[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 26th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 7 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
087/13:50:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
3
090/15:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
3
092/20:30:37
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
3
094/03:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
2
094/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 2564)
---------------------------------------
Vector Time (GMT): 2018/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4513885
12 A = 6782050
00 meter
Y = 2839265
78 meter E =
0006325
Z = -4197211
09 I = 51
98998
XDOT = -705
847610 Wp = 116
44920
YDOT = 6649
149661 meter/sec RA = 70
13377 deg
ZDOT = 3740
420787 TA = 191
83203
MA = 191
84689
Ha = 220
457 n
mi
Hp = 215
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14809334
38 X = 4502187
86
Y = 9315176
45 feet Y = 2889677
44 meter
Z = -13770377
61 Z = -4175313
02
XDOT = -2315
773000 XDOT = -798
316585
YDOT = 21814
795475 feet/sec YDOT = 6640
739632 meter/sec
ZDOT = 12271
721741 ZDOT = 3736
766984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15368793
05 X = 4684408
12
Y = 8518288
78 feet Y = 2596374
42 meter
Z = -13673008
18 Z = -4167532
89
XDOT = -625
921495 XDOT = -190
780872
YDOT = 20790
843188 feet/sec YDOT = 6337
049004 meter/sec
ZDOT = 12254
463392 ZDOT = 3735
160442
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 18085
50922039
00016717 00000-0 10270-3 0 9009
2 25544 51
6373 70
8887 0001657 261
5188 98
5776 15
54102035 25651
Satellite: ISS
Catalog Number: 25544
Epoch time: 18085
50922039 = yrday
fracday
Element set: 900
Inclination: 51
6373 deg
RA of node: 70
8887 deg
Eccentricity:
0001657
Arg of perigee: 261
5188 deg
Mean anomaly: 98
5776 deg
Mean motion: 15
54102035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2565
Checksum: 324
Coasting Arc #2 (Orbit 2580)
---------------------------------------
Vector Time (GMT): 2018/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4453270
42 A = 6785751
59 meter
Y = -4200733
17 meter E =
0011594
Z = 2914705
18 I = 51
99103
XDOT = 1831
213533 Wp = 100
14618
YDOT = -5464
100602 meter/sec RA = 65
17358 deg
ZDOT = -5062
065092 TA = 46
78913
MA = 46
69236
Ha = 220
403 n
mi
Hp = 215
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14610467
25 X = -4420123
66
Y = -13781932
96 feet Y = -4250347
10 meter
Z = 9562681
03 Z = 2893153
85
XDOT = 6007
918414 XDOT = 1916
767090
YDOT = -17926
839247 feet/sec YDOT = -5443
144817 meter/sec
ZDOT = -16607
825105 ZDOT = -5052
961490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15598383
62 X = -4754387
33
Y = -12724682
28 feet Y = -3878483
16 meter
Z = 9467057
99 Z = 2885559
28
XDOT = 3924
778370 XDOT = 1196
272447
YDOT = -17173
544005 feet/sec YDOT = -5234
496213 meter/sec
ZDOT = -16566
395293 ZDOT = -5049
437285
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 18086
53805200
00016717 00000-0 10270-3 0 9014
2 25544 51
6377 65
7592 0001741 268
2254 91
8699 15
54144908 25816
Satellite: ISS
Catalog Number: 25544
Epoch time: 18086
53805200 = yrday
fracday
Element set: 901
Inclination: 51
6377 deg
RA of node: 65
7592 deg
Eccentricity:
0001741
Arg of perigee: 268
2254 deg
Mean anomaly: 91
8699 deg
Mean motion: 15
54144908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2581
Checksum: 324
Coasting Arc #3 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2018/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4176957
92 A = 6788521
76 meter
Y = 5172698
34 meter E =
0007923
Z = -1351567
45 I = 51
98573
XDOT = -3004
962539 Wp = 28
25154
YDOT = 3948
359803 meter/sec RA = 60
22251 deg
ZDOT = 5845
147016 TA = 317
10209
MA = 317
16386
Ha = 220
405 n
mi
Hp = 215
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13703930
17 X = 4125370
10
Y = 16970795
08 feet Y = 5219119
36 meter
Z = -4434276
41 Z = -1331403
30
XDOT = -9858
800980 XDOT = -3077
283219
YDOT = 12953
936362 feet/sec YDOT = 3914
352528 meter/sec
ZDOT = 19176
991523 ZDOT = 5830
373994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15155168
11 X = 4619295
24
Y = 15713379
77 feet Y = 4789438
15 meter
Z = -4344993
75 Z = -1324354
10
XDOT = -7676
257191 XDOT = -2339
723192
YDOT = 12668
694348 feet/sec YDOT = 3861
418037 meter/sec
ZDOT = 19110
462267 ZDOT = 5824
868899
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 18087
50257849
00016717 00000-0 10270-3 0 9023
2 25544 51
6378 60
9511 0001610 269
6268 90
4700 15
54149216 25961
Satellite: ISS
Catalog Number: 25544
Epoch time: 18087
50257849 = yrday
fracday
Element set: 902
Inclination: 51
6378 deg
RA of node: 60
9511 deg
Eccentricity:
0001610
Arg of perigee: 269
6268 deg
Mean anomaly: 90
4700 deg
Mean motion: 15
54149216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 318
Coasting Arc #4 (Orbit 2597)
---------------------------------------
Vector Time (GMT): 2018/087/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 903546
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1006646
63 A = 6781128
52 meter
Y = 5081020
54 meter E =
0007813
Z = 4372099
22 I = 51
96156
XDOT = -5497
447265 Wp = 112
75892
YDOT = -4075
984526 meter/sec RA = 59
87797 deg
ZDOT = 3463
284830 TA = 302
22230
MA = 302
29802
Ha = 220
309 n
mi
Hp = 215
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3302646
43 X = -1084626
33
Y = 16670014
91 feet Y = 5069328
01 meter
Z = 14344157
56 Z = 4367019
36
XDOT = -18036
244309 XDOT = -5468
282577
YDOT = -13372
652643 feet/sec YDOT = -4137
297302 meter/sec
ZDOT = 11362
483039 ZDOT = 3436
651684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6143114
25 X = 1872421
22
Y = 15866007
64 feet Y = 4835959
13 meter
Z = 14320742
84 Z = 4364962
42
XDOT = -21307
105351 XDOT = -6494
405711
YDOT = -1922
504393 feet/sec YDOT = -585
979339 meter/sec
ZDOT = 11244
159583 ZDOT = 3427
219841
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 18087
63118087
00016717 00000-0 10270-3 0 9038
2 25544 51
6393 60
3099 0001832 271
4166 88
6777 15
54168056 25985
Satellite: ISS
Catalog Number: 25544
Epoch time: 18087
63118087 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 60
3099 deg
Eccentricity:
0001832
Arg of perigee: 271
4166 deg
Mean anomaly: 88
6777 deg
Mean motion: 15
54168056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2598
Checksum: 337
Coasting Arc #5 (Orbit 2612)
---------------------------------------
Vector Time (GMT): 2018/088/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 903546
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2185221
63 A = 6778217
19 meter
Y = -3872836
50 meter E =
0011824
Z = -5126293
08 I = 51
93412
XDOT = 5314
177347 Wp = 74
06159
YDOT = 5247
749572 meter/sec RA = 54
90418 deg
ZDOT = -1699
372519 TA = 179
57093
MA = 179
56991
Ha = 220
337 n
mi
Hp = 215
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7169362
30 X = 2253267
01
Y = -12706156
49 feet Y = -3848020
05 meter
Z = -16818546
85 Z = -5115512
33
XDOT = 17434
965049 XDOT = 5263
355229
YDOT = 17217
026155 feet/sec YDOT = 5306
891976 meter/sec
ZDOT = -5575
369158 ZDOT = -1673
682375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -986051
89 X = -300548
61
Y = -14611963
92 feet Y = -4453726
60 meter
Z = -16769850
88 Z = -5111450
55
XDOT = 23019
963896 XDOT = 7016
484995
YDOT = 4714
194070 feet/sec YDOT = 1436
886352 meter/sec
ZDOT = -5461
436298 ZDOT = -1664
645784
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 18088
59570550
00016717 00000-0 10270-3 0 9042
2 25544 51
6392 55
5013 0001749 278
9892 81
1063 15
54147951 26136
Satellite: ISS
Catalog Number: 25544
Epoch time: 18088
59570550 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 55
5013 deg
Eccentricity:
0001749
Arg of perigee: 278
9892 deg
Mean anomaly: 81
1063 deg
Mean motion: 15
54147951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2613
Checksum: 322
Coasting Arc #6 (Orbit 2628)
---------------------------------------
Vector Time (GMT): 2018/089/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 903546
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3366475
72 A = 6777236
97 meter
Y = 2487230
65 meter E =
0001084
Z = 5329826
07 I = 51
91218
XDOT = -4793
073988 Wp = 28
57669
YDOT = -5982
614015 meter/sec RA = 49
92482 deg
ZDOT = -234
637507 TA = 63
65656
MA = 63
64543
Ha = 220
355 n
mi
Hp = 215
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11044867
86 X = -3419927
84
Y = 8160205
56 feet Y = 2449286
28 meter
Z = 17486306
00 Z = 5313342
76
XDOT = -15725
308361 XDOT = -4724
678797
YDOT = -19627
998737 feet/sec YDOT = -6035
831080 meter/sec
ZDOT = -769
808094 ZDOT = -257
753588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4539221
90 X = -1383554
84
Y = 13059647
03 feet Y = 3980580
42 meter
Z = 17412353
15 Z = 5307285
24
XDOT = -23139
913189 XDOT = -7053
045540
YDOT = -6875
917671 feet/sec YDOT = -2095
779706 meter/sec
ZDOT = -872
127637 ZDOT = -265
824504
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 18089
62452593
00016717 00000-0 10270-3 0 9054
2 25544 51
6401 50
3733 0001973 282
3159 77
7772 15
54174275 26297
Satellite: ISS
Catalog Number: 25544
Epoch time: 18089
62452593 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 50
3733 deg
Eccentricity:
0001973
Arg of perigee: 282
3159 deg
Mean anomaly: 77
7772 deg
Mean motion: 15
54174275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2629
Checksum: 325
Coasting Arc #7 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2018/090/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 903546
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4472840
65 A = 6778826
56 meter
Y = -1065560
92 meter E =
0010624
Z = -4990786
98 I = 51
89592
XDOT = 3879
451940 Wp = 105
02133
YDOT = 6247
341025 meter/sec RA = 44
94318 deg
ZDOT = 2144
119553 TA = 185
80975
MA = 185
82208
Ha = 220
353 n
mi
Hp = 215
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14674674
05 X = 4508666
29
Y = -3495934
79 feet Y = -1015342
93 meter
Z = -16373973
03 Z = -4968972
26
XDOT = 12727
860694 XDOT = 3798
889114
YDOT = 20496
525673 feet/sec YDOT = 6290
273575 meter/sec
ZDOT = 7034
512970 ZDOT = 2162
768076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9975696
65 X = 3040592
34
Y = -11455907
71 feet Y = -3491760
67 meter
Z = -16276432
85 Z = -4961056
73
XDOT = 21414
084528 XDOT = 6527
012964
YDOT = 8540
919557 feet/sec YDOT = 2603
272281 meter/sec
ZDOT = 7116
833399 ZDOT = 2169
210820
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 18090
58904254
00016717 00000-0 10270-3 0 9068
2 25544 51
6408 45
5642 0001810 289
1778 70
9178 15
54157832 26443
Satellite: ISS
Catalog Number: 25544
Epoch time: 18090
58904254 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 45
5642 deg
Eccentricity:
0001810
Arg of perigee: 289
1778 deg
Mean anomaly: 70
9178 deg
Mean motion: 15
54157832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2644
Checksum: 325
Coasting Arc #8 (Orbit 2644)
---------------------------------------
Vector Time (GMT): 2018/090/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903546
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3433651
27 A = 6787682
37 meter
Y = -5526397
41 meter E =
0005490
Z = -1925905
28 I = 51
92579
XDOT = 5065
368421 Wp = 151
08300
YDOT = -1189
268867 meter/sec RA = 44
73843 deg
ZDOT = -5629
674307 TA = 50
05144
MA = 50
00323
Ha = 220
327 n
mi
Hp = 215
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11265260
07 X = -3362243
34
Y = -18131225
09 feet Y = -5564395
86 meter
Z = -6318586
88 Z = -1942410
60
XDOT = 16618
662797 XDOT = 5105
636747
YDOT = -3901
800744 feet/sec YDOT = -1132
400066 meter/sec
ZDOT = -18470
060062 ZDOT = -5604
970471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21237119
56 X = -6473074
04
Y = -1925127
24 feet Y = -586778
78 meter
Z = -6391446
32 Z = -1948112
84
XDOT = 6799
522565 XDOT = 2072
494478
YDOT = -14177
450172 feet/sec YDOT = -4321
286812 meter/sec
ZDOT = -18359
604493 ZDOT = -5596
007450
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 18090
65334363
00016717 00000-0 10270-3 0 9075
2 25544 51
6421 45
2444 0001840 285
7547 74
3403 15
54140456 26458
Satellite: ISS
Catalog Number: 25544
Epoch time: 18090
65334363 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 45
2444 deg
Eccentricity:
0001840
Arg of perigee: 285
7547 deg
Mean anomaly: 74
3403 deg
Mean motion: 15
54140456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2645
Checksum: 297
Coasting Arc #9 (Orbit 2660)
---------------------------------------
Vector Time (GMT): 2018/091/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903546
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2302459
35 A = 6784304
73 meter
Y = 5391448
90 meter E =
0010789
Z = 3404290
04 I = 51
89016
XDOT = -6096
335825 Wp = 86
02971
YDOT = -336
098358 meter/sec RA = 39
77899 deg
ZDOT = 4643
564729 TA = 313
62886
MA = 313
71830
Ha = 220
369 n
mi
Hp = 215
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7554000
49 X = 2225463
22
Y = 17688480
65 feet Y = 5416766
52 meter
Z = 11168930
57 Z = 3415286
94
XDOT = -20001
101787 XDOT = -6114
680530
YDOT = -1102
684900 feet/sec YDOT = -404
373748 meter/sec
ZDOT = 15234
792419 ZDOT = 4613
906141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18711371
39 X = 5703226
00
Y = 4330025
31 feet Y = 1319791
71 meter
Z = 11217207
45 Z = 3419004
83
XDOT = -12377
268722 XDOT = -3772
591506
YDOT = 14261
229020 feet/sec YDOT = 4346
822605 meter/sec
ZDOT = 15102
455374 ZDOT = 4603
228398
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 18091
68215715
00016717 00000-0 10270-3 0 9089
2 25544 51
6418 40
1157 0001781 293
8284 66
2682 15
54151368 26612
Satellite: ISS
Catalog Number: 25544
Epoch time: 18091
68215715 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 40
1157 deg
Eccentricity:
0001781
Arg of perigee: 293
8284 deg
Mean anomaly: 66
2682 deg
Mean motion: 15
54151368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2661
Checksum: 315
Coasting Arc #10 (Orbit 2675)
---------------------------------------
Vector Time (GMT): 2018/092/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903546
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -878726
43 A = 6780391
05 meter
Y = -4960510
22 meter E =
0008598
Z = -4546860
91 I = 51
85236
XDOT = 6773
129096 Wp = 59
89858
YDOT = 1691
331709 meter/sec RA = 34
80829 deg
ZDOT = -3154
427767 TA = 178
52888
MA = 178
52634
Ha = 220
284 n
mi
Hp = 215
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2882960
74 X = -801104
89
Y = -16274639
82 feet Y = -4969903
24 meter
Z = -14917522
68 Z = -4550940
41
XDOT = 22221
552151 XDOT = 6769
035460
YDOT = 5548
988545 feet/sec YDOT = 1767
050258 meter/sec
ZDOT = -10349
172463 ZDOT = -3121
536089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14933666
90 X = -4551781
67
Y = -7045559
66 feet Y = -2147486
59 meter
Z = -14934976
69 Z = -4552180
90
XDOT = 16806
617306 XDOT = 5122
656955
YDOT = -13997
594271 feet/sec YDOT = -4266
466734 meter/sec
ZDOT = -10202
620646 ZDOT = -3109
758773
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 18092
64666480
00016717 00000-0 10270-3 0 9096
2 25544 51
6427 35
3085 0001978 295
2406 64
8542 15
54185321 26769
Satellite: ISS
Catalog Number: 25544
Epoch time: 18092
64666480 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 35
3085 deg
Eccentricity:
0001978
Arg of perigee: 295
2406 deg
Mean anomaly: 64
8542 deg
Mean motion: 15
54185321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2676
Checksum: 329
Coasting Arc #11 (Orbit 2679)
---------------------------------------
Vector Time (GMT): 2018/092/20:30:37
000
Vector Time (MET): N/A
Weight (LBS) : 903546
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1701343
33 A = 6777471
77 meter
Y = 3869281
03 meter E =
0001174
Z = 5297121
43 I = 51
83128
XDOT = -6629
733640 Wp = 119
86752
YDOT = -3801
578618 meter/sec RA = 33
64516 deg
ZDOT = 646
829363 TA = 323
97049
MA = 323
97840
Ha = 220
492 n
mi
Hp = 215
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5581835
07 X = -1770215
11
Y = 12694491
58 feet Y = 3849870
92 meter
Z = 17379007
33 Z = 5288689
13
XDOT = -21751
094620 XDOT = -6589
872604
YDOT = -12472
370795 feet/sec YDOT = -3875
493917 meter/sec
ZDOT = 2122
143578 ZDOT = 614
721336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12736807
68 X = 3882178
98
Y = -5604278
78 feet Y = -1708184
17 meter
Z = 17340780
97 Z = 5285470
04
XDOT = 7384
733946 XDOT = 2250
866907
YDOT = 22914
841428 feet/sec YDOT = 6984
443667 meter/sec
ZDOT = 1979
414268 ZDOT = 603
325469
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 18092
90386757
00016717 00000-0 10270-3 0 9103
2 25544 51
6382 34
0215 0001739 290
5108 69
5858 15
54127122 26804
Satellite: ISS
Catalog Number: 25544
Epoch time: 18092
90386757 = yrday
fracday
Element set: 910
Inclination: 51
6382 deg
RA of node: 34
0215 deg
Eccentricity:
0001739
Arg of perigee: 290
5108 deg
Mean anomaly: 69
5858 deg
Mean motion: 15
54127122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2680
Checksum: 311
Coasting Arc #12 (Orbit 2694)
---------------------------------------
Vector Time (GMT): 2018/093/20:30:37
000
Vector Time (MET): N/A
Weight (LBS) : 903546
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3256938
65 A = 6777800
91 meter
Y = -2887854
39 meter E =
0012389
Z = -5206228
22 I = 51
80588
XDOT = 6067
454380 Wp = 98
26520
YDOT = 4487
966767 meter/sec RA = 28
65730 deg
ZDOT = 1307
190952 TA = 184
27157
MA = 184
28216
Ha = 220
397 n
mi
Hp = 215
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10685494
25 X = 3314278
73
Y = -9474587
88 feet Y = -2851112
89 meter
Z = -17080801
26 Z = -5190267
47
XDOT = 19906
346391 XDOT = 6010
468058
YDOT = 14724
300416 feet/sec YDOT = 4555
498699 meter/sec
ZDOT = 4288
684225 ZDOT = 1336
526043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14366257
18 X = -4378835
19
Y = 42488
89 feet Y = 12950
61 meter
Z = -17009121
78 Z = -5184380
32
XDOT = -5296
601681 XDOT = -1614
404192
YDOT = -23115
318372 feet/sec YDOT = -7045
549040 meter/sec
ZDOT = 4418
916510 ZDOT = 1346
885752
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 18093
86836948
00016717 00000-0 10270-3 0 9112
2 25544 51
6393 29
2132 0001587 292
8211 67
2774 15
54181882 26952
Satellite: ISS
Catalog Number: 25544
Epoch time: 18093
86836948 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 29
2132 deg
Eccentricity:
0001587
Arg of perigee: 292
8211 deg
Mean anomaly: 67
2774 deg
Mean motion: 15
54181882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2695
Checksum: 338
Coasting Arc #13 (Orbit 2699)
---------------------------------------
Vector Time (GMT): 2018/094/03:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 903546
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1275327
25 A = 6777256
31 meter
Y = 4031187
09 meter E =
0000959
Z = 5295923
97 I = 51
79863
XDOT = -7008
696985 Wp = 116
04112
YDOT = -3049
797197 meter/sec RA = 27
25384 deg
ZDOT = 633
180290 TA = 327
92566
MA = 327
93149
Ha = 220
322 n
mi
Hp = 215
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4184144
54 X = -1346035
37
Y = 13225679
42 feet Y = 4016530
57 meter
Z = 17375078
63 Z = 5289556
75
XDOT = -22994
412679 XDOT = -6977
148108
YDOT = -10005
896316 feet/sec YDOT = -3127
996819 meter/sec
ZDOT = 2077
363155 ZDOT = 599
211002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9687365
43 X = -2952708
98
Y = -9979425
65 feet Y = -3041728
94 meter
Z = 17346037
98 Z = 5287072
38
XDOT = 18866
372557 XDOT = 5750
470355
YDOT = -14963
236199 feet/sec YDOT = -4560
794393 meter/sec
ZDOT = 1926
230040 ZDOT = 587
114916
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 18094
18986751
00016717 00000-0 10270-3 0 9127
2 25544 51
6418 27
6132 0001920 292
7819 67
3131 15
54198530 27009
Satellite: ISS
Catalog Number: 25544
Epoch time: 18094
18986751 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 27
6132 deg
Eccentricity:
0001920
Arg of perigee: 292
7819 deg
Mean anomaly: 67
3131 deg
Mean motion: 15
54198530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2700
Checksum: 310
Coasting Arc #14 (Orbit 2704)
---------------------------------------
Vector Time (GMT): 2018/094/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925333
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1186964
85 A = 6779538
23 meter
Y = 4704017
10 meter E =
0005745
Z = 4732225
25 I = 51
79573
XDOT = -7086
006075 Wp = 116
06539
YDOT = -996
120133 meter/sec RA = 25
69039 deg
ZDOT = 2762
474144 TA = 306
62989
MA = 306
68270
Ha = 220
277 n
mi
Hp = 215
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3894241
62 X = 1111288
15
Y = 15433126
98 feet Y = 4716867
77 meter
Z = 15525673
38 Z = 4737807
01
XDOT = -23248
051428 XDOT = -7087
759317
YDOT = -3268
110674 feet/sec YDOT = -1075
370330 meter/sec
ZDOT = 9063
235382 ZDOT = 2728
048266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2935473
88 X = 894732
44
Y = 15619797
91 feet Y = 4760914
40 meter
Z = 15549854
23 Z = 4739595
57
XDOT = -21952
960767 XDOT = -6691
262442
YDOT = -4760
678227 feet/sec YDOT = -1451
054724 meter/sec
ZDOT = 8909
749799 ZDOT = 2715
691739
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 18094
51136765
00016717 00000-0 10270-3 0 9137
2 25544 51
6403 26
0115 0001971 301
1411 58
9548 15
54215732 27053
Satellite: ISS
Catalog Number: 25544
Epoch time: 18094
51136765 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 26
0115 deg
Eccentricity:
0001971
Arg of perigee: 301
1411 deg
Mean anomaly: 58
9548 deg
Mean motion: 15
54215732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2705
Checksum: 284
Coasting Arc #15 (Orbit 2719)
---------------------------------------
Vector Time (GMT): 2018/095/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925333
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 528527
63 A = 6777421
53 meter
Y = -4241329
08 meter E =
0013176
Z = -5271243
27 I = 51
75806
XDOT = 7333
494298 Wp = 77
16578
YDOT = 2021
415303 meter/sec RA = 20
70208 deg
ZDOT = -890
182749 TA = 184
31831
MA = 184
32969
Ha = 220
401 n
mi
Hp = 215
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1734014
54 X = 601521
18
Y = -13915121
67 feet Y = -4235010
90 meter
Z = -17294105
22 Z = -5268498
31
XDOT = 24060
020664 XDOT = 7314
669316
YDOT = 6631
939972 feet/sec YDOT = 2103
318174 meter/sec
ZDOT = -2920
547076 ZDOT = -854
604726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2374493
73 X = 723745
69
Y = -13836390
60 feet Y = -4217331
86 meter
Z = -17281191
15 Z = -5267307
06
XDOT = 22801
075627 XDOT = 6949
767851
YDOT = 7366
717808 feet/sec YDOT = 2245
375588 meter/sec
ZDOT = -2762
089492 ZDOT = -841
884877
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 18095
47586548
00016717 00000-0 10270-3 0 9142
2 25544 51
6402 21
2031 0001945 307
4811 52
6164 15
54186917 27204
Satellite: ISS
Catalog Number: 25544
Epoch time: 18095
47586548 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 21
2031 deg
Eccentricity:
0001945
Arg of perigee: 307
4811 deg
Mean anomaly: 52
6164 deg
Mean motion: 15
54186917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2720
Checksum: 300
Coasting Arc #16 (Orbit 2735)
---------------------------------------
Vector Time (GMT): 2018/096/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925333
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2286665
03 A = 6777544
36 meter
Y = 3646760
21 meter E =
0003864
Z = 5234348
35 I = 51
72804
XDOT = -7034
334131 Wp = 24
99549
YDOT = -2860
634275 meter/sec RA = 15
70961 deg
ZDOT = -1076
292497 TA = 75
32277
MA = 75
27994
Ha = 220
474 n
mi
Hp = 215
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7502181
84 X = -2352700
00
Y = 11964436
38 feet Y = 3620820
19 meter
Z = 17173058
90 Z = 5223079
89
XDOT = -23078
524052 XDOT = -6996
594840
YDOT = -9385
283054 feet/sec YDOT = -2939
086080 meter/sec
ZDOT = -3531
143363 ZDOT = -1110
371254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7861730
48 X = -2396255
45
Y = 11805419
34 feet Y = 3598291
81 meter
Z = 17122198
76 Z = 5218846
18
XDOT = -21994
424323 XDOT = -6703
900534
YDOT = -9287
938600 feet/sec YDOT = -2830
963685 meter/sec
ZDOT = -3682
768660 ZDOT = -1122
507888
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 18096
50465551
00016717 00000-0 10270-3 0 9158
2 25544 51
6408 16
0750 0002071 311
1883 48
9091 15
54204395 27367
Satellite: ISS
Catalog Number: 25544
Epoch time: 18096
50465551 = yrday
fracday
Element set: 915
Inclination: 51
6408 deg
RA of node: 16
0750 deg
Eccentricity:
0002071
Arg of perigee: 311
1883 deg
Mean anomaly: 48
9091 deg
Mean motion: 15
54204395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2736
Checksum: 299
Coasting Arc #17 (Orbit 2750)
---------------------------------------
Vector Time (GMT): 2018/097/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925333
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3922990
89 A = 6780024
57 meter
Y = -2998217
80 meter E =
0008597
Z = -4654633
80 I = 51
70426
XDOT = 6149
212105 Wp = 103
18310
YDOT = 3512
621353 meter/sec RA = 10
71722 deg
ZDOT = 2922
666900 TA = 195
88709
MA = 195
91408
Ha = 220
491 n
mi
Hp = 215
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12870705
01 X = 3978836
06
Y = -9836672
57 feet Y = -2954036
19 meter
Z = -15271108
27 Z = -4635441
42
XDOT = 20174
580396 XDOT = 6095
279164
YDOT = 11524
348271 feet/sec YDOT = 3581
084658 meter/sec
ZDOT = 9588
802164 ZDOT = 2952
406591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13005826
76 X = 3964176
00
Y = -9792160
57 feet Y = -2984650
54 meter
Z = -15184992
08 Z = -4628385
59
XDOT = 19356
074702 XDOT = 5899
731569
YDOT = 10647
390829 feet/sec YDOT = 3245
324725 meter/sec
ZDOT = 9720
953199 ZDOT = 2962
946535
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 18097
46914095
00016717 00000-0 10270-3 0 9167
2 25544 51
6408 11
2659 0002010 317
4345 42
6652 15
54208629 27512
Satellite: ISS
Catalog Number: 25544
Epoch time: 18097
46914095 = yrday
fracday
Element set: 916
Inclination: 51
6408 deg
RA of node: 11
2659 deg
Eccentricity:
0002010
Arg of perigee: 317
4345 deg
Mean anomaly: 42
6652 deg
Mean motion: 15
54208629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2751
Checksum: 303
Coasting Arc #18 (Orbit 2766)
---------------------------------------
Vector Time (GMT): 2018/098/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925333
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5298734
65 A = 6783832
86 meter
Y = 2291522
40 meter E =
0011030
Z = 3555307
82 I = 51
68447
XDOT = -4752
643902 Wp = 79
16370
YDOT = -4029
074471 meter/sec RA = 5
73313 deg
ZDOT = -4472
524404 TA = 58
89728
MA = 58
78910
Ha = 220
568 n
mi
Hp = 215
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17384300
04 X = -5341235
11
Y = 7518118
12 feet Y = 2232030
85 meter
Z = 11664395
75 Z = 3529465
02
XDOT = -15592
663721 XDOT = -4685
511260
YDOT = -13218
748264 feet/sec YDOT = -4081
846671 meter/sec
ZDOT = -14673
636496 ZDOT = -4495
447884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17356450
11 X = -5290245
99
Y = 7757242
40 feet Y = 2364407
48 meter
Z = 11548720
54 Z = 3520050
02
XDOT = -15109
171713 XDOT = -4605
275538
YDOT = -11740
980250 feet/sec YDOT = -3578
650780 meter/sec
ZDOT = -14775
283904 ZDOT = -4503
506534
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 18098
49792093
00016717 00000-0 10270-3 0 9174
2 25544 51
6408 6
1377 0002051 319
9740 40
1261 15
54211572 27670
Satellite: ISS
Catalog Number: 25544
Epoch time: 18098
49792093 = yrday
fracday
Element set: 917
Inclination: 51
6408 deg
RA of node: 6
1377 deg
Eccentricity:
0002051
Arg of perigee: 319
9740 deg
Mean anomaly: 40
1261 deg
Mean motion: 15
54211572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2767
Checksum: 308
Coasting Arc #19 (Orbit 2781)
---------------------------------------
Vector Time (GMT): 2018/099/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925333
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6256101
05 A = 6787267
14 meter
Y = -1576044
61 meter E =
0007276
Z = -2097255
08 I = 51
66374
XDOT = 2960
206216 Wp = 23
70914
YDOT = 4411
263329 meter/sec RA =
75615 deg
ZDOT = 5528
478339 TA = 313
07890
MA = 313
13978
Ha = 220
551 n
mi
Hp = 215
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20525265
91 X = 6283447
21
Y = -5170750
02 feet Y = -1505931
80 meter
Z = -6880758
13 Z = -2066798
59
XDOT = 9711
962652 XDOT = 2883
803814
YDOT = 14472
648718 feet/sec YDOT = 4443
939519 meter/sec
ZDOT = 18138
052293 ZDOT = 5542
672177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20400765
63 X = 6218153
36
Y = -5804043
88 feet Y = -1769072
58 meter
Z = -6744617
49 Z = -2055759
41
XDOT = 9611
097096 XDOT = 2929
462395
YDOT = 12683
307083 feet/sec YDOT = 3865
871999 meter/sec
ZDOT = 18200
684045 ZDOT = 5547
568497
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 18099
46239722
00016717 00000-0 10270-3 0 9188
2 25544 51
6413 1
3291 0002108 321
7923 38
3080 15
54220061 27823
Satellite: ISS
Catalog Number: 25544
Epoch time: 18099
46239722 = yrday
fracday
Element set: 918
Inclination: 51
6413 deg
RA of node: 1
3291 deg
Eccentricity:
0002108
Arg of perigee: 321
7923 deg
Mean anomaly: 38
3080 deg
Mean motion: 15
54220061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2782
Checksum: 285
Coasting Arc #20 (Orbit 2797)
---------------------------------------
Vector Time (GMT): 2018/100/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925333
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6726121
02 A = 6789031
30 meter
Y = 798826
87 meter E =
0010737
Z = 381943
16 I = 51
63765
XDOT = -904
006023 Wp = 127
86089
YDOT = -4692
651441 meter/sec RA = 355
78513 deg
ZDOT = -5996
558084 TA = 48
02167
MA = 47
93025
Ha = 220
564 n
mi
Hp = 214
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22067326
20 X = -6736409
10
Y = 2620823
06 feet Y = 723553
26 meter
Z = 1253094
36 Z = 349244
97
XDOT = -2965
899024 XDOT = -822
336216
YDOT = -15395
838060 feet/sec YDOT = -4702
304424 meter/sec
ZDOT = -19673
746994 ZDOT = -6000
750748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21923617
05 X = -6682318
48
Y = 3679024
92 feet Y = 1121366
79 meter
Z = 1107084
21 Z = 337439
27
XDOT = -3304
458409 XDOT = -1007
198923
YDOT = -13644
556995 feet/sec YDOT = -4158
860972 meter/sec
ZDOT = -19691
711787 ZDOT = -6002
033753
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 18100
49116612
00016717 00000-0 10270-3 0 9197
2 25544 51
6422 356
2000 0002057 326
7228 33
3795 15
54214225 27989
Satellite: ISS
Catalog Number: 25544
Epoch time: 18100
49116612 = yrday
fracday
Element set: 919
Inclination: 51
6422 deg
RA of node: 356
2000 deg
Eccentricity:
0002057
Arg of perigee: 326
7228 deg
Mean anomaly: 33
3795 deg
Mean motion: 15
54214225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2798
Checksum: 290
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