[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 23rd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
023/19:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 213
7
029/16:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
3
030/15:25:11
379 1
1 1
1 1
1
N/A -0
5 -0
1 222
1
000/00:00:22
759 0
0 -0
0 213
8
037/00:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
6
Coasting Arc #1 (Orbit 1585)
---------------------------------------
Vector Time (GMT): 2018/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3927685
71 A = 6784765
03 meter
Y = 4522125
51 meter E =
0015247
Z = 3169674
28 I = 51
80379
XDOT = -5739
320421 Wp = 75
03004
YDOT = 1579
306108 meter/sec RA = 24
41823 deg
ZDOT = 4843
121681 TA = 321
49389
MA = 321
60258
Ha = 221
775 n
mi
Hp = 213
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12886107
98 X = 3861429
80
Y = 14836369
80 feet Y = 4565677
16 meter
Z = 10399193
82 Z = 3188592
35
XDOT = -18829
791406 XDOT = -5780
079072
YDOT = 5181
450484 feet/sec YDOT = 1514
897252 meter/sec
ZDOT = 15889
506828 ZDOT = 4815
143458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6143071
11 X = -1872408
07
Y = 18619595
66 feet Y = 5675252
76 meter
Z = 10482662
56 Z = 3195115
55
XDOT = -12817
220143 XDOT = -3906
688700
YDOT = -13132
574959 feet/sec YDOT = -4002
808847 meter/sec
ZDOT = 15764
639136 ZDOT = 4805
062009
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 18022
55770642
00016717 00000-0 10270-3 0 9006
2 25544 51
6386 24
7077 0003586 33
2975 326
8402 15
54208615 15861
Satellite: ISS
Catalog Number: 25544
Epoch time: 18022
55770642 = yrday
fracday
Element set: 900
Inclination: 51
6386 deg
RA of node: 24
7077 deg
Eccentricity:
0003586
Arg of perigee: 33
2975 deg
Mean anomaly: 326
8402 deg
Mean motion: 15
54208615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1586
Checksum: 311
Coasting Arc #2 (Orbit 1600)
---------------------------------------
Vector Time (GMT): 2018/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2478629
86 A = 6780930
98 meter
Y = -4545316
36 meter E =
0012363
Z = -4392143
21 I = 51
76074
XDOT = 6841
867583 Wp = 59
97220
YDOT = -435
767227 meter/sec RA = 19
44152 deg
ZDOT = -3411
279704 TA = 175
47974
MA = 175
46856
Ha = 221
953 n
mi
Hp = 213
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8131987
72 X = -2406284
22
Y = -14912455
27 feet Y = -4572629
65 meter
Z = -14409918
67 Z = -4404007
63
XDOT = 22447
072124 XDOT = 6862
801955
YDOT = -1429
682502 feet/sec YDOT = -359
139764 meter/sec
ZDOT = -11191
862547 ZDOT = -3377
993825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8413219
64 X = 2564349
35
Y = -14704611
34 feet Y = -4481965
54 meter
Z = -14461965
39 Z = -4408007
05
XDOT = 12044
209484 XDOT = 3671
075051
YDOT = 17748
694701 feet/sec YDOT = 5409
802145 meter/sec
ZDOT = -11043
565920 ZDOT = -3366
078892
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 18023
52219569
00016717 00000-0 10270-3 0 9011
2 25544 51
6389 19
8988 0003730 38
2323 321
9093 15
54190275 16015
Satellite: ISS
Catalog Number: 25544
Epoch time: 18023
52219569 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 19
8988 deg
Eccentricity:
0003730
Arg of perigee: 38
2323 deg
Mean anomaly: 321
9093 deg
Mean motion: 15
54190275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1601
Checksum: 310
Coasting Arc #3 (Orbit 1605)
---------------------------------------
Vector Time (GMT): 2018/023/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1744675
73 A = 6779422
29 meter
Y = -4508653
50 meter E =
0014331
Z = -4766600
82 I = 51
74949
XDOT = 7167
019696 Wp = 61
70175
YDOT = 74
869773 meter/sec RA = 17
83258 deg
ZDOT = -2693
637950 TA = 181
68247
MA = 181
68729
Ha = 221
844 n
mi
Hp = 213
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5724001
75 X = -1670975
70
Y = -14792170
27 feet Y = -4527751
63 meter
Z = -15638454
13 Z = -4774896
71
XDOT = 23513
844146 XDOT = 7178
733949
YDOT = 245
635739 feet/sec YDOT = 155
081770 meter/sec
ZDOT = -8837
394848 ZDOT = -2658
794979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15548956
25 X = -4739321
86
Y = -2944511
85 feet Y = -897487
21 meter
Z = -15674614
97 Z = -4777622
64
XDOT = 12319
826172 XDOT = 3755
083017
YDOT = -18830
229879 feet/sec YDOT = -5739
454067 meter/sec
ZDOT = -8682
256413 ZDOT = -2646
351755
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 18023
84369045
00016717 00000-0 10270-3 0 9022
2 25544 51
6424 18
2976 0003712 33
1058 327
0327 15
54216517 16064
Satellite: ISS
Catalog Number: 25544
Epoch time: 18023
84369045 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 18
2976 deg
Eccentricity:
0003712
Arg of perigee: 33
1058 deg
Mean anomaly: 327
0327 deg
Mean motion: 15
54216517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1606
Checksum: 290
Coasting Arc #4 (Orbit 1621)
---------------------------------------
Vector Time (GMT): 2018/024/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -31485
48 A = 6777302
58 meter
Y = 4258211
27 meter E =
0005306
Z = 5267853
90 I = 51
71056
XDOT = -7555
344969 Wp = 73
70943
YDOT = -1062
584657 meter/sec RA = 12
84032 deg
ZDOT = 814
546279 TA = 8
52198
MA = 8
51298
Ha = 221
959 n
mi
Hp = 213
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -103298
82 X = -104687
85
Y = 13970509
43 feet Y = 4257449
89 meter
Z = 17282985
24 Z = 5267523
15
XDOT = -24787
877194 XDOT = -7546
857937
YDOT = -3486
170134 feet/sec YDOT = -1147
026247 meter/sec
ZDOT = 2672
395927 ZDOT = 777
865958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11923060
20 X = 3634148
75
Y = 7287172
17 feet Y = 2221130
08 meter
Z = 17280773
71 Z = 5267179
83
XDOT = -15076
028262 XDOT = -4595
173414
YDOT = 18722
547049 feet/sec YDOT = 5706
632340 meter/sec
ZDOT = 2509
258822 ZDOT = 764
822089
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 18024
87247258
00016717 00000-0 10270-3 0 9038
2 25544 51
6423 13
1682 0003750 38
4209 321
7211 15
54208502 16225
Satellite: ISS
Catalog Number: 25544
Epoch time: 18024
87247258 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 13
1682 deg
Eccentricity:
0003750
Arg of perigee: 38
4209 deg
Mean anomaly: 321
7211 deg
Mean motion: 15
54208502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1622
Checksum: 277
Coasting Arc #5 (Orbit 1636)
---------------------------------------
Vector Time (GMT): 2018/025/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1850317
37 A = 6777546
15 meter
Y = -3915732
93 meter E =
0016406
Z = -5227346
41 I = 51
67778
XDOT = 7320
203621 Wp = 87
52009
YDOT = 1927
032764 meter/sec RA = 7
84324 deg
ZDOT = 1151
426593 TA = 193
50893
MA = 193
55290
Ha = 221
936 n
mi
Hp = 213
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6070595
05 X = 1919358
14
Y = -12846892
81 feet Y = -3894655
31 meter
Z = -17150086
63 Z = -5218190
64
XDOT = 24016
416081 XDOT = 7292
517990
YDOT = 6322
285971 feet/sec YDOT = 2008
737483 meter/sec
ZDOT = 3777
646302 ZDOT = 1186
918118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8126184
08 X = -2476860
91
Y = -11716646
17 feet Y = -3571233
75 meter
Z = -17108640
67 Z = -5214713
68
XDOT = 16479
720681 XDOT = 5023
018864
YDOT = -17157
693937 feet/sec YDOT = -5229
665112 meter/sec
ZDOT = 3935
329589 ZDOT = 1199
488459
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 18025
83695241
00016717 00000-0 10270-3 0 9045
2 25544 51
6409 8
3595 0003740 40
9086 319
2347 15
54226902 16370
Satellite: ISS
Catalog Number: 25544
Epoch time: 18025
83695241 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 8
3595 deg
Eccentricity:
0003740
Arg of perigee: 40
9086 deg
Mean anomaly: 319
2347 deg
Mean motion: 15
54226902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1637
Checksum: 309
Coasting Arc #6 (Orbit 1652)
---------------------------------------
Vector Time (GMT): 2018/026/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3571996
22 A = 6780057
93 meter
Y = 3464898
91 meter E =
0012017
Z = 4599138
61 I = 51
65449
XDOT = -6516
789259 Wp = 58
34803
YDOT = -2707
768618 meter/sec RA = 2
84829 deg
ZDOT = -3009
436377 TA = 61
72338
MA = 61
60216
Ha = 221
960 n
mi
Hp = 213
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11719147
69 X = -3632816
17
Y = 11367778
58 feet Y = 3424614
19 meter
Z = 15089037
45 Z = 4581639
63
XDOT = -21380
542189 XDOT = -6471
407790
YDOT = -8883
755309 feet/sec YDOT = -2780
389986 meter/sec
ZDOT = -9873
478927 ZDOT = -3040
982273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4332545
03 X = 1320559
72
Y = 15816353
71 feet Y = 4820824
61 meter
Z = 15010525
38 Z = 4575208
14
XDOT = -16843
090837 XDOT = -5133
774087
YDOT = 14154
494459 feet/sec YDOT = 4314
289911 meter/sec
ZDOT = -10013
451409 ZDOT = -3052
099989
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 18026
86572624
00016717 00000-0 10270-3 0 9059
2 25544 51
6416 3
2307 0003682 41
4603 318
6828 15
54259945 16537
Satellite: ISS
Catalog Number: 25544
Epoch time: 18026
86572624 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 3
2307 deg
Eccentricity:
0003682
Arg of perigee: 41
4603 deg
Mean anomaly: 318
6828 deg
Mean motion: 15
54259945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1653
Checksum: 310
Coasting Arc #7 (Orbit 1667)
---------------------------------------
Vector Time (GMT): 2018/027/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4997472
04 A = 6783914
76 meter
Y = -2964144
13 meter E =
0008013
Z = -3505799
60 I = 51
63327
XDOT = 5175
034452 Wp = 72
82993
YDOT = 3389
091252 meter/sec RA = 357
85871 deg
ZDOT = 4522
335000 TA = 245
95408
MA = 246
03795
Ha = 222
009 n
mi
Hp = 213
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16395905
63 X = 5047275
61
Y = -9724882
32 feet Y = -2907980
34 meter
Z = -11501967
19 Z = -3481403
06
XDOT = 16978
459489 XDOT = 5114
785236
YDOT = 11119
065788 feet/sec YDOT = 3446
624950 meter/sec
ZDOT = 14837
057085 ZDOT = 4547
327060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -992910
08 X = -302638
99
Y = -19102662
31 feet Y = -5822491
47 meter
Z = -11392836
74 Z = -3472536
64
XDOT = 16279
886858 XDOT = 4962
109514
YDOT = -9739
572333 feet/sec YDOT = -2968
621647 meter/sec
ZDOT = 14947
728280 ZDOT = 4556
067580
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 18027
83019921
00016717 00000-0 10270-3 0 9064
2 25544 51
6407 358
4207 0003682 46
6517 313
4942 15
54231999 16687
Satellite: ISS
Catalog Number: 25544
Epoch time: 18027
83019921 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 358
4207 deg
Eccentricity:
0003682
Arg of perigee: 46
6517 deg
Mean anomaly: 313
4942 deg
Mean motion: 15
54231999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1668
Checksum: 325
Coasting Arc #8 (Orbit 1683)
---------------------------------------
Vector Time (GMT): 2018/028/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6042306
47 A = 6787315
69 meter
Y = 2346525
38 meter E =
0016034
Z = 1993570
41 I = 51
61172
XDOT = -3410
975738 Wp = 99
63522
YDOT = -4020
962942 meter/sec RA = 352
87928 deg
ZDOT = -5569
878327 TA = 58
33769
MA = 58
18140
Ha = 222
010 n
mi
Hp = 213
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19823840
11 X = -6077780
43
Y = 7698574
07 feet Y = 2278757
71 meter
Z = 6540585
35 Z = 1964133
43
XDOT = -11190
865282 XDOT = -3338
703645
YDOT = -13192
135635 feet/sec YDOT = -4058
702409 meter/sec
ZDOT = -18273
879025 ZDOT = -5586
272081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2011041
90 X = -612965
57
Y = 21211099
71 feet Y = 6465143
19 meter
Z = 6409125
97 Z = 1953501
60
XDOT = -15207
153851 XDOT = -4635
140494
YDOT = 4137
647514 feet/sec YDOT = 1261
154962 meter/sec
ZDOT = -18346
160249 ZDOT = -5591
909644
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 18028
85896516
00016717 00000-0 10270-3 0 9071
2 25544 51
6402 353
2918 0003804 49
3597 310
7886 15
54265679 16845
Satellite: ISS
Catalog Number: 25544
Epoch time: 18028
85896516 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 353
2918 deg
Eccentricity:
0003804
Arg of perigee: 49
3597 deg
Mean anomaly: 310
7886 deg
Mean motion: 15
54265679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1684
Checksum: 350
Coasting Arc #9 (Orbit 1697)
---------------------------------------
Vector Time (GMT): 2018/029/16:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3123436
90 A = 6778462
92 meter
Y = 3387004
52 meter E =
0008295
Z = 4965170
49 I = 51
55549
XDOT = -6704
563678 Wp = 97
87413
YDOT = 3076
860143 meter/sec RA = 348
50221 deg
ZDOT = 2114
607291 TA = 331
50401
MA = 331
54934
Ha = 222
000 n
mi
Hp = 213
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10247496
40 X = 3061212
70
Y = 11112219
55 feet Y = 3421584
76 meter
Z = 16289929
44 Z = 4980191
79
XDOT = -21996
599994 XDOT = -6748
743096
YDOT = 10094
685510 feet/sec YDOT = 3001
637988 meter/sec
ZDOT = 6937
687962 ZDOT = 2081
932388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13637369
93 X = 4156670
36
Y = 6352231
22 feet Y = 1936160
08 meter
Z = 16356213
09 Z = 4985373
75
XDOT = -15991
852083 XDOT = -4874
316515
YDOT = 16809
715642 feet/sec YDOT = 5123
601328 meter/sec
ZDOT = 6791
690190 ZDOT = 2070
107170
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 18029
75913513
00016717 00000-0 10270-3 0 9089
2 25544 51
6424 348
8050 0003785 55
9633 304
1878 15
54231579 16983
Satellite: ISS
Catalog Number: 25544
Epoch time: 18029
75913513 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 348
8050 deg
Eccentricity:
0003785
Arg of perigee: 55
9633 deg
Mean anomaly: 304
1878 deg
Mean motion: 15
54231579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1698
Checksum: 336
Coasting Arc #10 (Orbit 1711)
---------------------------------------
Vector Time (GMT): 2018/030/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1594347
92 A = 6777621
57 meter
Y = -3926982
12 meter E =
0017326
Z = -5303922
39 I = 51
52124
XDOT = 7252
018511 Wp = 80
79729
YDOT = -2422
620186 meter/sec RA = 343
81896 deg
ZDOT = -384
618582 TA = 185
51358
MA = 185
53269
Ha = 222
063 n
mi
Hp = 213
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5230800
26 X = -1524553
86
Y = -12883799
60 feet Y = -3944420
78 meter
Z = -17401320
17 Z = -5311497
60
XDOT = 23792
711649 XDOT = 7280
438150
YDOT = -7948
228957 feet/sec YDOT = -2341
364227 meter/sec
ZDOT = -1261
871989 ZDOT = -349
322766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5180858
24 X = -1579125
59
Y = -12859280
96 feet Y = -3919508
84 meter
Z = -17434365
72 Z = -5313994
67
XDOT = 22822
425644 XDOT = 6956
275336
YDOT = -7690
417635 feet/sec YDOT = -2344
039295 meter/sec
ZDOT = -1104
325581 ZDOT = -336
598437
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 18030
65929924
00016717 00000-0 10270-3 0 9094
2 25544 51
6428 344
3163 0003036 49
9915 310
1504 15
54051236 17128
Satellite: ISS
Catalog Number: 25544
Epoch time: 18030
65929924 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 344
3163 deg
Eccentricity:
0003036
Arg of perigee: 49
9915 deg
Mean anomaly: 310
1504 deg
Mean motion: 15
54051236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1712
Checksum: 296
Coasting Arc #11 (Orbit 1727)
---------------------------------------
Vector Time (GMT): 2018/031/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -122246
95 A = 6778283
98 meter
Y = 4424440
28 meter E =
0007852
Z = 5129279
53 I = 51
49228
XDOT = -7357
745696 Wp = 53
21597
YDOT = 1559
761139 meter/sec RA = 338
81131 deg
ZDOT = -1514
566587 TA = 51
43118
MA = 51
36085
Ha = 222
025 n
mi
Hp = 213
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -401072
67 X = -196627
76
Y = 14515880
18 feet Y = 4422657
29 meter
Z = 16828344
91 Z = 5128505
10
XDOT = -24139
585616 XDOT = -7367
283777
YDOT = 5117
326570 feet/sec YDOT = 1477
428466 meter/sec
ZDOT = -4969
050483 ZDOT = -1550
330078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -188999
32 X = -57606
99
Y = 14525059
45 feet Y = 4427238
12 meter
Z = 16824142
07 Z = 5127998
50
XDOT = -22927
340805 XDOT = -6988
253477
YDOT = 5665
593007 feet/sec YDOT = 1726
872749 meter/sec
ZDOT = -5128
522730 ZDOT = -1563
173728
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 18031
68819154
00016717 00000-0 10270-3 0 9103
2 25544 51
6426 339
1882 0003005 51
8740 308
2683 15
54084544 17281
Satellite: ISS
Catalog Number: 25544
Epoch time: 18031
68819154 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 339
1882 deg
Eccentricity:
0003005
Arg of perigee: 51
8740 deg
Mean anomaly: 308
2683 deg
Mean motion: 15
54084544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1728
Checksum: 308
Coasting Arc #12 (Orbit 1742)
---------------------------------------
Vector Time (GMT): 2018/032/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1730691
45 A = 6781172
16 meter
Y = -4812306
21 meter E =
0011228
Z = -4463643
70 I = 51
47115
XDOT = 6916
687738 Wp = 97
52312
YDOT = -520
084353 meter/sec RA = 333
80688 deg
ZDOT = 3248
110594 TA = 205
27654
MA = 205
33152
Ha = 222
089 n
mi
Hp = 213
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5678121
57 X = 1806056
73
Y = -15788406
19 feet Y = -4792531
13 meter
Z = -14644500
33 Z = -4455053
70
XDOT = 22692
545071 XDOT = 6906
212257
YDOT = -1706
313493 feet/sec YDOT = -442
795712 meter/sec
ZDOT = 10656
530821 ZDOT = 3281
683051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5147391
25 X = 1568924
85
Y = -16005042
85 feet Y = -4878337
06 meter
Z = -14605450
74 Z = -4451741
38
XDOT = 21369
828552 XDOT = 6513
523743
YDOT = -2971
563551 feet/sec YDOT = -905
732570 meter/sec
ZDOT = 10806
064276 ZDOT = 3293
688391
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 18032
65277642
00016717 00000-0 10270-3 0 9112
2 25544 51
6424 334
3812 0002968 55
0805 305
0626 15
54049292 17434
Satellite: ISS
Catalog Number: 25544
Epoch time: 18032
65277642 = yrday
fracday
Element set: 911
Inclination: 51
6424 deg
RA of node: 334
3812 deg
Eccentricity:
0002968
Arg of perigee: 55
0805 deg
Mean anomaly: 305
0626 deg
Mean motion: 15
54049292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1743
Checksum: 300
Coasting Arc #13 (Orbit 1758)
---------------------------------------
Vector Time (GMT): 2018/033/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3159426
86 A = 6784914
56 meter
Y = 4999160
11 meter E =
0015311
Z = 3313979
35 I = 51
45512
XDOT = -6038
722765 Wp = 85
35502
YDOT = -701
668531 meter/sec RA = 328
80936 deg
ZDOT = -4678
732711 TA = 55
96016
MA = 55
81486
Ha = 222
157 n
mi
Hp = 213
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10365573
68 X = -3231191
14
Y = 16401443
95 feet Y = 4963428
13 meter
Z = 10872635
67 Z = 3298457
83
XDOT = -19812
082561 XDOT = -6007
701505
YDOT = -2302
062109 feet/sec YDOT = -769
024439 meter/sec
ZDOT = -15350
172936 ZDOT = -4707
990566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9491633
61 X = -2893049
93
Y = 16966937
13 feet Y = 5171522
44 meter
Z = 10802713
69 Z = 3292667
13
XDOT = -18571
979783 XDOT = -5660
739438
YDOT = -491
525752 feet/sec YDOT = -149
817049 meter/sec
ZDOT = -15480
288080 ZDOT = -4718
391807
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 18033
68166085
00016717 00000-0 10270-3 0 9125
2 25544 51
6428 329
2534 0003064 59
1240 301
0213 15
54065839 17598
Satellite: ISS
Catalog Number: 25544
Epoch time: 18033
68166085 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 329
2534 deg
Eccentricity:
0003064
Arg of perigee: 59
1240 deg
Mean anomaly: 301
0213 deg
Mean motion: 15
54065839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1759
Checksum: 297
Coasting Arc #14 (Orbit 1773)
---------------------------------------
Vector Time (GMT): 2018/034/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4250077
71 A = 6788052
53 meter
Y = -4949769
36 meter E =
0010108
Z = -1864269
63 I = 51
43795
XDOT = 4811
086037 Wp = 44
87458
YDOT = 2026
162683 meter/sec RA = 323
81857 deg
ZDOT = 5614
132074 TA = 294
55370
MA = 294
65902
Ha = 222
126 n
mi
Hp = 213
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13943824
50 X = 4314166
92
Y = -16239400
80 feet Y = -4901883
85 meter
Z = -6116370
17 Z = -1843468
73
XDOT = 15784
403009 XDOT = 4760
801507
YDOT = 6647
515363 feet/sec YDOT = 2079
682742 meter/sec
ZDOT = 18419
068483 ZDOT = 5637
379863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12747504
72 X = 3885439
44
Y = -17227399
33 feet Y = -5250911
32 meter
Z = -6022972
66 Z = -1835802
07
XDOT = 14854
259328 XDOT = 4527
578243
YDOT = 4545
697658 feet/sec YDOT = 1385
528646 meter/sec
ZDOT = 18522
208290 ZDOT = 5645
569087
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 18034
64623365
00016717 00000-0 10270-3 0 9132
2 25544 51
6425 324
4451 0003018 61
0735 299
0721 15
54074405 17746
Satellite: ISS
Catalog Number: 25544
Epoch time: 18034
64623365 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 324
4451 deg
Eccentricity:
0003018
Arg of perigee: 61
0735 deg
Mean anomaly: 299
0721 deg
Mean motion: 15
54074405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1774
Checksum: 292
Coasting Arc #15 (Orbit 1789)
---------------------------------------
Vector Time (GMT): 2018/035/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5009969
26 A = 6789599
01 meter
Y = 4571168
54 meter E =
0013916
Z = 179721
34 I = 51
41576
XDOT = -3348
277697 Wp = 121
59456
YDOT = -3420
981138 meter/sec RA = 318
83369 deg
ZDOT = -5990
322417 TA = 56
46339
MA = 56
33054
Ha = 222
174 n
mi
Hp = 213
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16436907
03 X = -5061585
93
Y = 14997272
10 feet Y = 4514855
03 meter
Z = 589636
94 Z = 155259
44
XDOT = -10985
163048 XDOT = -3280
677239
YDOT = -11223
691399 feet/sec YDOT = -3458
046299 meter/sec
ZDOT = -19653
288770 ZDOT = -6006
422462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15008677
64 X = -4574644
95
Y = 16430061
75 feet Y = 5007882
82 meter
Z = 480022
09 Z = 146310
73
XDOT = -10632
943828 XDOT = -3240
921279
YDOT = -9097
302418 feet/sec YDOT = -2772
857777 meter/sec
ZDOT = -19724
386478 ZDOT = -6011
992998
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 18035
67510876
00016717 00000-0 10270-3 0 9149
2 25544 51
6414 319
3171 0002971 68
5620 291
5850 15
54032490 17904
Satellite: ISS
Catalog Number: 25544
Epoch time: 18035
67510876 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 319
3171 deg
Eccentricity:
0002971
Arg of perigee: 68
5620 deg
Mean anomaly: 291
5850 deg
Mean motion: 15
54032490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1790
Checksum: 307
Coasting Arc #16 (Orbit 1805)
---------------------------------------
Vector Time (GMT): 2018/036/15:25:22
759
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5362230
20 A = 6788454
17 meter
Y = -3877636
82 meter E =
0016737
Z = 1478889
94 I = 51
38827
XDOT = 1824
712256 Wp = 62
62786
YDOT = 4734
174917 meter/sec RA = 313
84652 deg
ZDOT = 5754
239860 TA = 313
58009
MA = 313
71890
Ha = 222
011 n
mi
Hp = 213
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17592618
77 X = 5398008
90
Y = -12721905
57 feet Y = -3817472
54 meter
Z = 4852001
13 Z = 1505024
52
XDOT = 5986
588767 XDOT = 1743
687196
YDOT = 15532
069939 feet/sec YDOT = 4754
127411 meter/sec
ZDOT = 18878
739698 ZDOT = 5762
906459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16082973
08 X = 4902090
19
Y = -14544301
16 feet Y = -4433102
99 meter
Z = 4968934
70 Z = 1514531
30
XDOT = 6445
371659 XDOT = 1964
549282
YDOT = 13636
537285 feet/sec YDOT = 4156
416564 meter/sec
ZDOT = 18916
545496 ZDOT = 5765
763067
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 18036
70397587
00016717 00000-0 10270-3 0 9157
2 25544 51
6411 314
1883 0002857 67
9515 292
1941 15
54096791 18063
Satellite: ISS
Catalog Number: 25544
Epoch time: 18036
70397587 = yrday
fracday
Element set: 915
Inclination: 51
6411 deg
RA of node: 314
1883 deg
Eccentricity:
0002857
Arg of perigee: 67
9515 deg
Mean anomaly: 292
1941 deg
Mean motion: 15
54096791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1806
Checksum: 334
Coasting Arc #17 (Orbit 1810)
---------------------------------------
Vector Time (GMT): 2018/037/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4158134
62 A = 6778208
77 meter
Y = -1531503
97 meter E =
0016518
Z = -5143953
27 I = 51
34575
XDOT = 4110
385731 Wp = 78
72164
YDOT = -6294
135389 meter/sec RA = 312
01839 deg
ZDOT = -1449
501285 TA = 177
25206
MA = 177
24298
Ha = 222
066 n
mi
Hp = 213
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13642173
94 X = -4115713
65
Y = -5024619
31 feet Y = -1577766
18 meter
Z = -16876487
11 Z = -5164048
63
XDOT = 13485
517491 XDOT = 4187
503773
YDOT = -20650
050490 feet/sec YDOT = -6247
739124 meter/sec
ZDOT = -4755
581645 ZDOT = -1429
347099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6628845
37 X = 2020472
07
Y = 12821698
28 feet Y = 3908053
64 meter
Z = -16965670
89 Z = -5171136
49
XDOT = -22958
498561 XDOT = -6997
750361
YDOT = 5700
487262 feet/sec YDOT = 1737
508518 meter/sec
ZDOT = -4664
878220 ZDOT = -1421
854881
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 18037
02549707
00016717 00000-0 10270-3 0 9167
2 25544 51
6414 312
5825 0002695 78
5006 281
6449 15
54066480 18111
Satellite: ISS
Catalog Number: 25544
Epoch time: 18037
02549707 = yrday
fracday
Element set: 916
Inclination: 51
6414 deg
RA of node: 312
5825 deg
Eccentricity:
0002695
Arg of perigee: 78
5006 deg
Mean anomaly: 281
6449 deg
Mean motion: 15
54066480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1811
Checksum: 312
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