[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 25th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 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
238/15:14:30
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
0
242/21:52:00
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
1
249/00:35:06
532 0
6 0
7 0
7
N/A -0
2 -0
1 223
0
000/00:00:13
064 0
2 -0
0 213
8
249/22:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
8
Coasting Arc #1 (Orbit 913)
---------------------------------------
Vector Time (GMT): 2018/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4522949
55 A = 6789237
44 meter
Y = 4859699
86 meter E =
0018964
Z = 1385158
72 I = 51
88991
XDOT = -4376
535981 Wp = 69
69056
YDOT = 2396
087167 meter/sec RA = 37
63619 deg
ZDOT = 5826
202576 TA = 305
35480
MA = 305
53189
Ha = 223
505 n
mi
Hp = 212
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14839073
34 X = 4461542
65
Y = 15943897
17 feet Y = 4909935
29 meter
Z = 4544484
00 Z = 1406979
99
XDOT = -14358
713849 XDOT = -4431
304509
YDOT = 7861
178369 feet/sec YDOT = 2346
839599 meter/sec
ZDOT = 19114
837849 ZDOT = 5804
810213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5530912
53 X = -1685822
14
Y = -21045694
26 feet Y = -6414727
61 meter
Z = 4641772
16 Z = 1414812
16
XDOT = 14946
750262 XDOT = 4555
769480
YDOT = 307
674964 feet/sec YDOT = 93
779329 meter/sec
ZDOT = 19018
444902 ZDOT = 5796
822006
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 18236
56155964
00016717 00000-0 10270-3 0 9008
2 25544 51
6376 37
9599 0005754 93
2352 266
9459 15
53870189 9149
Satellite: ISS
Catalog Number: 25544
Epoch time: 18236
56155964 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 37
9599 deg
Eccentricity:
0005754
Arg of perigee: 93
2352 deg
Mean anomaly: 266
9459 deg
Mean motion: 15
53870189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 914
Checksum: 351
Coasting Arc #2 (Orbit 928)
---------------------------------------
Vector Time (GMT): 2018/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3564462
70 A = 6786423
39 meter
Y = -4995357
44 meter E =
0010223
Z = -2903085
77 I = 51
85396
XDOT = 5646
857354 Wp = 103
43803
YDOT = -1098
908214 meter/sec RA = 32
67890 deg
ZDOT = -5059
688244 TA = 109
50184
MA = 109
39139
Ha = 223
482 n
mi
Hp = 212
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11694431
44 X = -3494236
92
Y = -16388967
99 feet Y = -5034825
19 meter
Z = -9524559
62 Z = -2920229
62
XDOT = 18526
434890 XDOT = 5683
302807
YDOT = -3605
341910 feet/sec YDOT = -1035
557557 meter/sec
ZDOT = -16600
027046 ZDOT = -5032
169723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2861774
63 X = 872268
91
Y = 19892453
67 feet Y = 6063219
88 meter
Z = -9600821
18 Z = -2926330
30
XDOT = -16775
741419 XDOT = -5113
245984
YDOT = -5511
543787 feet/sec YDOT = -1679
918546 meter/sec
ZDOT = -16476
317540 ZDOT = -5021
981586
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 18237
52625490
00016717 00000-0 10270-3 0 9012
2 25544 51
6377 33
1529 0005781 95
7392 264
4420 15
53878780 9294
Satellite: ISS
Catalog Number: 25544
Epoch time: 18237
52625490 = yrday
fracday
Element set: 901
Inclination: 51
6377 deg
RA of node: 33
1529 deg
Eccentricity:
0005781
Arg of perigee: 95
7392 deg
Mean anomaly: 264
4420 deg
Mean motion: 15
53878780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 929
Checksum: 330
Coasting Arc #3 (Orbit 944)
---------------------------------------
Vector Time (GMT): 2018/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2333596
03 A = 6782833
32 meter
Y = 4866068
10 meter E =
0016122
Z = 4097651
10 I = 51
81460
XDOT = -6639
115103 Wp = 102
11801
YDOT = -69
308793 meter/sec RA = 27
71045 deg
ZDOT = 3847
190059 TA = 308
17803
MA = 308
32314
Ha = 223
379 n
mi
Hp = 212
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7656154
95 X = 2259104
99
Y = 15964790
36 feet Y = 4891747
71 meter
Z = 13443737
20 Z = 4108805
51
XDOT = -21781
873697 XDOT = -6656
533943
YDOT = -227
391053 feet/sec YDOT = -143
649159 meter/sec
ZDOT = 12622
014629 ZDOT = 3814
897796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 256392
04 X = 78148
29
Y = -17666217
55 feet Y = -5384663
11 meter
Z = 13493121
59 Z = 4112703
46
XDOT = 18232
407803 XDOT = 5557
237898
YDOT = 9834
452056 feet/sec YDOT = 2997
540987 meter/sec
ZDOT = 12477
047744 ZDOT = 3803
004152
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 18238
55526028
00016717 00000-0 10270-3 0 9024
2 25544 51
6386 28
0247 0005635 101
0018 259
1769 15
53893055 9455
Satellite: ISS
Catalog Number: 25544
Epoch time: 18238
55526028 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 28
0247 deg
Eccentricity:
0005635
Arg of perigee: 101
0018 deg
Mean anomaly: 259
1769 deg
Mean motion: 15
53893055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 945
Checksum: 313
Coasting Arc #4 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2018/238/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1527377
58 A = 6778013
17 meter
Y = 3913881
90 meter E =
0008078
Z = 5312116
92 I = 51
79765
XDOT = -6956
500563 Wp = 101
90154
YDOT = -3220
176086 meter/sec RA = 27
01815 deg
ZDOT = 370
289389 TA = 344
56608
MA = 344
59070
Ha = 223
411 n
mi
Hp = 213
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5011081
31 X = -1596833
21
Y = 12840819
90 feet Y = 3896413
67 meter
Z = 17428205
11 Z = 5304528
65
XDOT = -22823
164576 XDOT = -6921
773285
YDOT = -10564
882172 feet/sec YDOT = -3297
774300 meter/sec
ZDOT = 1214
860199 ZDOT = 336
582227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -194596
50 X = -59313
01
Y = -13826258
88 feet Y = -4214243
71 meter
Z = 17393579
92 Z = 5301563
16
XDOT = 24128
807859 XDOT = 7354
460636
YDOT = 1007
606496 feet/sec YDOT = 307
118460 meter/sec
ZDOT = 1063
991823 ZDOT = 324
304708
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 18238
68388472
00016717 00000-0 10270-3 0 9038
2 25544 51
6416 27
3850 0005524 101
3830 258
7943 15
53909568 9471
Satellite: ISS
Catalog Number: 25544
Epoch time: 18238
68388472 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 27
3850 deg
Eccentricity:
0005524
Arg of perigee: 101
3830 deg
Mean anomaly: 258
7943 deg
Mean motion: 15
53909568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 947
Checksum: 333
Coasting Arc #5 (Orbit 961)
---------------------------------------
Vector Time (GMT): 2018/239/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3063596
29 A = 6778798
42 meter
Y = -3157536
25 meter E =
0019325
Z = -5174363
51 I = 51
77017
XDOT = 6447
220370 Wp = 101
45327
YDOT = 3854
755452 meter/sec RA = 22
03207 deg
ZDOT = 1465
844104 TA = 182
65367
MA = 182
66394
Ha = 223
408 n
mi
Hp = 213
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10051168
93 X = 3123811
02
Y = -10359370
89 feet Y = -3122940
68 meter
Z = -16976258
23 Z = -5159335
36
XDOT = 21152
297801 XDOT = 6396
516062
YDOT = 12646
835474 feet/sec YDOT = 3926
569337 meter/sec
ZDOT = 4809
199815 ZDOT = 1497
038590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5176554
29 X = -1577813
75
Y = 13559021
66 feet Y = 4132789
80 meter
Z = -16908344
77 Z = -5153663
49
XDOT = -23425
533581 XDOT = -7140
102635
YDOT = -2775
983903 feet/sec YDOT = -846
119894 meter/sec
ZDOT = 4948
685425 ZDOT = 1508
359318
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 18239
64857531
00016717 00000-0 10270-3 0 9043
2 25544 51
6418 22
5789 0005638 103
0354 257
1428 15
53893531 9627
Satellite: ISS
Catalog Number: 25544
Epoch time: 18239
64857531 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 22
5789 deg
Eccentricity:
0005638
Arg of perigee: 103
0354 deg
Mean anomaly: 257
1428 deg
Mean motion: 15
53893531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 962
Checksum: 324
Coasting Arc #6 (Orbit 977)
---------------------------------------
Vector Time (GMT): 2018/240/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4462762
51 A = 6781454
21 meter
Y = 2357541
22 meter E =
0013850
Z = 4518378
38 I = 51
74784
XDOT = -5501
505801 Wp = 82
22841
YDOT = -4306
516065 meter/sec RA = 17
04749 deg
ZDOT = -3176
636758 TA = 39
62952
MA = 39
52838
Ha = 223
512 n
mi
Hp = 213
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14641609
30 X = -4510741
18
Y = 7734715
30 feet Y = 2307367
62 meter
Z = 14824076
05 Z = 4496583
34
XDOT = -18049
559714 XDOT = -5437
510000
YDOT = -14128
989713 feet/sec YDOT = -4367
680150 meter/sec
ZDOT = -10422
036608 ZDOT = -3203
205097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10195413
44 X = 3107562
02
Y = -13158911
63 feet Y = -4010836
26 meter
Z = 14725907
92 Z = 4488456
73
XDOT = 21264
769716 XDOT = 6481
501809
YDOT = 4642
346211 feet/sec YDOT = 1414
987125 meter/sec
ZDOT = -10540
679137 ZDOT = -3212
799001
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 18240
67757561
00016717 00000-0 10270-3 0 9051
2 25544 51
6417 17
4514 0005618 106
3720 253
8051 15
53892501 9784
Satellite: ISS
Catalog Number: 25544
Epoch time: 18240
67757561 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 17
4514 deg
Eccentricity:
0005618
Arg of perigee: 106
3720 deg
Mean anomaly: 253
8051 deg
Mean motion: 15
53892501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 978
Checksum: 309
Coasting Arc #7 (Orbit 992)
---------------------------------------
Vector Time (GMT): 2018/241/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5611011
94 A = 6785040
04 meter
Y = -1602095
38 meter E =
0010274
Z = -3472849
22 I = 51
72752
XDOT = 4122
114331 Wp = 100
90015
YDOT = 4563
877889 meter/sec RA = 12
07007 deg
ZDOT = 4564
182312 TA = 218
44966
MA = 218
52291
Ha = 223
361 n
mi
Hp = 213
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18408831
84 X = 5645379
16
Y = -5256218
43 feet Y = -1539157
29 meter
Z = -11393862
26 Z = -3445509
44
XDOT = 13523
997149 XDOT = 4048
603173
YDOT = 14973
352654 feet/sec YDOT = 4609
563586 meter/sec
ZDOT = 14974
351418 ZDOT = 4584
027052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14414561
61 X = -4393558
38
Y = 12709039
66 feet Y = 3873715
29 meter
Z = -11270924
69 Z = -3435377
85
XDOT = -17639
892385 XDOT = -5376
639199
YDOT = -6676
973220 feet/sec YDOT = -2035
141438 meter/sec
ZDOT = 15062
767523 ZDOT = 4591
131541
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 18241
64226096
00016717 00000-0 10270-3 0 9064
2 25544 51
6414 12
6453 0005516 110
7059 249
4685 15
53884632 9938
Satellite: ISS
Catalog Number: 25544
Epoch time: 18241
64226096 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 12
6453 deg
Eccentricity:
0005516
Arg of perigee: 110
7059 deg
Mean anomaly: 249
4685 deg
Mean motion: 15
53884632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 993
Checksum: 316
Coasting Arc #8 (Orbit 1008)
---------------------------------------
Vector Time (GMT): 2018/242/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6405618
52 A = 6788307
28 meter
Y = 837338
00 meter E =
0019524
Z = 2054958
71 I = 51
70618
XDOT = -2409
050816 Wp = 111
31799
YDOT = -4717
377823 meter/sec RA = 7
09897 deg
ZDOT = -5551
698982 TA = 45
96170
MA = 45
80103
Ha = 223
392 n
mi
Hp = 213
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21015808
79 X = -6424487
67
Y = 2747171
90 feet Y = 765600
59 meter
Z = 6741990
53 Z = 2023796
63
XDOT = -7903
710025 XDOT = -2329
153587
YDOT = -15476
961360 feet/sec YDOT = -4743
871207 meter/sec
ZDOT = -18214
235506 ZDOT = -5563
206852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17619082
89 X = 5370296
47
Y = -11859462
99 feet Y = -3614764
32 meter
Z = 6602019
72 Z = 2012295
61
XDOT = 13008
494770 XDOT = 3964
989206
YDOT = 9091
956412 feet/sec YDOT = 2771
228314 meter/sec
ZDOT = -18265
205216 ZDOT = -5567
234550
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 18242
67125543
00016717 00000-0 10270-3 0 9074
2 25544 51
6417 7
5177 0005587 112
6171 247
5573 15
53891285 10097
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
67125543 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 7
5177 deg
Eccentricity:
0005587
Arg of perigee: 112
6171 deg
Mean anomaly: 247
5573 deg
Mean motion: 15
53891285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1009
Checksum: 315
Coasting Arc #9 (Orbit 1012)
---------------------------------------
Vector Time (GMT): 2018/242/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -478562
72 A = 6778280
22 meter
Y = -4244941
68 meter E =
0019818
Z = -5279850
67 I = 51
66082
XDOT = 7610
555197 Wp = 90
84359
YDOT = 131
610927 meter/sec RA = 5
74980 deg
ZDOT = -798
509907 TA = 171
52913
MA = 171
49563
Ha = 223
405 n
mi
Hp = 213
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1570087
67 X = -405412
35
Y = -13926974
03 feet Y = -4249884
70 meter
Z = -17322344
72 Z = -5281997
36
XDOT = 24969
013114 XDOT = 7612
396590
YDOT = 431
794379 feet/sec YDOT = 216
727663 meter/sec
ZDOT = -2619
783161 ZDOT = -761
536072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10387041
24 X = 3165970
17
Y = -9392677
67 feet Y = -2862888
15 meter
Z = -17331370
05 Z = -5282601
59
XDOT = 13708
768754 XDOT = 4178
432716
YDOT = 19670
521741 feet/sec YDOT = 5995
575027 meter/sec
ZDOT = -2453
873062 ZDOT = -747
940509
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 18242
92850402
00016717 00000-0 10270-3 0 9082
2 25544 51
6389 6
2368 0005645 110
0299 250
1462 15
53876462 10133
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
92850402 = yrday
fracday
Element set: 908
Inclination: 51
6389 deg
RA of node: 6
2368 deg
Eccentricity:
0005645
Arg of perigee: 110
0299 deg
Mean anomaly: 250
1462 deg
Mean motion: 15
53876462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1013
Checksum: 299
Coasting Arc #10 (Orbit 1028)
---------------------------------------
Vector Time (GMT): 2018/243/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1236689
85 A = 6778448
34 meter
Y = 4123957
77 meter E =
0008260
Z = 5228398
96 I = 51
62769
XDOT = -7545
389067 Wp = 90
27396
YDOT = -930
332346 meter/sec RA =
75352 deg
ZDOT = -1049
531115 TA = 9
77966
MA = 9
76359
Ha = 223
368 n
mi
Hp = 213
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4057381
39 X = -1308110
01
Y = 13530045
19 feet Y = 4109729
25 meter
Z = 17153539
90 Z = 5222217
82
XDOT = -24755
213476 XDOT = -7529
326971
YDOT = -3052
271477 feet/sec YDOT = -1014
620372 meter/sec
ZDOT = -3443
343553 ZDOT = -1086
144960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13304761
62 X = -4055291
34
Y = 4845501
50 feet Y = 1476908
86 meter
Z = 17125210
39 Z = 5219764
13
XDOT = -12147
006846 XDOT = -3702
407687
YDOT = -20587
185062 feet/sec YDOT = -6274
974007 meter/sec
ZDOT = -3607
509190 ZDOT = -1099
568801
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 18243
95749488
00016717 00000-0 10270-3 0 9098
2 25544 51
6381 1
1095 0005529 113
6005 246
5729 15
53885984 10292
Satellite: ISS
Catalog Number: 25544
Epoch time: 18243
95749488 = yrday
fracday
Element set: 909
Inclination: 51
6381 deg
RA of node: 1
1095 deg
Eccentricity:
0005529
Arg of perigee: 113
6005 deg
Mean anomaly: 246
5729 deg
Mean motion: 15
53885984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1029
Checksum: 334
Coasting Arc #11 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2018/244/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2876364
38 A = 6780757
26 meter
Y = -3957182
54 meter E =
0016129
Z = -4710991
89 I = 51
60238
XDOT = 6919
604069 Wp = 111
45401
YDOT = 1706
575326 meter/sec RA = 355
75779 deg
ZDOT = 2793
311555 TA = 186
28577
MA = 186
30603
Ha = 223
298 n
mi
Hp = 213
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9436891
02 X = 2943284
47
Y = -12982882
35 feet Y = -3924643
08 meter
Z = -15456010
15 Z = -4696856
77
XDOT = 22702
113088 XDOT = 6886
437932
YDOT = 5599
000415 feet/sec YDOT = 1783
769817 meter/sec
ZDOT = 9164
407988 ZDOT = 2826
844019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16103446
58 X = 4908330
52
Y = -513082
77 feet Y = -156387
63 meter
Z = -15392015
80 Z = -4691486
42
XDOT = 9537
156609 XDOT = 2906
925335
YDOT = 20092
746525 feet/sec YDOT = 6124
269141 meter/sec
ZDOT = 9314
623335 ZDOT = 2839
097192
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 18244
92217073
00016717 00000-0 10270-3 0 9108
2 25544 51
6384 356
3025 0005475 116
8894 243
2819 15
53878416 10447
Satellite: ISS
Catalog Number: 25544
Epoch time: 18244
92217073 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 356
3025 deg
Eccentricity:
0005475
Arg of perigee: 116
8894 deg
Mean anomaly: 243
2819 deg
Mean motion: 15
53878416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1044
Checksum: 319
Coasting Arc #12 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2018/245/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4309156
26 A = 6784204
51 meter
Y = 3682899
32 meter E =
0016511
Z = 3711758
92 I = 51
58208
XDOT = -5848
808998 Wp = 95
19483
YDOT = -2500
010977 meter/sec RA = 350
76717 deg
ZDOT = -4294
598547 TA = 40
44394
MA = 40
32131
Ha = 223
275 n
mi
Hp = 213
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14137651
79 X = -4368048
98
Y = 12083003
02 feet Y = 3634382
16 meter
Z = 12177686
75 Z = 3690683
38
XDOT = -19189
005898 XDOT = -5799
557576
YDOT = -8202
135752 feet/sec YDOT = -2565
141149 meter/sec
ZDOT = -14089
890245 ZDOT = -4322
890359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18345679
02 X = -5591762
97
Y = -3408103
49 feet Y = -1038789
94 meter
Z = 12082595
18 Z = 3682775
01
XDOT = -5930
544200 XDOT = -1807
629872
YDOT = -18652
825582 feet/sec YDOT = -5685
381238 meter/sec
ZDOT = -14216
468815 ZDOT = -4333
179695
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 18245
95115386
00016717 00000-0 10270-3 0 9117
2 25544 51
6392 351
1744 0005395 119
6415 240
5275 15
53910670 10601
Satellite: ISS
Catalog Number: 25544
Epoch time: 18245
95115386 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 351
1744 deg
Eccentricity:
0005395
Arg of perigee: 119
6415 deg
Mean anomaly: 240
5275 deg
Mean motion: 15
53910670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 302
Coasting Arc #13 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2018/246/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5408102
48 A = 6787649
19 meter
Y = -3332571
38 meter E =
0008685
Z = -2396854
54 I = 51
56038
XDOT = 4386
177288 Wp = 82
46855
YDOT = 3276
551089 meter/sec RA = 345
78416 deg
ZDOT = 5358
778929 TA = 250
74268
MA = 250
83665
Ha = 223
217 n
mi
Hp = 213
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17743118
37 X = 5456608
91
Y = -10933633
15 feet Y = -3271823
06 meter
Z = -7863696
01 Z = -2370466
05
XDOT = 14390
345432 XDOT = 4323
181928
YDOT = 10749
839532 feet/sec YDOT = 3325
248215 meter/sec
ZDOT = 17581
295698 ZDOT = 5379
932357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19826076
38 X = 6042988
08
Y = 6568463
42 feet Y = 2002067
65 meter
Z = -7744822
91 Z = -2360622
02
XDOT = 1449
196412 XDOT = 441
715066
YDOT = 16397
192974 feet/sec YDOT = 4997
864418 meter/sec
ZDOT = 17675
730862 ZDOT = 5387
562767
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 18246
91582244
00016717 00000-0 10270-3 0 9126
2 25544 51
6386 346
3674 0005390 122
5465 237
6208 15
53892207 10759
Satellite: ISS
Catalog Number: 25544
Epoch time: 18246
91582244 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 346
3674 deg
Eccentricity:
0005390
Arg of perigee: 122
5465 deg
Mean anomaly: 237
6208 deg
Mean motion: 15
53892207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 319
Coasting Arc #14 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2018/247/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6119023
33 A = 6789739
55 meter
Y = 2808218
97 meter E =
0018685
Z = 806170
18 I = 51
53655
XDOT = -2660
026296 Wp = 126
36866
YDOT = -4067
498602 meter/sec RA = 340
80636 deg
ZDOT = -5936
484681 TA = 44
89779
MA = 44
74681
Ha = 223
127 n
mi
Hp = 213
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20075535
87 X = -6153886
76
Y = 9213316
82 feet Y = 2739596
89 meter
Z = 2644915
28 Z = 776361
55
XDOT = -8727
120395 XDOT = -2585
508563
YDOT = -13344
811687 feet/sec YDOT = -4096
828276 meter/sec
ZDOT = -19476
655779 ZDOT = -5949
225050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20149242
99 X = -6141489
26
Y = -9089109
87 feet Y = -2770360
69 meter
Z = 2510779
30 Z = 765285
53
XDOT = 3746
255729 XDOT = 1141
858746
YDOT = -13781
920407 feet/sec YDOT = -4200
729340 meter/sec
ZDOT = -19533
232529 ZDOT = -5953
729275
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 18247
94480004
00016717 00000-0 10270-3 0 9132
2 25544 51
6394 341
2393 0005381 127
0526 233
1119 15
53903727 10918
Satellite: ISS
Catalog Number: 25544
Epoch time: 18247
94480004 = yrday
fracday
Element set: 913
Inclination: 51
6394 deg
RA of node: 341
2393 deg
Eccentricity:
0005381
Arg of perigee: 127
0526 deg
Mean anomaly: 233
1119 deg
Mean motion: 15
53903727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 294
Coasting Arc #15 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2018/248/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6381817
45 A = 6789616
50 meter
Y = -2156412
72 meter E =
0015517
Z = 811945
74 I = 51
50581
XDOT = 851
498523 Wp = 73
21590
YDOT = 4786
167859 meter/sec RA = 335
82931 deg
ZDOT = 5929
070540 TA = 295
57885
MA = 295
73915
Ha = 223
036 n
mi
Hp = 213
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20937721
31 X = 6401512
79
Y = -7074844
90 feet Y = -2084936
68 meter
Z = 2663863
97 Z = 842993
96
XDOT = 2793
630326 XDOT = 769
114976
YDOT = 15702
650455 feet/sec YDOT = 4795
229391 meter/sec
ZDOT = 19452
331169 ZDOT = 5933
006592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19268994
87 X = 5873189
64
Y = 10788151
65 feet Y = 3288228
62 meter
Z = 2803461
40 Z = 854495
03
XDOT = -9085
225650 XDOT = -2769
176778
YDOT = 11095
367392 feet/sec YDOT = 3381
867981 meter/sec
ZDOT = 19469
310810 ZDOT = 5934
245935
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 18248
97377250
00016717 00000-0 10270-3 0 9145
2 25544 51
6397 336
1118 0005314 131
0930 229
0682 15
53923872 11079
Satellite: ISS
Catalog Number: 25544
Epoch time: 18248
97377250 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 336
1118 deg
Eccentricity:
0005314
Arg of perigee: 131
0930 deg
Mean anomaly: 229
0682 deg
Mean motion: 15
53923872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 308
Coasting Arc #16 (Orbit 1107)
---------------------------------------
Vector Time (GMT): 2018/249/00:35:13
064
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -288739
86 A = 6778977
87 meter
Y = -4397787
80 meter E =
0018021
Z = -5166785
58 I = 51
46809
XDOT = 7224
638937 Wp = 108
84105
YDOT = -2111
196924 meter/sec RA = 335
24429 deg
ZDOT = 1391
529526 TA = 174
60698
MA = 174
58754
Ha = 223
011 n
mi
Hp = 213
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -947309
26 X = -214443
87
Y = -14428437
66 feet Y = -4400601
39 meter
Z = -16951396
25 Z = -5168007
61
XDOT = 23702
883652 XDOT = 7240
950733
YDOT = -6926
499095 feet/sec YDOT = -2030
314771 meter/sec
ZDOT = 4565
385583 ZDOT = 1426
663609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 933064
78 X = 284398
14
Y = -14423654
74 feet Y = -4396329
97 meter
Z = -16956255
98 Z = -5168266
82
XDOT = 23288
685707 XDOT = 7098
391403
YDOT = -4052
695023 feet/sec YDOT = -1235
261443 meter/sec
ZDOT = 4723
306085 ZDOT = 1439
663695
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 18249
03808319
00016717 00000-0 10270-3 0 9159
2 25544 51
6422 335
7921 0004808 133
8607 226
2944 15
53809103 11084
Satellite: ISS
Catalog Number: 25544
Epoch time: 18249
03808319 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 335
7921 deg
Eccentricity:
0004808
Arg of perigee: 133
8607 deg
Mean anomaly: 226
2944 deg
Mean motion: 15
53809103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1108
Checksum: 307
Coasting Arc #17 (Orbit 1122)
---------------------------------------
Vector Time (GMT): 2018/249/22:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5752733
25 A = 6784711
51 meter
Y = 46495
53 meter E =
0015878
Z = 3587325
21 I = 51
45829
XDOT = -2809
703317 Wp = 105
22415
YDOT = 5609
861663 meter/sec RA = 330
67797 deg
ZDOT = 4412
577929 TA = 297
34618
MA = 297
50770
Ha = 222
931 n
mi
Hp = 213
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18873796
75 X = 5734360
67
Y = 152544
38 feet Y = 110723
99 meter
Z = 11769439
68 Z = 3615224
99
XDOT = -9218
186737 XDOT = -2893
659212
YDOT = 18405
057951 feet/sec YDOT = 5577
972365 meter/sec
ZDOT = 14476
961708 ZDOT = 4398
725413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15443437
95 X = 4707159
89
Y = 10713636
02 feet Y = 3265516
26 meter
Z = 11894595
90 Z = 3625472
83
XDOT = -17282
502278 XDOT = -5267
706694
YDOT = 8835
776689 feet/sec YDOT = 2693
144735 meter/sec
ZDOT = 14414
032253 ZDOT = 4393
397031
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 18250
00281734
00016717 00000-0 10270-3 0 9165
2 25544 51
6404 330
9849 0004853 135
9565 224
1975 15
53800536 11235
Satellite: ISS
Catalog Number: 25544
Epoch time: 18250
00281734 = yrday
fracday
Element set: 916
Inclination: 51
6404 deg
RA of node: 330
9849 deg
Eccentricity:
0004853
Arg of perigee: 135
9565 deg
Mean anomaly: 224
1975 deg
Mean motion: 15
53800536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1123
Checksum: 304
Coasting Arc #18 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2018/250/22:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4855793
98 A = 6781112
37 meter
Y = -1134602
92 meter E =
0012921
Z = -4606572
06 I = 51
41873
XDOT = 4149
712817 Wp = 90
08714
YDOT = -5707
385564 meter/sec RA = 325
67869 deg
ZDOT = -2975
751566 TA = 150
14391
MA = 150
07013
Ha = 222
887 n
mi
Hp = 213
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15931082
62 X = -4820369
68
Y = -3722450
54 feet Y = -1188706
01 meter
Z = -15113425
41 Z = -4630073
36
XDOT = 13614
543363 XDOT = 4227
680390
YDOT = -18725
018255 feet/sec YDOT = -5660
544851 meter/sec
ZDOT = -9762
964456 ZDOT = -2955
404258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11187354
70 X = -3409905
71
Y = -11802799
35 feet Y = -3597493
24 meter
Z = -15218695
12 Z = -4638658
27
XDOT = 20852
874606 XDOT = 6355
956180
YDOT = -7326
260553 feet/sec YDOT = -2233
044217 meter/sec
ZDOT = -9670
901125 ZDOT = -2947
690663
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 18250
96754894
00016717 00000-0 10270-3 0 9173
2 25544 51
6410 326
1785 0004811 139
0369 221
1146 15
53824063 11383
Satellite: ISS
Catalog Number: 25544
Epoch time: 18250
96754894 = yrday
fracday
Element set: 917
Inclination: 51
6410 deg
RA of node: 326
1785 deg
Eccentricity:
0004811
Arg of perigee: 139
0369 deg
Mean anomaly: 221
1146 deg
Mean motion: 15
53824063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 310
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