[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 25th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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
057/06:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 213
9
058/23:08:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 213
9
060/14:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
1
063/17:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2018/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2992333
59 A = 6777325
90 meter
Y = 3004591
83 meter E =
0017559
Z = -5301984
94 I = 51
34856
XDOT = -5453
342827 Wp = 96
41211
YDOT = -5372
980798 meter/sec RA = 224
38857 deg
ZDOT = 31
098959 TA = 173
89664
MA = 173
87522
Ha = 222
007 n
mi
Hp = 213
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9817367
42 X = -2999955
34
Y = 9857584
73 feet Y = 2971086
60 meter
Z = -17394963
70 Z = -5316539
19
XDOT = -17891
544708 XDOT = -5393
006460
YDOT = -17627
889757 feet/sec YDOT = -5433
626459 meter/sec
ZDOT = 102
030704 ZDOT = 4
755584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13160316
91 X = -4011264
59
Y = 4252877
33 feet Y = 1296277
01 meter
Z = -17460141
33 Z = -5321851
08
XDOT = -7403
012309 XDOT = -2256
438152
YDOT = -22943
631035 feet/sec YDOT = -6993
218739 meter/sec
ZDOT = -14
609912 ZDOT = -4
453101
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 18054
51611082
00016717 00000-0 10270-3 0 9009
2 25544 51
6368 225
3935 0003190 125
8429 234
3021 15
54140528 20837
Satellite: ISS
Catalog Number: 25544
Epoch time: 18054
51611082 = yrday
fracday
Element set: 900
Inclination: 51
6368 deg
RA of node: 225
3935 deg
Eccentricity:
0003190
Arg of perigee: 125
8429 deg
Mean anomaly: 234
3021 deg
Mean motion: 15
54140528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 280
Coasting Arc #2 (Orbit 2098)
---------------------------------------
Vector Time (GMT): 2018/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4237978
99 A = 6778629
40 meter
Y = -1695886
57 meter E =
0007237
Z = 5005431
23 I = 51
37552
XDOT = 4624
916757 Wp = 81
44004
YDOT = 5805
490615 meter/sec RA = 219
36986 deg
ZDOT = -1945
382449 TA = 27
51536
MA = 27
47706
Ha = 221
897 n
mi
Hp = 213
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13904130
53 X = 4232314
43
Y = -5563932
32 feet Y = -1648526
05 meter
Z = 16422018
46 Z = 5026003
91
XDOT = 15173
611407 XDOT = 4569
103983
YDOT = 19046
885219 feet/sec YDOT = 5856
897464 meter/sec
ZDOT = -6382
488350 ZDOT = -1923
052274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14826910
28 X = 4519242
25
Y = 1191885
80 feet Y = 363286
79 meter
Z = 16513843
24 Z = 5033419
42
XDOT = 5181
842426 XDOT = 1579
425571
YDOT = 22758
155469 feet/sec YDOT = 6936
685787 meter/sec
ZDOT = -6283
751259 ZDOT = -1915
287384
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 18055
54493747
00016717 00000-0 10270-3 0 9010
2 25544 51
6354 220
2641 0003197 130
5210 229
6221 15
54104949 20991
Satellite: ISS
Catalog Number: 25544
Epoch time: 18055
54493747 = yrday
fracday
Element set: 901
Inclination: 51
6354 deg
RA of node: 220
2641 deg
Eccentricity:
0003197
Arg of perigee: 130
5210 deg
Mean anomaly: 229
6221 deg
Mean motion: 15
54104949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2099
Checksum: 295
Coasting Arc #3 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2018/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5309903
74 A = 6781658
97 meter
Y = 436701
10 meter E =
0011065
Z = -4207764
99 I = 51
41401
XDOT = -3368
853792 Wp = 117
20227
YDOT = -5829
792900 meter/sec RA = 214
35957 deg
ZDOT = 3648
670907 TA = 190
34046
MA = 190
36324
Ha = 221
907 n
mi
Hp = 213
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17420944
04 X = -5293953
65
Y = 1432746
41 feet Y = 377411
14 meter
Z = -13805003
23 Z = -4233519
51
XDOT = -11052
669921 XDOT = -3321
136119
YDOT = -19126
617127 feet/sec YDOT = -5867
198798 meter/sec
ZDOT = 11970
705076 ZDOT = 3632
422561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16250049
77 X = -4953015
17
Y = -6188388
42 feet Y = -1886220
79 meter
Z = -13919766
49 Z = -4242744
83
XDOT = -2237
319508 XDOT = -681
934986
YDOT = -20871
992440 feet/sec YDOT = -6361
783296 meter/sec
ZDOT = 11899
037229 ZDOT = 3626
826547
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 18056
50945749
00016717 00000-0 10270-3 0 9022
2 25544 51
6372 215
4558 0003149 134
4837 225
6573 15
54146916 21143
Satellite: ISS
Catalog Number: 25544
Epoch time: 18056
50945749 = yrday
fracday
Element set: 902
Inclination: 51
6372 deg
RA of node: 215
4558 deg
Eccentricity:
0003149
Arg of perigee: 134
4837 deg
Mean anomaly: 225
6573 deg
Mean motion: 15
54146916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 319
Coasting Arc #4 (Orbit 2126)
---------------------------------------
Vector Time (GMT): 2018/057/06:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1706669
06 A = 6781564
89 meter
Y = -4966088
61 meter E =
0012331
Z = 4284256
43 I = 51
43777
XDOT = 6775
028351 Wp = 112
04833
YDOT = 724
012959 meter/sec RA = 210
46081 deg
ZDOT = 3525
430538 TA = 301
89774
MA = 302
01765
Ha = 221
823 n
mi
Hp = 213
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5599307
93 X = -1671820
31
Y = -16292941
65 feet Y = -4984978
73 meter
Z = 14055959
42 Z = 4276051
03
XDOT = 22227
783304 XDOT = 6749
304369
YDOT = 2375
370599 feet/sec YDOT = 799
632292 meter/sec
ZDOT = 11566
373156 ZDOT = 3558
278114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17040702
33 X = 5194006
07
Y = -2726948
17 feet Y = -831173
80 meter
Z = 14020000
35 Z = 4273296
11
XDOT = -6447
647002 XDOT = -1965
242806
YDOT = 20141
131060 feet/sec YDOT = 6139
016747 meter/sec
ZDOT = 11712
606527 ZDOT = 3570
002469
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 18057
34537198
00016717 00000-0 10270-3 0 9031
2 25544 51
6399 211
2932 0002593 130
2258 229
9121 15
54133048 21277
Satellite: ISS
Catalog Number: 25544
Epoch time: 18057
34537198 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 211
2932 deg
Eccentricity:
0002593
Arg of perigee: 130
2258 deg
Mean anomaly: 229
9121 deg
Mean motion: 15
54133048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2127
Checksum: 302
Coasting Arc #5 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2018/058/06:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 77335
28 A = 6778339
58 meter
Y = 4511507
54 meter E =
0014646
Z = -5071260
18 I = 51
45477
XDOT = -7211
411850 Wp = 85
29728
YDOT = -1866
909428 meter/sec RA = 205
45222 deg
ZDOT = -1774
073042 TA = 167
49025
MA = 167
45385
Ha = 221
679 n
mi
Hp = 213
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 253724
68 X = 51513
57
Y = 14801533
91 feet Y = 4512227
69 meter
Z = -16637992
72 Z = -5070947
49
XDOT = -23659
487696 XDOT = -7181
382290
YDOT = -6125
030932 feet/sec YDOT = -1947
384584 meter/sec
ZDOT = -5820
449614 ZDOT = -1809
029718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14668621
61 X = -4470995
87
Y = -2002511
64 feet Y = -610365
55 meter
Z = -16637129
30 Z = -5070997
01
XDOT = 9669
663123 XDOT = 2947
313320
YDOT = -21271
006761 feet/sec YDOT = -6483
402861 meter/sec
ZDOT = -5975
967266 ZDOT = -1821
474823
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 18058
30988488
00016717 00000-0 10270-3 0 9041
2 25544 51
6385 206
4839 0002544 134
8111 225
3249 15
54168021 21425
Satellite: ISS
Catalog Number: 25544
Epoch time: 18058
30988488 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 206
4839 deg
Eccentricity:
0002544
Arg of perigee: 134
8111 deg
Mean anomaly: 225
3249 deg
Mean motion: 15
54168021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 310
Coasting Arc #6 (Orbit 2152)
---------------------------------------
Vector Time (GMT): 2018/058/23:08:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1326053
98 A = 6779581
55 meter
Y = -4631962
12 meter E =
0010168
Z = 4764695
59 I = 51
47697
XDOT = 7177
994659 Wp = 123
91409
YDOT = 656
845734 meter/sec RA = 202
09257 deg
ZDOT = 2626
648343 TA = 300
08276
MA = 300
18354
Ha = 221
713 n
mi
Hp = 213
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4350570
79 X = -1297303
37
Y = -15196726
13 feet Y = -4646629
87 meter
Z = 15632203
36 Z = 4758324
40
XDOT = 23549
851245 XDOT = 7157
357597
YDOT = 2155
005688 feet/sec YDOT = 736
999801 meter/sec
ZDOT = 8617
612674 ZDOT = 2661
465515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5333000
01 X = -1625498
40
Y = 14909626
87 feet Y = 4544454
27 meter
Z = 15604354
22 Z = 4756207
17
XDOT = -16646
919902 XDOT = -5073
981186
YDOT = -15168
847707 feet/sec YDOT = -4623
464781 meter/sec
ZDOT = 8772
665698 ZDOT = 2673
908505
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 18059
01719440
00016717 00000-0 10270-3 0 9051
2 25544 51
6363 202
9577 0002692 139
1990 220
9364 15
54176984 21536
Satellite: ISS
Catalog Number: 25544
Epoch time: 18059
01719440 = yrday
fracday
Element set: 905
Inclination: 51
6363 deg
RA of node: 202
9577 deg
Eccentricity:
0002692
Arg of perigee: 139
1990 deg
Mean anomaly: 220
9364 deg
Mean motion: 15
54176984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2153
Checksum: 321
Coasting Arc #7 (Orbit 2167)
---------------------------------------
Vector Time (GMT): 2018/059/23:08:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -421890
36 A = 6777490
86 meter
Y = 4256512
72 meter E =
0016218
Z = -5271201
08 I = 51
50174
XDOT = -7436
478877 Wp = 92
31590
YDOT = -1661
852143 meter/sec RA = 197
08358 deg
ZDOT = -749
398302 TA = 170
51523
MA = 170
48456
Ha = 221
708 n
mi
Hp = 213
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1384154
74 X = -443852
41
Y = 13964936
75 feet Y = 4251671
54 meter
Z = -17293966
78 Z = -5273304
18
XDOT = -24397
896578 XDOT = -7413
702815
YDOT = -5452
270812 feet/sec YDOT = -1744
884685 meter/sec
ZDOT = -2458
655846 ZDOT = -785
465754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9055330
00 X = 2760064
58
Y = -10704917
88 feet Y = -3262858
97 meter
Z = -17303825
06 Z = -5274205
88
XDOT = 16053
775130 XDOT = 4893
190660
YDOT = 17799
706899 feet/sec YDOT = 5425
350663 meter/sec
ZDOT = -2619
185560 ZDOT = -798
327759
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 18059
98170455
00016717 00000-0 10270-3 0 9065
2 25544 51
6373 198
1484 0002724 140
0798 220
0556 15
54155592 21685
Satellite: ISS
Catalog Number: 25544
Epoch time: 18059
98170455 = yrday
fracday
Element set: 906
Inclination: 51
6373 deg
RA of node: 198
1484 deg
Eccentricity:
0002724
Arg of perigee: 140
0798 deg
Mean anomaly: 220
0556 deg
Mean motion: 15
54155592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2168
Checksum: 324
Coasting Arc #8 (Orbit 2177)
---------------------------------------
Vector Time (GMT): 2018/060/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3821789
41 A = 6783067
84 meter
Y = 4088091
35 meter E =
0007495
Z = -3838384
70 I = 51
54393
XDOT = -6162
261382 Wp = 98
96235
YDOT = 1869
821920 meter/sec RA = 193
92308 deg
ZDOT = -4152
237354 TA = 127
28217
MA = 127
21382
Ha = 221
696 n
mi
Hp = 214
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12538679
17 X = 3794435
63
Y = 13412373
21 feet Y = 4130675
85 meter
Z = -12593125
64 Z = -3819887
11
XDOT = -20217
392984 XDOT = -6162
543345
YDOT = 6134
586353 feet/sec YDOT = 1800
909229 meter/sec
ZDOT = -13622
825965 ZDOT = -4182
171669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15615223
84 X = 4759520
23
Y = 9763851
63 feet Y = 2976021
98 meter
Z = -12511156
20 Z = -3813400
41
XDOT = -17195
765488 XDOT = -5241
269321
YDOT = 9908
048047 feet/sec YDOT = 3019
973045 meter/sec
ZDOT = -13756
437036 ZDOT = -4192
962008
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 18060
62470803
00016717 00000-0 10270-3 0 9079
2 25544 51
6408 194
9408 0002971 150
2795 209
8527 15
54162446 21788
Satellite: ISS
Catalog Number: 25544
Epoch time: 18060
62470803 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 194
9408 deg
Eccentricity:
0002971
Arg of perigee: 150
2795 deg
Mean anomaly: 209
8527 deg
Mean motion: 15
54162446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2178
Checksum: 321
Coasting Arc #9 (Orbit 2193)
---------------------------------------
Vector Time (GMT): 2018/061/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2257299
20 A = 6779364
24 meter
Y = -4213268
15 meter E =
0009948
Z = 4803378
27 I = 51
56460
XDOT = 7175
026623 Wp = 128
70318
YDOT = -923
280995 meter/sec RA = 188
92717 deg
ZDOT = 2552
315390 TA = 296
11067
MA = 296
21300
Ha = 221
606 n
mi
Hp = 214
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7405837
26 X = -2233349
34
Y = -13823058
23 feet Y = -4238376
26 meter
Z = 15759115
06 Z = 4792472
05
XDOT = 23540
113594 XDOT = 7172
420188
YDOT = -3029
137124 feet/sec YDOT = -843
059146 meter/sec
ZDOT = 8373
738156 ZDOT = 2587
162270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10971015
52 X = -3343965
53
Y = -11272755
08 feet Y = -3435935
75 meter
Z = 15710979
70 Z = 4788706
61
XDOT = 20965
568301 XDOT = 6390
305218
YDOT = -8472
878394 feet/sec YDOT = -2582
533335 meter/sec
ZDOT = 8529
148812 ZDOT = 2599
684558
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 18061
65351004
00016717 00000-0 10270-3 0 9085
2 25544 51
6412 189
8123 0002896 153
2160 206
9142 15
54206751 21942
Satellite: ISS
Catalog Number: 25544
Epoch time: 18061
65351004 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 189
8123 deg
Eccentricity:
0002896
Arg of perigee: 153
2160 deg
Mean anomaly: 206
9142 deg
Mean motion: 15
54206751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2194
Checksum: 291
Coasting Arc #10 (Orbit 2208)
---------------------------------------
Vector Time (GMT): 2018/062/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 456437
14 A = 6777416
04 meter
Y = 4232897
97 meter E =
0015689
Z = -5286691
99 I = 51
58975
XDOT = -7628
635218 Wp = 94
85825
YDOT = 1
434228 meter/sec RA = 183
92548 deg
ZDOT = -660
475341 TA = 168
83932
MA = 168
80448
Ha = 221
532 n
mi
Hp = 214
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1497497
17 X = 434749
37
Y = 13887460
55 feet Y = 4237880
14 meter
Z = -17344790
01 Z = -5284528
10
XDOT = -25028
330769 XDOT = -7624
876093
YDOT = 4
705471 feet/sec YDOT = -83
853494 meter/sec
ZDOT = -2166
913849 ZDOT = -697
522896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5532539
57 X = 1686318
06
Y = 12837960
30 feet Y = 3913010
30 meter
Z = -17335615
94 Z = -5283895
74
XDOT = -23021
986118 XDOT = -7017
101369
YDOT = 6785
561858 feet/sec YDOT = 2068
239254 meter/sec
ZDOT = -2332
044834 ZDOT = -710
807265
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 18062
61801113
00016717 00000-0 10270-3 0 9094
2 25544 51
6406 185
0049 0002818 157
1904 202
9375 15
54165715 22098
Satellite: ISS
Catalog Number: 25544
Epoch time: 18062
61801113 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 185
0049 deg
Eccentricity:
0002818
Arg of perigee: 157
1904 deg
Mean anomaly: 202
9375 deg
Mean motion: 15
54165715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2209
Checksum: 296
Coasting Arc #11 (Orbit 2224)
---------------------------------------
Vector Time (GMT): 2018/063/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1381637
13 A = 6777572
13 meter
Y = -4133783
86 meter E =
0004297
Z = 5186463
83 I = 51
62484
XDOT = 7510
145107 Wp = 93
49632
YDOT = 884
481426 meter/sec RA = 178
92285 deg
ZDOT = -1295
019308 TA = 8
94123
MA = 8
93358
Ha = 221
333 n
mi
Hp = 214
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4532930
23 X = 1402566
71
Y = -13562282
99 feet Y = -4118215
67 meter
Z = 17015957
45 Z = 5193226
70
XDOT = 24639
583684 XDOT = 7505
986882
YDOT = 2901
841948 feet/sec YDOT = 968
441597 meter/sec
ZDOT = -4248
751009 ZDOT = -1258
548264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 93791
70 X = 28587
71
Y = -14262947
55 feet Y = -4347346
41 meter
Z = 17046563
13 Z = 5195792
44
XDOT = 23343
295791 XDOT = 7115
036557
YDOT = -4732
881769 feet/sec YDOT = -1442
582363 meter/sec
ZDOT = -4086
272745 ZDOT = -1245
495933
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 18063
64680488
00016717 00000-0 10270-3 0 9100
2 25544 51
6415 179
8758 0002702 161
0108 199
1146 15
54226390 22256
Satellite: ISS
Catalog Number: 25544
Epoch time: 18063
64680488 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 179
8758 deg
Eccentricity:
0002702
Arg of perigee: 161
0108 deg
Mean anomaly: 199
1146 deg
Mean motion: 15
54226390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2225
Checksum: 310
Coasting Arc #12 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2018/063/17:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3798566
61 A = 6780811
06 meter
Y = -3416919
96 meter E =
0011480
Z = 4452702
79 I = 51
63763
XDOT = 6354
944743 Wp = 119
69180
YDOT = -2777
786451 meter/sec RA = 178
35726 deg
ZDOT = 3277
821257 TA = 297
22852
MA = 297
34545
Ha = 221
628 n
mi
Hp = 214
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12462488
87 X = -3781704
02
Y = -11210367
32 feet Y = -3459303
22 meter
Z = 14608604
95 Z = 4434292
31
XDOT = 20849
556244 XDOT = 6369
612634
YDOT = -9113
472607 feet/sec YDOT = -2706
638608 meter/sec
ZDOT = 10754
006749 ZDOT = 3308
727063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15875660
02 X = -4838901
17
Y = 5597272
06 feet Y = 1706048
52 meter
Z = 14526915
28 Z = 4427803
78
XDOT = 2443
824193 XDOT = 744
877614
YDOT = -21439
376910 feet/sec YDOT = -6534
722082 meter/sec
ZDOT = 10892
085031 ZDOT = 3319
907517
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 18063
77540554
00016717 00000-0 10270-3 0 9114
2 25544 51
6401 179
2357 0002729 151
0185 209
1120 15
54196004 22277
Satellite: ISS
Catalog Number: 25544
Epoch time: 18063
77540554 = yrday
fracday
Element set: 911
Inclination: 51
6401 deg
RA of node: 179
2357 deg
Eccentricity:
0002729
Arg of perigee: 151
0185 deg
Mean anomaly: 209
1120 deg
Mean motion: 15
54196004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2227
Checksum: 285
Coasting Arc #13 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2018/064/17:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2117451
01 A = 6777941
29 meter
Y = 3864126
27 meter E =
0014492
Z = -5162850
67 I = 51
66177
XDOT = -7241
692576 Wp = 89
27073
YDOT = 2011
433401 meter/sec RA = 173
36273 deg
ZDOT = -1467
982559 TA = 166
60233
MA = 166
56381
Ha = 221
473 n
mi
Hp = 214
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6947017
74 X = 2099162
15
Y = 12677579
63 feet Y = 3887702
14 meter
Z = -16938486
47 Z = -5152609
83
XDOT = -23758
833910 XDOT = -7256
516122
YDOT = 6599
190947 feet/sec YDOT = 1930
368741 meter/sec
ZDOT = -4816
215744 ZDOT = -1503
196186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14505482
80 X = 4421271
16
Y = -321099
21 feet Y = -97871
04 meter
Z = -16893261
04 Z = -5149065
97
XDOT = -5269
920099 XDOT = -1606
271646
YDOT = 23003
969054 feet/sec YDOT = 7011
609768 meter/sec
ZDOT = -4973
428436 ZDOT = -1515
900987
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 18064
73989596
00016717 00000-0 10270-3 0 9125
2 25544 51
6410 174
4278 0002652 156
0530 204
0747 15
54188475 22429
Satellite: ISS
Catalog Number: 25544
Epoch time: 18064
73989596 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 174
4278 deg
Eccentricity:
0002652
Arg of perigee: 156
0530 deg
Mean anomaly: 204
0747 deg
Mean motion: 15
54188475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 318
Coasting Arc #14 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2018/065/17:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -308073
88 A = 6777173
70 meter
Y = -4210360
45 meter E =
0003923
Z = 5298492
47 I = 51
69012
XDOT = 7567
283987 Wp = 113
87819
YDOT = -1165
176961 meter/sec RA = 168
36522 deg
ZDOT = -487
166830 TA = 340
75617
MA = 340
77098
Ha = 221
461 n
mi
Hp = 214
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1010741
08 X = -286706
73
Y = -13813518
55 feet Y = -4213685
48 meter
Z = 17383505
47 Z = 5297048
33
XDOT = 24827
047202 XDOT = 7582
117284
YDOT = -3822
759060 feet/sec YDOT = -1080
471506 meter/sec
ZDOT = -1598
316371 ZDOT = -450
371651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12830762
46 X = -3910816
40
Y = -5235825
41 feet Y = -1595879
58 meter
Z = 17377537
84 Z = 5296673
53
XDOT = 7428
238436 XDOT = 2264
127075
YDOT = -22949
443221 feet/sec YDOT = -6994
990294 meter/sec
ZDOT = -1434
128353 ZDOT = -437
122322
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 18065
76868104
00016717 00000-0 10270-3 0 9131
2 25544 51
6390 169
2989 0002655 156
4112 203
7163 15
54208805 22585
Satellite: ISS
Catalog Number: 25544
Epoch time: 18065
76868104 = yrday
fracday
Element set: 913
Inclination: 51
6390 deg
RA of node: 169
2989 deg
Eccentricity:
0002655
Arg of perigee: 156
4112 deg
Mean anomaly: 203
7163 deg
Mean motion: 15
54208805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2258
Checksum: 320
Coasting Arc #15 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2018/066/17:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1490222
95 A = 6778997
25 meter
Y = 4469051
27 meter E =
0013522
Z = -4887315
24 I = 51
72936
XDOT = -7270
225837 Wp = 116
18558
YDOT = 197
749675 meter/sec RA = 163
37143 deg
ZDOT = 2396
962851 TA = 177
31463
MA = 177
30736
Ha = 221
321 n
mi
Hp = 214
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4889182
89 X = -1516346
47
Y = 14662241
70 feet Y = 4452240
04 meter
Z = -16034498
84 Z = -4894618
07
XDOT = -23852
446973 XDOT = -7283
539908
YDOT = 648
785022 feet/sec YDOT = 116
374798 meter/sec
ZDOT = 7864
051349 ZDOT = 2361
614467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11104393
61 X = 3384619
17
Y = 10701229
37 feet Y = 3261734
71 meter
Z = -16067567
53 Z = -4897394
58
XDOT = -9065
887349 XDOT = -2763
282464
YDOT = 20981
686305 feet/sec YDOT = 6395
217986 meter/sec
ZDOT = 7706
403574 ZDOT = 2348
911809
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 18066
73316136
00016717 00000-0 10270-3 0 9143
2 25544 51
6403 164
4907 0002462 163
4657 196
6577 15
54193288 22739
Satellite: ISS
Catalog Number: 25544
Epoch time: 18066
73316136 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 164
4907 deg
Eccentricity:
0002462
Arg of perigee: 163
4657 deg
Mean anomaly: 196
6577 deg
Mean motion: 15
54193288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2273
Checksum: 326
Coasting Arc #16 (Orbit 2288)
---------------------------------------
Vector Time (GMT): 2018/067/17:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3113091
62 A = 6782362
23 meter
Y = -4561105
03 meter E =
0011558
Z = 3927387
83 I = 51
77105
XDOT = 6446
200530 Wp = 92
09519
YDOT = 890
693189 meter/sec RA = 158
38698 deg
ZDOT = -4065
343969 TA = 40
36099
MA = 40
27527
Ha = 221
171 n
mi
Hp = 214
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10213555
18 X = 3144786
71
Y = -14964255
35 feet Y = -4526114
75 meter
Z = 12885130
68 Z = 3942587
41
XDOT = 21148
951870 XDOT = 6455
508628
YDOT = 2922
221750 feet/sec YDOT = 962
830737 meter/sec
ZDOT = -13337
742679 ZDOT = -4034
008247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9311759
16 X = -2838224
19
Y = -15484569
25 feet Y = -4719696
71 meter
Z = 12953435
70 Z = 3948207
20
XDOT = 10457
385716 XDOT = 3187
411166
YDOT = -17356
367776 feet/sec YDOT = -5290
220898 meter/sec
ZDOT = -13198
094204 ZDOT = -4022
779113
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 18067
76193444
00016717 00000-0 10270-3 0 9153
2 25544 51
6389 159
3613 0002374 163
1906 196
9326 15
54248027 22899
Satellite: ISS
Catalog Number: 25544
Epoch time: 18067
76193444 = yrday
fracday
Element set: 915
Inclination: 51
6389 deg
RA of node: 159
3613 deg
Eccentricity:
0002374
Arg of perigee: 163
1906 deg
Mean anomaly: 196
9326 deg
Mean motion: 15
54248027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2289
Checksum: 336
Coasting Arc #17 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2018/068/17:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4416530
49 A = 6786146
29 meter
Y = 4468496
65 meter E =
0004679
Z = -2567753
11 I = 51
81322
XDOT = -5154
446820 Wp = 81
30648
YDOT = -2065
172542 meter/sec RA = 153
41618 deg
ZDOT = 5280
653664 TA = 249
92157
MA = 249
97194
Ha = 221
203 n
mi
Hp = 214
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14489929
42 X = -4453697
50
Y = 14660422
07 feet Y = 4418899
95 meter
Z = -8424386
84 Z = -2589297
51
XDOT = -16910
914764 XDOT = -5156
620825
YDOT = -6775
500466 feet/sec YDOT = -2122
824853 meter/sec
ZDOT = 17324
979211 ZDOT = 5255
610247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7554828
94 X = 2302711
86
Y = 19135661
43 feet Y = 5832549
61 meter
Z = -8520994
35 Z = -2597199
08
XDOT = -11695
453826 XDOT = -3564
774326
YDOT = 12269
622704 feet/sec YDOT = 3739
781000 meter/sec
ZDOT = 17213
513963 ZDOT = 5246
679056
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 18068
72640625
00016717 00000-0 10270-3 0 9169
2 25544 51
6383 154
5536 0002446 166
0881 194
0339 15
54238504 23048
Satellite: ISS
Catalog Number: 25544
Epoch time: 18068
72640625 = yrday
fracday
Element set: 916
Inclination: 51
6383 deg
RA of node: 154
5536 deg
Eccentricity:
0002446
Arg of perigee: 166
0881 deg
Mean anomaly: 194
0339 deg
Mean motion: 15
54238504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 311
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