[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 7th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8342 03 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 905 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 520)
---------------------------------------
Vector Time (GMT): 2015/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4380521
92 A = 6777794
85 meter
Y = 105142
11 meter E =
0009591
Z = 5169322
84 I = 51
27089
XDOT = 1304
103248 Wp = 22
87542
YDOT = 7454
841269 meter/sec RA = 252
48229 deg
ZDOT = -1247
263590 TA = 79
20997
MA = 79
10202
Ha = 222
106 n
mi
Hp = 214
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14371791
07 X = 4353909
85
Y = 344954
42 feet Y = 153979
65 meter
Z = 16959720
61 Z = 5190538
03
XDOT = 4278
553964 XDOT = 1226
703250
YDOT = 24458
140646 feet/sec YDOT = 7468
991731 meter/sec
ZDOT = -4092
072147 ZDOT = -1241
117139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13975336
70 X = -4259682
63
Y = 2871944
76 feet Y = 875368
76 meter
Z = 17051140
51 Z = 5197187
63
XDOT = -9488
347129 XDOT = -2892
048205
YDOT = -21842
783323 feet/sec YDOT = -6657
680357 meter/sec
ZDOT = -4066
857096 ZDOT = -1239
578043
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 15278
54613016
00016717 00000-0 10270-3 0 9006
2 25544 51
6398 253
1888 0006530 2
8300 357
2888 15
54151030 5210
Satellite: ISS
Catalog Number: 25544
Epoch time: 15278
54613016 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 253
1888 deg
Eccentricity:
0006530
Arg of perigee: 2
8300 deg
Mean anomaly: 357
2888 deg
Mean motion: 15
54151030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 521
Checksum: 290
Coasting Arc #2 (Orbit 535)
---------------------------------------
Vector Time (GMT): 2015/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4697556
15 A = 6780357
45 meter
Y = -1793523
34 meter E =
0010669
Z = -4555878
51 I = 51
28999
XDOT = -268
061821 Wp = 73
37146
YDOT = -7023
305458 meter/sec RA = 247
46069 deg
ZDOT = 3050
226555 TA = 227
25996
MA = 227
34980
Ha = 222
271 n
mi
Hp = 213
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15411929
62 X = -4655020
56
Y = -5884262
94 feet Y = -1845817
14 meter
Z = -14947107
98 Z = -4578594
92
XDOT = -879
467916 XDOT = -204
322507
YDOT = -23042
340743 feet/sec YDOT = -7025
946408 meter/sec
ZDOT = 10007
304969 ZDOT = 3049
079881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16284688
65 X = 4963573
10
Y = 2008359
10 feet Y = 612147
85 meter
Z = -15044719
05 Z = -4585630
37
XDOT = 6632
112971 XDOT = 2021
468034
YDOT = 20942
441810 feet/sec YDOT = 6383
256264 meter/sec
ZDOT = 10003
551193 ZDOT = 3049
082404
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 15279
51063760
00016717 00000-0 10270-3 0 9010
2 25544 51
6399 248
3802 0006591 6
6060 353
5178 15
54150373 5361
Satellite: ISS
Catalog Number: 25544
Epoch time: 15279
51063760 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 248
3802 deg
Eccentricity:
0006591
Arg of perigee: 6
6060 deg
Mean anomaly: 353
5178 deg
Mean motion: 15
54150373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 536
Checksum: 305
Coasting Arc #3 (Orbit 551)
---------------------------------------
Vector Time (GMT): 2015/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4822921
31 A = 6784068
63 meter
Y = 3317744
66 meter E =
0015027
Z = 3423747
94 I = 51
31598
XDOT = -938
989338 Wp = 63
65373
YDOT = 6093
140714 meter/sec RA = 242
44850 deg
ZDOT = -4559
623899 TA = 76
04901
MA = 75
88194
Ha = 222
316 n
mi
Hp = 213
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15823232
65 X = 4768831
68
Y = 10884989
06 feet Y = 3371375
70 meter
Z = 11232768
85 Z = 3447045
09
XDOT = -3080
673682 XDOT = -984
905498
YDOT = 19990
619142 feet/sec YDOT = 6082
383068 meter/sec
ZDOT = -14959
395993 ZDOT = -4564
297560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18029197
57 X = -5495299
42
Y = -6446094
01 feet Y = -1964769
45 meter
Z = 11332637
87 Z = 3454188
02
XDOT = -2751
722380 XDOT = -838
724981
YDOT = -18767
015944 feet/sec YDOT = -5720
186460 meter/sec
ZDOT = -14980
561504 ZDOT = -4566
075147
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 15280
53943340
00016717 00000-0 10270-3 0 9026
2 25544 51
6399 243
2504 0006649 9
7866 350
3415 15
54198979 5527
Satellite: ISS
Catalog Number: 25544
Epoch time: 15280
53943340 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 243
2504 deg
Eccentricity:
0006649
Arg of perigee: 9
7866 deg
Mean anomaly: 350
3415 deg
Mean motion: 15
54198979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 552
Checksum: 327
Coasting Arc #4 (Orbit 566)
---------------------------------------
Vector Time (GMT): 2015/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4710151
28 A = 6787433
51 meter
Y = -4469325
95 meter E =
0013075
Z = -1956973
13 I = 51
34297
XDOT = 2232
756891 Wp = 27
30277
YDOT = -4779
482206 meter/sec RA = 237
44806 deg
ZDOT = 5567
637705 TA = 311
01018
MA = 311
12317
Ha = 222
374 n
mi
Hp = 213
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15453252
22 X = -4650317
82
Y = -14663142
89 feet Y = -4521663
67 meter
Z = -6420515
53 Z = -1979708
36
XDOT = 7325
317885 XDOT = 2258
990638
YDOT = -15680
715900 feet/sec YDOT = -4754
366669 meter/sec
ZDOT = 18266
527903 ZDOT = 5578
548376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18850069
21 X = 5745501
10
Y = 9860383
78 feet Y = 3005444
98 meter
Z = -6517783
80 Z = -1986620
50
XDOT = -1900
058163 XDOT = -579
137728
YDOT = 15682
278566 feet/sec YDOT = 4779
958507 meter/sec
ZDOT = 18314
352536 ZDOT = 5582
214653
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 15281
50391827
00016717 00000-0 10270-3 0 9032
2 25544 51
6401 238
4416 0006641 13
8701 346
2633 15
54203498 5670
Satellite: ISS
Catalog Number: 25544
Epoch time: 15281
50391827 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 238
4416 deg
Eccentricity:
0006641
Arg of perigee: 13
8701 deg
Mean anomaly: 346
2633 deg
Mean motion: 15
54203498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 567
Checksum: 296
Coasting Arc #5 (Orbit 582)
---------------------------------------
Vector Time (GMT): 2015/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4277805
63 A = 6789003
26 meter
Y = 5264420
20 meter E =
0011455
Z = 229983
13 I = 51
36734
XDOT = -3582
460156 Wp = 100
55148
YDOT = 3183
387351 meter/sec RA = 232
45583 deg
ZDOT = -5981
238275 TA = 76
96241
MA = 76
83456
Ha = 222
486 n
mi
Hp = 213
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14034795
39 X = 4217502
49
Y = 17271719
83 feet Y = 5311920
30 meter
Z = 754537
82 Z = 250616
85
XDOT = -11753
478202 XDOT = -3588
736472
YDOT = 10444
184222 feet/sec YDOT = 3143
290024 meter/sec
ZDOT = -19623
485153 ZDOT = -5998
656971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18454883
59 X = -5625048
52
Y = -12432391
66 feet Y = -3789392
98 meter
Z = 842629
25 Z = 256833
40
XDOT = 7172
600220 XDOT = 2186
208547
YDOT = -12032
539198 feet/sec YDOT = -3667
517947 meter/sec
ZDOT = -19699
099533 ZDOT = -6004
285538
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 15282
53268988
00016717 00000-0 10270-3 0 9048
2 25544 51
6411 233
3115 0006663 16
9666 343
1709 15
54229634 5837
Satellite: ISS
Catalog Number: 25544
Epoch time: 15282
53268988 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 233
3115 deg
Eccentricity:
0006663
Arg of perigee: 16
9666 deg
Mean anomaly: 343
1709 deg
Mean motion: 15
54229634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 583
Checksum: 319
Coasting Arc #6 (Orbit 598)
---------------------------------------
Vector Time (GMT): 2015/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3522904
82 A = 6788061
88 meter
Y = -5595439
95 meter E =
0019364
Z = 1485730
23 I = 51
38464
XDOT = 4848
020520 Wp = 48
73313
YDOT = -1514
691865 meter/sec RA = 227
46628 deg
ZDOT = 5754
616403 TA = 327
56172
MA = 327
68060
Ha = 222
493 n
mi
Hp = 213
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11558086
68 X = -3467290
62
Y = -18357742
63 feet Y = -5634524
23 meter
Z = 4874443
01 Z = 1468752
33
XDOT = 15905
579135 XDOT = 4836
643782
YDOT = -4969
461498 feet/sec YDOT = -1460
540911 meter/sec
ZDOT = 18879
975075 ZDOT = 5778
139971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16678096
41 X = 5083483
79
Y = 13897362
79 feet Y = 4235916
18 meter
Z = 4802154
15 Z = 1463696
58
XDOT = -12474
895916 XDOT = -3802
348275
YDOT = 8370
232639 feet/sec YDOT = 2551
246909 meter/sec
ZDOT = 18981
638220 ZDOT = 5785
603330
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 15283
56144828
00016717 00000-0 10270-3 0 9059
2 25544 51
6413 228
1821 0006618 20
6641 339
4779 15
54254491 5991
Satellite: ISS
Catalog Number: 25544
Epoch time: 15283
56144828 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 228
1821 deg
Eccentricity:
0006618
Arg of perigee: 20
6641 deg
Mean anomaly: 339
4779 deg
Mean motion: 15
54254491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 599
Checksum: 324
Coasting Arc #7 (Orbit 613)
---------------------------------------
Vector Time (GMT): 2015/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2413107
91 A = 6784903
35 meter
Y = 5547324
00 meter E =
0008513
Z = -3084236
29 I = 51
39749
XDOT = -5908
023855 Wp = 55
92029
YDOT = -135
681370 meter/sec RA = 222
47210 deg
ZDOT = -4871
481795 TA = 159
61534
MA = 159
58134
Ha = 222
571 n
mi
Hp = 213
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7917020
71 X = 2365879
32
Y = 18199881
89 feet Y = 5574044
46 meter
Z = -10118885
47 Z = -3072629
21
XDOT = -19383
280363 XDOT = -5882
403359
YDOT = -445
148853 feet/sec YDOT = -201
606219 meter/sec
ZDOT = -15982
551821 ZDOT = -4900
119982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13450720
21 X = -4099779
52
Y = -14628237
32 feet Y = -4458686
74 meter
Z = -10069734
83 Z = -3069255
18
XDOT = 17317
401249 XDOT = 5278
343901
YDOT = -4847
777554 feet/sec YDOT = -1477
602599 meter/sec
ZDOT = -16106
005163 ZDOT = -4909
110374
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 15284
52589794
00016717 00000-0 10270-3 0 9062
2 25544 51
6422 223
3728 0006714 23
9152 336
2312 15
54277936 6149
Satellite: ISS
Catalog Number: 25544
Epoch time: 15284
52589794 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 223
3728 deg
Eccentricity:
0006714
Arg of perigee: 23
9152 deg
Mean anomaly: 336
2312 deg
Mean motion: 15
54277936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 614
Checksum: 315
Coasting Arc #8 (Orbit 629)
---------------------------------------
Vector Time (GMT): 2015/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1019889
60 A = 6780919
89 meter
Y = -5120191
50 meter E =
0012651
Z = 4314748
32 I = 51
40892
XDOT = 6653
583464 Wp = 77
29582
YDOT = 1606
995104 meter/sec RA = 217
46982 deg
ZDOT = 3473
826348 TA = 337
29566
MA = 337
35157
Ha = 222
546 n
mi
Hp = 212
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3346094
49 X = -983518
38
Y = -16798528
54 feet Y = -5131392
63 meter
Z = 14155998
42 Z = 4309882
84
XDOT = 21829
342072 XDOT = 6618
244292
YDOT = 5272
293649 feet/sec YDOT = 1681
202741 meter/sec
ZDOT = 11397
068070 ZDOT = 3506
062677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8949602
30 X = 2727838
78
Y = 14624015
87 feet Y = 4457400
04 meter
Z = 14135840
23 Z = 4308604
10
XDOT = -21185
377555 XDOT = -6457
303079
YDOT = 1795
637006 feet/sec YDOT = 547
310159 meter/sec
ZDOT = 11535
808125 ZDOT = 3516
114316
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 15285
55463095
00016717 00000-0 10270-3 0 9072
2 25544 51
6426 218
2437 0006575 27
6711 332
4790 15
54305973 6309
Satellite: ISS
Catalog Number: 25544
Epoch time: 15285
55463095 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 218
2437 deg
Eccentricity:
0006575
Arg of perigee: 27
6711 deg
Mean anomaly: 332
4790 deg
Mean motion: 15
54305973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 630
Checksum: 315
Coasting Arc #9 (Orbit 644)
---------------------------------------
Vector Time (GMT): 2015/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -584282
16 A = 6777787
30 meter
Y = 4447099
13 meter E =
0018644
Z = -5097884
49 I = 51
42482
XDOT = -6916
859531 Wp = 62
48673
YDOT = -2823
817215 meter/sec RA = 212
45787 deg
ZDOT = -1666
836836 TA = 191
31980
MA = 191
36179
Ha = 222
644 n
mi
Hp = 212
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1916936
22 X = -609203
15
Y = 14590220
24 feet Y = 4440425
32 meter
Z = -16725342
80 Z = -5100783
97
XDOT = -22693
108699 XDOT = -6876
671802
YDOT = -9264
492174 feet/sec YDOT = -2900
941607 meter/sec
ZDOT = -5468
624790 ZDOT = -1700
340316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3510682
77 X = -1070056
11
Y = -14275226
62 feet Y = -4351089
07 meter
Z = -16738556
52 Z = -5101912
03
XDOT = 23431
037186 XDOT = 7141
780134
YDOT = 833
174872 feet/sec YDOT = 253
951701 meter/sec
ZDOT = -5612
645481 ZDOT = -1710
734343
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 15286
51905774
00016717 00000-0 10270-3 0 9085
2 25544 51
6430 213
4343 0006708 31
1642 328
9908 15
54315926 6454
Satellite: ISS
Catalog Number: 25544
Epoch time: 15286
51905774 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 213
4343 deg
Eccentricity:
0006708
Arg of perigee: 31
1642 deg
Mean anomaly: 328
9908 deg
Mean motion: 15
54315926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 645
Checksum: 313
Coasting Arc #10 (Orbit 660)
---------------------------------------
Vector Time (GMT): 2015/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2276070
31 A = 6776699
56 meter
Y = -3566742
58 meter E =
0008635
Z = 5288488
21 I = 51
44906
XDOT = 6679
037717 Wp = 45
48669
YDOT = 3764
254977 meter/sec RA = 207
44249 deg
ZDOT = -329
519161 TA = 47
69743
MA = 47
62428
Ha = 222
501 n
mi
Hp = 212
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7467422
27 X = 2290095
25
Y = -11701911
36 feet Y = -3541211
05 meter
Z = 17350683
09 Z = 5299579
63
XDOT = 21912
853401 XDOT = 6638
049213
YDOT = 12349
917902 feet/sec YDOT = 3838
715164 meter/sec
ZDOT = -1081
099608 ZDOT = -297
172943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2467470
34 X = -752084
96
Y = 13598778
99 feet Y = 4144907
84 meter
Z = 17399084
13 Z = 5303240
84
XDOT = -23950
782025 XDOT = -7300
198361
YDOT = -3114
047259 feet/sec YDOT = -949
161604 meter/sec
ZDOT = -942
206801 ZDOT = -287
184633
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 15287
54776502
00016717 00000-0 10270-3 0 9095
2 25544 51
6429 208
3051 0006618 33
7057 326
4516 15
54358721 6615
Satellite: ISS
Catalog Number: 25544
Epoch time: 15287
54776502 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 208
3051 deg
Eccentricity:
0006618
Arg of perigee: 33
7057 deg
Mean anomaly: 326
4516 deg
Mean motion: 15
54358721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 661
Checksum: 314
Coasting Arc #11 (Orbit 675)
---------------------------------------
Vector Time (GMT): 2015/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3877850
19 A = 6778391
81 meter
Y = 2628750
67 meter E =
0015980
Z = -4911982
40 I = 51
48365
XDOT = -5851
178886 Wp = 83
80315
YDOT = -4380
853209 meter/sec RA = 202
42932 deg
ZDOT = 2282
902798 TA = 208
54977
MA = 208
63738
Ha = 222
680 n
mi
Hp = 212
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12722605
60 X = -3883096
17
Y = 8624510
09 feet Y = 2585356
19 meter
Z = -16115427
81 Z = -4930833
68
XDOT = -19196
781123 XDOT = -5812
845993
YDOT = -14372
877982 feet/sec YDOT = -4446
070397 meter/sec
ZDOT = 7489
838577 ZDOT = 2254
571772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8278258
49 X = 2523213
19
Y = -12848214
00 feet Y = -3916135
63 meter
Z = -16197151
43 Z = -4936891
75
XDOT = 22379
191826 XDOT = 6821
177668
YDOT = 5163
550471 feet/sec YDOT = 1573
850184 meter/sec
ZDOT = 7368
347626 ZDOT = 2245
872356
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 15288
51216847
00016717 00000-0 10270-3 0 9106
2 25544 51
6433 203
4956 0006705 37
8060 322
3563 15
54343987 6767
Satellite: ISS
Catalog Number: 25544
Epoch time: 15288
51216847 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 203
4956 deg
Eccentricity:
0006705
Arg of perigee: 37
8060 deg
Mean anomaly: 322
3563 deg
Mean motion: 15
54343987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 676
Checksum: 317
Coasting Arc #12 (Orbit 691)
---------------------------------------
Vector Time (GMT): 2015/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5266452
86 A = 6781954
23 meter
Y = -1630407
74 meter E =
0016772
Z = 3941955
83 I = 51
52501
XDOT = 4490
309171 Wp = 65
68558
YDOT = 4752
282276 meter/sec RA = 197
42626 deg
ZDOT = -4013
243822 TA = 66
33173
MA = 66
15579
Ha = 222
660 n
mi
Hp = 212
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17278388
66 X = 5265144
07
Y = -5349106
77 feet Y = -1571521
79 meter
Z = 12932925
95 Z = 3967536
78
XDOT = 14731
985468 XDOT = 4456
329553
YDOT = 15591
477282 feet/sec YDOT = 4802
305558 meter/sec
ZDOT = -13166
810440 ZDOT = -3991
513184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13565480
26 X = -4134758
38
Y = 11843157
30 feet Y = 3609794
34 meter
Z = 13043527
22 Z = 3975667
10
XDOT = -18990
276325 XDOT = -5788
236224
YDOT = -7280
505880 feet/sec YDOT = -2219
098192 meter/sec
ZDOT = -13073
835773 ZDOT = -3984
905144
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 15289
54085200
00016717 00000-0 10270-3 0 9118
2 25544 51
6428 198
3658 0006705 41
9424 318
2241 15
54358302 6924
Satellite: ISS
Catalog Number: 25544
Epoch time: 15289
54085200 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 198
3658 deg
Eccentricity:
0006705
Arg of perigee: 41
9424 deg
Mean anomaly: 318
2241 deg
Mean motion: 15
54358302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 692
Checksum: 306
Coasting Arc #13 (Orbit 706)
---------------------------------------
Vector Time (GMT): 2015/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6242260
12 A = 6785682
57 meter
Y = 704537
20 meter E =
0011728
Z = -2561212
65 I = 51
56892
XDOT = -2700
884518 Wp = 48
68755
YDOT = -4873
801083 meter/sec RA = 192
43585 deg
ZDOT = 5265
234108 TA = 282
49950
MA = 282
63069
Ha = 222
655 n
mi
Hp = 212
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20479856
05 X = -6237232
80
Y = 2311473
77 feet Y = 634760
07 meter
Z = -8402928
63 Z = -2591524
83
XDOT = -8861
169680 XDOT = -2671
760846
YDOT = -15990
161033 feet/sec YDOT = -4903
840961 meter/sec
ZDOT = 17274
390118 ZDOT = 5252
184517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17566928
24 X = 5354399
73
Y = -10674915
12 feet Y = -3253714
13 meter
Z = -8533805
92 Z = -2601104
05
XDOT = 14077
940166 XDOT = 4290
956163
YDOT = 9461
851925 feet/sec YDOT = 2883
972467 meter/sec
ZDOT = 17218
873435 ZDOT = 5248
312623
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 15290
50523017
00016717 00000-0 10270-3 0 9120
2 25544 51
6432 193
5562 0006667 45
0061 315
1631 15
54393854 7076
Satellite: ISS
Catalog Number: 25544
Epoch time: 15290
50523017 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 193
5562 deg
Eccentricity:
0006667
Arg of perigee: 45
0061 deg
Mean anomaly: 315
1631 deg
Mean motion: 15
54393854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 707
Checksum: 290
Coasting Arc #14 (Orbit 722)
---------------------------------------
Vector Time (GMT): 2015/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6729867
45 A = 6788279
51 meter
Y = 219225
39 meter E =
0016290
Z = 828025
82 I = 51
60846
XDOT = 584
916420 Wp = 102
83626
YDOT = 4819
214637 meter/sec RA = 187
45735 deg
ZDOT = -5934
925004 TA = 68
20505
MA = 68
03180
Ha = 222
777 n
mi
Hp = 212
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22079617
61 X = 6722893
52
Y = 719243
40 feet Y = 294444
26 meter
Z = 2716620
13 Z = 860701
88
XDOT = 1919
017126 XDOT = 559
813516
YDOT = 15811
071645 feet/sec YDOT = 4825
614856 meter/sec
ZDOT = -19471
538726 ZDOT = -5932
144791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20173122
59 X = -6148767
77
Y = 8960261
78 feet Y = 2731087
79 meter
Z = 2857566
00 Z = 870986
12
XDOT = -8071
010666 XDOT = -2460
044051
YDOT = -11870
407414 feet/sec YDOT = -3618
100180 meter/sec
ZDOT = -19460
313629 ZDOT = -5931
503594
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 15291
53388876
00016717 00000-0 10270-3 0 9137
2 25544 51
6430 188
4257 0006613 49
2347 310
9379 15
54379170 7237
Satellite: ISS
Catalog Number: 25544
Epoch time: 15291
53388876 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 188
4257 deg
Eccentricity:
0006613
Arg of perigee: 49
2347 deg
Mean anomaly: 310
9379 deg
Mean motion: 15
54379170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 723
Checksum: 328
Coasting Arc #15 (Orbit 738)
---------------------------------------
Vector Time (GMT): 2015/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6629525
22 A = 6788159
15 meter
Y = -1042357
21 meter E =
0020151
Z = 952706
62 I = 51
64005
XDOT = 1587
792060 Wp = 54
02517
YDOT = -4619
728245 meter/sec RA = 182
48425 deg
ZDOT = 5918
495455 TA = 316
30080
MA = 316
46015
Ha = 222
779 n
mi
Hp = 212
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21750410
82 X = -6622004
57
Y = -3419807
14 feet Y = -1116450
83 meter
Z = 3125677
89 Z = 920519
48
XDOT = 5209
291537 XDOT = 1610
582676
YDOT = -15156
588729 feet/sec YDOT = -4601
844753 meter/sec
ZDOT = 19417
636008 ZDOT = 5926
264376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20972997
51 X = 6392569
64
Y = -6764376
85 feet Y = -2061782
06 meter
Z = 2986954
17 Z = 910423
63
XDOT = 1801
575177 XDOT = 549
120114
YDOT = 14290
260087 feet/sec YDOT = 4355
671275 meter/sec
ZDOT = 19451
897936 ZDOT = 5928
938491
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 15292
56253363
00016717 00000-0 10270-3 0 9144
2 25544 51
6431 183
2953 0006692 51
2479 308
9271 15
54412707 7399
Satellite: ISS
Catalog Number: 25544
Epoch time: 15292
56253363 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 183
2953 deg
Eccentricity:
0006692
Arg of perigee: 51
2479 deg
Mean anomaly: 308
9271 deg
Mean motion: 15
54412707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 739
Checksum: 317
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