[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 7th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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
222/19:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 213
6
227/00:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 633)
---------------------------------------
Vector Time (GMT): 2018/218/12:48:06
555
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4655506
81 A = 6780044
35 meter
Y = 231436
82 meter E =
0016471
Z = -4938803
63 I = 51
92898
XDOT = -2784
628870 Wp = 59
51187
YDOT = 6747
264895 meter/sec RA = 126
75512 deg
ZDOT = -2306
306621 TA = 187
97381
MA = 188
00003
Ha = 222
987 n
mi
Hp = 214
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15273972
47 X = 4676562
75
Y = 759307
16 feet Y = 283615
96 meter
Z = -16203423
97 Z = -4916137
79
XDOT = -9135
921491 XDOT = -2848
668947
YDOT = 22136
695849 feet/sec YDOT = 6715
767326 meter/sec
ZDOT = -7566
622771 ZDOT = -2319
988402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12353217
66 X = -3765260
74
Y = -9195321
75 feet Y = -2802734
07 meter
Z = -16101732
89 Z = -4907808
19
XDOT = 19203
174646 XDOT = 5853
127632
YDOT = -12425
451878 feet/sec YDOT = -3787
277732 meter/sec
ZDOT = -7628
800219 ZDOT = -2325
258307
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 18218
55358688
00016717 00000-0 10270-3 0 9005
2 25544 51
6411 127
6976 0005582 28
0120 332
1332 15
53822689 6340
Satellite: ISS
Catalog Number: 25544
Epoch time: 18218
55358688 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 127
6976 deg
Eccentricity:
0005582
Arg of perigee: 28
0120 deg
Mean anomaly: 332
1332 deg
Mean motion: 15
53822689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 634
Checksum: 309
Coasting Arc #2 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2018/219/12:48:06
555
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3852442
53 A = 6778308
66 meter
Y = -1679830
26 meter E =
0006596
Z = 5313074
86 I = 51
94286
XDOT = 3667
070661 Wp = 57
00529
YDOT = -6718
429539 meter/sec RA = 121
78009 deg
ZDOT = 537
804508 TA = 27
90537
MA = 27
87001
Ha = 223
157 n
mi
Hp = 213
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12639247
15 X = -3859179
74
Y = -5511254
14 feet Y = -1722949
01 meter
Z = 17431347
96 Z = 5294344
72
XDOT = 12031
071724 XDOT = 3739
313107
YDOT = -22042
091664 feet/sec YDOT = -6677
017929 meter/sec
ZDOT = 1764
450484 ZDOT = 555
792641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7725197
24 X = 2354640
12
Y = 11548275
94 feet Y = 3519914
51 meter
Z = 17347479
15 Z = 5287511
64
XDOT = -21212
685501 XDOT = -6465
626541
YDOT = 11432
168898 feet/sec YDOT = 3484
525080 meter/sec
ZDOT = 1845
972459 ZDOT = 562
652405
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 18219
58263431
00016717 00000-0 10270-3 0 9011
2 25544 51
6416 122
5699 0005553 31
7423 328
4063 15
53832265 6504
Satellite: ISS
Catalog Number: 25544
Epoch time: 18219
58263431 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 122
5699 deg
Eccentricity:
0005553
Arg of perigee: 31
7423 deg
Mean anomaly: 328
4063 deg
Mean motion: 15
53832265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 650
Checksum: 299
Coasting Arc #3 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2018/220/12:48:06
555
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3004202
71 A = 6778755
83 meter
Y = 3122926
25 meter E =
0017250
Z = -5227146
03 I = 51
96045
XDOT = -4265
106719 Wp = 82
56696
YDOT = 6228
360319 meter/sec RA = 116
80566 deg
ZDOT = 1275
574191 TA = 199
61320
MA = 199
67963
Ha = 223
133 n
mi
Hp = 213
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9856308
11 X = 2994448
36
Y = 10245821
03 feet Y = 3156467
19 meter
Z = -17149429
23 Z = -5212576
31
XDOT = -13993
132279 XDOT = -4340
632949
YDOT = 20434
253016 feet/sec YDOT = 6180
242554 meter/sec
ZDOT = 4184
954696 ZDOT = 1254
673136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3057931
91 X = -932057
65
Y = -13964201
65 feet Y = -4256288
66 meter
Z = -17084399
48 Z = -5207324
96
XDOT = 21678
008195 XDOT = 6607
456898
YDOT = -9728
253788 feet/sec YDOT = -2965
171754 meter/sec
ZDOT = 4090
394449 ZDOT = 1246
752228
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 18220
54736556
00016717 00000-0 10270-3 0 9023
2 25544 51
6413 117
7637 0005638 34
8995 325
2527 15
53824281 6656
Satellite: ISS
Catalog Number: 25544
Epoch time: 18220
54736556 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 117
7637 deg
Eccentricity:
0005638
Arg of perigee: 34
8995 deg
Mean anomaly: 325
2527 deg
Mean motion: 15
53824281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 323
Coasting Arc #4 (Orbit 680)
---------------------------------------
Vector Time (GMT): 2018/221/12:48:06
555
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2111649
27 A = 6781039
48 meter
Y = -4471255
72 meter E =
0013538
Z = 4634661
29 I = 51
98295
XDOT = 4651
336545 Wp = 54
00009
YDOT = -5314
748169 meter/sec RA = 111
83571 deg
ZDOT = -2994
277172 TA = 65
76990
MA = 65
62849
Ha = 223
125 n
mi
Hp = 213
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6927983
16 X = -2084005
81
Y = -14669474
15 feet Y = -4494715
40 meter
Z = 15205581
65 Z = 4624470
66
XDOT = 15260
290501 XDOT = 4724
966163
YDOT = -17436
837826 feet/sec YDOT = -5262
321812 meter/sec
ZDOT = -9823
744003 ZDOT = -2971
504575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1497203
74 X = -456347
70
Y = 16196348
88 feet Y = 4936647
14 meter
Z = 15160369
38 Z = 4620880
59
XDOT = -20921
921545 XDOT = -6377
001687
YDOT = 7207
680001 feet/sec YDOT = 2196
900864 meter/sec
ZDOT = -9720
872291 ZDOT = -2962
921874
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 18221
57640819
00016717 00000-0 10270-3 0 9034
2 25544 51
6418 112
6369 0005600 36
8430 323
3107 15
53862660 6816
Satellite: ISS
Catalog Number: 25544
Epoch time: 18221
57640819 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 112
6369 deg
Eccentricity:
0005600
Arg of perigee: 36
8430 deg
Mean anomaly: 323
3107 deg
Mean motion: 15
53862660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 681
Checksum: 294
Coasting Arc #5 (Orbit 695)
---------------------------------------
Vector Time (GMT): 2018/222/12:48:06
555
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1290705
42 A = 6784599
77 meter
Y = 5573158
69 meter E =
0009658
Z = -3652220
72 I = 52
00585
XDOT = -4817
463457 Wp = 69
42292
YDOT = 4000
726292 meter/sec RA = 106
87381 deg
ZDOT = 4415
171122 TA = 247
51271
MA = 247
61499
Ha = 223
210 n
mi
Hp = 213
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4234597
84 X = 1246029
03
Y = 18284641
36 feet Y = 5587342
62 meter
Z = -11982351
44 Z = -3646059
31
XDOT = -15805
326302 XDOT = -4883
288701
YDOT = 13125
742429 feet/sec YDOT = 3946
485823 meter/sec
ZDOT = 14485
469561 ZDOT = 4391
610431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5373968
08 X = 1637985
47
Y = -18000734
50 feet Y = -5486623
88 meter
Z = -11955362
76 Z = -3643994
57
XDOT = 19015
522444 XDOT = 5795
931241
YDOT = -3845
403162 feet/sec YDOT = -1172
078884 meter/sec
ZDOT = 14379
202894 ZDOT = 4382
781042
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 18222
54113461
00016717 00000-0 10270-3 0 9041
2 25544 51
6418 107
8299 0005598 40
1412 320
0153 15
53819507 6961
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
54113461 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 107
8299 deg
Eccentricity:
0005598
Arg of perigee: 40
1412 deg
Mean anomaly: 320
0153 deg
Mean motion: 15
53819507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 696
Checksum: 296
Coasting Arc #6 (Orbit 700)
---------------------------------------
Vector Time (GMT): 2018/222/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4286844
91 A = 6778585
99 meter
Y = 120278
93 meter E =
0007187
Z = 5243254
61 I = 51
98718
XDOT = 1168
174183 Wp = 77
88381
YDOT = -7500
134204 meter/sec RA = 105
51918 deg
ZDOT = 1127
311825 TA = 1
37114
MA = 1
36917
Ha = 223
267 n
mi
Hp = 213
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14064451
80 X = -4313339
63
Y = 394615
91 feet Y = 72192
11 meter
Z = 17202278
89 Z = 5222366
77
XDOT = 3832
592463 XDOT = 1246
480183
YDOT = -24606
739514 feet/sec YDOT = -7486
633082 meter/sec
ZDOT = 3698
529608 ZDOT = 1133
176156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4277326
37 X = 1303729
08
Y = -13523583
26 feet Y = -4121988
18 meter
Z = 17108480
35 Z = 5214664
81
XDOT = 21009
285932 XDOT = 6403
630352
YDOT = 11357
656432 feet/sec YDOT = 3461
813681 meter/sec
ZDOT = 3725
769517 ZDOT = 1135
614549
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 18222
86270921
00016717 00000-0 10270-3 0 9052
2 25544 51
6404 106
2219 0005276 46
0500 314
1087 15
53847656 7010
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
86270921 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 106
2219 deg
Eccentricity:
0005276
Arg of perigee: 46
0500 deg
Mean anomaly: 314
1087 deg
Mean motion: 15
53847656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 701
Checksum: 286
Coasting Arc #7 (Orbit 715)
---------------------------------------
Vector Time (GMT): 2018/223/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3940143
48 A = 6778360
51 meter
Y = 1529731
80 meter E =
0018860
Z = -5315123
99 I = 51
99355
XDOT = -1927
695547 Wp = 83
87957
YDOT = 7374
710092 meter/sec RA = 100
54798 deg
ZDOT = 697
554190 TA = 192
73814
MA = 192
78586
Ha = 223
225 n
mi
Hp = 213
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12926979
92 X = 3948562
17
Y = 5018805
11 feet Y = 1573840
33 meter
Z = -17438070
84 Z = -5295964
17
XDOT = -6324
460457 XDOT = -2013
406587
YDOT = 24195
243083 feet/sec YDOT = 7352
674020 meter/sec
ZDOT = 2288
563617 ZDOT = 687
982256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8833556
41 X = -2692467
99
Y = 10828206
08 feet Y = 3300437
21 meter
Z = -17352226
46 Z = -5288958
63
XDOT = -20223
513688 XDOT = -6164
126972
YDOT = -12922
583465 feet/sec YDOT = -3938
803440 meter/sec
ZDOT = 2244
683150 ZDOT = 684
179424
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 18223
82743284
00016717 00000-0 10270-3 0 9067
2 25544 51
6398 101
4164 0005382 51
0292 309
1339 15
53837932 7166
Satellite: ISS
Catalog Number: 25544
Epoch time: 18223
82743284 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 101
4164 deg
Eccentricity:
0005382
Arg of perigee: 51
0292 deg
Mean anomaly: 309
1339 deg
Mean motion: 15
53837932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 716
Checksum: 307
Coasting Arc #8 (Orbit 731)
---------------------------------------
Vector Time (GMT): 2018/224/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3516299
90 A = 6780302
43 meter
Y = -3134741
63 meter E =
0012434
Z = 4870137
94 I = 52
00492
XDOT = 2603
424503 Wp = 57
77278
YDOT = -6780
335868 meter/sec RA = 95
57689 deg
ZDOT = -2473
514159 TA = 56
43367
MA = 56
31501
Ha = 223
428 n
mi
Hp = 213
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11536416
99 X = -3504641
02
Y = -10284585
41 feet Y = -3173998
06 meter
Z = 15978142
84 Z = 4853085
75
XDOT = 8541
418974 XDOT = 2691
065345
YDOT = -22245
196418 feet/sec YDOT = -6750
732587 meter/sec
ZDOT = -8115
203934 ZDOT = -2460
654946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13263351
09 X = 4042669
41
Y = -8085413
51 feet Y = -2464434
04 meter
Z = 15901958
03 Z = 4846916
81
XDOT = 18124
917212 XDOT = 5524
474766
YDOT = 13815
203708 feet/sec YDOT = 4210
874090 meter/sec
ZDOT = -8056
626842 ZDOT = -2455
659861
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 18224
85646945
00016717 00000-0 10270-3 0 9078
2 25544 51
6400 96
2882 0005395 55
1313 305
0346 15
53801432 7328
Satellite: ISS
Catalog Number: 25544
Epoch time: 18224
85646945 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 96
2882 deg
Eccentricity:
0005395
Arg of perigee: 55
1313 deg
Mean anomaly: 305
0346 deg
Mean motion: 15
53801432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 732
Checksum: 300
Coasting Arc #9 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2018/225/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3083481
97 A = 6783464
81 meter
Y = 4526400
44 meter E =
0011074
Z = -4011248
94 I = 52
01873
XDOT = -3183
944920 Wp = 85
53684
YDOT = 5704
117069 meter/sec RA = 90
61413 deg
ZDOT = 3999
469343 TA = 225
90425
MA = 225
99544
Ha = 223
311 n
mi
Hp = 213
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10116410
65 X = 3052121
49
Y = 14850395
16 feet Y = 4560706
58 meter
Z = -13160265
54 Z = -3996347
08
XDOT = -10446
013518 XDOT = -3266
920229
YDOT = 18714
294845 feet/sec YDOT = 5668
048194 meter/sec
ZDOT = 13121
618579 ZDOT = 3983
801413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17105924
79 X = -5213885
88
Y = 5657330
67 feet Y = 1724354
39 meter
Z = -13093912
20 Z = -3991024
44
XDOT = -14622
600593 XDOT = -4456
968661
YDOT = -14087
169830 feet/sec YDOT = -4293
769364 meter/sec
ZDOT = 13050
553496 ZDOT = 3977
808706
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 18225
82118659
00016717 00000-0 10270-3 0 9083
2 25544 51
6408 91
4816 0005347 56
9335 303
2330 15
53825914 7470
Satellite: ISS
Catalog Number: 25544
Epoch time: 18225
82118659 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 91
4816 deg
Eccentricity:
0005347
Arg of perigee: 56
9335 deg
Mean anomaly: 303
2330 deg
Mean motion: 15
53825914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 317
Coasting Arc #10 (Orbit 762)
---------------------------------------
Vector Time (GMT): 2018/226/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2572304
81 A = 6787097
42 meter
Y = -5644404
13 meter E =
0018045
Z = 2739112
18 I = 52
02938
XDOT = 3739
154448 Wp = 90
21552
YDOT = -4235
875686 meter/sec RA = 85
65979 deg
ZDOT = -5187
960536 TA = 58
95941
MA = 58
78236
Ha = 223
411 n
mi
Hp = 213
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8439320
25 X = -2522301
31
Y = -18518386
25 feet Y = -5672889
72 meter
Z = 8986588
53 Z = 2726738
70
XDOT = 12267
567088 XDOT = 3811
443278
YDOT = -13897
229941 feet/sec YDOT = -4193
657901 meter/sec
ZDOT = -17020
867901 ZDOT = -5169
621542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20098695
63 X = 6126082
43
Y = -3343358
04 feet Y = -1019055
53 meter
Z = 8931736
67 Z = 2722393
34
XDOT = 9920
173132 XDOT = 3023
668771
YDOT = 14127
149534 feet/sec YDOT = 4305
955178 meter/sec
ZDOT = -16937
984032 ZDOT = -5162
697533
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 18226
85021752
00016717 00000-0 10270-3 0 9095
2 25544 51
6401 86
3538 0005453 62
0849 298
0855 15
53816807 7635
Satellite: ISS
Catalog Number: 25544
Epoch time: 18226
85021752 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 86
3538 deg
Eccentricity:
0005453
Arg of perigee: 62
0849 deg
Mean anomaly: 298
0855 deg
Mean motion: 15
53816807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 763
Checksum: 324
Coasting Arc #11 (Orbit 765)
---------------------------------------
Vector Time (GMT): 2018/227/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3411332
85 A = 6783969
50 meter
Y = -4433410
84 meter E =
0016789
Z = 3827707
78 I = 52
01813
XDOT = 2768
046316 Wp = 74
73065
YDOT = -5783
680041 meter/sec RA = 84
71637 deg
ZDOT = -4212
322422 TA = 59
50711
MA = 59
34145
Ha = 223
429 n
mi
Hp = 213
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11192036
92 X = -3380096
41
Y = -14545311
16 feet Y = -4471383
91 meter
Z = 12558096
38 Z = 3811213
00
XDOT = 9081
516784 XDOT = 2852
976249
YDOT = -18975
328220 feet/sec YDOT = -5752
251137 meter/sec
ZDOT = -13819
955454 ZDOT = -4198
669884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -405570
85 X = -123617
99
Y = -18398482
20 feet Y = -5607857
37 meter
Z = 12484587
17 Z = 3805302
17
XDOT = 17323
372929 XDOT = 5280
164069
YDOT = -9761
503292 feet/sec YDOT = -2975
306204 meter/sec
ZDOT = -13757
919061 ZDOT = -4193
413730
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 18227
04315887
00016717 00000-0 10270-3 0 9104
2 25544 51
6394 85
3952 0005669 58
7034 301
4673 15
53859506 7665
Satellite: ISS
Catalog Number: 25544
Epoch time: 18227
04315887 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 85
3952 deg
Eccentricity:
0005669
Arg of perigee: 58
7034 deg
Mean anomaly: 301
4673 deg
Mean motion: 15
53859506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 766
Checksum: 333
Coasting Arc #12 (Orbit 780)
---------------------------------------
Vector Time (GMT): 2018/228/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3025053
32 A = 6787348
08 meter
Y = 5510000
34 meter E =
0010895
Z = -2559309
12 I = 52
02609
XDOT = -3427
299830 Wp = 57
49580
YDOT = 4337
052755 meter/sec RA = 79
76316 deg
ZDOT = 5308
436203 TA = 273
92484
MA = 274
04939
Ha = 223
451 n
mi
Hp = 213
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9924715
60 X = 2975645
79
Y = 18077428
94 feet Y = 5543552
23 meter
Z = -8396683
46 Z = -2544734
81
XDOT = -11244
422015 XDOT = -3501
328545
YDOT = 14229
175707 feet/sec YDOT = 4298
312590 meter/sec
ZDOT = 17416
129274 ZDOT = 5291
607785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2384834
42 X = -726897
53
Y = 20510703
54 feet Y = 6251662
44 meter
Z = -8331945
46 Z = -2539576
98
XDOT = -16019
306944 XDOT = -4882
684757
YDOT = 5151
655934 feet/sec YDOT = 1570
224729 meter/sec
ZDOT = 17340
006045 ZDOT = 5285
233843
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 18228
00787454
00016717 00000-0 10270-3 0 9115
2 25544 51
6400 80
5881 0005744 64
0323 296
1420 15
53867789 7815
Satellite: ISS
Catalog Number: 25544
Epoch time: 18228
00787454 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 80
5881 deg
Eccentricity:
0005744
Arg of perigee: 64
0323 deg
Mean anomaly: 296
1420 deg
Mean motion: 15
53867789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 781
Checksum: 314
Coasting Arc #13 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2018/229/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2499103
63 A = 6789753
79 meter
Y = -6227160
60 meter E =
0017325
Z = 1000613
59 I = 52
02719
XDOT = 4093
081843 Wp = 107
74767
YDOT = -2609
264159 meter/sec RA = 74
81735 deg
ZDOT = -5936
508705 TA = 61
46858
MA = 61
29427
Ha = 223
503 n
mi
Hp = 213
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8199158
89 X = -2434144
48
Y = -20430316
93 feet Y = -6254744
07 meter
Z = 3282852
99 Z = 988631
84
XDOT = 13428
746205 XDOT = 4150
791351
YDOT = -8560
577948 feet/sec YDOT = -2563
169958 meter/sec
ZDOT = -19476
734596 ZDOT = -5916
485862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4815427
18 X = 1467742
20
Y = -21489086
24 feet Y = -6549873
49 meter
Z = 3229862
78 Z = 984462
18
XDOT = 14455
365438 XDOT = 4405
995385
YDOT = 285
793363 feet/sec YDOT = 87
109817 meter/sec
ZDOT = -19386
483378 ZDOT = -5909
000133
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 18229
03690070
00016717 00000-0 10270-3 0 9127
2 25544 51
6403 75
4602 0005798 66
5398 293
6364 15
53841972 7972
Satellite: ISS
Catalog Number: 25544
Epoch time: 18229
03690070 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 75
4602 deg
Eccentricity:
0005798
Arg of perigee: 66
5398 deg
Mean anomaly: 293
6364 deg
Mean motion: 15
53841972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 333
Coasting Arc #14 (Orbit 812)
---------------------------------------
Vector Time (GMT): 2018/230/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1882958
87 A = 6790021
88 meter
Y = 6488003
53 meter E =
0018787
Z = 594730
64 I = 52
01872
XDOT = -4701
776109 Wp = 56
60786
YDOT = 802
270526 meter/sec RA = 69
87490 deg
ZDOT = 6007
919346 TA = 309
77996
MA = 309
94526
Ha = 223
552 n
mi
Hp = 213
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6177686
58 X = 1807379
41
Y = 21286100
83 feet Y = 6508637
50 meter
Z = 1951216
01 Z = 603693
69
XDOT = -15425
774636 XDOT = -4739
580975
YDOT = 2632
121148 feet/sec YDOT = 749
480703 meter/sec
ZDOT = 19711
021477 ZDOT = 5984
988079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6631781
56 X = -2021367
02
Y = 21145356
95 feet Y = 6445104
80 meter
Z = 1990602
12 Z = 606735
53
XDOT = -12876
679836 XDOT = -3924
812014
YDOT = -5922
552571 feet/sec YDOT = -1805
194024 meter/sec
ZDOT = 19607
944599 ZDOT = 5976
501514
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 18230
06592494
00016717 00000-0 10270-3 0 9134
2 25544 51
6406 70
3332 0005862 68
8142 291
3637 15
53838417 8130
Satellite: ISS
Catalog Number: 25544
Epoch time: 18230
06592494 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 70
3332 deg
Eccentricity:
0005862
Arg of perigee: 68
8142 deg
Mean anomaly: 291
3637 deg
Mean motion: 15
53838417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 813
Checksum: 308
Coasting Arc #15 (Orbit 827)
---------------------------------------
Vector Time (GMT): 2018/231/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1073285
99 A = 6788152
46 meter
Y = -6335343
58 meter E =
0010086
Z = -2191586
20 I = 51
99883
XDOT = 5226
600674 Wp = 106
36268
YDOT = 1012
465645 meter/sec RA = 64
92949 deg
ZDOT = -5510
136835 TA = 97
82074
MA = 97
70622
Ha = 223
533 n
mi
Hp = 213
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3521279
49 X = -991717
17
Y = -20785247
98 feet Y = -6346889
73 meter
Z = -7190243
44 Z = -2196601
70
XDOT = 17147
640008 XDOT = 5241
655690
YDOT = 3321
737679 feet/sec YDOT = 1070
997286 meter/sec
ZDOT = -18077
876755 ZDOT = -5484
711448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8265299
61 X = 2519263
32
Y = -19385528
66 feet Y = -5908709
14 meter
Z = -7211909
92 Z = -2198190
14
XDOT = 11348
886912 XDOT = 3459
140731
YDOT = 11492
903599 feet/sec YDOT = 3503
037017 meter/sec
ZDOT = -17963
843599 ZDOT = -5475
379529
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 18231
03063410
00016717 00000-0 10270-3 0 9144
2 25544 51
6394 65
5263 0005741 73
4699 286
7084 15
53827088 8282
Satellite: ISS
Catalog Number: 25544
Epoch time: 18231
03063410 = yrday
fracday
Element set: 914
Inclination: 51
6394 deg
RA of node: 65
5263 deg
Eccentricity:
0005741
Arg of perigee: 73
4699 deg
Mean anomaly: 286
7084 deg
Mean motion: 15
53827088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 828
Checksum: 320
Coasting Arc #16 (Orbit 843)
---------------------------------------
Vector Time (GMT): 2018/232/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 149122
85 A = 6784857
05 meter
Y = 5780383
75 meter E =
0017743
Z = 3533243
86 I = 51
97281
XDOT = -5610
202609 Wp = 86
53742
YDOT = -2633
265101 meter/sec RA = 59
97602 deg
ZDOT = 4526
329533 TA = 314
90921
MA = 315
05306
Ha = 223
548 n
mi
Hp = 213
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 489248
21 X = 67311
45
Y = 18964513
62 feet Y = 5781593
88 meter
Z = 11592007
40 Z = 3533769
58
XDOT = -18406
176540 XDOT = -5602
326068
YDOT = -8639
321198 feet/sec YDOT = -2695
958263 meter/sec
ZDOT = 14850
162511 ZDOT = 4499
096479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9584450
58 X = -2921340
54
Y = 16370524
33 feet Y = 4989735
82 meter
Z = 11593576
51 Z = 3533722
12
XDOT = -10042
741827 XDOT = -3061
027709
YDOT = -16353
148548 feet/sec YDOT = -4984
439678 meter/sec
ZDOT = 14728
236246 ZDOT = 4489
166408
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 18232
05965492
00016717 00000-0 10270-3 0 9159
2 25544 51
6392 60
3988 0005772 75
4410 284
7383 15
53844424 8445
Satellite: ISS
Catalog Number: 25544
Epoch time: 18232
05965492 = yrday
fracday
Element set: 915
Inclination: 51
6392 deg
RA of node: 60
3988 deg
Eccentricity:
0005772
Arg of perigee: 75
4410 deg
Mean anomaly: 284
7383 deg
Mean motion: 15
53844424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 844
Checksum: 328
Coasting Arc #17 (Orbit 858)
---------------------------------------
Vector Time (GMT): 2018/233/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 948998
98 A = 6781260
94 meter
Y = -4913451
63 meter E =
0015893
Z = -4591840
75 I = 51
94323
XDOT = 5750
936983 Wp = 72
86689
YDOT = 3995
947339 meter/sec RA = 55
01223 deg
ZDOT = -3091
541129 TA = 166
29725
MA = 166
25406
Ha = 223
580 n
mi
Hp = 213
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3113513
72 X = 1026176
50
Y = -16120248
11 feet Y = -4902407
68 meter
Z = -15065094
33 Z = -4587043
50
XDOT = 18867
903489 XDOT = 5720
842676
YDOT = 13110
063447 feet/sec YDOT = 4060
090063 meter/sec
ZDOT = -10142
851472 ZDOT = -3063
678448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10974011
61 X = 3344878
74
Y = -12239138
63 feet Y = -3730489
45 meter
Z = -15042871
69 Z = -4585067
29
XDOT = 8729
681728 XDOT = 2660
806991
YDOT = 20123
351620 feet/sec YDOT = 6133
597574 meter/sec
ZDOT = -10018
291696 ZDOT = -3053
575309
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 18233
02435969
00016717 00000-0 10270-3 0 9169
2 25544 51
6390 55
5918 0005898 78
8145 281
3670 15
53848281 8596
Satellite: ISS
Catalog Number: 25544
Epoch time: 18233
02435969 = yrday
fracday
Element set: 916
Inclination: 51
6390 deg
RA of node: 55
5918 deg
Eccentricity:
0005898
Arg of perigee: 78
8145 deg
Mean anomaly: 281
3670 deg
Mean motion: 15
53848281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 859
Checksum: 349
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