[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 29th 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) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
303/21:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 215
1
311/16:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 214
2
Coasting Arc #1 (Orbit 1939)
---------------------------------------
Vector Time (GMT): 2018/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3863979
81 A = 6778056
54 meter
Y = 1580706
75 meter E =
0004141
Z = 5338506
65 I = 51
97724
XDOT = -2838
187646 Wp = 20
10076
YDOT = -7125
018251 meter/sec RA = 68
62635 deg
ZDOT = 59
192978 TA = 69
36010
MA = 69
31570
Ha = 221
744 n
mi
Hp = 215
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12677099
12 X = -3907300
72
Y = 5186045
77 feet Y = 1537254
70 meter
Z = 17514785
60 Z = 5319631
20
XDOT = -9311
639260 XDOT = -2758
590300
YDOT = -23376
044131 feet/sec YDOT = -7156
311780 meter/sec
ZDOT = 194
202685 ZDOT = 45
598926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7118155
21 X = 2169613
71
Y = -11828382
57 feet Y = -3605291
01 meter
Z = 17429654
60 Z = 5312558
72
XDOT = 20617
862138 XDOT = 6284
324380
YDOT = 12586
590934 feet/sec YDOT = 3836
392917 meter/sec
ZDOT = 133
945714 ZDOT = 40
826654
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 18302
54832628
00016717 00000-0 10270-3 0 9009
2 25544 51
6407 69
1603 0004081 346
3919 13
7122 15
53884609 19407
Satellite: ISS
Catalog Number: 25544
Epoch time: 18302
54832628 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 69
1603 deg
Eccentricity:
0004081
Arg of perigee: 346
3919 deg
Mean anomaly: 13
7122 deg
Mean motion: 15
53884609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1940
Checksum: 300
Coasting Arc #2 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2018/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4463338
59 A = 6779081
28 meter
Y = 1236
93 meter E =
0012317
Z = -5112721
32 I = 51
96740
XDOT = 2013
781037 Wp = 85
47901
YDOT = 7176
060564 meter/sec RA = 63
65394 deg
ZDOT = 1764
335336 TA = 201
49997
MA = 201
55174
Ha = 221
738 n
mi
Hp = 215
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14643499
30 X = 4487828
33
Y = 4058
18 feet Y = 51286
12 meter
Z = -16774020
08 Z = -5090980
14
XDOT = 6606
893165 XDOT = 1924
816310
YDOT = 23543
505787 feet/sec YDOT = 7198
082592 meter/sec
ZDOT = 5788
501760 ZDOT = 1773
901810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11648381
98 X = -3550426
83
Y = 9056466
87 feet Y = 2760411
10 meter
Z = -16676193
90 Z = -5082903
90
XDOT = -18978
971315 XDOT = -5784
790457
YDOT = -13702
326526 feet/sec YDOT = -4176
469125 meter/sec
ZDOT = 5830
617414 ZDOT = 1777
172188
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 18303
51301494
00016717 00000-0 10270-3 0 9010
2 25544 51
6405 64
3547 0004021 351
4894 8
6189 15
53893620 19557
Satellite: ISS
Catalog Number: 25544
Epoch time: 18303
51301494 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 64
3547 deg
Eccentricity:
0004021
Arg of perigee: 351
4894 deg
Mean anomaly: 8
6189 deg
Mean motion: 15
53893620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1955
Checksum: 301
Coasting Arc #3 (Orbit 1961)
---------------------------------------
Vector Time (GMT): 2018/303/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 12079
05 A = 6784770
90 meter
Y = 5800518
85 meter E =
0012321
Z = 3505487
42 I = 51
97826
XDOT = -5528
050761 Wp = 70
74685
YDOT = -2747
862652 meter/sec RA = 61
68199 deg
ZDOT = 4556
878733 TA = 330
29127
MA = 330
36118
Ha = 221
836 n
mi
Hp = 215
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 39629
41 X = -69812
93
Y = 19030573
67 feet Y = 5800195
99 meter
Z = 11500942
98 Z = 3505347
29
XDOT = -18136
649478 XDOT = -5519
047770
YDOT = -9015
297415 feet/sec YDOT = -2809
630889 meter/sec
ZDOT = 14950
389545 ZDOT = 4530
046814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1465005
34 X = 446533
63
Y = 18974981
87 feet Y = 5783574
47 meter
Z = 11499557
24 Z = 3505065
05
XDOT = -17506
531669 XDOT = -5335
990853
YDOT = -7653
913940 feet/sec YDOT = -2332
912969 meter/sec
ZDOT = 14830
013756 ZDOT = 4520
188193
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 18303
96320078
00016717 00000-0 10270-3 0 9029
2 25544 51
6381 62
1148 0004416 352
9926 7
1164 15
53903163 19622
Satellite: ISS
Catalog Number: 25544
Epoch time: 18303
96320078 = yrday
fracday
Element set: 902
Inclination: 51
6381 deg
RA of node: 62
1148 deg
Eccentricity:
0004416
Arg of perigee: 352
9926 deg
Mean anomaly: 7
1164 deg
Mean motion: 15
53903163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1962
Checksum: 295
Coasting Arc #4 (Orbit 1976)
---------------------------------------
Vector Time (GMT): 2018/304/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1056069
64 A = 6781253
53 meter
Y = -4908923
55 meter E =
0012092
Z = -4569696
62 I = 51
94976
XDOT = 5639
647664 Wp = 48
59761
YDOT = 4128
359909 meter/sec RA = 56
71767 deg
ZDOT = -3129
063285 TA = 190
13175
MA = 190
15615
Ha = 221
969 n
mi
Hp = 215
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3464795
41 X = 1133081
54
Y = -16105392
22 feet Y = -4896683
25 meter
Z = -14992442
98 Z = -4564379
48
XDOT = 18502
781050 XDOT = 5608
263558
YDOT = 13544
487889 feet/sec YDOT = 4191
250882 meter/sec
ZDOT = -10265
955660 ZDOT = -3101
743744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2001030
11 X = 609913
98
Y = -16374385
69 feet Y = -4990912
76 meter
Z = -14967871
72 Z = -4562207
30
XDOT = 18591
649301 XDOT = 5666
734707
YDOT = 11551
535748 feet/sec YDOT = 3520
908096 meter/sec
ZDOT = -10143
570864 ZDOT = -3091
760399
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 18304
92788690
00016717 00000-0 10270-3 0 9035
2 25544 51
6383 57
3067 0004531 357
6149 2
4981 15
53879231 19776
Satellite: ISS
Catalog Number: 25544
Epoch time: 18304
92788690 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 57
3067 deg
Eccentricity:
0004531
Arg of perigee: 357
6149 deg
Mean anomaly: 2
4981 deg
Mean motion: 15
53879231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1977
Checksum: 335
Coasting Arc #5 (Orbit 1992)
---------------------------------------
Vector Time (GMT): 2018/305/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2205654
95 A = 6778623
11 meter
Y = 3763467
23 meter E =
0004162
Z = 5185036
75 I = 51
92311
XDOT = -5489
117953 Wp = 59
21477
YDOT = -5168
153947 meter/sec RA = 51
74514 deg
ZDOT = 1417
439956 TA = 17
21693
MA = 17
20282
Ha = 222
107 n
mi
Hp = 214
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7236400
76 X = -2272761
62
Y = 12347333
42 feet Y = 3738426
96 meter
Z = 17011275
43 Z = 5174159
25
XDOT = -18008
917167 XDOT = -5437
803504
YDOT = -16955
885652 feet/sec YDOT = -5229
250128 meter/sec
ZDOT = 4650
393556 ZDOT = 1390
900176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5904954
76 X = -1799830
21
Y = 13100893
32 feet Y = 3993152
28 meter
Z = 16961831
68 Z = 5169966
30
XDOT = -18886
890146 XDOT = -5756
724116
YDOT = -14374
793505 feet/sec YDOT = -4381
437060 meter/sec
ZDOT = 4531
662609 ZDOT = 1381
250763
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 18305
95687911
00016717 00000-0 10270-3 0 9044
2 25544 51
6393 52
1793 0004645 359
6705
4444 15
53905932 19930
Satellite: ISS
Catalog Number: 25544
Epoch time: 18305
95687911 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 52
1793 deg
Eccentricity:
0004645
Arg of perigee: 359
6705 deg
Mean anomaly:
4444 deg
Mean motion: 15
53905932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1993
Checksum: 328
Coasting Arc #6 (Orbit 2007)
---------------------------------------
Vector Time (GMT): 2018/306/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3371994
19 A = 6778132
79 meter
Y = -2513106
45 meter E =
0015557
Z = -5328481
52 I = 51
89952
XDOT = 4987
312066 Wp = 75
59249
YDOT = 5794
577151 meter/sec RA = 46
76617 deg
ZDOT = 427
970091 TA = 198
45205
MA = 198
50854
Ha = 222
176 n
mi
Hp = 214
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11062973
07 X = 3425729
13
Y = -8245099
89 feet Y = -2475098
23 meter
Z = -17481894
76 Z = -5311970
72
XDOT = 16362
572395 XDOT = 4920
065939
YDOT = 19011
079892 feet/sec YDOT = 5849
972760 meter/sec
ZDOT = 1404
101349 ZDOT = 452
033474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10009965
91 X = 3051037
61
Y = -9631989
93 feet Y = -2935830
53 meter
Z = -17407269
81 Z = -5305735
84
XDOT = 17987
044187 XDOT = 5482
451068
YDOT = 15989
723679 feet/sec YDOT = 4873
667777 meter/sec
ZDOT = 1511
595384 ZDOT = 460
734273
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 18306
92155728
00016717 00000-0 10270-3 0 9059
2 25544 51
6390 47
3717 0004714 4
3686 355
7507 15
53886182 20087
Satellite: ISS
Catalog Number: 25544
Epoch time: 18306
92155728 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 47
3717 deg
Eccentricity:
0004714
Arg of perigee: 4
3686 deg
Mean anomaly: 355
7507 deg
Mean motion: 15
53886182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2008
Checksum: 320
Coasting Arc #7 (Orbit 2023)
---------------------------------------
Vector Time (GMT): 2018/307/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4472622
70 A = 6779740
52 meter
Y = 1208630
20 meter E =
0010248
Z = 4947228
41 I = 51
88209
XDOT = -4133
148834 Wp = 37
03963
YDOT = -6057
686534 meter/sec RA = 41
78794 deg
ZDOT = -2246
328020 TA = 74
87292
MA = 74
75958
Ha = 222
335 n
mi
Hp = 214
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14673958
99 X = -4509836
95
Y = 3965322
17 feet Y = 1158406
40 meter
Z = 16231064
34 Z = 4925411
15
XDOT = -13560
199585 XDOT = -4054
191249
YDOT = -19874
299653 feet/sec YDOT = -6103
464910 meter/sec
ZDOT = -7369
842585 ZDOT = -2266
213672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14036381
01 X = -4278288
93
Y = 6100075
82 feet Y = 1859303
11 meter
Z = 16132742
63 Z = 4917259
96
XDOT = -15845
582824 XDOT = -4829
733645
YDOT = -16644
923227 feet/sec YDOT = -5073
372599 meter/sec
ZDOT = -7458
491373 ZDOT = -2273
348170
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 18307
95054442
00016717 00000-0 10270-3 0 9065
2 25544 51
6396 42
2445 0004714 7
6847 352
4377 15
53897258 20243
Satellite: ISS
Catalog Number: 25544
Epoch time: 18307
95054442 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 42
2445 deg
Eccentricity:
0004714
Arg of perigee: 7
6847 deg
Mean anomaly: 352
4377 deg
Mean motion: 15
53897258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2024
Checksum: 322
Coasting Arc #8 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2018/308/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5390884
98 A = 6782935
56 meter
Y = -6427
90 meter E =
0008144
Z = -4121628
43 I = 51
86802
XDOT = 2931
077507 Wp = 72
91560
YDOT = 5952
263413 meter/sec RA = 36
81425 deg
ZDOT = 3832
995559 TA = 236
53608
MA = 236
61396
Ha = 222
360 n
mi
Hp = 214
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17686630
51 X = 5410577
31
Y = -21088
91 feet Y = 53966
62 meter
Z = -13522402
97 Z = -4095393
00
XDOT = 9616
396020 XDOT = 2845
680732
YDOT = 19528
423271 feet/sec YDOT = 5984
563471 meter/sec
ZDOT = 12575
444747 ZDOT = 3847
026291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17531178
58 X = 5343503
23
Y = -2941641
58 feet Y = -896612
35 meter
Z = -13404374
22 Z = -4085653
26
XDOT = 12396
328960 XDOT = 3778
401067
YDOT = 16419
916805 feet/sec YDOT = 5004
790642 meter/sec
ZDOT = 12637
752832 ZDOT = 3851
987063
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 18308
91521569
00016717 00000-0 10270-3 0 9072
2 25544 51
6403 37
4374 0004770 10
3675 349
7575 15
53894898 20393
Satellite: ISS
Catalog Number: 25544
Epoch time: 18308
91521569 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 37
4374 deg
Eccentricity:
0004770
Arg of perigee: 10
3675 deg
Mean anomaly: 349
7575 deg
Mean motion: 15
53894898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 339
Coasting Arc #9 (Orbit 2054)
---------------------------------------
Vector Time (GMT): 2018/309/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6045989
46 A = 6786558
90 meter
Y = -1101908
61 meter E =
0014657
Z = 2870174
25 I = 51
85358
XDOT = -1407
452532 Wp = 79
70433
YDOT = -5570
063782 meter/sec RA = 31
84806 deg
ZDOT = -5078
657800 TA = 67
74340
MA = 67
58802
Ha = 222
441 n
mi
Hp = 214
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19835923
41 X = -6047160
39
Y = -3615185
73 feet Y = -1169525
49 meter
Z = 9416582
19 Z = 2840801
41
XDOT = -4617
626416 XDOT = -1320
391865
YDOT = -18274
487473 feet/sec YDOT = -5585
316320 meter/sec
ZDOT = -16662
263123 ZDOT = -5085
283191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20223724
37 X = -6164191
19
Y = 50883
82 feet Y = 15509
39 meter
Z = 9284601
72 Z = 2829946
60
XDOT = -7739
868944 XDOT = -2359
112054
YDOT = -15681
834706 feet/sec YDOT = -4779
823219 meter/sec
ZDOT = -16691
296950 ZDOT = -5087
507310
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 18309
94419475
00016717 00000-0 10270-3 0 9089
2 25544 51
6408 32
3097 0004918 14
9315 345
1982 15
53914874 20556
Satellite: ISS
Catalog Number: 25544
Epoch time: 18309
94419475 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 32
3097 deg
Eccentricity:
0004918
Arg of perigee: 14
9315 deg
Mean anomaly: 345
1982 deg
Mean motion: 15
53914874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 329
Coasting Arc #10 (Orbit 2069)
---------------------------------------
Vector Time (GMT): 2018/310/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6334082
79 A = 6789220
92 meter
Y = 1993225
38 meter E =
0013467
Z = -1382936
33 I = 51
83310
XDOT = -303
088160 Wp = 30
21114
YDOT = 4979
800751 meter/sec RA = 26
88920 deg
ZDOT = 5825
125147 TA = 314
75851
MA = 314
86801
Ha = 222
524 n
mi
Hp = 214
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20781111
52 X = 6318040
98
Y = 6539453
36 feet Y = 2063967
77 meter
Z = -4537192
67 Z = -1352205
72
XDOT = -994
383728 XDOT = -387
047322
YDOT = 16337
928972 feet/sec YDOT = 4975
942110 meter/sec
ZDOT = 19111
302975 ZDOT = 5823
448756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21693799
03 X = 6612269
95
Y = 2287122
30 feet Y = 697114
88 meter
Z = -4399240
68 Z = -1340888
56
XDOT = 2304
090713 XDOT = 702
286849
YDOT = 14655
779749 feet/sec YDOT = 4467
081668 meter/sec
ZDOT = 19103
064826 ZDOT = 5822
614159
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 18310
90886019
00016717 00000-0 10270-3 0 9090
2 25544 51
6402 27
5034 0004888 17
9487 342
1837 15
53902780 20702
Satellite: ISS
Catalog Number: 25544
Epoch time: 18310
90886019 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 27
5034 deg
Eccentricity:
0004888
Arg of perigee: 17
9487 deg
Mean anomaly: 342
1837 deg
Mean motion: 15
53902780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2070
Checksum: 316
Coasting Arc #11 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2018/311/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4224461
26 A = 6780331
81 meter
Y = 2297138
35 meter E =
0011693
Z = 4776263
98 I = 51
77905
XDOT = -5524
895676 Wp = 46
46552
YDOT = -4609
496534 meter/sec RA = 22
92769 deg
ZDOT = -2657
734666 TA = 69
76728
MA = 69
64160
Ha = 222
555 n
mi
Hp = 214
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13859781
04 X = -4273035
77
Y = 7536543
15 feet Y = 2249625
93 meter
Z = 15670157
41 Z = 4755624
42
XDOT = -18126
298149 XDOT = -5460
030132
YDOT = -15123
020125 feet/sec YDOT = -4670
917091 meter/sec
ZDOT = -8719
601923 ZDOT = -2684
415871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13280979
71 X = -4048042
62
Y = -8684444
98 feet Y = -2647018
83 meter
Z = 15576997
14 Z = 4747868
73
XDOT = 4052
947294 XDOT = 1235
338335
YDOT = -22122
918004 feet/sec YDOT = -6743
065408 meter/sec
ZDOT = -8838
960236 ZDOT = -2694
115080
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 18311
74489917
00016717 00000-0 10270-3 0 9101
2 25544 51
6394 23
3367 0004753 21
9195 338
2160 15
53932494 20831
Satellite: ISS
Catalog Number: 25544
Epoch time: 18311
74489917 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 23
3367 deg
Eccentricity:
0004753
Arg of perigee: 21
9195 deg
Mean anomaly: 338
2160 deg
Mean motion: 15
53932494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 316
Coasting Arc #12 (Orbit 2097)
---------------------------------------
Vector Time (GMT): 2018/312/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5405134
48 A = 6783822
11 meter
Y = -1434029
62 meter E =
0008664
Z = -3844854
63 I = 51
75982
XDOT = 4241
162473 Wp = 69
57825
YDOT = 4829
506703 meter/sec RA = 17
94938 deg
ZDOT = 4171
547137 TA = 244
25670
MA = 244
34615
Ha = 222
686 n
mi
Hp = 214
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17733380
83 X = 5439445
28
Y = -4704821
60 feet Y = -1373393
76 meter
Z = -12614352
47 Z = -3818514
31
XDOT = 13914
575042 XDOT = 4166
578618
YDOT = 15844
838263 feet/sec YDOT = 4876
517241 meter/sec
ZDOT = 13686
178271 ZDOT = 4191
968731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12856404
93 X = 3918632
22
Y = 13202308
59 feet Y = 4024063
66 meter
Z = -12495676
47 Z = -3808682
19
XDOT = -6041
119380 XDOT = -1841
333187
YDOT = 18889
671402 feet/sec YDOT = 5757
571843 meter/sec
ZDOT = 13777
337318 ZDOT = 4199
332415
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 18312
70955875
00016717 00000-0 10270-3 0 9110
2 25544 51
6397 18
5302 0004939 26
7751 333
3656 15
53908083 20985
Satellite: ISS
Catalog Number: 25544
Epoch time: 18312
70955875 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 18
5302 deg
Eccentricity:
0004939
Arg of perigee: 26
7751 deg
Mean anomaly: 333
3656 deg
Mean motion: 15
53908083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2098
Checksum: 329
Coasting Arc #13 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2018/313/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6276074
05 A = 6787269
46 meter
Y = 581788
97 meter E =
0015625
Z = 2505893
82 I = 51
73857
XDOT = -2585
064052 Wp = 86
46440
YDOT = -4892
457797 meter/sec RA = 12
97713 deg
ZDOT = -5308
999415 TA = 65
46786
MA = 65
30505
Ha = 222
642 n
mi
Hp = 213
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20590794
14 X = -6294285
96
Y = 1908756
46 feet Y = 511503
63 meter
Z = 8221436
42 Z = 2475361
81
XDOT = -8481
181273 XDOT = -2504
374098
YDOT = -16051
370726 feet/sec YDOT = -4920
914428 meter/sec
ZDOT = -17417
977083 ZDOT = -5321
361274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12102829
65 X = -3688942
48
Y = -16834074
66 feet Y = -5131025
96 meter
Z = 8084034
65 Z = 2464013
76
XDOT = 8376
993777 XDOT = 2553
307703
YDOT = -14460
664505 feet/sec YDOT = -4407
610541 meter/sec
ZDOT = -17472
867743 ZDOT = -5325
730088
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 18313
73852432
00016717 00000-0 10270-3 0 9120
2 25544 51
6384 13
4017 0005014 28
1013 332
0409 15
53952950 21143
Satellite: ISS
Catalog Number: 25544
Epoch time: 18313
73852432 = yrday
fracday
Element set: 912
Inclination: 51
6384 deg
RA of node: 13
4017 deg
Eccentricity:
0005014
Arg of perigee: 28
1013 deg
Mean anomaly: 332
0409 deg
Mean motion: 15
53952950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 267
Coasting Arc #14 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2018/314/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6710904
90 A = 6789467
59 meter
Y = 172239
38 meter E =
0014818
Z = -968834
06 I = 51
71315
XDOT = 722
566106 Wp = 37
03782
YDOT = 4821
582418 meter/sec RA = 8
01172 deg
ZDOT = 5920
867339 TA = 312
47705
MA = 312
60219
Ha = 222
697 n
mi
Hp = 213
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22017404
52 X = 6713186
29
Y = 565089
82 feet Y = 247298
18 meter
Z = -3178589
44 Z = -936228
51
XDOT = 2370
623706 XDOT = 639
835006
YDOT = 15818
839954 feet/sec YDOT = 4829
199789 meter/sec
ZDOT = 19425
417778 ZDOT = 5924
176685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11005192
12 X = 3354382
56
Y = 19101877
51 feet Y = 5822252
27 meter
Z = -3031976
46 Z = -924146
42
XDOT = -10939
962147 XDOT = -3334
500462
YDOT = 9356
431711 feet/sec YDOT = 2851
840386 meter/sec
ZDOT = 19439
599697 ZDOT = 5925
189988
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 18314
70317855
00016717 00000-0 10270-3 0 9134
2 25544 51
6380 8
5952 0004876 34
5266 325
6202 15
53955849 21293
Satellite: ISS
Catalog Number: 25544
Epoch time: 18314
70317855 = yrday
fracday
Element set: 913
Inclination: 51
6380 deg
RA of node: 8
5952 deg
Eccentricity:
0004876
Arg of perigee: 34
5266 deg
Mean anomaly: 325
6202 deg
Mean motion: 15
53955849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2129
Checksum: 321
Coasting Arc #15 (Orbit 2144)
---------------------------------------
Vector Time (GMT): 2018/315/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6688158
22 A = 6789609
48 meter
Y = -917220
49 meter E =
0010385
Z = -709321
94 I = 51
68170
XDOT = 1261
942854 Wp = 111
43871
YDOT = -4649
711479 meter/sec RA = 3
04579 deg
ZDOT = -5960
227511 TA = 76
21523
MA = 76
09968
Ha = 222
729 n
mi
Hp = 213
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21942776
30 X = -6673958
94
Y = -3009253
59 feet Y = -991932
69 meter
Z = -2327171
72 Z = -741776
90
XDOT = 4140
232459 XDOT = 1342
795646
YDOT = -15254
958921 feet/sec YDOT = -4635
147160 meter/sec
ZDOT = -19554
552201 ZDOT = -5953
901178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9208524
24 X = -2806758
19
Y = -20125708
73 feet Y = -6134316
02 meter
Z = -2472993
45 Z = -753768
40
XDOT = 13701
863650 XDOT = 4176
328040
YDOT = -3898
115999 feet/sec YDOT = -1188
145756 meter/sec
ZDOT = -19525
422738 ZDOT = -5951
348851
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 18315
73213812
00016717 00000-0 10270-3 0 9147
2 25544 51
6390 3
4661 0005061 35
9339 324
2153 15
53947406 21456
Satellite: ISS
Catalog Number: 25544
Epoch time: 18315
73213812 = yrday
fracday
Element set: 914
Inclination: 51
6390 deg
RA of node: 3
4661 deg
Eccentricity:
0005061
Arg of perigee: 35
9339 deg
Mean anomaly: 324
2153 deg
Mean motion: 15
53947406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2145
Checksum: 287
Coasting Arc #16 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2018/316/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6183206
86 A = 6787485
89 meter
Y = 1592852
17 meter E =
0018097
Z = 2273769
81 I = 51
64148
XDOT = -3144
672919 Wp = 63
72522
YDOT = 4410
340944 meter/sec RA = 358
07655 deg
ZDOT = 5436
240718 TA = 321
60396
MA = 321
73263
Ha = 222
614 n
mi
Hp = 213
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20286111
74 X = 6153890
63
Y = 5225892
93 feet Y = 1661833
04 meter
Z = 7459874
71 Z = 2303735
06
XDOT = -10317
168368 XDOT = -3220
163689
YDOT = 14469
622519 feet/sec YDOT = 4374
752647 meter/sec
ZDOT = 17835
435428 ZDOT = 5420
781609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6771765
06 X = 2064033
99
Y = 19772565
94 feet Y = 6026678
10 meter
Z = 7594396
06 Z = 2314771
92
XDOT = -16383
675094 XDOT = -4993
744169
YDOT = -1244
073572 feet/sec YDOT = -379
193625 meter/sec
ZDOT = 17765
271344 ZDOT = 5414
854706
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 18316
76109258
00016717 00000-0 10270-3 0 9150
2 25544 51
6387 358
3389 0004870 39
6881 320
4627 15
53982566 21619
Satellite: ISS
Catalog Number: 25544
Epoch time: 18316
76109258 = yrday
fracday
Element set: 915
Inclination: 51
6387 deg
RA of node: 358
3389 deg
Eccentricity:
0004870
Arg of perigee: 39
6881 deg
Mean anomaly: 320
4627 deg
Mean motion: 15
53982566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2161
Checksum: 343
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