[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 9th 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 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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 664)
---------------------------------------
Vector Time (GMT): 2018/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3418764
54 A = 6778243
07 meter
Y = -2446796
31 meter E =
0008081
Z = 5312403
76 I = 51
95847
XDOT = 3854
689853 Wp = 45
76559
YDOT = -6610
420322 meter/sec RA = 116
97680 deg
ZDOT = -557
961762 TA = 49
56776
MA = 49
49730
Ha = 223
168 n
mi
Hp = 213
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11216419
09 X = -3416954
18
Y = -8027546
94 feet Y = -2485017
59 meter
Z = 17429146
19 Z = 5295801
03
XDOT = 12646
620251 XDOT = 3931
033155
YDOT = -21687
730714 feet/sec YDOT = -6566
887610 meter/sec
ZDOT = -1830
583209 ZDOT = -539
052384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2592618
23 X = 790230
04
Y = 13642218
09 feet Y = 4158148
07 meter
Z = 17354910
55 Z = 5289776
74
XDOT = -23168
298744 XDOT = -7061
697457
YDOT = 6647
998103 feet/sec YDOT = 2026
309822 meter/sec
ZDOT = -1744
918530 ZDOT = -531
851168
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
54736158
00016717 00000-0 10270-3 0 9009
2 25544 51
6412 117
7634 0005589 34
8042 325
3475 15
53852044 6651
Satellite: ISS
Catalog Number: 25544
Epoch time: 18220
54736158 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 117
7634 deg
Eccentricity:
0005589
Arg of perigee: 34
8042 deg
Mean anomaly: 325
3475 deg
Mean motion: 15
53852044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 304
Coasting Arc #2 (Orbit 679)
---------------------------------------
Vector Time (GMT): 2018/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2603331
18 A = 6779976
28 meter
Y = 3863560
12 meter E =
0015075
Z = -4938455
97 I = 51
97867
XDOT = -4330
009808 Wp = 86
65747
YDOT = 5873
818005 meter/sec RA = 112
00494 deg
ZDOT = 2319
693441 TA = 205
92085
MA = 205
99644
Ha = 223
158 n
mi
Hp = 213
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8541112
80 X = 2583922
25
Y = 12675722
17 feet Y = 3892564
19 meter
Z = -16202283
36 Z = -4925857
00
XDOT = -14206
068925 XDOT = -4406
638276
YDOT = 19271
056446 feet/sec YDOT = 5824
968223 meter/sec
ZDOT = 7610
542785 ZDOT = 2298
474462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2304197
39 X = 702319
36
Y = -15170031
83 feet Y = -4623825
70 meter
Z = -16146186
40 Z = -4921357
61
XDOT = 22459
153841 XDOT = 6845
550091
YDOT = -4562
430989 feet/sec YDOT = -1390
628965 meter/sec
ZDOT = 7514
579249 ZDOT = 2290
443755
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
51208968
00016717 00000-0 10270-3 0 9011
2 25544 51
6419 112
9572 0005568 37
7056 322
4486 15
53823268 6803
Satellite: ISS
Catalog Number: 25544
Epoch time: 18221
51208968 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 112
9572 deg
Eccentricity:
0005568
Arg of perigee: 37
7056 deg
Mean anomaly: 322
4486 deg
Mean motion: 15
53823268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 680
Checksum: 318
Coasting Arc #3 (Orbit 695)
---------------------------------------
Vector Time (GMT): 2018/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1763480
22 A = 6783126
54 meter
Y = -5119325
16 meter E =
0015602
Z = 4078367
33 I = 52
00134
XDOT = 4629
338316 Wp = 65
02165
YDOT = -4713
906685 meter/sec RA = 107
03985 deg
ZDOT = -3897
313111 TA = 65
20580
MA = 65
04358
Ha = 223
225 n
mi
Hp = 213
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5785696
25 X = -1725913
53
Y = -16795686
22 feet Y = -5138835
77 meter
Z = 13380470
25 Z = 4069892
15
XDOT = 15188
117835 XDOT = 4700
637103
YDOT = -15465
573114 feet/sec YDOT = -4661
739378 meter/sec
ZDOT = -12786
460338 ZDOT = -3874
652987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6860534
71 X = -2091090
98
Y = 16416538
43 feet Y = 5003760
91 meter
Z = 13343038
28 Z = 4066958
07
XDOT = -20500
920902 XDOT = -6248
680691
YDOT = 1790
271416 feet/sec YDOT = 545
674728 meter/sec
ZDOT = -12684
151137 ZDOT = -3866
129266
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
54112833
00016717 00000-0 10270-3 0 9021
2 25544 51
6423 107
8300 0005703 40
9269 319
2311 15
53849022 6967
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
54112833 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 107
8300 deg
Eccentricity:
0005703
Arg of perigee: 40
9269 deg
Mean anomaly: 319
2311 deg
Mean motion: 15
53849022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 696
Checksum: 282
Coasting Arc #4 (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 = -4286137
32 A = 6778577
77 meter
Y = 115861
40 meter E =
0007181
Z = 5243927
26 I = 51
98734
XDOT = 1171
402102 Wp = 77
79425
YDOT = -7500
225509 meter/sec RA = 105
51904 deg
ZDOT = 1123
347515 TA = 1
49906
MA = 1
49690
Ha = 223
264 n
mi
Hp = 213
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14062130
33 X = -4312585
97
Y = 380122
69 feet Y = 67782
75 meter
Z = 17204485
77 Z = 5223042
97
XDOT = 3843
182748 XDOT = 1249
728139
YDOT = -24607
039073 feet/sec YDOT = -7486
688178 meter/sec
ZDOT = 3685
523343 ZDOT = 1129
227575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4290260
59 X = 1307671
43
Y = -13516649
59 feet Y = -4119874
79 meter
Z = 17110703
70 Z = 5215342
49
XDOT = 21006
572966 XDOT = 6402
803440
YDOT = 11366
897404 feet/sec YDOT = 3464
630329 meter/sec
ZDOT = 3712
833882 ZDOT = 1131
671767
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
86270233
00016717 00000-0 10270-3 0 9036
2 25544 51
6405 106
2218 0005277 46
0078 314
1509 15
53849442 7015
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
86270233 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 106
2218 deg
Eccentricity:
0005277
Arg of perigee: 46
0078 deg
Mean anomaly: 314
1509 deg
Mean motion: 15
53849442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 701
Checksum: 285
Coasting Arc #5 (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 = 3938816
88 A = 6778358
37 meter
Y = 1534730
78 meter E =
0018854
Z = -5314656
32 I = 51
99372
XDOT = -1931
083122 Wp = 83
89397
YDOT = 7373
395213 meter/sec RA = 100
54784 deg
ZDOT = 702
151051 TA = 192
76764
MA = 192
81545
Ha = 223
223 n
mi
Hp = 213
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12922627
55 X = 3947177
49
Y = 5035205
97 feet Y = 1578824
15 meter
Z = -17436536
49 Z = -5295503
09
XDOT = -6335
574546 XDOT = -2016
801535
YDOT = 24190
929176 feet/sec YDOT = 7351
321217 meter/sec
ZDOT = 2303
645179 ZDOT = 692
562643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8847779
93 X = -2696803
32
Y = 10818947
87 feet Y = 3297615
31 meter
Z = -17350722
29 Z = -5288500
16
XDOT = -20216
594903 XDOT = -6162
018126
YDOT = -12930
856812 feet/sec YDOT = -3941
325156 meter/sec
ZDOT = 2259
690905 ZDOT = 688
753788
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
82742496
00016717 00000-0 10270-3 0 9049
2 25544 51
6400 101
4164 0005383 50
9911 309
1720 15
53839355 7162
Satellite: ISS
Catalog Number: 25544
Epoch time: 18223
82742496 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 101
4164 deg
Eccentricity:
0005383
Arg of perigee: 50
9911 deg
Mean anomaly: 309
1720 deg
Mean motion: 15
53839355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 716
Checksum: 295
Coasting Arc #6 (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 = -3514341
36 A = 6780307
16 meter
Y = -3139801
76 meter E =
0012447
Z = 4868297
93 I = 52
00511
XDOT = 2606
769029 Wp = 57
78399
YDOT = -6777
342595 meter/sec RA = 95
57677 deg
ZDOT = -2478
182978 TA = 56
47098
MA = 56
35215
Ha = 223
426 n
mi
Hp = 213
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11529991
33 X = -3502617
10
Y = -10301186
87 feet Y = -3179035
91 meter
Z = 15972106
08 Z = 4851255
42
XDOT = 8552
391827 XDOT = 2694
398829
YDOT = -22235
375967 feet/sec YDOT = -6747
701975 meter/sec
ZDOT = -8130
521580 ZDOT = -2465
307546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13277302
52 X = 4046921
81
Y = -8074332
66 feet Y = -2461056
60 meter
Z = 15895965
33 Z = 4845090
23
XDOT = 18113
073019 XDOT = 5520
864656
YDOT = 13821
866246 feet/sec YDOT = 4212
904832 meter/sec
ZDOT = -8071
872025 ZDOT = -2460
306593
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
85646077
00016717 00000-0 10270-3 0 9052
2 25544 51
6401 96
2882 0005396 55
0978 305
0681 15
53802398 7320
Satellite: ISS
Catalog Number: 25544
Epoch time: 18224
85646077 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 96
2882 deg
Eccentricity:
0005396
Arg of perigee: 55
0978 deg
Mean anomaly: 305
0681 deg
Mean motion: 15
53802398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 732
Checksum: 326
Coasting Arc #7 (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 = 3080953
79 A = 6783473
84 meter
Y = 4530902
77 meter E =
0011063
Z = -4008093
28 I = 52
01893
XDOT = -3187
032795 Wp = 85
45981
YDOT = 5699
564435 meter/sec RA = 90
61404 deg
ZDOT = 4003
525963 TA = 226
03241
MA = 226
12370
Ha = 223
311 n
mi
Hp = 213
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10108116
10 X = 3049527
82
Y = 14865166
58 feet Y = 4565180
27 meter
Z = -13149912
33 Z = -3993203
86
XDOT = -10456
144339 XDOT = -3269
976670
YDOT = 18699
358383 feet/sec YDOT = 5663
461205 meter/sec
ZDOT = 13134
927700 ZDOT = 3987
843110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17117778
44 X = -5217498
87
Y = 5645179
52 feet Y = 1720650
72 meter
Z = -13083615
41 Z = -3987885
98
XDOT = -14606
293808 XDOT = -4451
998353
YDOT = -14091
953566 feet/sec YDOT = -4295
227447 meter/sec
ZDOT = 13063
796171 ZDOT = 3981
845073
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
82117743
00016717 00000-0 10270-3 0 9064
2 25544 51
6410 91
4816 0005349 56
8961 303
2704 15
53826439 7477
Satellite: ISS
Catalog Number: 25544
Epoch time: 18225
82117743 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 91
4816 deg
Eccentricity:
0005349
Arg of perigee: 56
8961 deg
Mean anomaly: 303
2704 deg
Mean motion: 15
53826439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 315
Coasting Arc #8 (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 = -2569259
45 A = 6787106
47 meter
Y = -5647844
94 meter E =
0018047
Z = 2734901
82 I = 52
02958
XDOT = 3741
808444 Wp = 90
25337
YDOT = -4230
008526 meter/sec RA = 85
65975 deg
ZDOT = -5190
822527 TA = 58
97424
MA = 58
79714
Ha = 223
411 n
mi
Hp = 213
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8429328
92 X = -2519197
25
Y = -18529675
01 feet Y = -5676296
15 meter
Z = 8972775
01 Z = 2722543
27
XDOT = 12276
274422 XDOT = 3814
045370
YDOT = -13877
980729 feet/sec YDOT = -4187
761353 meter/sec
ZDOT = -17030
257635 ZDOT = -5172
470767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20106944
97 X = 6128596
83
Y = -3330666
64 feet Y = -1015187
19 meter
Z = 8917990
65 Z = 2718203
55
XDOT = 9900
223697 XDOT = 3017
588183
YDOT = 14129
960834 feet/sec YDOT = 4306
812062 meter/sec
ZDOT = -16947
317181 ZDOT = -5165
542277
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
85020812
00016717 00000-0 10270-3 0 9079
2 25544 51
6403 86
3538 0005455 62
0531 298
1174 15
53817024 7634
Satellite: ISS
Catalog Number: 25544
Epoch time: 18226
85020812 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 86
3538 deg
Eccentricity:
0005455
Arg of perigee: 62
0531 deg
Mean anomaly: 298
1174 deg
Mean motion: 15
53817024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 763
Checksum: 297
Coasting Arc #9 (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 = -3409068
18 A = 6783980
22 meter
Y = -4438119
02 meter E =
0016798
Z = 3824285
55 I = 52
01833
XDOT = 2771
582210 Wp = 74
76801
YDOT = -5779
061326 meter/sec RA = 84
71631 deg
ZDOT = -4216
325015 TA = 59
52259
MA = 59
35680
Ha = 223
429 n
mi
Hp = 213
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11184606
90 X = -3377762
64
Y = -14560757
93 feet Y = -4476066
37 meter
Z = 12546868
59 Z = 3807801
94
XDOT = 9093
117487 XDOT = 2856
479675
YDOT = -18960
174953 feet/sec YDOT = -5747
593062 meter/sec
ZDOT = -13833
087318 ZDOT = -4202
655380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -390346
88 X = -118977
73
Y = -18406430
49 feet Y = -5610280
01 meter
Z = 12473410
13 Z = 3801895
41
XDOT = 17323
168596 XDOT = 5280
101788
YDOT = -9743
480951 feet/sec YDOT = -2969
812994 meter/sec
ZDOT = -13770
974735 ZDOT = -4197
393099
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
04314945
00016717 00000-0 10270-3 0 9085
2 25544 51
6395 85
3952 0005672 58
6762 301
4945 15
53859610 7665
Satellite: ISS
Catalog Number: 25544
Epoch time: 18227
04314945 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 85
3952 deg
Eccentricity:
0005672
Arg of perigee: 58
6762 deg
Mean anomaly: 301
4945 deg
Mean motion: 15
53859610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 766
Checksum: 334
Coasting Arc #10 (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 = 3022272
34 A = 6787357
96 meter
Y = 5513506
14 meter E =
0010907
Z = -2555020
66 I = 52
02629
XDOT = -3430
406008 Wp = 57
41644
YDOT = 4331
362982 meter/sec RA = 79
76314 deg
ZDOT = 5311
095266 TA = 274
05654
MA = 274
18120
Ha = 223
452 n
mi
Hp = 213
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9915591
66 X = 2972804
98
Y = 18088930
89 feet Y = 5547026
60 meter
Z = -8382613
71 Z = -2540460
01
XDOT = -11254
612886 XDOT = -3504
383783
YDOT = 14210
508470 feet/sec YDOT = 4292
588365 meter/sec
ZDOT = 17424
853234 ZDOT = 5294
251883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2399020
57 X = -731221
47
Y = 20514707
11 feet Y = 6252882
73 meter
Z = -8317937
48 Z = -2535307
34
XDOT = -16016
505729 XDOT = -4881
830946
YDOT = 5131
543809 feet/sec YDOT = 1564
094553 meter/sec
ZDOT = 17348
663537 ZDOT = 5287
872646
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
00786517
00016717 00000-0 10270-3 0 9091
2 25544 51
6402 80
5881 0005747 64
0072 296
1672 15
53867548 7813
Satellite: ISS
Catalog Number: 25544
Epoch time: 18228
00786517 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 80
5881 deg
Eccentricity:
0005747
Arg of perigee: 64
0072 deg
Mean anomaly: 296
1672 deg
Mean motion: 15
53867548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 781
Checksum: 328
Coasting Arc #11 (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 = -2495883
14 A = 6789759
50 meter
Y = -6229213
19 meter E =
0017319
Z = 995952
48 I = 52
02736
XDOT = 4095
571719 Wp = 107
77032
YDOT = -2603
004830 meter/sec RA = 74
81738 deg
ZDOT = -5937
524540 TA = 61
49681
MA = 61
32252
Ha = 223
505 n
mi
Hp = 213
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8188592
99 X = -2430878
63
Y = -20437051
16 feet Y = -6256760
40 meter
Z = 3267560
63 Z = 983986
48
XDOT = 13436
915089 XDOT = 4153
215982
YDOT = -8540
042092 feet/sec YDOT = -2556
883151 meter/sec
ZDOT = -19480
067389 ZDOT = -5917
489761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4828032
85 X = 1471584
41
Y = -21488584
11 feet Y = -6549720
44 meter
Z = 3214641
43 Z = 979822
71
XDOT = 14450
502114 XDOT = 4404
513044
YDOT = 306
433171 feet/sec YDOT = 93
400830 meter/sec
ZDOT = -19389
763388 ZDOT = -5909
999881
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
03689163
00016717 00000-0 10270-3 0 9106
2 25544 51
6404 75
4603 0005802 66
5195 293
6567 15
53841331 7979
Satellite: ISS
Catalog Number: 25544
Epoch time: 18229
03689163 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 75
4603 deg
Eccentricity:
0005802
Arg of perigee: 66
5195 deg
Mean anomaly: 293
6567 deg
Mean motion: 15
53841331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 319
Coasting Arc #12 (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 = 1879474
16 A = 6790022
52 meter
Y = 6488596
52 meter E =
0018799
Z = 599179
22 I = 52
01887
XDOT = -4703
544078 Wp = 56
63597
YDOT = 796
112607 meter/sec RA = 69
87495 deg
ZDOT = 6007
366206 TA = 309
79982
MA = 309
96517
Ha = 223
555 n
mi
Hp = 213
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6166253
81 X = 1803866
72
Y = 21288046
33 feet Y = 6509191
36 meter
Z = 1965811
08 Z = 608125
27
XDOT = -15431
575060 XDOT = -4741
277266
YDOT = 2611
918001 feet/sec YDOT = 743
303414 meter/sec
ZDOT = 19709
206712 ZDOT = 5984
426525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6642464
88 X = -2024623
29
Y = 21140604
69 feet Y = 6443656
31 meter
Z = 2005120
80 Z = 611160
82
XDOT = -12870
679735 XDOT = -3922
983183
YDOT = -5941
808418 feet/sec YDOT = -1811
063206 meter/sec
ZDOT = 19606
092869 ZDOT = 5975
937107
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
06591642
00016717 00000-0 10270-3 0 9116
2 25544 51
6408 70
3334 0005866 68
7964 291
3815 15
53837418 8137
Satellite: ISS
Catalog Number: 25544
Epoch time: 18230
06591642 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 70
3334 deg
Eccentricity:
0005866
Arg of perigee: 68
7964 deg
Mean anomaly: 291
3815 deg
Mean motion: 15
53837418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 813
Checksum: 317
Coasting Arc #13 (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 = -1069747
68 A = 6788149
37 meter
Y = -6334661
30 meter E =
0010083
Z = -2195321
65 I = 51
99897
XDOT = 5227
505569 Wp = 106
27825
YDOT = 1017
941321 meter/sec RA = 64
92955 deg
ZDOT = -5508
248348 TA = 97
94894
MA = 97
83450
Ha = 223
537 n
mi
Hp = 213
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3509670
86 X = -988168
61
Y = -20783009
52 feet Y = -6346167
82 meter
Z = -7202498
86 Z = -2200319
93
XDOT = 17150
608822 XDOT = 5242
490113
YDOT = 3339
702497 feet/sec YDOT = 1076
482687 meter/sec
ZDOT = -18071
680931 ZDOT = -5482
818737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8273945
22 X = 2521898
50
Y = -19377348
77 feet Y = -5906215
90 meter
Z = -7224088
13 Z = -2201902
06
XDOT = 11342
276853 XDOT = 3457
125985
YDOT = 11508
988055 feet/sec YDOT = 3507
939559 meter/sec
ZDOT = -17957
629544 ZDOT = -5473
485485
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
03062630
00016717 00000-0 10270-3 0 9125
2 25544 51
6395 65
5264 0005746 73
4534 286
7249 15
53825776 8282
Satellite: ISS
Catalog Number: 25544
Epoch time: 18231
03062630 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 65
5264 deg
Eccentricity:
0005746
Arg of perigee: 73
4534 deg
Mean anomaly: 286
7249 deg
Mean motion: 15
53825776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 828
Checksum: 321
Coasting Arc #14 (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 = 145805
38 A = 6784854
08 meter
Y = 5778822
23 meter E =
0017740
Z = 3535928
09 I = 51
97295
XDOT = -5610
299408 Wp = 86
56181
YDOT = -2637
657267 meter/sec RA = 59
97608 deg
ZDOT = 4523
656086 TA = 314
92320
MA = 315
06701
Ha = 223
553 n
mi
Hp = 213
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 478364
11 X = 63998
64
Y = 18959390
52 feet Y = 5779995
29 meter
Z = 11600813
95 Z = 3536437
71
XDOT = -18406
494122 XDOT = -5602
360759
YDOT = -8653
731192 feet/sec YDOT = -2700
351165 meter/sec
ZDOT = 14841
391359 ZDOT = 4496
422712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9591087
63 X = -2923363
51
Y = 16360428
59 feet Y = 4986658
63 meter
Z = 11602310
96 Z = 3536384
38
XDOT = -10036
149443 XDOT = -3059
018350
YDOT = -16365
075293 feet/sec YDOT = -4988
074949 meter/sec
ZDOT = 14719
464261 ZDOT = 4486
492707
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
05964815
00016717 00000-0 10270-3 0 9135
2 25544 51
6393 60
3990 0005777 75
4303 284
7490 15
53842691 8448
Satellite: ISS
Catalog Number: 25544
Epoch time: 18232
05964815 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 60
3990 deg
Eccentricity:
0005777
Arg of perigee: 75
4303 deg
Mean anomaly: 284
7490 deg
Mean motion: 15
53842691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 844
Checksum: 327
Coasting Arc #15 (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 = 951796
10 A = 6781261
19 meter
Y = -4911505
06 meter E =
0015907
Z = -4593360
24 I = 51
94338
XDOT = 5750
329056 Wp = 72
86986
YDOT = 3998
993644 meter/sec RA = 55
01231 deg
ZDOT = -3088
701434 TA = 166
32571
MA = 166
28257
Ha = 223
586 n
mi
Hp = 213
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3122690
62 X = 1028959
03
Y = -16113861
74 feet Y = -4900429
92 meter
Z = -15070079
53 Z = -4588549
44
XDOT = 18865
908975 XDOT = 5720
186935
YDOT = 13120
057886 feet/sec YDOT = 4063
129302 meter/sec
ZDOT = -10133
534888 ZDOT = -3060
841823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10978686
84 X = 3346303
75
Y = -12228953
16 feet Y = -3727384
92 meter
Z = -15047796
31 Z = -4586568
32
XDOT = 8723
565574 XDOT = 2658
942787
YDOT = 20130
566289 feet/sec YDOT = 6135
796605 meter/sec
ZDOT = -10008
989315 ZDOT = -3050
739943
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
02435410
00016717 00000-0 10270-3 0 9148
2 25544 51
6392 55
5920 0005903 78
8098 281
3717 15
53846213 8590
Satellite: ISS
Catalog Number: 25544
Epoch time: 18233
02435410 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 55
5920 deg
Eccentricity:
0005903
Arg of perigee: 78
8098 deg
Mean anomaly: 281
3717 deg
Mean motion: 15
53846213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 859
Checksum: 312
Coasting Arc #16 (Orbit 874)
---------------------------------------
Vector Time (GMT): 2018/234/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2109849
37 A = 6778800
80 meter
Y = 3810762
18 meter E =
0009437
Z = 5186427
42 I = 51
91369
XDOT = -5633
751586 Wp = 99
75436
YDOT = -5021
932734 meter/sec RA = 50
03926 deg
ZDOT = 1394
366169 TA = 336
87865
MA = 336
92108
Ha = 223
649 n
mi
Hp = 213
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6922077
97 X = -2177498
12
Y = 12502500
61 feet Y = 3786790
09 meter
Z = 17015837
98 Z = 5176014
38
XDOT = -18483
436963 XDOT = -5583
949234
YDOT = -16476
157263 feet/sec YDOT = -5084
654793 meter/sec
ZDOT = 4574
692157 ZDOT = 1367
120666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12295790
86 X = -3747757
05
Y = 7392454
78 feet Y = 2253220
22 meter
Z = 16968546
39 Z = 5172012
94
XDOT = -7411
266412 XDOT = -2258
954002
YDOT = -22576
585519 feet/sec YDOT = -6881
343266 meter/sec
ZDOT = 4453
053910 ZDOT = 1357
290832
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 18234
05337287
00016717 00000-0 10270-3 0 9156
2 25544 51
6377 50
4644 0005765 81
7075 278
4731 15
53837496 8758
Satellite: ISS
Catalog Number: 25544
Epoch time: 18234
05337287 = yrday
fracday
Element set: 915
Inclination: 51
6377 deg
RA of node: 50
4644 deg
Eccentricity:
0005765
Arg of perigee: 81
7075 deg
Mean anomaly: 278
4731 deg
Mean motion: 15
53837496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 875
Checksum: 338
Coasting Arc #17 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2018/235/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3309945
15 A = 6778310
94 meter
Y = -2601742
28 meter E =
0020487
Z = -5329994
71 I = 51
89020
XDOT = 5146
402848 Wp = 90
92603
YDOT = 5646
728028 meter/sec RA = 45
06073 deg
ZDOT = 440
724068 TA = 183
26465
MA = 183
27804
Ha = 223
582 n
mi
Hp = 213
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10859400
09 X = 3364682
42
Y = -8535899
85 feet Y = -2564422
12 meter
Z = -17486859
28 Z = -5313783
47
XDOT = 16884
523779 XDOT = 5080
736315
YDOT = 18526
010590 feet/sec YDOT = 5703
911502 meter/sec
ZDOT = 1445
945105 ZDOT = 465
563606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13724242
22 X = 4183149
03
Y = -2233079
24 feet Y = -680642
55 meter
Z = -17413699
68 Z = -5307695
66
XDOT = 5769
085850 XDOT = 1758
417367
YDOT = 23346
285651 feet/sec YDOT = 7115
947866 meter/sec
ZDOT = 1556
684504 ZDOT = 474
477437
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 18235
01807654
00016717 00000-0 10270-3 0 9164
2 25544 51
6381 45
6576 0005781 85
1523 275
0289 15
53828463 8909
Satellite: ISS
Catalog Number: 25544
Epoch time: 18235
01807654 = yrday
fracday
Element set: 916
Inclination: 51
6381 deg
RA of node: 45
6576 deg
Eccentricity:
0005781
Arg of perigee: 85
1523 deg
Mean anomaly: 275
0289 deg
Mean motion: 15
53828463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 327
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