[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 21st 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 ET - UTC (sec) : 68 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
270/16:51:48
844 -0
9 1
4 1
4
N/A -0
9 0
0 220
7
000/00:03:37
689 -0
6 0
0 215
8
274/01:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
6
277/10:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 215
2
Coasting Arc #1 (Orbit 3656)
---------------------------------------
Vector Time (GMT): 2017/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4132807
60 A = 6781827
06 meter
Y = 3489485
97 meter E =
0005846
Z = -4097468
59 I = 51
26999
XDOT = -1688
862231 Wp = 39
06166
YDOT = -6445
021236 meter/sec RA = 282
41156 deg
ZDOT = -3783
780884 TA = 191
65724
MA = 191
67078
Ha = 219
881 n
mi
Hp = 215
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13559080
05 X = -4151617
26
Y = 11448444
80 feet Y = 3443164
35 meter
Z = -13443138
43 Z = -4117590
71
XDOT = -5540
886585 XDOT = -1598
286974
YDOT = -21145
082796 feet/sec YDOT = -6463
401343 meter/sec
ZDOT = -12413
979279 ZDOT = -3791
763967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13726357
56 X = 4183793
78
Y = -11139410
17 feet Y = -3395292
22 meter
Z = -13532707
05 Z = -4124769
11
XDOT = 4166
884141 XDOT = 1270
066286
YDOT = 20263
346418 feet/sec YDOT = 6176
267988 meter/sec
ZDOT = -12448
317873 ZDOT = -3794
247288
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 17263
52308588
00016717 00000-0 10270-3 0 9005
2 25544 51
6401 283
0712 0003992 301
2220 58
8541 15
54230277 36573
Satellite: ISS
Catalog Number: 25544
Epoch time: 17263
52308588 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 283
0712 deg
Eccentricity:
0003992
Arg of perigee: 301
2220 deg
Mean anomaly: 58
8541 deg
Mean motion: 15
54230277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3657
Checksum: 292
Coasting Arc #2 (Orbit 3672)
---------------------------------------
Vector Time (GMT): 2017/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4247616
12 A = 6778506
63 meter
Y = -1823735
75 meter E =
0002179
Z = 4956418
66 I = 51
25153
XDOT = 728
271374 Wp = 116
06516
YDOT = 7346
762665 meter/sec RA = 277
39075 deg
ZDOT = 2077
495077 TA = 313
60215
MA = 313
62023
Ha = 219
893 n
mi
Hp = 215
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13935748
43 X = 4243617
92
Y = -5983385
00 feet Y = -1776257
66 meter
Z = 16261216
07 Z = 4977042
93
XDOT = 2389
341777 XDOT = 635
972274
YDOT = 24103
552049 feet/sec YDOT = 7354
390909 meter/sec
ZDOT = 6815
928730 ZDOT = 2080
807598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13861151
46 X = -4224878
96
Y = 5906715
14 feet Y = 1800366
77 meter
Z = 16352746
71 Z = 4984317
20
XDOT = -1782
682170 XDOT = -543
361526
YDOT = -23105
740285 feet/sec YDOT = -7042
629639 meter/sec
ZDOT = 6829
477903 ZDOT = 2081
624865
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 17264
55185657
00016717 00000-0 10270-3 0 9010
2 25544 51
6388 277
9410 0003952 307
2642 52
8149 15
54223349 36732
Satellite: ISS
Catalog Number: 25544
Epoch time: 17264
55185657 = yrday
fracday
Element set: 901
Inclination: 51
6388 deg
RA of node: 277
9410 deg
Eccentricity:
0003952
Arg of perigee: 307
2642 deg
Mean anomaly: 52
8149 deg
Mean motion: 15
54223349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3673
Checksum: 326
Coasting Arc #3 (Orbit 3687)
---------------------------------------
Vector Time (GMT): 2017/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4249498
14 A = 6777118
71 meter
Y = -11184
85 meter E =
0012048
Z = -5289529
40 I = 51
24311
XDOT = 201
247123 Wp = 76
21341
YDOT = -7656
139775 meter/sec RA = 272
36422 deg
ZDOT = -142
943538 TA = 192
40054
MA = 192
43021
Ha = 220
092 n
mi
Hp = 215
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13941923
02 X = -4223363
04
Y = -36695
71 feet Y = -58560
21 meter
Z = -17354099
09 Z = -5310108
87
XDOT = 660
259590 XDOT = 287
539515
YDOT = -25118
568817 feet/sec YDOT = -7653
406822 meter/sec
ZDOT = -468
974861 ZDOT = -141
755322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13827306
86 X = 4214563
13
Y = -124504
93 feet Y = -37949
10 meter
Z = -17445154
14 Z = -5317282
98
XDOT = -376
936935 XDOT = -114
890378
YDOT = 24116
367666 feet/sec YDOT = 7350
668865 meter/sec
ZDOT = -462
576650 ZDOT = -140
993363
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 17265
51632661
00016717 00000-0 10270-3 0 9020
2 25544 51
6384 273
1331 0004080 309
2624 50
8167 15
54212263 36880
Satellite: ISS
Catalog Number: 25544
Epoch time: 17265
51632661 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 273
1331 deg
Eccentricity:
0004080
Arg of perigee: 309
2624 deg
Mean anomaly: 50
8167 deg
Mean motion: 15
54212263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3688
Checksum: 294
Coasting Arc #4 (Orbit 3703)
---------------------------------------
Vector Time (GMT): 2017/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4133868
05 A = 6778137
95 meter
Y = 1869532
99 meter E =
0006134
Z = 5036098
26 I = 51
24591
XDOT = -1114
525113 Wp = 14
45054
YDOT = 7366
912544 meter/sec RA = 267
33546 deg
ZDOT = -1813
617040 TA = 93
23916
MA = 93
16898
Ha = 220
094 n
mi
Hp = 215
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13562559
21 X = 4088192
00
Y = 6133638
41 feet Y = 1915505
93 meter
Z = 16522632
09 Z = 5056068
39
XDOT = -3656
578455 XDOT = -1188
011285
YDOT = 24169
660578 feet/sec YDOT = 7354
038061 meter/sec
ZDOT = -5950
187138 ZDOT = -1819
210490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13625933
41 X = -4153184
50
Y = -5742812
48 feet Y = -1750409
24 meter
Z = 16610717
85 Z = 5062946
80
XDOT = 2497
266274 XDOT = 761
166760
YDOT = -23270
174451 feet/sec YDOT = -7092
749173 meter/sec
ZDOT = -5976
022306 ZDOT = -1821
491599
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 17266
54509142
00016717 00000-0 10270-3 0 9032
2 25544 51
6379 268
0031 0004117 313
7831 46
2981 15
54236456 37047
Satellite: ISS
Catalog Number: 25544
Epoch time: 17266
54509142 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 268
0031 deg
Eccentricity:
0004117
Arg of perigee: 313
7831 deg
Mean anomaly: 46
2981 deg
Mean motion: 15
54236456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3704
Checksum: 303
Coasting Arc #5 (Orbit 3718)
---------------------------------------
Vector Time (GMT): 2017/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3919048
27 A = 6781327
89 meter
Y = -3551180
20 meter E =
0005109
Z = -4248841
77 I = 51
25942
XDOT = 2011
259986 Wp = 86
72977
YDOT = -6479
439609 meter/sec RA = 262
31426 deg
ZDOT = 3564
374159 TA = 219
85580
MA = 219
89333
Ha = 220
330 n
mi
Hp = 215
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12857769
93 X = -3858407
69
Y = -11650853
67 feet Y = -3594667
05 meter
Z = -13939769
57 Z = -4267731
88
XDOT = 6598
622002 XDOT = 2066
251110
YDOT = -21258
003966 feet/sec YDOT = -6456
640483 meter/sec
ZDOT = 11694
140943 ZDOT = 3574
278606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13290201
96 X = 4050853
56
Y = 11050448
45 feet Y = 3368176
69 meter
Z = -14022836
21 Z = -4274160
48
XDOT = -4728
033811 XDOT = -1441
104706
YDOT = 20566
229265 feet/sec YDOT = 6268
586680 meter/sec
ZDOT = 11738
911422 ZDOT = 3578
020202
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 17267
50955515
00016717 00000-0 10270-3 0 9049
2 25544 51
6383 263
1949 0004160 319
6753 40
4091 15
54217185 37194
Satellite: ISS
Catalog Number: 25544
Epoch time: 17267
50955515 = yrday
fracday
Element set: 904
Inclination: 51
6383 deg
RA of node: 263
1949 deg
Eccentricity:
0004160
Arg of perigee: 319
6753 deg
Mean anomaly: 40
4091 deg
Mean motion: 15
54217185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3719
Checksum: 317
Coasting Arc #6 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2017/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3561120
47 A = 6785116
24 meter
Y = 4944983
04 meter E =
0010586
Z = 2977163
37 I = 51
27670
XDOT = -2916
292467 Wp = 79
85103
YDOT = 5085
872337 meter/sec RA = 257
30292 deg
ZDOT = -4942
303824 TA = 65
90948
MA = 65
79877
Ha = 220
407 n
mi
Hp = 215
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11683466
12 X = 3491097
90
Y = 16223697
63 feet Y = 4984414
67 meter
Z = 9767596
36 Z = 2994291
89
XDOT = -9567
888671 XDOT = -2948
939693
YDOT = 16685
932864 feet/sec YDOT = 5053
077376 meter/sec
ZDOT = -16214
907558 ZDOT = -4956
550210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12623256
68 X = -3847568
64
Y = -15456157
70 feet Y = -4711036
87 meter
Z = 9842675
66 Z = 3000047
54
XDOT = 7258
712163 XDOT = 2212
455467
YDOT = -16329
745888 feet/sec YDOT = -4977
306547 meter/sec
ZDOT = -16278
681948 ZDOT = -4961
742258
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 17268
53831249
00016717 00000-0 10270-3 0 9051
2 25544 51
6371 258
0652 0004355 322
9580 37
1271 15
54265589 37358
Satellite: ISS
Catalog Number: 25544
Epoch time: 17268
53831249 = yrday
fracday
Element set: 905
Inclination: 51
6371 deg
RA of node: 258
0652 deg
Eccentricity:
0004355
Arg of perigee: 322
9580 deg
Mean anomaly: 37
1271 deg
Mean motion: 15
54265589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3735
Checksum: 323
Coasting Arc #7 (Orbit 3749)
---------------------------------------
Vector Time (GMT): 2017/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3058276
79 A = 6788080
70 meter
Y = -5888621
49 meter E =
0010609
Z = -1402125
06 I = 51
29474
XDOT = 3790
098281 Wp = 16
34884
YDOT = -3337
923467 meter/sec RA = 252
30314 deg
ZDOT = 5772
366758 TA = 328
28841
MA = 328
35227
Ha = 220
466 n
mi
Hp = 215
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10033716
50 X = -2985390
44
Y = -19319624
30 feet Y = -5922413
80 meter
Z = -4600147
85 Z = -1416803
90
XDOT = 12434
705645 XDOT = 3799
102470
YDOT = -10951
192477 feet/sec YDOT = -3295
489193 meter/sec
ZDOT = 18938
211147 ZDOT = 5790
800241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11525806
54 X = 3513065
83
Y = 18452239
26 feet Y = 5624242
53 meter
Z = -4664264
15 Z = -1421667
71
XDOT = -10043
481184 XDOT = -3061
253065
YDOT = 11064
390573 feet/sec YDOT = 3372
426247 meter/sec
ZDOT = 19020
260529 ZDOT = 5797
375409
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 17269
50277136
00016717 00000-0 10270-3 0 9069
2 25544 51
6371 253
2573 0004101 326
9103 33
1793 15
54262503 37506
Satellite: ISS
Catalog Number: 25544
Epoch time: 17269
50277136 = yrday
fracday
Element set: 906
Inclination: 51
6371 deg
RA of node: 253
2573 deg
Eccentricity:
0004101
Arg of perigee: 326
9103 deg
Mean anomaly: 33
1793 deg
Mean motion: 15
54262503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3750
Checksum: 289
Coasting Arc #8 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2017/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2349317
41 A = 6788880
23 meter
Y = 6356466
12 meter E =
0007265
Z = -355462
40 I = 51
30921
XDOT = -4607
948618 Wp = 129
00868
YDOT = 1374
078504 meter/sec RA = 247
30828 deg
ZDOT = -5970
063622 TA = 54
83933
MA = 54
77129
Ha = 220
679 n
mi
Hp = 215
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7707734
27 X = 2279789
78
Y = 20854547
63 feet Y = 6382349
01 meter
Z = -1166215
22 Z = -344219
36
XDOT = -15117
941661 XDOT = -4593
971508
YDOT = 4508
131576 feet/sec YDOT = 1322
626992 meter/sec
ZDOT = -19586
822907 ZDOT = -5992
413995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9714106
60 X = -2960859
69
Y = -20001725
71 feet Y = -6096526
00 meter
Z = -1117355
71 Z = -340570
02
XDOT = 13019
104907 XDOT = 3968
223176
YDOT = -5239
808145 feet/sec YDOT = -1597
093523 meter/sec
ZDOT = -19685
929826 ZDOT = -6000
271411
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 17270
53152200
00016717 00000-0 10270-3 0 9079
2 25544 51
6380 248
1271 0004348 331
6368 28
4548 15
54264842 37663
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
53152200 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 248
1271 deg
Eccentricity:
0004348
Arg of perigee: 331
6368 deg
Mean anomaly: 28
4548 deg
Mean motion: 15
54264842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 306
Coasting Arc #9 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2017/270/16:53:37
689
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2402803
16 A = 6779783
44 meter
Y = 4133340
18 meter E =
0010498
Z = -4816662
61 I = 51
28216
XDOT = -4621
891036 Wp = 49
30489
YDOT = -5581
780268 meter/sec RA = 246
30420 deg
ZDOT = -2481
117761 TA = 196
15000
MA = 196
18348
Ha = 220
663 n
mi
Hp = 215
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7883212
45 X = -2425447
46
Y = 13560827
35 feet Y = 4106343
43 meter
Z = -15802698
85 Z = -4828390
10
XDOT = -15163
684500 XDOT = -4547
078397
YDOT = -18312
927388 feet/sec YDOT = -5633
047283 meter/sec
ZDOT = -8140
150135 ZDOT = -2503
387586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11863396
51 X = -3615963
26
Y = -10180342
78 feet Y = -3102968
48 meter
Z = -15855182
50 Z = -4832659
63
XDOT = 20076
206134 XDOT = 6119
227630
YDOT = -10549
219739 feet/sec YDOT = -3215
402176 meter/sec
ZDOT = -8237
922331 ZDOT = -2510
918726
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 17270
72441435
00016717 00000-0 10270-3 0 9082
2 25544 51
6414 247
1668 0004531 316
9710 43
1088 15
54012782 37691
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
72441435 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 247
1668 deg
Eccentricity:
0004531
Arg of perigee: 316
9710 deg
Mean anomaly: 43
1088 deg
Mean motion: 15
54012782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3769
Checksum: 307
Coasting Arc #10 (Orbit 3784)
---------------------------------------
Vector Time (GMT): 2017/271/16:53:37
689
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3332960
19 A = 6777817
72 meter
Y = -2683908
10 meter E =
0002088
Z = 5256114
07 I = 51
28905
XDOT = 4129
608232 Wp = 353
88842
YDOT = 6427
530582 meter/sec RA = 241
28312 deg
ZDOT = 665
498075 TA = 89
73831
MA = 89
71439
Ha = 220
598 n
mi
Hp = 215
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10934908
76 X = 3337192
82
Y = -8805472
75 feet Y = -2646612
62 meter
Z = 17244468
74 Z = 5272315
16
XDOT = 13548
583437 XDOT = 4054
194262
YDOT = 21087
698760 feet/sec YDOT = 6473
289060 meter/sec
ZDOT = 2183
392633 ZDOT = 685
374966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6832698
12 X = 2082606
39
Y = 12162717
09 feet Y = 3707196
17 meter
Z = 17316547
91 Z = 5278083
80
XDOT = -22197
617332 XDOT = -6765
833763
YDOT = 9247
082293 feet/sec YDOT = 2818
510683 meter/sec
ZDOT = 2270
474768 ZDOT = 692
040709
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 17271
75333675
00016717 00000-0 10270-3 0 9093
2 25544 51
6406 242
0387 0004529 319
5639 40
5176 15
54021058 37853
Satellite: ISS
Catalog Number: 25544
Epoch time: 17271
75333675 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 242
0387 deg
Eccentricity:
0004529
Arg of perigee: 319
5639 deg
Mean anomaly: 40
5176 deg
Mean motion: 15
54021058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3785
Checksum: 320
Coasting Arc #11 (Orbit 3799)
---------------------------------------
Vector Time (GMT): 2017/272/16:53:37
689
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4217848
10 A = 6778148
29 meter
Y = 1163854
99 meter E =
0011249
Z = -5186174
85 I = 51
30689
XDOT = -3357
804848 Wp = 82
93033
YDOT = -6777
469459 meter/sec RA = 236
26124 deg
ZDOT = 1213
523241 TA = 198
75932
MA = 198
80081
Ha = 220
795 n
mi
Hp = 215
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13838084
31 X = -4205357
11
Y = 3818421
90 feet Y = 1116757
59 meter
Z = -17015009
35 Z = -5206633
72
XDOT = -11016
420106 XDOT = -3287
662558
YDOT = -22235
792187 feet/sec YDOT = -6814
626442 meter/sec
ZDOT = 3981
375463 ZDOT = 1197
382846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1667517
87 X = -508259
45
Y = -14149095
99 feet Y = -4312644
46 meter
Z = -17105728
08 Z = -5213825
92
XDOT = 22633
737502 XDOT = 6898
763191
YDOT = -7381
223673 feet/sec YDOT = -2249
796975 meter/sec
ZDOT = 3910
859950 ZDOT = 1192
030113
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 17272
71794957
00016717 00000-0 10270-3 0 9106
2 25544 51
6408 237
2315 0004624 322
7224 37
3607 15
54016671 38000
Satellite: ISS
Catalog Number: 25544
Epoch time: 17272
71794957 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 237
2315 deg
Eccentricity:
0004624
Arg of perigee: 322
7224 deg
Mean anomaly: 37
3607 deg
Mean motion: 15
54016671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3800
Checksum: 300
Coasting Arc #12 (Orbit 3815)
---------------------------------------
Vector Time (GMT): 2017/273/16:53:37
689
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4982547
56 A = 6780506
75 meter
Y = 346007
93 meter E =
0008990
Z = 4585191
68 I = 51
33468
XDOT = 2295
186773 Wp = 33
95244
YDOT = 6678
203519 meter/sec RA = 231
24392 deg
ZDOT = -2987
871707 TA = 86
03672
MA = 85
93395
Ha = 220
830 n
mi
Hp = 215
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16346940
80 X = 4956035
38
Y = 1135196
61 feet Y = 401578
33 meter
Z = 15043279
78 Z = 4609331
03
XDOT = 7530
140332 XDOT = 2234
852421
YDOT = 21910
116532 feet/sec YDOT = 6703
532254 meter/sec
ZDOT = -9802
728696 ZDOT = -2976
869476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3340267
55 X = -1018113
55
Y = 15941414
43 feet Y = 4858943
12 meter
Z = 15150093
40 Z = 4617748
47
XDOT = -21577
436477 XDOT = -6576
802638
YDOT = 4780
972993 feet/sec YDOT = 1457
240568 meter/sec
ZDOT = -9754
924990 ZDOT = -2973
301137
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 17273
74686347
00016717 00000-0 10270-3 0 9114
2 25544 51
6413 232
1033 0004775 326
7225 33
3627 15
54052747 38168
Satellite: ISS
Catalog Number: 25544
Epoch time: 17273
74686347 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 232
1033 deg
Eccentricity:
0004775
Arg of perigee: 326
7225 deg
Mean anomaly: 33
3627 deg
Mean motion: 15
54052747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3816
Checksum: 306
Coasting Arc #13 (Orbit 3821)
---------------------------------------
Vector Time (GMT): 2017/274/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3503766
66 A = 6789002
97 meter
Y = -5662813
39 meter E =
0014193
Z = 1277213
25 I = 51
36941
XDOT = 4736
884151 Wp = 41
98592
YDOT = -1613
096452 meter/sec RA = 229
43658 deg
ZDOT = 5815
486687 TA = 331
96718
MA = 332
04355
Ha = 220
890 n
mi
Hp = 215
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11495297
44 X = -3446387
27
Y = -18578784
10 feet Y = -5701673
96 meter
Z = 4190332
20 Z = 1260332
86
XDOT = 15540
958501 XDOT = 4726
321269
YDOT = -5292
311195 feet/sec YDOT = -1560
183903 meter/sec
ZDOT = 19079
680732 ZDOT = 5838
471588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20037538
06 X = -6107441
60
Y = -8742115
74 feet Y = -2664596
88 meter
Z = 4116363
27 Z = 1254667
52
XDOT = 9042
342444 XDOT = 2756
105977
YDOT = -11651
024857 feet/sec YDOT = -3551
232376 meter/sec
ZDOT = 19181
650157 ZDOT = 5846
566968
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 17274
13270664
00016717 00000-0 10270-3 0 9120
2 25544 51
6406 230
1750 0004184 326
4325 33
6562 15
54012849 38223
Satellite: ISS
Catalog Number: 25544
Epoch time: 17274
13270664 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 230
1750 deg
Eccentricity:
0004184
Arg of perigee: 326
4325 deg
Mean anomaly: 33
6562 deg
Mean motion: 15
54012849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3822
Checksum: 287
Coasting Arc #14 (Orbit 3836)
---------------------------------------
Vector Time (GMT): 2017/275/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2515915
36 A = 6786300
18 meter
Y = 5633559
31 meter E =
0002293
Z = -2829518
35 I = 51
38199
XDOT = -5750
540637 Wp = 57
34570
YDOT = 25
694244 meter/sec RA = 224
44491 deg
ZDOT = -5063
824085 TA = 154
89850
MA = 154
88735
Ha = 220
965 n
mi
Hp = 215
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8254315
50 X = 2466476
89
Y = 18482806
12 feet Y = 5661417
25 meter
Z = -9283196
68 Z = -2817417
46
XDOT = -18866
603140 XDOT = -5725
802886
YDOT = 84
298700 feet/sec YDOT = -38
474468 meter/sec
ZDOT = -16613
596080 ZDOT = -5091
698460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17521029
95 X = 5340409
93
Y = 10185255
76 feet Y = 3104465
96 meter
Z = -9230366
28 Z = -2813415
64
XDOT = -14459
169836 XDOT = -4407
154966
YDOT = 9710
633754 feet/sec YDOT = 2959
801168 meter/sec
ZDOT = -16737
008757 ZDOT = -5101
440269
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 17275
09730897
00016717 00000-0 10270-3 0 9136
2 25544 51
6402 225
3679 0004167 328
6801 31
4103 15
54016228 38377
Satellite: ISS
Catalog Number: 25544
Epoch time: 17275
09730897 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 225
3679 deg
Eccentricity:
0004167
Arg of perigee: 328
6801 deg
Mean anomaly: 31
4103 deg
Mean motion: 15
54016228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3837
Checksum: 307
Coasting Arc #15 (Orbit 3852)
---------------------------------------
Vector Time (GMT): 2017/276/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1265834
76 A = 6782493
74 meter
Y = -5261004
12 meter E =
0008498
Z = 4081010
65 I = 51
39444
XDOT = 6503
988268 Wp = 81
31307
YDOT = 1402
080352 meter/sec RA = 219
44530 deg
ZDOT = 3819
309588 TA = 329
08826
MA = 329
13826
Ha = 220
977 n
mi
Hp = 215
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4153001
17 X = -1226734
39
Y = -17260512
19 feet Y = -5274940
40 meter
Z = 13389142
56 Z = 4074957
22
XDOT = 21338
544185 XDOT = 6469
273998
YDOT = 4600
001156 feet/sec YDOT = 1474
618773 meter/sec
ZDOT = 12530
543267 ZDOT = 3850
819631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13693576
44 X = -4173802
10
Y = -11329491
11 feet Y = -3453228
89 meter
Z = 13363024
87 Z = 4073049
98
XDOT = 18982
848348 XDOT = 5785
972176
YDOT = -7978
385456 feet/sec YDOT = -2431
811887 meter/sec
ZDOT = 12669
877865 ZDOT = 3861
778773
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 17276
12621238
00016717 00000-0 10270-3 0 9140
2 25544 51
6409 220
2396 0004167 331
8137 28
2789 15
54057242 38535
Satellite: ISS
Catalog Number: 25544
Epoch time: 17276
12621238 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 220
2396 deg
Eccentricity:
0004167
Arg of perigee: 331
8137 deg
Mean anomaly: 28
2789 deg
Mean motion: 15
54057242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3853
Checksum: 309
Coasting Arc #16 (Orbit 3867)
---------------------------------------
Vector Time (GMT): 2017/277/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -192165
16 A = 6779316
77 meter
Y = 4649369
56 meter E =
0012420
Z = -4941264
18 I = 51
40974
XDOT = -6866
382480 Wp = 54
02360
YDOT = -2601
391441 meter/sec RA = 214
43806 deg
ZDOT = -2177
383080 TA = 194
62884
MA = 194
66482
Ha = 221
161 n
mi
Hp = 215
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -630463
13 X = -220138
91
Y = 15253837
13 feet Y = 4647063
55 meter
Z = -16211496
65 Z = -4942266
24
XDOT = -22527
501576 XDOT = -6826
205947
YDOT = -8534
748823 feet/sec YDOT = -2677
951674 meter/sec
ZDOT = -7143
645276 ZDOT = -2210
640195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8886289
65 X = 2708541
08
Y = 12407562
50 feet Y = 3781825
05 meter
Z = -16216531
81 Z = -4942798
89
XDOT = -22116
460867 XDOT = -6741
097272
YDOT = 6296
942584 feet/sec YDOT = 1919
308100 meter/sec
ZDOT = -7290
574959 ZDOT = -2222
167248
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 17277
09080650
00016717 00000-0 10270-3 0 9155
2 25544 51
6414 215
4324 0004320 335
3055 24
7890 15
54018048 38688
Satellite: ISS
Catalog Number: 25544
Epoch time: 17277
09080650 = yrday
fracday
Element set: 915
Inclination: 51
6414 deg
RA of node: 215
4324 deg
Eccentricity:
0004320
Arg of perigee: 335
3055 deg
Mean anomaly: 24
7890 deg
Mean motion: 15
54018048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3868
Checksum: 297
Coasting Arc #17 (Orbit 3873)
---------------------------------------
Vector Time (GMT): 2017/277/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 631949
34 A = 6780243
23 meter
Y = 4852889
88 meter E =
0011831
Z = -4703936
18 I = 51
42132
XDOT = -6912
964985 Wp = 47
61413
YDOT = -1787
498470 meter/sec RA = 212
52011 deg
ZDOT = -2769
474446 TA = 194
81538
MA = 194
85008
Ha = 221
374 n
mi
Hp = 215
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2073324
61 X = 600485
72
Y = 15921554
72 feet Y = 4859780
19 meter
Z = -15432861
50 Z = -4700943
43
XDOT = -22680
331316 XDOT = -6879
010021
YDOT = -5864
496294 feet/sec YDOT = -1864
614493 meter/sec
ZDOT = -9086
202250 ZDOT = -2802
973118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1186642
23 X = -361688
55
Y = -16024236
68 feet Y = -4884187
34 meter
Z = -15420230
63 Z = -4700086
30
XDOT = 21046
090342 XDOT = 6414
848336
YDOT = 7338
291541 feet/sec YDOT = 2236
711262 meter/sec
ZDOT = -9234
311510 ZDOT = -2814
618148
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 17277
47664312
00016717 00000-0 10270-3 0 9161
2 25544 51
6392 213
5109 0004711 341
9505 18
1480 15
54039858 38741
Satellite: ISS
Catalog Number: 25544
Epoch time: 17277
47664312 = yrday
fracday
Element set: 916
Inclination: 51
6392 deg
RA of node: 213
5109 deg
Eccentricity:
0004711
Arg of perigee: 341
9505 deg
Mean anomaly: 18
1480 deg
Mean motion: 15
54039858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3874
Checksum: 316
Coasting Arc #18 (Orbit 3888)
---------------------------------------
Vector Time (GMT): 2017/278/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904844
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 960327
77 A = 6777851
19 meter
Y = -4200294
20 meter E =
0003180
Z = 5230162
23 I = 51
44187
XDOT = 7069
692581 Wp = 33
85665
YDOT = 2814
863735 meter/sec RA = 207
51087 deg
ZDOT = 964
807849 TA = 46
90023
MA = 46
87362
Ha = 221
334 n
mi
Hp = 215
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3150681
66 X = 981819
25
Y = -13780492
79 feet Y = -4189434
28 meter
Z = 17159324
90 Z = 5234880
04
XDOT = 23194
529466 XDOT = 7033
003953
YDOT = 9235
117240 feet/sec YDOT = 2893
716856 meter/sec
ZDOT = 3165
380082 ZDOT = 999
061246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3649747
81 X = -1112443
13
Y = 13629832
24 feet Y = 4154372
87 meter
Z = 17180751
47 Z = 5236693
05
XDOT = -21744
272072 XDOT = -6627
654127
YDOT = -9993
876431 feet/sec YDOT = -3046
133536 meter/sec
ZDOT = 3316
714471 ZDOT = 1010
934571
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 17278
50553439
00016717 00000-0 10270-3 0 9174
2 25544 51
6393 208
3836 0004777 344
2115 15
8888 15
54070700 38899
Satellite: ISS
Catalog Number: 25544
Epoch time: 17278
50553439 = yrday
fracday
Element set: 917
Inclination: 51
6393 deg
RA of node: 208
3836 deg
Eccentricity:
0004777
Arg of perigee: 344
2115 deg
Mean anomaly: 15
8888 deg
Mean motion: 15
54070700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3889
Checksum: 337
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