[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 2nd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 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
215/16:37:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 214
4
216/02:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 214
4
222/19:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
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 555)
---------------------------------------
Vector Time (GMT): 2018/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4491104
38 A = 6787938
93 meter
Y = -4511670
20 meter E =
0014412
Z = 2346101
34 I = 51
82682
XDOT = 4993
243782 Wp = 84
43646
YDOT = 2142
048965 meter/sec RA = 151
71108 deg
ZDOT = -5409
311191 TA = 69
46786
MA = 69
31325
Ha = 222
689 n
mi
Hp = 214
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14734594
41 X = 4529825
38
Y = -14802067
60 feet Y = -4461231
10 meter
Z = 7697182
87 Z = 2368011
22
XDOT = 16382
033406 XDOT = 4995
194871
YDOT = 7027
719700 feet/sec YDOT = 2197
897851 meter/sec
ZDOT = -17747
083961 ZDOT = -5385
051350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20749473
77 X = -6324439
60
Y = -2034367
53 feet Y = -620075
22 meter
Z = 7795946
96 Z = 2376204
63
XDOT = -5122
582866 XDOT = -1561
363257
YDOT = -15716
526508 feet/sec YDOT = -4790
397280 meter/sec
ZDOT = -17638
499299 ZDOT = -5376
214586
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 18213
53694446
00016717 00000-0 10270-3 0 9003
2 25544 51
6391 152
6922 0005524 11
7191 348
4089 15
53784787 5567
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
53694446 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 152
6922 deg
Eccentricity:
0005524
Arg of perigee: 11
7191 deg
Mean anomaly: 348
4089 deg
Mean motion: 15
53784787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 556
Checksum: 324
Coasting Arc #2 (Orbit 570)
---------------------------------------
Vector Time (GMT): 2018/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5241374
95 A = 6790030
42 meter
Y = 4221836
76 meter E =
0015234
Z = -837247
95 I = 51
86169
XDOT = -3565
985183 Wp = 30
98118
YDOT = -3257
366436 meter/sec RA = 146
75460 deg
ZDOT = 5959
394389 TA = 319
98855
MA = 320
10069
Ha = 222
740 n
mi
Hp = 214
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17196112
04 X = -5284128
28
Y = 13851170
46 feet Y = 4162985
04 meter
Z = -2746876
46 Z = -862812
22
XDOT = -11699
426455 XDOT = -3558
242638
YDOT = -10686
897756 feet/sec YDOT = -3297
200524 meter/sec
ZDOT = 19551
818861 ZDOT = 5942
091041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21663444
39 X = 6603017
85
Y = 4196495
19 feet Y = 1279091
73 meter
Z = -2862014
64 Z = -872342
06
XDOT = -232
576184 XDOT = -70
889221
YDOT = 14351
745516 feet/sec YDOT = 4374
412033 meter/sec
ZDOT = 19474
552787 ZDOT = 5935
843689
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 18214
50168841
00016717 00000-0 10270-3 0 9017
2 25544 51
6386 147
8861 0005474 14
4435 345
6873 15
53776382 5713
Satellite: ISS
Catalog Number: 25544
Epoch time: 18214
50168841 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 147
8861 deg
Eccentricity:
0005474
Arg of perigee: 14
4435 deg
Mean anomaly: 345
6873 deg
Mean motion: 15
53776382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 571
Checksum: 324
Coasting Arc #3 (Orbit 586)
---------------------------------------
Vector Time (GMT): 2018/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5660578
64 A = 6790075
32 meter
Y = -3663488
22 meter E =
0008789
Z = -792120
69 I = 51
89029
XDOT = 2004
721920 Wp = 108
69345
YDOT = 4374
732227 meter/sec RA = 141
80216 deg
ZDOT = -5963
600414 TA = 79
83422
MA = 79
73511
Ha = 222
831 n
mi
Hp = 214
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18571452
22 X = 5704971
74
Y = -12019318
30 feet Y = -3599939
48 meter
Z = -2598821
15 Z = -764516
03
XDOT = 6577
171654 XDOT = 1984
621242
YDOT = 14352
796021 feet/sec YDOT = 4397
038126 meter/sec
ZDOT = -19565
618157 ZDOT = -5953
910999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21281386
82 X = -6486566
70
Y = -6090630
01 feet Y = -1856424
03 meter
Z = -2474575
26 Z = -754250
54
XDOT = 5950
978340 XDOT = 1813
858198
YDOT = -12941
059087 feet/sec YDOT = -3944
434810 meter/sec
ZDOT = -19522
629763 ZDOT = -5950
497552
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 18215
53074616
00016717 00000-0 10270-3 0 9028
2 25544 51
6399 142
7584 0005480 17
8906 342
2439 15
53786960 5871
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
53074616 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 142
7584 deg
Eccentricity:
0005480
Arg of perigee: 17
8906 deg
Mean anomaly: 342
2439 deg
Mean motion: 15
53786960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 587
Checksum: 333
Coasting Arc #4 (Orbit 589)
---------------------------------------
Vector Time (GMT): 2018/215/16:37:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5484138
58 A = 6790287
81 meter
Y = -3971309
54 meter E =
0009530
Z = -488797
46 I = 51
89643
XDOT = 2435
464054 Wp = 109
70388
YDOT = 4090
326483 meter/sec RA = 140
84472 deg
ZDOT = -6005
610592 TA = 75
54610
MA = 75
44037
Ha = 222
808 n
mi
Hp = 214
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17992580
63 X = 5530513
57
Y = -13029230
76 feet Y = -3909722
80 meter
Z = -1603666
20 Z = -462045
07
XDOT = 7990
367631 XDOT = 2418
715742
YDOT = 13419
706309 feet/sec YDOT = 4117
467994 meter/sec
ZDOT = -19703
446823 ZDOT = -5993
820647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12273491
39 X = -3740960
18
Y = 18526388
32 feet Y = 5646843
16 meter
Z = -1483206
74 Z = -452081
41
XDOT = -10968
669505 XDOT = -3343
250465
YDOT = -8811
956954 feet/sec YDOT = -2685
884480 meter/sec
ZDOT = -19651
003618 ZDOT = -5989
625903
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 18215
72369274
00016717 00000-0 10270-3 0 9037
2 25544 51
6405 141
7978 0005372 16
9187 343
2137 15
53767228 5902
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
72369274 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 141
7978 deg
Eccentricity:
0005372
Arg of perigee: 16
9187 deg
Mean anomaly: 343
2137 deg
Mean motion: 15
53767228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 590
Checksum: 323
Coasting Arc #5 (Orbit 595)
---------------------------------------
Vector Time (GMT): 2018/216/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3681944
17 A = 6788594
18 meter
Y = 5329059
16 meter E =
0011660
Z = -2016348
36 I = 51
90102
XDOT = -5061
578949 Wp = 31
45401
YDOT = -1391
426693 meter/sec RA = 138
76858 deg
ZDOT = 5589
445874 TA = 306
35500
MA = 306
46256
Ha = 222
771 n
mi
Hp = 214
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12079869
34 X = -3731467
25
Y = 17483789
91 feet Y = 5287608
27 meter
Z = -6615316
14 Z = -2034354
00
XDOT = -16606
230148 XDOT = -5072
793835
YDOT = -4565
048204 feet/sec YDOT = -1448
091608 meter/sec
ZDOT = 18338
077015 ZDOT = 5564
831379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14957650
76 X = -4559091
95
Y = 15059600
96 feet Y = 4590166
37 meter
Z = -6696690
47 Z = -2041151
26
XDOT = -14548
899899 XDOT = -4434
504689
YDOT = -6379
775996 feet/sec YDOT = -1944
555724 meter/sec
ZDOT = 18227
796784 ZDOT = 5555
832460
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 18216
10958806
00016717 00000-0 10270-3 0 9046
2 25544 51
6400 139
8732 0005249 19
1281 341
0067 15
53772453 5966
Satellite: ISS
Catalog Number: 25544
Epoch time: 18216
10958806 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 139
8732 deg
Eccentricity:
0005249
Arg of perigee: 19
1281 deg
Mean anomaly: 341
0067 deg
Mean motion: 15
53772453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 596
Checksum: 306
Coasting Arc #6 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2018/217/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4442650
50 A = 6790158
21 meter
Y = -5113241
33 meter E =
0012579
Z = 427282
17 I = 51
93020
XDOT = 3829
770264 Wp = 106
20776
YDOT = 2812
940377 meter/sec RA = 133
81780 deg
ZDOT = -6014
610992 TA = 69
20557
MA = 69
07086
Ha = 222
873 n
mi
Hp = 214
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14575625
00 X = 4497422
49
Y = -16775726
13 feet Y = -5063254
30 meter
Z = 1401844
40 Z = 448995
74
XDOT = 12564
863071 XDOT = 3827
246192
YDOT = 9228
807010 feet/sec YDOT = 2855
753638 meter/sec
ZDOT = -19732
975694 ZDOT = -5996
013422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17079544
63 X = 5205845
20
Y = -14208399
20 feet Y = -4330720
08 meter
Z = 1499848
88 Z = 457153
94
XDOT = 10006
145626 XDOT = 3049
873187
YDOT = 9907
546891 feet/sec YDOT = 3019
820292 meter/sec
ZDOT = -19649
844741 ZDOT = -5989
272677
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 18217
13864185
00016717 00000-0 10270-3 0 9057
2 25544 51
6395 134
7461 0005342 24
8164 335
3245 15
53812190 6125
Satellite: ISS
Catalog Number: 25544
Epoch time: 18217
13864185 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 134
7461 deg
Eccentricity:
0005342
Arg of perigee: 24
8164 deg
Mean anomaly: 335
3245 deg
Mean motion: 15
53812190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 296
Coasting Arc #7 (Orbit 627)
---------------------------------------
Vector Time (GMT): 2018/218/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4858967
26 A = 6789857
59 meter
Y = 4584180
88 meter E =
0018592
Z = 1157917
00 I = 51
95039
XDOT = -2544
061191 Wp = 49
41677
YDOT = -4198
801575 meter/sec RA = 128
86955 deg
ZDOT = 5897
296986 TA = 323
10925
MA = 323
23700
Ha = 223
064 n
mi
Hp = 214
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15941493
63 X = -4915492
22
Y = 15039963
52 feet Y = 4529528
44 meter
Z = 3798940
28 Z = 1134176
94
XDOT = -8346
657450 XDOT = -2525
565733
YDOT = -13775
595718 feet/sec YDOT = -4227
147944 meter/sec
ZDOT = 19348
087225 ZDOT = 5884
983580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17968125
70 X = -5476684
71
Y = 12580943
24 feet Y = 3834671
50 meter
Z = 3691882
36 Z = 1125285
74
XDOT = -5482
885119 XDOT = -1671
183384
YDOT = -13541
897761 feet/sec YDOT = -4127
570438 meter/sec
ZDOT = 19293
311225 ZDOT = 5880
601261
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
16769467
00016717 00000-0 10270-3 0 9069
2 25544 51
6391 129
6188 0005431 28
3887 331
7561 15
53764666 6282
Satellite: ISS
Catalog Number: 25544
Epoch time: 18218
16769467 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 129
6188 deg
Eccentricity:
0005431
Arg of perigee: 28
3887 deg
Mean anomaly: 331
7561 deg
Mean motion: 15
53764666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 628
Checksum: 345
Coasting Arc #8 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2018/219/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5019560
45 A = 6787262
32 meter
Y = -3704326
02 meter E =
0007169
Z = -2682187
11 I = 51
96337
XDOT = 1247
852446 Wp = 76
87978
YDOT = 5463
916605 meter/sec RA = 123
91863 deg
ZDOT = -5220
979607 TA = 133
21915
MA = 133
15926
Ha = 223
039 n
mi
Hp = 213
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16468374
18 X = 5073638
72
Y = -12153300
58 feet Y = -3647891
26 meter
Z = -8799826
48 Z = -2657672
95
XDOT = 4094
004087 XDOT = 1212
021228
YDOT = 17926
235581 feet/sec YDOT = 5477
670982 meter/sec
ZDOT = -17129
198185 ZDOT = -5215
004660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17937608
34 X = 5467383
02
Y = -9954093
02 feet Y = -3034007
55 meter
Z = -8689375
61 Z = -2648521
69
XDOT = 1168
567374 XDOT = 356
179335
YDOT = 17006
392977 feet/sec YDOT = 5183
548580 meter/sec
ZDOT = -17103
017993 ZDOT = -5212
999884
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
13242571
00016717 00000-0 10270-3 0 9070
2 25544 51
6403 124
8116 0005450 32
7186 327
4303 15
53816358 6435
Satellite: ISS
Catalog Number: 25544
Epoch time: 18219
13242571 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 124
8116 deg
Eccentricity:
0005450
Arg of perigee: 32
7186 deg
Mean anomaly: 327
4303 deg
Mean motion: 15
53816358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 289
Coasting Arc #9 (Orbit 658)
---------------------------------------
Vector Time (GMT): 2018/220/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4909092
19 A = 6783809
23 meter
Y = 2530133
20 meter E =
0014566
Z = 3925047
38 I = 51
96899
XDOT = -65
576769 Wp = 79
64504
YDOT = -6492
198087 meter/sec RA = 118
96195 deg
ZDOT = 4092
633289 TA = 327
70094
MA = 327
79005
Ha = 223
242 n
mi
Hp = 213
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16105945
51 X = -4956085
56
Y = 8300961
95 feet Y = 2474973
28 meter
Z = 12877452
04 Z = 3901087
07
XDOT = -215
146879 XDOT = -12
853949
YDOT = -21299
862491 feet/sec YDOT = -6492
636944 meter/sec
ZDOT = 13427
274570 ZDOT = 4092
442284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17006455
00 X = -5183567
49
Y = 6469457
09 feet Y = 1971890
52 meter
Z = 12769605
88 Z = 3892175
87
XDOT = 2513
547216 XDOT = 766
129192
YDOT = -19962
793502 feet/sec YDOT = -6084
659460 meter/sec
ZDOT = 13427
183686 ZDOT = 4092
605588
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
16147029
00016717 00000-0 10270-3 0 9088
2 25544 51
6400 119
6847 0005502 36
5108 323
6419 15
53814462 6596
Satellite: ISS
Catalog Number: 25544
Epoch time: 18220
16147029 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 119
6847 deg
Eccentricity:
0005502
Arg of perigee: 36
5108 deg
Mean anomaly: 323
6419 deg
Mean motion: 15
53814462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 659
Checksum: 298
Coasting Arc #10 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2018/221/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4634127
66 A = 6780494
71 meter
Y = -1100449
47 meter E =
0016286
Z = -4841347
54 I = 51
97380
XDOT = -984
502385 Wp = 61
79612
YDOT = 7144
567747 meter/sec RA = 113
99705 deg
ZDOT = -2565
417538 TA = 183
01976
MA = 183
02961
Ha = 223
145 n
mi
Hp = 213
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15203830
90 X = 4669605
07
Y = -3610398
53 feet Y = -1048428
72 meter
Z = -15883686
16 Z = -4818750
87
XDOT = -3229
994702 XDOT = -1051
860518
YDOT = 23440
182896 feet/sec YDOT = 7133
181931 meter/sec
ZDOT = -8416
724207 ZDOT = -2570
362887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15578377
21 X = 4748289
37
Y = -2172998
97 feet Y = -662330
09 meter
Z = -15782115
73 Z = -4810388
88
XDOT = -5497
470739 XDOT = -1675
629081
YDOT = 21907
039724 feet/sec YDOT = 6677
265708 meter/sec
ZDOT = -8439
778337 ZDOT = -2572
444437
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
12619884
00016717 00000-0 10270-3 0 9099
2 25544 51
6409 114
8783 0005429 39
8215 320
3335 15
53805380 6741
Satellite: ISS
Catalog Number: 25544
Epoch time: 18221
12619884 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 114
8783 deg
Eccentricity:
0005429
Arg of perigee: 39
8215 deg
Mean anomaly: 320
3335 deg
Mean motion: 15
53805380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 314
Coasting Arc #11 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2018/222/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4206147
61 A = 6778447
30 meter
Y = -483881
66 meter E =
0007132
Z = 5287487
23 I = 51
97931
XDOT = 1875
254513 Wp = 69
93348
YDOT = -7396
151563 meter/sec RA = 109
02594 deg
ZDOT = 816
386943 TA = 12
31398
MA = 12
29656
Ha = 223
376 n
mi
Hp = 213
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13799696
90 X = -4226107
36
Y = -1587538
24 feet Y = -531029
62 meter
Z = 17347399
04 Z = 5267007
17
XDOT = 6152
409818 XDOT = 1953
855461
YDOT = -24265
589119 feet/sec YDOT = -7374
741734 meter/sec
ZDOT = 2678
434854 ZDOT = 825
686549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13754283
37 X = -4192305
57
Y = -2636516
64 feet Y = -803610
27 meter
Z = 17255510
27 Z = 5259479
53
XDOT = 7764
130458 XDOT = 2366
506964
YDOT = -22727
520998 feet/sec YDOT = -6927
348400 meter/sec
ZDOT = 2721
078698 ZDOT = 829
384787
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
15523837
00016717 00000-0 10270-3 0 9107
2 25544 51
6405 109
7511 0005605 43
4436 316
7157 15
53826758 6902
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
15523837 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 109
7511 deg
Eccentricity:
0005605
Arg of perigee: 43
4436 deg
Mean anomaly: 316
7157 deg
Mean motion: 15
53826758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 303
Coasting Arc #12 (Orbit 700)
---------------------------------------
Vector Time (GMT): 2018/222/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4286066
58 A = 6778574
40 meter
Y = 115215
19 meter E =
0007129
Z = 5244040
28 I = 51
98732
XDOT = 1171
925098 Wp = 77
85897
YDOT = -7500
186935 meter/sec RA = 105
51971 deg
ZDOT = 1122
801199 TA = 1
43950
MA = 1
43745
Ha = 223
243 n
mi
Hp = 213
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14061898
23 X = -4312508
55
Y = 378002
59 feet Y = 67137
37 meter
Z = 17204856
57 Z = 5223156
35
XDOT = 3844
898615 XDOT = 1250
253319
YDOT = -24606
912517 feet/sec YDOT = -7486
643743 meter/sec
ZDOT = 3683
730968 ZDOT = 1128
683805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4292188
00 X = 1308258
90
Y = -13515737
16 feet Y = -4119596
69 meter
Z = 17111076
20 Z = 5215456
02
XDOT = 21005
953281 XDOT = 6402
614560
YDOT = 11368
347496 feet/sec YDOT = 3465
072317 meter/sec
ZDOT = 3711
052930 ZDOT = 1131
128933
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
86270127
00016717 00000-0 10270-3 0 9117
2 25544 51
6406 106
2223 0005228 45
7949 314
3632 15
53850469 7011
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
86270127 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 106
2223 deg
Eccentricity:
0005228
Arg of perigee: 45
7949 deg
Mean anomaly: 314
3632 deg
Mean motion: 15
53850469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 701
Checksum: 292
Coasting Arc #13 (Orbit 715)
---------------------------------------
Vector Time (GMT): 2018/223/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3938478
07 A = 6778354
50 meter
Y = 1535915
98 meter E =
0018801
Z = -5314517
44 I = 51
99371
XDOT = -1931
946891 Wp = 83
93446
YDOT = 7373
110958 meter/sec RA = 100
54849 deg
ZDOT = 703
193604 TA = 192
73722
MA = 192
78479
Ha = 223
201 n
mi
Hp = 213
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12921515
99 X = 3946824
78
Y = 5039094
41 feet Y = 1580005
49 meter
Z = -17436080
84 Z = -5295365
88
XDOT = -6338
408434 XDOT = -2017
667125
YDOT = 24189
996583 feet/sec YDOT = 7351
027294 meter/sec
ZDOT = 2307
065630 ZDOT = 693
600996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8851127
13 X = -2697823
55
Y = 10816676
58 feet Y = 3296923
02 meter
Z = -17350274
33 Z = -5288363
62
XDOT = -20214
984103 XDOT = -6161
527155
YDOT = -12933
036235 feet/sec YDOT = -3941
989445 meter/sec
ZDOT = 2263
092533 ZDOT = 689
790604
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
82742311
00016717 00000-0 10270-3 0 9124
2 25544 51
6400 101
4169 0005334 50
7926 309
3699 15
53840824 7167
Satellite: ISS
Catalog Number: 25544
Epoch time: 18223
82742311 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 101
4169 deg
Eccentricity:
0005334
Arg of perigee: 50
7926 deg
Mean anomaly: 309
3699 deg
Mean motion: 15
53840824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 716
Checksum: 295
Coasting Arc #14 (Orbit 731)
---------------------------------------
Vector Time (GMT): 2018/224/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3513694
92 A = 6780304
20 meter
Y = -3141471
84 meter E =
0012399
Z = 4867721
40 I = 52
00511
XDOT = 2607
924532 Wp = 57
71934
YDOT = -6776
315818 meter/sec RA = 95
57741 deg
ZDOT = -2479
683107 TA = 56
55115
MA = 56
43266
Ha = 223
403 n
mi
Hp = 213
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11527870
48 X = -3501949
24
Y = -10306666
15 feet Y = -3180698
65 meter
Z = 15970214
55 Z = 4850682
07
XDOT = 8556
182849 XDOT = 2695
550051
YDOT = -22232
007277 feet/sec YDOT = -6746
662301 meter/sec
ZDOT = -8135
443264 ZDOT = -2466
802072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13281907
33 X = 4048325
35
Y = -8070676
03 feet Y = -2459942
05 meter
Z = 15894088
33 Z = 4844518
12
XDOT = 18108
992245 XDOT = 5519
620836
YDOT = 13824
188577 feet/sec YDOT = 4213
612678 meter/sec
ZDOT = -8076
768680 ZDOT = -2461
799094
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
85645780
00016717 00000-0 10270-3 0 9131
2 25544 51
6402 96
2887 0005346 54
9019 305
2634 15
53804240 7323
Satellite: ISS
Catalog Number: 25544
Epoch time: 18224
85645780 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 96
2887 deg
Eccentricity:
0005346
Arg of perigee: 54
9019 deg
Mean anomaly: 305
2634 deg
Mean motion: 15
53804240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 732
Checksum: 308
Coasting Arc #15 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2018/225/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3079714
96 A = 6783472
23 meter
Y = 4533018
93 meter E =
0011004
Z = -4006599
62 I = 52
01893
XDOT = -3188
540237 Wp = 85
46494
YDOT = 5697
445707 meter/sec RA = 90
61467 deg
ZDOT = 4005
406442 TA = 226
05112
MA = 226
14196
Ha = 223
288 n
mi
Hp = 213
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10104051
72 X = 3048258
17
Y = 14872109
37 feet Y = 4567282
41 meter
Z = -13145011
88 Z = -3991716
29
XDOT = -10461
090017 XDOT = -3271
469443
YDOT = 18692
407174 feet/sec YDOT = 5661
325702 meter/sec
ZDOT = 13141
097250 ZDOT = 3989
716303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17123303
53 X = -5219182
91
Y = 5639308
85 feet Y = 1718861
34 meter
Z = -13078742
58 Z = -3986400
74
XDOT = -14598
656237 XDOT = -4449
670421
YDOT = -14094
400841 feet/sec YDOT = -4295
973376 meter/sec
ZDOT = 13069
933265 ZDOT = 3983
715659
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
82117315
00016717 00000-0 10270-3 0 9148
2 25544 51
6410 91
4821 0005299 56
6746 303
4913 15
53828681 7471
Satellite: ISS
Catalog Number: 25544
Epoch time: 18225
82117315 = yrday
fracday
Element set: 914
Inclination: 51
6410 deg
RA of node: 91
4821 deg
Eccentricity:
0005299
Arg of perigee: 56
6746 deg
Mean anomaly: 303
4913 deg
Mean motion: 15
53828681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 313
Coasting Arc #16 (Orbit 762)
---------------------------------------
Vector Time (GMT): 2018/226/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2567361
84 A = 6787104
39 meter
Y = -5649955
45 meter E =
0017994
Z = 2732355
03 I = 52
02959
XDOT = 3743
477841 Wp = 90
30694
YDOT = -4226
380822 meter/sec RA = 85
66037 deg
ZDOT = -5192
550534 TA = 58
95250
MA = 58
77597
Ha = 223
387 n
mi
Hp = 213
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8423103
15 X = -2517263
81
Y = -18536599
24 feet Y = -5678385
23 meter
Z = 8964419
38 Z = 2720005
78
XDOT = 12281
751447 XDOT = 3815
682471
YDOT = -13866
078811 feet/sec YDOT = -4184
115160 meter/sec
ZDOT = -17035
926950 ZDOT = -5174
190744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20111979
55 X = 6130131
37
Y = -3322788
89 feet Y = -1012786
05 meter
Z = 8909677
07 Z = 2715669
57
XDOT = 9887
866829 XDOT = 3013
821809
YDOT = 14131
792974 feet/sec YDOT = 4307
370498 meter/sec
ZDOT = -16952
950892 ZDOT = -5167
259432
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
85020218
00016717 00000-0 10270-3 0 9158
2 25544 51
6404 86
3543 0005404 61
8477 298
3221 15
53819731 7633
Satellite: ISS
Catalog Number: 25544
Epoch time: 18226
85020218 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 86
3543 deg
Eccentricity:
0005404
Arg of perigee: 61
8477 deg
Mean anomaly: 298
3221 deg
Mean motion: 15
53819731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 763
Checksum: 305
Coasting Arc #17 (Orbit 765)
---------------------------------------
Vector Time (GMT): 2018/227/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3407581
55 A = 6783979
22 meter
Y = -4441179
25 meter E =
0016749
Z = 3822094
71 I = 52
01834
XDOT = 2773
928215 Wp = 74
77180
YDOT = -5776
032361 meter/sec RA = 84
71692 deg
ZDOT = -4218
887411 TA = 59
55263
MA = 59
38727
Ha = 223
405 n
mi
Hp = 213
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11179729
50 X = -3376231
26
Y = -14570798
06 feet Y = -4479109
73 meter
Z = 12539680
79 Z = 3805618
42
XDOT = 9100
814355 XDOT = 2858
804082
YDOT = -18950
237404 feet/sec YDOT = -5744
537984 meter/sec
ZDOT = -13841
494131 ZDOT = -4205
206433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -380413
56 X = -115950
05
Y = -18411568
60 feet Y = -5611846
11 meter
Z = 12466255
63 Z = 3799714
72
XDOT = 17323
110518 XDOT = 5280
084086
YDOT = -9731
605941 feet/sec YDOT = -2966
193491 meter/sec
ZDOT = -13779
330995 ZDOT = -4199
940087
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
04314317
00016717 00000-0 10270-3 0 9167
2 25544 51
6396 85
3957 0005622 58
4423 301
7278 15
53862368 7664
Satellite: ISS
Catalog Number: 25544
Epoch time: 18227
04314317 = yrday
fracday
Element set: 916
Inclination: 51
6396 deg
RA of node: 85
3957 deg
Eccentricity:
0005622
Arg of perigee: 58
4423 deg
Mean anomaly: 301
7278 deg
Mean motion: 15
53862368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 766
Checksum: 325
Coasting Arc #18 (Orbit 780)
---------------------------------------
Vector Time (GMT): 2018/228/00:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 923003
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3019791
09 A = 6787356
84 meter
Y = 5516559
03 meter E =
0010866
Z = -2551279
45 I = 52
02630
XDOT = -3433
154184 Wp = 57
21268
YDOT = 4326
428695 meter/sec RA = 79
76374 deg
ZDOT = 5313
390544 TA = 274
30576
MA = 274
42991
Ha = 223
427 n
mi
Hp = 213
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9907451
08 X = 2970271
61
Y = 18098946
95 feet Y = 5550051
45 meter
Z = -8370339
41 Z = -2536730
98
XDOT = -11263
629213 XDOT = -3507
087728
YDOT = 14194
319867 feet/sec YDOT = 4287
623594 meter/sec
ZDOT = 17432
383673 ZDOT = 5296
533919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2411533
12 X = -735035
30
Y = 20518079
87 feet Y = 6253910
74 meter
Z = -8305718
25 Z = -2531582
92
XDOT = -16014
228835 XDOT = -4881
136949
YDOT = 5114
013821 feet/sec YDOT = 1558
751413 meter/sec
ZDOT = 17356
135148 ZDOT = 5290
149993
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
00785704
00016717 00000-0 10270-3 0 9177
2 25544 51
6402 80
5886 0005696 63
7875 296
3863 15
53870672 7814
Satellite: ISS
Catalog Number: 25544
Epoch time: 18228
00785704 = yrday
fracday
Element set: 917
Inclination: 51
6402 deg
RA of node: 80
5886 deg
Eccentricity:
0005696
Arg of perigee: 63
7875 deg
Mean anomaly: 296
3863 deg
Mean motion: 15
53870672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 781
Checksum: 345
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