[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 19th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
354/01:40:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 214
1
358/04:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
6
361/02:52:51
545 -1
8 2
1 2
1
N/A 1
0 -0
0 221
4
000/00:05:43
091 0
6 -0
0 216
2
361/09:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 216
2
364/12:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 216
6
Coasting Arc #1 (Orbit 2735)
---------------------------------------
Vector Time (GMT): 2018/353/17:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6507948
17 A = 6788170
40 meter
Y = 635586
84 meter E =
0012441
Z = -1801374
13 I = 51
69538
XDOT = -2025
215527 Wp = 151
90717
YDOT = 4756
509212 meter/sec RA = 173
00982 deg
ZDOT = -5664
997412 TA = 47
87536
MA = 47
76969
Ha = 222
288 n
mi
Hp = 214
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21351535
98 X = 6509107
38
Y = 2085258
68 feet Y = 708369
91 meter
Z = -5910020
11 Z = -1769757
58
XDOT = -6644
407897 XDOT = -2050
735793
YDOT = 15605
345183 feet/sec YDOT = 4733
719725 meter/sec
ZDOT = -18585
949515 ZDOT = -5674
896807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19753138
67 X = 6020756
67
Y = 8468326
40 feet Y = 2581145
89 meter
Z = -5767641
72 Z = -1757977
20
XDOT = -10324
388331 XDOT = -3146
873563
YDOT = 11454
239918 feet/sec YDOT = 3491
252327 meter/sec
ZDOT = -18631
017619 ZDOT = -5678
734170
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 18353
73708299
00016717 00000-0 10270-3 0 9002
2 25544 51
6384 174
0345 0005215 165
5934 194
5368 15
54075545 27364
Satellite: ISS
Catalog Number: 25544
Epoch time: 18353
73708299 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 174
0345 deg
Eccentricity:
0005215
Arg of perigee: 165
5934 deg
Mean anomaly: 194
5368 deg
Mean motion: 15
54075545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2736
Checksum: 330
Coasting Arc #2 (Orbit 2741)
---------------------------------------
Vector Time (GMT): 2018/354/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3598909
70 A = 6779972
79 meter
Y = -3237752
94 meter E =
0011505
Z = 4743502
21 I = 51
67693
XDOT = 6438
699808 Wp = 135
57484
YDOT = -3164
587488 meter/sec RA = 171
21734 deg
ZDOT = 2713
005431 TA = 287
56380
MA = 287
68945
Ha = 222
131 n
mi
Hp = 214
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11807446
54 X = -3585478
41
Y = -10622549
01 feet Y = -3277923
87 meter
Z = 15562671
29 Z = 4726052
05
XDOT = 21124
343202 XDOT = 6460
430100
YDOT = -10382
504883 feet/sec YDOT = -3092
464268 meter/sec
ZDOT = 8900
936454 ZDOT = 2744
335136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5164492
86 X = -1574137
42
Y = 15100112
33 feet Y = 4602514
24 meter
Z = 15484369
53 Z = 4719635
83
XDOT = -16643
834452 XDOT = -5073
040741
YDOT = -15005
613881 feet/sec YDOT = -4573
711111 meter/sec
ZDOT = 9042
405824 ZDOT = 2756
125295
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 18354
12290720
00016717 00000-0 10270-3 0 9012
2 25544 51
6353 172
1147 0004725 165
9959 194
1326 15
54095117 27429
Satellite: ISS
Catalog Number: 25544
Epoch time: 18354
12290720 = yrday
fracday
Element set: 901
Inclination: 51
6353 deg
RA of node: 172
1147 deg
Eccentricity:
0004725
Arg of perigee: 165
9959 deg
Mean anomaly: 194
1326 deg
Mean motion: 15
54095117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2742
Checksum: 305
Coasting Arc #3 (Orbit 2756)
---------------------------------------
Vector Time (GMT): 2018/355/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1943129
03 A = 6777811
20 meter
Y = 3809444
90 meter E =
0015566
Z = -5271265
47 I = 51
70272
XDOT = -7194
955217 Wp = 100
89495
YDOT = 2472
135549 meter/sec RA = 166
22317 deg
ZDOT = -870
740416 TA = 160
80347
MA = 160
74475
Ha = 222
035 n
mi
Hp = 214
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6375095
23 X = 1925991
54
Y = 12498178
80 feet Y = 3831079
20 meter
Z = -17294178
05 Z = -5261867
47
XDOT = -23605
496118 XDOT = -7217
834956
YDOT = 8110
680936 feet/sec YDOT = 2391
548746 meter/sec
ZDOT = -2856
759894 ZDOT = -905
746523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8809562
05 X = 2685154
51
Y = -10985800
46 feet Y = -3348471
98 meter
Z = -17252208
89 Z = -5258473
27
XDOT = 16146
711586 XDOT = 4921
517691
YDOT = 17656
413762 feet/sec YDOT = 5381
674915 meter/sec
ZDOT = -3014
753086 ZDOT = -918
896741
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 18355
08746978
00016717 00000-0 10270-3 0 9020
2 25544 51
6359 167
3055 0004697 167
9894 192
1371 15
54068502 27579
Satellite: ISS
Catalog Number: 25544
Epoch time: 18355
08746978 = yrday
fracday
Element set: 902
Inclination: 51
6359 deg
RA of node: 167
3055 deg
Eccentricity:
0004697
Arg of perigee: 167
9894 deg
Mean anomaly: 192
1371 deg
Mean motion: 15
54068502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2757
Checksum: 353
Coasting Arc #4 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2018/356/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -216481
26 A = 6777839
96 meter
Y = -4290638
64 meter E =
0004546
Z = 5238799
88 I = 51
73538
XDOT = 7418
989632 Wp = 125
64637
YDOT = -1649
605863 meter/sec RA = 161
22972 deg
ZDOT = -1046
425869 TA = 334
34653
MA = 334
36907
Ha = 221
953 n
mi
Hp = 214
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -710240
37 X = -193933
45
Y = -14076898
42 feet Y = -4292934
19 meter
Z = 17187663
66 Z = 5237802
41
XDOT = 24340
517166 XDOT = 7441
967592
YDOT = -5412
092726 feet/sec YDOT = -1566
512931 meter/sec
ZDOT = -3433
155737 ZDOT = -1010
331309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12429892
52 X = -3788631
24
Y = 6655893
85 feet Y = 2028716
44 meter
Z = 17183600
95 Z = 5237561
57
XDOT = -14651
768553 XDOT = -4465
859055
YDOT = -18935
740837 feet/sec YDOT = -5771
613807 meter/sec
ZDOT = -3270
309413 ZDOT = -996
790309
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 18356
11633445
00016717 00000-0 10270-3 0 9030
2 25544 51
6362 162
1769 0004580 171
8101 188
3127 15
54071160 27732
Satellite: ISS
Catalog Number: 25544
Epoch time: 18356
11633445 = yrday
fracday
Element set: 903
Inclination: 51
6362 deg
RA of node: 162
1769 deg
Eccentricity:
0004580
Arg of perigee: 171
8101 deg
Mean anomaly: 188
3127 deg
Mean motion: 15
54071160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 296
Coasting Arc #5 (Orbit 2787)
---------------------------------------
Vector Time (GMT): 2018/357/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1468470
11 A = 6780180
16 meter
Y = 4683140
08 meter E =
0013202
Z = -4690670
73 I = 51
77409
XDOT = -7072
799425 Wp = 128
02942
YDOT = 650
777949 meter/sec RA = 156
24149 deg
ZDOT = 2861
510389 TA = 170
38747
MA = 170
36218
Ha = 221
819 n
mi
Hp = 214
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4817815
32 X = -1497944
42
Y = 15364632
80 feet Y = 4666554
55 meter
Z = -15389339
65 Z = -4697874
89
XDOT = -23204
722522 XDOT = -7093
450606
YDOT = 2135
098257 feet/sec YDOT = 571
569079 meter/sec
ZDOT = 9388
157443 ZDOT = 2827
103222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15884172
68 X = 4841495
83
Y = -2441524
52 feet Y = -744176
67 meter
Z = -15422291
55 Z = -4700714
46
XDOT = 11871
186798 XDOT = 3618
337736
YDOT = 18859
784443 feet/sec YDOT = 5748
462298 meter/sec
ZDOT = 9232
987820 ZDOT = 2814
214688
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 18357
08089451
00016717 00000-0 10270-3 0 9040
2 25544 51
6360 157
3688 0004505 176
0332 184
0857 15
54061646 27883
Satellite: ISS
Catalog Number: 25544
Epoch time: 18357
08089451 = yrday
fracday
Element set: 904
Inclination: 51
6360 deg
RA of node: 157
3688 deg
Eccentricity:
0004505
Arg of perigee: 176
0332 deg
Mean anomaly: 184
0857 deg
Mean motion: 15
54061646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2788
Checksum: 327
Coasting Arc #6 (Orbit 2803)
---------------------------------------
Vector Time (GMT): 2018/358/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2956765
50 A = 6783748
30 meter
Y = -4889054
99 meter E =
0012294
Z = 3643589
79 I = 51
81760
XDOT = 6268
132054 Wp = 107
04458
YDOT = 507
126179 meter/sec RA = 151
26410 deg
ZDOT = -4397
392958 TA = 29
79606
MA = 29
72611
Ha = 221
645 n
mi
Hp = 214
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9700674
21 X = 2993518
06
Y = -16040206
67 feet Y = -4855785
43 meter
Z = 11954034
73 Z = 3658041
14
XDOT = 20564
737710 XDOT = 6283
355382
YDOT = 1663
799799 feet/sec YDOT = 577
306555 meter/sec
ZDOT = -14427
142250 ZDOT = -4366
907775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18653866
89 X = -5685698
63
Y = -1360337
30 feet Y = -414630
81 meter
Z = 12019691
73 Z = 3663602
04
XDOT = -7925
507792 XDOT = -2415
694775
YDOT = -17832
735756 feet/sec YDOT = -5435
417858 meter/sec
ZDOT = -14289
745399 ZDOT = -4355
514398
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 18358
10975868
00016717 00000-0 10270-3 0 9051
2 25544 51
6373 152
2402 0004468 180
2822 179
8329 15
54087905 28045
Satellite: ISS
Catalog Number: 25544
Epoch time: 18358
10975868 = yrday
fracday
Element set: 905
Inclination: 51
6373 deg
RA of node: 152
2402 deg
Eccentricity:
0004468
Arg of perigee: 180
2822 deg
Mean anomaly: 179
8329 deg
Mean motion: 15
54087905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2804
Checksum: 330
Coasting Arc #7 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2018/358/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4990850
92 A = 6781281
41 meter
Y = -1197273
91 meter E =
0011730
Z = 4428987
65 I = 51
81401
XDOT = 4279
638015 Wp = 131
35685
YDOT = -5413
408982 meter/sec RA = 150
74598 deg
ZDOT = 3345
860525 TA = 284
86366
MA = 284
99355
Ha = 221
817 n
mi
Hp = 214
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16374182
80 X = -4998605
20
Y = -3928064
01 feet Y = -1253129
08 meter
Z = 14530799
37 Z = 4404725
05
XDOT = 14040
807137 XDOT = 4323
601940
YDOT = -17760
528155 feet/sec YDOT = -5365
305764 meter/sec
ZDOT = 10977
232695 ZDOT = 3366
755311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13804267
12 X = 4207540
62
Y = 9805582
65 feet Y = 2988741
59 meter
Z = 14421526
89 Z = 4395681
40
XDOT = -18883
596264 XDOT = -5755
720141
YDOT = 10235
477489 feet/sec YDOT = 3119
773539 meter/sec
ZDOT = 11071
996904 ZDOT = 3374
744656
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 18358
23836719
00016717 00000-0 10270-3 0 9067
2 25544 51
6391 151
6000 0004531 180
2707 179
8443 15
54077791 28066
Satellite: ISS
Catalog Number: 25544
Epoch time: 18358
23836719 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 151
6000 deg
Eccentricity:
0004531
Arg of perigee: 180
2707 deg
Mean anomaly: 179
8443 deg
Mean motion: 15
54077791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 317
Coasting Arc #8 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2018/359/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3748615
66 A = 6778291
14 meter
Y = 2343867
57 meter E =
0013024
Z = -5148796
16 I = 51
83432
XDOT = -5409
654008 Wp = 97
16853
YDOT = 5186
001326 meter/sec RA = 145
76431 deg
ZDOT = -1582
742276 TA = 157
62182
MA = 157
56495
Ha = 221
591 n
mi
Hp = 214
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12298607
82 X = 3747137
05
Y = 7689854
24 feet Y = 2385779
58 meter
Z = -16892375
85 Z = -5130590
24
XDOT = -17748
208688 XDOT = -5459
555260
YDOT = 17014
440045 feet/sec YDOT = 5125
227996 meter/sec
ZDOT = -5192
724001 ZDOT = -1609
140671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8833081
14 X = -2692323
13
Y = -11624336
60 feet Y = -3543097
80 meter
Z = -16810516
07 Z = -5123845
30
XDOT = 21784
881823 XDOT = 6640
031980
YDOT = -8895
376792 feet/sec YDOT = -2711
310846 meter/sec
ZDOT = -5312
301287 ZDOT = -1619
189432
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 18359
20292507
00016717 00000-0 10270-3 0 9077
2 25544 51
6406 146
7920 0004405 183
6857 176
4264 15
54104121 28211
Satellite: ISS
Catalog Number: 25544
Epoch time: 18359
20292507 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 146
7920 deg
Eccentricity:
0004405
Arg of perigee: 183
6857 deg
Mean anomaly: 176
4264 deg
Mean motion: 15
54104121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 302
Coasting Arc #9 (Orbit 2836)
---------------------------------------
Vector Time (GMT): 2018/360/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2361597
85 A = 6777396
32 meter
Y = -3466717
31 meter E =
0004204
Z = 5321650
59 I = 51
85815
XDOT = 6095
205295 Wp = 155
53707
YDOT = -4645
323946 meter/sec RA = 140
78015 deg
ZDOT = -324
894616 TA = 297
52877
MA = 297
57148
Ha = 221
520 n
mi
Hp = 214
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7748024
44 X = -2348505
87
Y = -11373744
46 feet Y = -3493053
66 meter
Z = 17459483
57 Z = 5310210
41
XDOT = 19997
392700 XDOT = 6148
275745
YDOT = -15240
564127 feet/sec YDOT = -4576
866354 meter/sec
ZDOT = -1065
927217 ZDOT = -295
158269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3499088
87 X = 1066522
29
Y = 13376732
22 feet Y = 4077227
98 meter
Z = 17408243
00 Z = 5306032
47
XDOT = -23035
595883 XDOT = -7021
249625
YDOT = 7222
085537 feet/sec YDOT = 2201
291672 meter/sec
ZDOT = -931
331866 ZDOT = -283
869953
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 18360
23178625
00016717 00000-0 10270-3 0 9087
2 25544 51
6403 141
6640 0004436 189
1452 170
9620 15
54120044 28371
Satellite: ISS
Catalog Number: 25544
Epoch time: 18360
23178625 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 141
6640 deg
Eccentricity:
0004436
Arg of perigee: 189
1452 deg
Mean anomaly: 170
9620 deg
Mean motion: 15
54120044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2837
Checksum: 292
Coasting Arc #10 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2018/361/02:55:43
091
Vector Time (MET): N/A
Weight (LBS) : 950686
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -365605
55 A = 6782367
03 meter
Y = 5149612
57 meter E =
0009085
Z = -4407863
50 I = 51
89381
XDOT = -6405
644557 Wp = 138
92926
YDOT = 2460
421333 meter/sec RA = 136
09892 deg
ZDOT = 3403
074414 TA = 165
46123
MA = 165
43508
Ha = 221
417 n
mi
Hp = 216
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1199493
28 X = -401752
06
Y = 16895054
35 feet Y = 5145322
33 meter
Z = -14461494
42 Z = -4409726
86
XDOT = -21015
894216 XDOT = -6449
211677
YDOT = 8072
248467 feet/sec YDOT = 2388
545105 meter/sec
ZDOT = 11164
942304 ZDOT = 3371
852877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11999923
58 X = 3657576
71
Y = -11942566
67 feet Y = -3640094
32 meter
Z = -14470431
99 Z = -4410587
67
XDOT = 20287
482877 XDOT = 6183
624781
YDOT = 7016
961794 feet/sec YDOT = 2138
769955 meter/sec
ZDOT = 11023
856138 ZDOT = 3360
071351
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 18361
13204212
00016717 00000-0 10270-3 0 9090
2 25544 51
6398 137
1760 0004389 214
0211 146
0661 15
53692769 28517
Satellite: ISS
Catalog Number: 25544
Epoch time: 18361
13204212 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 137
1760 deg
Eccentricity:
0004389
Arg of perigee: 214
0211 deg
Mean anomaly: 146
0661 deg
Mean motion: 15
53692769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2851
Checksum: 301
Coasting Arc #11 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2018/361/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 950686
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -931267
86 A = 6783788
69 meter
Y = 5398177
47 meter E =
0007263
Z = -4009598
17 I = 51
90146
XDOT = -6267
759704 Wp = 146
10010
YDOT = 1878
655608 meter/sec RA = 134
81049 deg
ZDOT = 3982
609814 TA = 165
26239
MA = 165
24121
Ha = 221
470 n
mi
Hp = 216
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3055340
75 X = -972086
37
Y = 17710556
01 feet Y = 5387535
44 meter
Z = -13154849
64 Z = -4014220
64
XDOT = -20563
516088 XDOT = -6307
646645
YDOT = 6163
568269 feet/sec YDOT = 1808
341861 meter/sec
ZDOT = 13066
305164 ZDOT = 3952
066932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12110655
26 X = -3691327
72
Y = -13257721
24 feet Y = -4040953
43 meter
Z = -13176259
97 Z = -4016124
04
XDOT = 6915
901434 XDOT = 2107
966757
YDOT = -19174
238314 feet/sec YDOT = -5844
307838 meter/sec
ZDOT = 12928
336176 ZDOT = 3940
556866
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 18361
38932280
00016717 00000-0 10270-3 0 9102
2 25544 51
6365 135
8907 0004645 213
5996 146
4862 15
53686714 28552
Satellite: ISS
Catalog Number: 25544
Epoch time: 18361
38932280 = yrday
fracday
Element set: 910
Inclination: 51
6365 deg
RA of node: 135
8907 deg
Eccentricity:
0004645
Arg of perigee: 213
5996 deg
Mean anomaly: 146
4862 deg
Mean motion: 15
53686714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 338
Coasting Arc #12 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2018/362/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 950686
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2015010
73 A = 6787219
53 meter
Y = -5836720
03 meter E =
0011777
Z = 2800588
38 I = 51
93604
XDOT = 5671
467678 Wp = 120
02722
YDOT = -513
363847 meter/sec RA = 129
85019 deg
ZDOT = -5140
131390 TA = 28
32929
MA = 28
26530
Ha = 221
260 n
mi
Hp = 216
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6610927
60 X = 2066525
20
Y = -19149343
93 feet Y = -5813898
89 meter
Z = 9188282
09 Z = 2810501
29
XDOT = 18607
177420 XDOT = 5701
754475
YDOT = -1684
264590 feet/sec YDOT = -449
771929 meter/sec
ZDOT = -16863
948131 ZDOT = -5112
508179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11324613
34 X = 3451742
14
Y = 16772591
05 feet Y = 5112285
75 meter
Z = 9233611
79 Z = 2814404
87
XDOT = -8721
714051 XDOT = -2658
378443
YDOT = 15122
683575 feet/sec YDOT = 4609
393954 meter/sec
ZDOT = -16739
278127 ZDOT = -5102
131973
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 18362
41844808
00016717 00000-0 10270-3 0 9116
2 25544 51
6369 130
7636 0004616 220
0086 140
0727 15
53699303 28716
Satellite: ISS
Catalog Number: 25544
Epoch time: 18362
41844808 = yrday
fracday
Element set: 911
Inclination: 51
6369 deg
RA of node: 130
7636 deg
Eccentricity:
0004616
Arg of perigee: 220
0086 deg
Mean anomaly: 140
0727 deg
Mean motion: 15
53699303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 306
Coasting Arc #13 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2018/363/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 950686
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2879195
82 A = 6789801
10 meter
Y = 5993739
55 meter E =
0004070
Z = -1364931
26 I = 51
96462
XDOT = -4862
960426 Wp = 36
10220
YDOT = -1009
552665 meter/sec RA = 124
89863 deg
ZDOT = 5836
812022 TA = 309
10672
MA = 309
14291
Ha = 221
290 n
mi
Hp = 216
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9446180
52 X = -2939375
46
Y = 19664499
83 feet Y = 5961205
96 meter
Z = -4478120
94 Z = -1379063
14
XDOT = -15954
594572 XDOT = -4879
661799
YDOT = -3312
180660 feet/sec YDOT = -1064
027342 meter/sec
ZDOT = 19149
645742 ZDOT = 5813
149044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10338722
30 X = -3151242
56
Y = -19195125
39 feet Y = -5850674
22 meter
Z = -4542513
60 Z = -1384558
14
XDOT = 10751
850186 XDOT = 3277
163937
YDOT = -10288
373671 feet/sec YDOT = -3135
896295 meter/sec
ZDOT = 19042
992975 ZDOT = 5804
304259
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 18363
38325509
00016717 00000-0 10270-3 0 9126
2 25544 51
6365 125
9567 0004567 219
2621 140
8201 15
53685167 28865
Satellite: ISS
Catalog Number: 25544
Epoch time: 18363
38325509 = yrday
fracday
Element set: 912
Inclination: 51
6365 deg
RA of node: 125
9567 deg
Eccentricity:
0004567
Arg of perigee: 219
2621 deg
Mean anomaly: 140
8201 deg
Mean motion: 15
53685167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 325
Coasting Arc #14 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2018/364/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 950686
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3527033
27 A = 6790492
26 meter
Y = -5789759
59 meter E =
0012559
Z = -211263
02 I = 51
98523
XDOT = 3940
428391 Wp = 157
19080
YDOT = 2616
009589 meter/sec RA = 119
95330 deg
ZDOT = -6038
465578 TA = 25
07493
MA = 25
01399
Ha = 221
062 n
mi
Hp = 216
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11571631
48 X = 3592540
05
Y = -18995274
26 feet Y = -5749951
57 meter
Z = -693120
13 Z = -193971
22
XDOT = 12927
914669 XDOT = 3940
214090
YDOT = 8582
708625 feet/sec YDOT = 2660
073330 meter/sec
ZDOT = -19811
238773 ZDOT = -6019
324831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8877721
39 X = 2705929
48
Y = 20396372
15 feet Y = 6216814
23 meter
Z = -614475
95 Z = -187292
27
XDOT = -13044
878472 XDOT = -3976
078958
YDOT = 5098
254230 feet/sec YDOT = 1553
947889 meter/sec
ZDOT = -19725
156847 ZDOT = -6012
227807
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 18364
41237964
00016717 00000-0 10270-3 0 9139
2 25544 51
6364 120
8298 0004477 226
1184 133
9599 15
53724160 29029
Satellite: ISS
Catalog Number: 25544
Epoch time: 18364
41237964 = yrday
fracday
Element set: 913
Inclination: 51
6364 deg
RA of node: 120
8298 deg
Eccentricity:
0004477
Arg of perigee: 226
1184 deg
Mean anomaly: 133
9599 deg
Mean motion: 15
53724160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 322
Coasting Arc #15 (Orbit 2903)
---------------------------------------
Vector Time (GMT): 2018/364/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950686
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4930737
07 A = 6784075
10 meter
Y = -2443706
85 meter E =
0003438
Z = -3968696
72 I = 51
96920
XDOT = -25
599917 Wp = 118
07780
YDOT = 6510
139931 meter/sec RA = 119
29891 deg
ZDOT = -4044
631218 TA = 109
87585
MA = 109
83880
Ha = 221
291 n
mi
Hp = 216
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16176958
88 X = 4976974
55
Y = -8017410
93 feet Y = -2388309
17 meter
Z = -13020658
52 Z = -3944632
87
XDOT = -83
989229 XDOT = -78
749647
YDOT = 21358
726807 feet/sec YDOT = 6509
556700 meter/sec
ZDOT = -13269
787459 ZDOT = -4044
884302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11778588
64 X = 3590113
82
Y = 13786234
20 feet Y = 4202044
19 meter
Z = -12911817
10 Z = -3935521
85
XDOT = -19692
768726 XDOT = -6002
355908
YDOT = 4408
247243 feet/sec YDOT = 1343
633760 meter/sec
ZDOT = -13271
631931 ZDOT = -4045
193413
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 18364
54102148
00016717 00000-0 10270-3 0 9149
2 25544 51
6400 120
1896 0004816 223
6708 136
4064 15
53678236 29047
Satellite: ISS
Catalog Number: 25544
Epoch time: 18364
54102148 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 120
1896 deg
Eccentricity:
0004816
Arg of perigee: 223
6708 deg
Mean anomaly: 136
4064 deg
Mean motion: 15
53678236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 300
Coasting Arc #16 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2018/365/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950686
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4633751
10 A = 6780752
47 meter
Y = 1075309
40 meter E =
0007318
Z = 4832463
83 I = 51
97469
XDOT = 1028
443821 Wp = 156
56217
YDOT = -7150
005750 meter/sec RA = 114
33446 deg
ZDOT = 2569
288025 TA = 268
21915
MA = 268
30297
Ha = 221
072 n
mi
Hp = 216
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15202595
48 X = -4668904
60
Y = 3527917
97 feet Y = 1023294
68 meter
Z = 15854540
13 Z = 4809869
45
XDOT = 3374
159518 XDOT = 1095
840554
YDOT = -23458
024115 feet/sec YDOT = -7138
128313 meter/sec
ZDOT = 8429
422654 ZDOT = 2574
447037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7431481
61 X = -2265115
60
Y = -13840680
65 feet Y = -4218639
46 meter
Z = 15752466
40 Z = 4801351
76
XDOT = 22494
778870 XDOT = 6856
408600
YDOT = -2427
400421 feet/sec YDOT = -739
871648 meter/sec
ZDOT = 8453
489808 ZDOT = 2576
623694
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 18365
57014441
00016717 00000-0 10270-3 0 9152
2 25544 51
6409 115
0625 0004699 228
3844 131
6906 15
53717322 29201
Satellite: ISS
Catalog Number: 25544
Epoch time: 18365
57014441 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 115
0625 deg
Eccentricity:
0004699
Arg of perigee: 228
3844 deg
Mean anomaly: 131
6906 deg
Mean motion: 15
53717322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 307
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