOT = 15205
340448 XDOT = 4634
587768
YDOT = 6148
572995 feet/sec YDOT = 1874
085049 meter/sec
ZDOT = 17759
151945 ZDOT = 5412
989513
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 15252
18467784
00016717 00000-0 10270-3 0 9074
2 25544 51
6448 24
6186 0001506 260
0623 100
0360 15
55080176 1119
Satellite: ISS
Catalog Number: 25544
Epoch time: 15252
18467784 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 24
6186 deg
Eccentricity:
0001506
Arg of perigee: 260
0623 deg
Mean anomaly: 100
0360 deg
Mean motion: 15
55080176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 111
Checksum: 277
Coasting Arc #9 (Orbit 126)
---------------------------------------
Vector Time (GMT): 2015/253/04:19:17
076
Vector Time (MET): N/A
Weight (LBS) : 941127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6490325
35 A = 6786614
45 meter
Y = -1923846
93 meter E =
0011840
Z = 384928
66 I = 51
78836
XDOT = 1017
431935 Wp = 136
59394
YDOT = -4655
385345 meter/sec RA = 19
07646 deg
ZDOT = -6011
108152 TA = 39
26270
MA = 39
17689
Ha = 219
003 n
mi
Hp = 213
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21293718
32 X = -6470199
87
Y = -6311833
74 feet Y = -1996313
45 meter
Z = 1262889
31 Z = 353449
37
XDOT = 3338
031284 XDOT = 1098
613333
YDOT = -15273
573965 feet/sec YDOT = -4643
554443 meter/sec
ZDOT = -19721
483439 ZDOT = -6005
968077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17890236
61 X = -5452944
12
Y = 13172879
46 feet Y = 4015093
66 meter
Z = 1127499
57 Z = 343661
87
XDOT = -9127
031533 XDOT = -2781
919211
YDOT = -10677
672959 feet/sec YDOT = -3254
554718 meter/sec
ZDOT = -19698
405526 ZDOT = -6004
074004
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 15253
21288449
00016717 00000-0 10270-3 0 9089
2 25544 51
6449 19
4856 0001531 259
4625 100
6356 15
55046023 1279
Satellite: ISS
Catalog Number: 25544
Epoch time: 15253
21288449 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 19
4856 deg
Eccentricity:
0001531
Arg of perigee: 259
4625 deg
Mean anomaly: 100
6356 deg
Mean motion: 15
55046023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 127
Checksum: 302
Coasting Arc #10 (Orbit 142)
---------------------------------------
Vector Time (GMT): 2015/254/04:19:17
076
Vector Time (MET): N/A
Weight (LBS) : 941127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5951166
60 A = 6785349
42 meter
Y = 2812896
08 meter E =
0012584
Z = 1620473
88 I = 51
75439
XDOT = -3373
029502 Wp = 59
62606
YDOT = 3815
316981 meter/sec RA = 14
10957 deg
ZDOT = 5737
643487 TA = 318
09437
MA = 318
19062
Ha = 218
870 n
mi
Hp = 213
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19524824
82 X = 5911398
24
Y = 9228661
67 feet Y = 2879223
77 meter
Z = 5316515
37 Z = 1649286
26
XDOT = -11066
369756 XDOT = -3443
313639
YDOT = 12517
444165 feet/sec YDOT = 3777
205227 meter/sec
ZDOT = 18824
289657 ZDOT = 5721
086988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18948809
97 X = 5775597
28
Y = -10295576
79 feet Y = -3138091
81 meter
Z = 5440221
98 Z = 1658179
66
XDOT = 2760
832798 XDOT = 841
501837
YDOT = 15035
618778 feet/sec YDOT = 4582
856604 meter/sec
ZDOT = 18752
143476 ZDOT = 5715
653332
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 15254
24107959
00016717 00000-0 10270-3 0 9090
2 25544 51
6450 14
3518 0001608 274
6128 85
4842 15
55097785 1431
Satellite: ISS
Catalog Number: 25544
Epoch time: 15254
24107959 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 14
3518 deg
Eccentricity:
0001608
Arg of perigee: 274
6128 deg
Mean anomaly: 85
4842 deg
Mean motion: 15
55097785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 143
Checksum: 315
Coasting Arc #11 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2015/255/04:19:17
076
Vector Time (MET): N/A
Weight (LBS) : 941127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4706965
66 A = 6781484
04 meter
Y = -3489307
21 meter E =
0003213
Z = -3417463
18 I = 51
71029
XDOT = 5434
626342 Wp = 83
75370
YDOT = -2815
563237 meter/sec RA = 9
13296 deg
ZDOT = -4613
891059 TA = 136
18034
MA = 136
15484
Ha = 218
822 n
mi
Hp = 213
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15442800
73 X = -4650996
93
Y = -11447858
30 feet Y = -3541631
10 meter
Z = -11212149
55 Z = -3440192
12
XDOT = 17830
138917 XDOT = 5488
119110
YDOT = -9237
412195 feet/sec YDOT = -2754
491164 meter/sec
ZDOT = -15137
437859 ZDOT = -4587
360634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18211406
12 X = -5550836
59
Y = 5973788
72 feet Y = 1820810
80 meter
Z = -11309482
17 Z = -3447130
17
XDOT = 3205
293223 XDOT = 976
973374
YDOT = -18647
978057 feet/sec YDOT = -5683
903712 meter/sec
ZDOT = -15022
482510 ZDOT = -4578
852669
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 15255
20500482
00016717 00000-0 10270-3 0 9107
2 25544 51
6449 9
5396 0001760 276
1670 83
9282 15
55093067 1583
Satellite: ISS
Catalog Number: 25544
Epoch time: 15255
20500482 = yrday
fracday
Element set: 910
Inclination: 51
6449 deg
RA of node: 9
5396 deg
Eccentricity:
0001760
Arg of perigee: 276
1670 deg
Mean anomaly: 83
9282 deg
Mean motion: 15
55093067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 158
Checksum: 304
Coasting Arc #12 (Orbit 173)
---------------------------------------
Vector Time (GMT): 2015/256/04:19:17
076
Vector Time (MET): N/A
Weight (LBS) : 941127
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2906582
94 A = 6777071
93 meter
Y = 3929664
68 meter E =
0006317
Z = 4691134
72 I = 51
66410
XDOT = -6917
966275 Wp = 119
15786
YDOT = 1738
446961 meter/sec RA = 4
13935 deg
ZDOT = 2824
167422 TA = 302
82201
MA = 302
88282
Ha = 218
848 n
mi
Hp = 213
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9536033
27 X = 2839636
79
Y = 12892600
64 feet Y = 3961794
33 meter
Z = 15390861
95 Z = 4705091
12
XDOT = -22696
739749 XDOT = -6950
610531
YDOT = 5703
566145 feet/sec YDOT = 1660
903570 meter/sec
ZDOT = 9265
641147 ZDOT = 2790
481936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15968808
80 X = 4867292
92
Y = -565564
21 feet Y = -172383
97 meter
Z = 15450274
96 Z = 4709243
81
XDOT = -8103
486660 XDOT = -2469
942734
YDOT = 20866
187301 feet/sec YDOT = 6360
013889 meter/sec
ZDOT = 9120
053668 ZDOT = 2779
792358
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 15256
23318370
00016717 00000-0 10270-3 0 9115
2 25544 51
6450 4
4061 0001594 286
5855 73
5124 15
55103104 1745
Satellite: ISS
Catalog Number: 25544
Epoch time: 15256
23318370 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 4
4061 deg
Eccentricity:
0001594
Arg of perigee: 286
5855 deg
Mean anomaly: 73
5124 deg
Mean motion: 15
55103104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 174
Checksum: 274
Coasting Arc #13 (Orbit 187)
---------------------------------------
Vector Time (GMT): 2015/257/01:50:48
562
Vector Time (MET): N/A
Weight (LBS) : 940372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4684644
85 A = 6784029
44 meter
Y = 3023695
58 meter E =
0008132
Z = 3855634
56 I = 51
64636
XDOT = -5546
196873 Wp = 70
23189
YDOT = 3308
123094 meter/sec RA = 359
66712 deg
ZDOT = 4139
965344 TA = 336
26045
MA = 336
29794
Ha = 221
296 n
mi
Hp = 216
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15369569
72 X = 4631755
79
Y = 9920261
07 feet Y = 3075787
19 meter
Z = 12649719
68 Z = 3878262
71
XDOT = -18196
183965 XDOT = -5602
887266
YDOT = 10853
422225 feet/sec YDOT = 3245
785481 meter/sec
ZDOT = 13582
563466 ZDOT = 4112
884889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17730190
48 X = 5404162
06
Y = 4220521
50 feet Y = 1286414
95 meter
Z = 12746693
89 Z = 3885192
30
XDOT = -13276
571267 XDOT = -4046
698922
YDOT = 15063
719226 feet/sec YDOT = 4591
421620 meter/sec
ZDOT = 13465
159854 ZDOT = 4104
180723
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 15257
13288998
00016717 00000-0 10270-3 0 9128
2 25544 51
6457 359
9148 0005584 322
4661 37
6101 15
53748478 1882
Satellite: ISS
Catalog Number: 25544
Epoch time: 15257
13288998 = yrday
fracday
Element set: 912
Inclination: 51
6457 deg
RA of node: 359
9148 deg
Eccentricity:
0005584
Arg of perigee: 322
4661 deg
Mean anomaly: 37
6101 deg
Mean motion: 15
53748478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 188
Checksum: 344
Coasting Arc #14 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2015/258/01:50:48
562
Vector Time (MET): N/A
Weight (LBS) : 940372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3341017
80 A = 6780603
91 meter
Y = -3485812
84 meter E =
0011199
Z = -4770614
62 I = 51
60383
XDOT = 6645
425537 Wp = 41
66217
YDOT = -2731
138184 meter/sec RA = 354
67899 deg
ZDOT = -2653
818064 TA = 202
07592
MA = 202
12419
Ha = 221
450 n
mi
Hp = 216
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10961344
49 X = -3278616
38
Y = -11436393
84 feet Y = -3522826
08 meter
Z = -15651622
78 Z = -4786692
60
XDOT = 21802
577222 XDOT = 6688
363161
YDOT = -8960
427112 feet/sec YDOT = -2656
584957 meter/sec
ZDOT = -8706
752178 ZDOT = -2621
431148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14188307
00 X = -4324595
97
Y = -6890634
89 feet Y = -2100265
51 meter
Z = -15720259
79 Z = -4791535
18
XDOT = 16811
076810 XDOT = 5124
016212
YDOT = -15037
199205 feet/sec YDOT = -4583
338318 meter/sec
ZDOT = -8566
594037 ZDOT = -2611
097863
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 15258
09764718
00016717 00000-0 10270-3 0 9134
2 25544 51
6460 355
1084 0005729 325
6947 34
3835 15
53789624 2030
Satellite: ISS
Catalog Number: 25544
Epoch time: 15258
09764718 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 355
1084 deg
Eccentricity:
0005729
Arg of perigee: 325
6947 deg
Mean anomaly: 34
3835 deg
Mean motion: 15
53789624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 203
Checksum: 328
Coasting Arc #15 (Orbit 218)
---------------------------------------
Vector Time (GMT): 2015/259/01:50:48
562
Vector Time (MET): N/A
Weight (LBS) : 940372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1774856
97 A = 6778576
27 meter
Y = 3908325
86 meter E =
0003197
Z = 5245933
07 I = 51
56537
XDOT = -7321
823395 Wp = 359
23297
YDOT = 2082
392213 meter/sec RA = 349
68094 deg
ZDOT = 928
904946 TA = 81
88941
MA = 81
85314
Ha = 221
551 n
mi
Hp = 216
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5823021
55 X = 1705538
30
Y = 12822591
39 feet Y = 3927786
61 meter
Z = 17211066
50 Z = 5254386
11
XDOT = -24021
730300 XDOT = -7349
077330
YDOT = 6831
995449 feet/sec YDOT = 2000
362502 meter/sec
ZDOT = 3047
588406 ZDOT = 893
270298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10026372
72 X = 3056038
40
Y = 9826944
95 feet Y = 2995252
82 meter
Z = 17246745
87 Z = 5256808
14
XDOT = -19130
577607 XDOT = -5831
000055
YDOT = 14458
486903 feet/sec YDOT = 4406
946808 meter/sec
ZDOT = 2893
567652 ZDOT = 881
959420
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 15259
12671402
00016717 00000-0 10270-3 0 9147
2 25544 51
6459 349
9810 0005714 329
3906 30
6913 15
53793618 2197
Satellite: ISS
Catalog Number: 25544
Epoch time: 15259
12671402 = yrday
fracday
Element set: 914
Inclination: 51
6459 deg
RA of node: 349
9810 deg
Eccentricity:
0005714
Arg of perigee: 329
3906 deg
Mean anomaly: 30
6913 deg
Mean motion: 15
53793618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 219
Checksum: 318
Coasting Arc #16 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2015/260/01:50:48
562
Vector Time (MET): N/A
Weight (LBS) : 940372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -150219
45 A = 6778549
89 meter
Y = -4288971
86 meter E =
0012135
Z = -5256602
01 I = 51
53389
XDOT = 7492
335811 Wp = 73
21542
YDOT = -1330
623909 meter/sec RA = 344
67781 deg
ZDOT = 876
680789 TA = 205
16024
MA = 205
21941
Ha = 221
674 n
mi
Hp = 215
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -492845
98 X = -76713
17
Y = -14071429
99 feet Y = -4290241
39 meter
Z = -17246069
60 Z = -5257152
66
XDOT = 24581
154234 XDOT = 7502
399702
YDOT = -4365
564007 feet/sec YDOT = -1246
783291 meter/sec
ZDOT = 2876
249309 ZDOT = 913
101979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5749999
67 X = -1752599
90
Y = -12850387
01 feet Y = -3916797
96 meter
Z = -17247608
91 Z = -5257071
20
XDOT = 20073
606433 XDOT = 6118
435241
YDOT = -13031
117868 feet/sec YDOT = -3971
884726 meter/sec
ZDOT = 3033
502691 ZDOT = 924
611620
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 15260
09145604
00016717 00000-0 10270-3 0 9156
2 25544 51
6455 345
1739 0005850 332
7845 27
3001 15
53813845 2345
Satellite: ISS
Catalog Number: 25544
Epoch time: 15260
09145604 = yrday
fracday
Element set: 915
Inclination: 51
6455 deg
RA of node: 345
1739 deg
Eccentricity:
0005850
Arg of perigee: 332
7845 deg
Mean anomaly: 27
3001 deg
Mean motion: 15
53813845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 234
Checksum: 295
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