[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 22nd 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
080/17:44:23
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
082/19:41:00
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
086/11:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
4
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
2
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2902724
12 A = 6785294
85 meter
Y = 5275538
64 meter E =
0011552
Z = 3117611
58 I = 52
02179
XDOT = -3427
764444 Wp = 88
99643
YDOT = -4795
210057 meter/sec RA = 94
97970 deg
ZDOT = 4907
383748 TA = 306
68659
MA = 306
79269
Ha = 220
600 n
mi
Hp = 215
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9523373
09 X = -2976644
69
Y = 17308197
65 feet Y = 5242665
40 meter
Z = 10228384
44 Z = 3103330
97
XDOT = -11245
946340 XDOT = -3397
725962
YDOT = -15732
316461 feet/sec YDOT = -4833
373203 meter/sec
ZDOT = 16100
340379 ZDOT = 4890
806231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10164022
38 X = -3097994
02
Y = 16978665
96 feet Y = 5175097
39 meter
Z = 10163943
14 Z = 3097969
87
XDOT = -9581
610031 XDOT = -2920
474738
YDOT = -15360
635386 feet/sec YDOT = -4681
921666 meter/sec
ZDOT = 16026
965828 ZDOT = 4885
019184
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 18080
55793995
00016717 00000-0 10270-3 0 9006
2 25544 51
6388 95
5699 0001706 234
6422 125
4572 15
54116955 24883
Satellite: ISS
Catalog Number: 25544
Epoch time: 18080
55793995 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 95
5699 deg
Eccentricity:
0001706
Arg of perigee: 234
6422 deg
Mean anomaly: 125
4572 deg
Mean motion: 15
54116955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 343
Coasting Arc #2 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2018/080/17:44:23
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3603717
79 A = 6779436
59 meter
Y = 3073307
60 meter E =
0010490
Z = -4860579
78 I = 52
00340
XDOT = -2418
210744 Wp = 114
71803
YDOT = 6817
931851 meter/sec RA = 93
75061 deg
ZDOT = 2518
010784 TA = 179
93661
MA = 179
93647
Ha = 220
472 n
mi
Hp = 215
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11823221
08 X = 3592693
66
Y = 10083030
18 feet Y = 3113544
72 meter
Z = -15946784
06 Z = -4843101
16
XDOT = -7933
762283 XDOT = -2506
502224
YDOT = 22368
542818 feet/sec YDOT = 6790
396341 meter/sec
ZDOT = 8261
190237 ZDOT = 2506
048757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11194703
61 X = 3412145
66
Y = -10890558
56 feet Y = -3319442
25 meter
Z = -15869162
59 Z = -4836920
76
XDOT = 20691
527071 XDOT = 6306
777451
YDOT = 9310
666408 feet/sec YDOT = 2837
891121 meter/sec
ZDOT = 8206
892090 ZDOT = 2501
460709
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 18080
75084803
00016717 00000-0 10270-3 0 9010
2 25544 51
6392 94
6086 0001738 241
8795 118
2182 15
54125532 24918
Satellite: ISS
Catalog Number: 25544
Epoch time: 18080
75084803 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 94
6086 deg
Eccentricity:
0001738
Arg of perigee: 241
8795 deg
Mean anomaly: 118
2182 deg
Mean motion: 15
54125532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 312
Coasting Arc #3 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2018/081/17:44:23
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3136432
74 A = 6782991
86 meter
Y = -4579131
39 meter E =
0009587
Z = 3891707
83 I = 52
01643
XDOT = 3112
881117 Wp = 84
27489
YDOT = -5658
210250 meter/sec RA = 88
78634 deg
ZDOT = -4139
253221 TA = 48
97363
MA = 48
89080
Ha = 220
535 n
mi
Hp = 215
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10290133
65 X = -3103898
49
Y = -15023396
96 feet Y = -4614022
92 meter
Z = 12768070
31 Z = 3876551
44
XDOT = 10212
864557 XDOT = 3196
027810
YDOT = -18563
681921 feet/sec YDOT = -5622
935301 meter/sec
ZDOT = -13580
227104 ZDOT = -4123
929455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15805821
95 X = -4817614
53
Y = 9136351
57 feet Y = 2784759
96 meter
Z = 12701023
52 Z = 3871271
97
XDOT = -17012
721881 XDOT = -5185
477629
YDOT = -10605
029235 feet/sec YDOT = -3232
412911 meter/sec
ZDOT = -13511
056822 ZDOT = -4118
170119
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 18081
77968429
00016717 00000-0 10270-3 0 9029
2 25544 51
6393 89
4809 0001759 245
8628 114
2341 15
54120982 25071
Satellite: ISS
Catalog Number: 25544
Epoch time: 18081
77968429 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 89
4809 deg
Eccentricity:
0001759
Arg of perigee: 245
8628 deg
Mean anomaly: 114
2341 deg
Mean motion: 15
54120982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 334
Coasting Arc #4 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2018/082/17:44:23
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2612200
22 A = 6786611
12 meter
Y = 5724916
43 meter E =
0003596
Z = -2539186
99 I = 52
02766
XDOT = -3736
781775 Wp = 39
76339
YDOT = 4061
186830 meter/sec RA = 83
83091 deg
ZDOT = 5319
057708 TA = 291
89787
MA = 291
93609
Ha = 220
388 n
mi
Hp = 215
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8570210
68 X = 2560322
55
Y = 18782534
24 feet Y = 5753837
63 meter
Z = -8330665
98 Z = -2526624
17
XDOT = -12259
782728 XDOT = -3807
754567
YDOT = 13324
103773 feet/sec YDOT = 4019
003070 meter/sec
ZDOT = 17450
976733 ZDOT = 5300
733052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19288101
74 X = 5879013
41
Y = -7424256
85 feet Y = -2262913
49 meter
Z = -8275363
46 Z = -2522330
78
XDOT = 11977
734893 XDOT = 3650
813595
YDOT = 11783
394540 feet/sec YDOT = 3591
578656 meter/sec
ZDOT = 17368
610585 ZDOT = 5293
952506
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 18082
74421551
00016717 00000-0 10270-3 0 9038
2 25544 51
6400 84
6724 0001840 250
1601 109
9354 15
54134534 25224
Satellite: ISS
Catalog Number: 25544
Epoch time: 18082
74421551 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 84
6724 deg
Eccentricity:
0001840
Arg of perigee: 250
1601 deg
Mean anomaly: 109
9354 deg
Mean motion: 15
54134534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 276
Coasting Arc #5 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2018/082/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3434031
68 A = 6779486
20 meter
Y = 3269122
88 meter E =
0006189
Z = 4843508
46 I = 52
00491
XDOT = -2766
166064 Wp = 132
21301
YDOT = -6685
413452 meter/sec RA = 83
47068 deg
ZDOT = 2544
993266 TA = 292
85241
MA = 292
91775
Ha = 220
510 n
mi
Hp = 215
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11266508
13 X = -3493859
92
Y = 10725468
78 feet Y = 3230386
96 meter
Z = 15890775
78 Z = 4826681
59
XDOT = -9075
347979 XDOT = -2703
564619
YDOT = -21933
771167 feet/sec YDOT = -6715
996438 meter/sec
ZDOT = 8349
715439 ZDOT = 2531
708639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14589058
03 X = 4446744
89
Y = 5614743
49 feet Y = 1711373
82 meter
Z = 15815204
15 Z = 4820474
22
XDOT = -15419
066439 XDOT = -4699
731451
YDOT = 16652
880123 feet/sec YDOT = 5075
797862 meter/sec
ZDOT = 8291
322916 ZDOT = 2527
195225
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 18082
87281905
00016717 00000-0 10270-3 0 9040
2 25544 51
6414 84
0321 0001813 250
9613 109
1344 15
54121750 25246
Satellite: ISS
Catalog Number: 25544
Epoch time: 18082
87281905 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 84
0321 deg
Eccentricity:
0001813
Arg of perigee: 250
9613 deg
Mean anomaly: 109
1344 deg
Mean motion: 15
54121750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 280
Coasting Arc #6 (Orbit 2538)
---------------------------------------
Vector Time (GMT): 2018/083/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3920764
18 A = 6777407
02 meter
Y = -1560142
22 meter E =
0012788
Z = -5314535
86 I = 51
99355
XDOT = 2026
977489 Wp = 85
74110
YDOT = 7356
137803 meter/sec RA = 78
49705 deg
ZDOT = -664
538412 TA = 177
93963
MA = 177
93435
Ha = 220
281 n
mi
Hp = 215
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12863399
52 X = 3963733
85
Y = -5118576
84 feet Y = -1516057
58 meter
Z = -17436141
27 Z = -5295385
75
XDOT = 6650
188612 XDOT = 1947
796476
YDOT = 24134
310378 feet/sec YDOT = 7378
362094 meter/sec
ZDOT = -2180
244133 ZDOT = -654
884820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10390184
44 X = -3166928
22
Y = -9310892
72 feet Y = -2837960
10 meter
Z = -17350424
86 Z = -5288409
50
XDOT = 17914
735950 XDOT = 5460
411517
YDOT = -16009
747027 feet/sec YDOT = -4879
770894 meter/sec
ZDOT = -2138
168341 ZDOT = -651
713710
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 18083
83734520
00016717 00000-0 10270-3 0 9054
2 25544 51
6415 79
2237 0001881 259
0350 101
0591 15
54159138 25394
Satellite: ISS
Catalog Number: 25544
Epoch time: 18083
83734520 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 79
2237 deg
Eccentricity:
0001881
Arg of perigee: 259
0350 deg
Mean anomaly: 101
0591 deg
Mean motion: 15
54159138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2539
Checksum: 302
Coasting Arc #7 (Orbit 2554)
---------------------------------------
Vector Time (GMT): 2018/084/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4319153
76 A = 6777773
33 meter
Y = -223324
03 meter E =
0002640
Z = 5217612
35 I = 51
98671
XDOT = -1165
176025 Wp = 36
00455
YDOT = -7471
380578 meter/sec RA = 73
52117 deg
ZDOT = -1281
918730 TA = 66
25745
MA = 66
22977
Ha = 220
386 n
mi
Hp = 215
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14170451
95 X = -4341679
72
Y = -732690
40 feet Y = -271749
41 meter
Z = 17118150
74 Z = 5196576
84
XDOT = -3822
755988 XDOT = -1075
315575
YDOT = -24512
403471 feet/sec YDOT = -7483
908017 meter/sec
ZDOT = -4205
770111 ZDOT = -1287
359990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5967402
38 X = 1818864
24
Y = 12997470
29 feet Y = 3961628
94 meter
Z = 17024262
20 Z = 5188995
12
XDOT = -19019
359075 XDOT = -5797
100646
YDOT = 14281
789232 feet/sec YDOT = 4353
089358 meter/sec
ZDOT = -4229
010679 ZDOT = -1289
002455
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 18084
86617046
00016717 00000-0 10270-3 0 9062
2 25544 51
6409 74
0950 0001939 262
3396 97
7537 15
54171194 25558
Satellite: ISS
Catalog Number: 25544
Epoch time: 18084
86617046 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 74
0950 deg
Eccentricity:
0001939
Arg of perigee: 262
3396 deg
Mean anomaly: 97
7537 deg
Mean motion: 15
54171194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2555
Checksum: 334
Coasting Arc #8 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2018/085/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4611910
89 A = 6780434
89 meter
Y = 1921445
22 meter E =
0008164
Z = -4592103
33 I = 51
98462
XDOT = 157
378184 Wp = 115
63565
YDOT = 7007
939443 meter/sec RA = 68
54843 deg
ZDOT = 3091
178554 TA = 185
16718
MA = 185
17561
Ha = 220
245 n
mi
Hp = 215
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15130941
23 X = 4612387
81
Y = 6303954
12 feet Y = 1973021
09 meter
Z = -15065955
82 Z = -4569699
48
XDOT = 516
332626 XDOT = 63
986628
YDOT = 22991
927308 feet/sec YDOT = 7009
177412 meter/sec
ZDOT = 10141
661923 ZDOT = 3091
715659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1750396
39 X = -533520
82
Y = -16389547
54 feet Y = -4995534
09 meter
Z = -14966198
21 Z = -4561697
21
XDOT = 18781
410753 XDOT = 5724
573997
YDOT = -11265
521969 feet/sec YDOT = -3433
731096 meter/sec
ZDOT = 10143
061656 ZDOT = 3091
605193
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
83069329
00016717 00000-0 10270-3 0 9076
2 25544 51
6404 69
2865 0001969 266
4760 93
6167 15
54157156 25700
Satellite: ISS
Catalog Number: 25544
Epoch time: 18085
83069329 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 69
2865 deg
Eccentricity:
0001969
Arg of perigee: 266
4760 deg
Mean anomaly: 93
6167 deg
Mean motion: 15
54157156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2570
Checksum: 340
Coasting Arc #9 (Orbit 2579)
---------------------------------------
Vector Time (GMT): 2018/086/11:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4735231
12 A = 6781314
58 meter
Y = 2099315
50 meter E =
0007239
Z = -4384344
99 I = 51
97668
XDOT = 165
617324 Wp = 115
94201
YDOT = 6836
633528 meter/sec RA = 65
35220 deg
ZDOT = 3453
732072 TA = 188
95948
MA = 188
97241
Ha = 220
404 n
mi
Hp = 215
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15535535
17 X = 4732700
69
Y = 6887518
05 feet Y = 2152253
57 meter
Z = -14384333
95 Z = -4361349
45
XDOT = 543
363925 XDOT = 72
379678
YDOT = 22429
900025 feet/sec YDOT = 6837
964564 meter/sec
ZDOT = 11331
141967 ZDOT = 3454
309498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14354372
49 X = 4375212
73
Y = 9256208
10 feet Y = 2821292
23 meter
Z = -14281961
46 Z = -4353141
85
XDOT = -2385
898669 XDOT = -727
221914
YDOT = 21179
159367 feet/sec YDOT = 6455
407775 meter/sec
ZDOT = 11332
740817 ZDOT = 3454
219401
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
47370653
00016717 00000-0 10270-3 0 9083
2 25544 51
6379 66
0800 0001683 265
4649 94
6311 15
54125001 25800
Satellite: ISS
Catalog Number: 25544
Epoch time: 18086
47370653 = yrday
fracday
Element set: 908
Inclination: 51
6379 deg
RA of node: 66
0800 deg
Eccentricity:
0001683
Arg of perigee: 265
4649 deg
Mean anomaly: 94
6311 deg
Mean motion: 15
54125001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2580
Checksum: 307
Coasting Arc #10 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2018/087/11:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4850683
56 A = 6785036
57 meter
Y = -3523028
82 meter E =
0011148
Z = 3166788
51 I = 51
97454
XDOT = 1056
115839 Wp = 94
58164
YDOT = -5837
307896 meter/sec RA = 60
38908 deg
ZDOT = -4862
453742 TA = 49
05316
MA = 48
95673
Ha = 220
358 n
mi
Hp = 215
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15914316
16 X = -4826310
03
Y = -11558493
51 feet Y = -3577135
87 meter
Z = 10389726
07 Z = 3143285
38
XDOT = 3464
946979 XDOT = 1144
930729
YDOT = -19151
272625 feet/sec YDOT = -5825
001628 meter/sec
ZDOT = -15952
932225 ZDOT = -4857
107184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14206054
22 X = -4330005
33
Y = -13682519
05 feet Y = -4170431
81 meter
Z = 10285297
01 Z = 3134958
53
XDOT = 5220
081371 XDOT = 1591
080802
YDOT = -17427
654533 feet/sec YDOT = -5311
949102 meter/sec
ZDOT = -15928
218036 ZDOT = -4854
920857
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
50252300
00016717 00000-0 10270-3 0 9097
2 25544 51
6375 60
9503 0001785 274
1771 85
9178 15
54171558 25964
Satellite: ISS
Catalog Number: 25544
Epoch time: 18087
50252300 = yrday
fracday
Element set: 909
Inclination: 51
6375 deg
RA of node: 60
9503 deg
Eccentricity:
0001785
Arg of perigee: 274
1771 deg
Mean anomaly: 85
9178 deg
Mean motion: 15
54171558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 325
Coasting Arc #11 (Orbit 2597)
---------------------------------------
Vector Time (GMT): 2018/087/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1032912
05 A = 6781019
30 meter
Y = 5061445
26 meter E =
0007700
Z = 4388575
87 I = 51
96121
XDOT = -5491
239635 Wp = 113
35486
YDOT = -4106
934174 meter/sec RA = 59
87739 deg
ZDOT = 3436
444460 TA = 301
93667
MA = 302
01152
Ha = 220
265 n
mi
Hp = 215
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3388819
07 X = -1110750
94
Y = 16605791
55 feet Y = 5049459
80 meter
Z = 14398214
79 Z = 4383368
76
XDOT = -18015
878068 XDOT = -5461
598946
YDOT = -13474
193485 feet/sec YDOT = -4168
174874 meter/sec
ZDOT = 11274
424081 ZDOT = 3409
842627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6035608
44 X = 1839653
45
Y = 15858682
22 feet Y = 4833726
34 meter
Z = 14374234
78 Z = 4381266
76
XDOT = -21344
845220 XDOT = -6505
908823
YDOT = -2011
445383 feet/sec YDOT = -613
088553 meter/sec
ZDOT = 11156
244909 ZDOT = 3400
423448
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
63112489
00016717 00000-0 10270-3 0 9106
2 25544 51
6392 60
3095 0001884 271
5514 88
5423 15
54184745 25985
Satellite: ISS
Catalog Number: 25544
Epoch time: 18087
63112489 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 60
3095 deg
Eccentricity:
0001884
Arg of perigee: 271
5514 deg
Mean anomaly: 88
5423 deg
Mean motion: 15
54184745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2598
Checksum: 325
Coasting Arc #12 (Orbit 2612)
---------------------------------------
Vector Time (GMT): 2018/088/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2215389
91 A = 6778129
25 meter
Y = -3842860
49 meter E =
0011837
Z = -5135789
94 I = 51
93383
XDOT = 5298
315240 Wp = 74
27466
YDOT = 5275
705010 meter/sec RA = 54
90328 deg
ZDOT = -1662
112065 TA = 179
72633
MA = 179
72568
Ha = 220
293 n
mi
Hp = 215
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7268339
61 X = 2283143
98
Y = -12607810
00 feet Y = -3817708
30 meter
Z = -16849704
54 Z = -5124863
35
XDOT = 17382
924017 XDOT = 5247
000706
YDOT = 17308
743471 feet/sec YDOT = 5334
667285 meter/sec
ZDOT = -5453
123572 ZDOT = -1636
500172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -848986
45 X = -258771
07
Y = -14585103
39 feet Y = -4445539
51 meter
Z = -16800361
84 Z = -5120750
29
XDOT = 23028
794170 XDOT = 7019
176463
YDOT = 4809
837182 feet/sec YDOT = 1466
038373 meter/sec
ZDOT = -5339
544151 ZDOT = -1627
493057
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
59563927
00016717 00000-0 10270-3 0 9110
2 25544 51
6391 55
5009 0001800 278
9743 81
1206 15
54164261 26135
Satellite: ISS
Catalog Number: 25544
Epoch time: 18088
59563927 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 55
5009 deg
Eccentricity:
0001800
Arg of perigee: 278
9743 deg
Mean anomaly: 81
1206 deg
Mean motion: 15
54164261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2613
Checksum: 309
Coasting Arc #13 (Orbit 2628)
---------------------------------------
Vector Time (GMT): 2018/089/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3398082
57 A = 6777199
72 meter
Y = 2447602
13 meter E =
0001163
Z = 5328102
35 I = 51
91206
XDOT = -4764
535950 Wp = 24
88662
YDOT = -6003
418947 meter/sec RA = 49
92368 deg
ZDOT = -279
782996 TA = 67
77615
MA = 67
76382
Ha = 220
314 n
mi
Hp = 215
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11148564
85 X = -3451080
83
Y = 8030190
70 feet Y = 2409306
84 meter
Z = 17480650
76 Z = 5311466
62
XDOT = -15631
679627 XDOT = -4695
690941
YDOT = -19696
256389 feet/sec YDOT = -6056
314371 meter/sec
ZDOT = -917
923214 ZDOT = -302
759354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4698420
81 X = -1432078
66
Y = 13011641
28 feet Y = 3965948
26 meter
Z = 17406023
25 Z = 5305355
89
XDOT = -23104
413219 XDOT = -7042
225149
YDOT = -6974
261849 feet/sec YDOT = -2125
755011 meter/sec
ZDOT = -1019
615923 ZDOT = -310
778933
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
62444879
00016717 00000-0 10270-3 0 9120
2 25544 51
6400 50
3727 0002021 282
4051 77
6876 15
54190054 26293
Satellite: ISS
Catalog Number: 25544
Epoch time: 18089
62444879 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 50
3727 deg
Eccentricity:
0002021
Arg of perigee: 282
4051 deg
Mean anomaly: 77
6876 deg
Mean motion: 15
54190054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2629
Checksum: 307
Coasting Arc #14 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2018/090/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4501856
44 A = 6778846
90 meter
Y = -1018483
69 meter E =
0010466
Z = -4974380
56 I = 51
89600
XDOT = 3836
508680 Wp = 105
35817
YDOT = 6257
357387 meter/sec RA = 44
94196 deg
ZDOT = 2192
041847 TA = 185
96070
MA = 185
97316
Ha = 220
311 n
mi
Hp = 215
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14769870
21 X = 4537073
80
Y = -3341481
94 feet Y = -967944
62 meter
Z = -16320146
19 Z = -4952426
37
XDOT = 12586
970734 XDOT = 3755
604258
YDOT = 20529
387754 feet/sec YDOT = 6299
807812 meter/sec
ZDOT = 7191
738344 ZDOT = 2210
480935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10142773
11 X = 3091517
24
Y = -11385645
34 feet Y = -3470344
70 meter
Z = -16221990
41 Z = -4944462
68
XDOT = 21323
023382 XDOT = 6499
257527
YDOT = 8638
152647 feet/sec YDOT = 2632
908927 meter/sec
ZDOT = 7273
122354 ZDOT = 2216
847693
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
58895511
00016717 00000-0 10270-3 0 9131
2 25544 51
6406 45
5636 0001859 289
0920 71
0031 15
54174580 26444
Satellite: ISS
Catalog Number: 25544
Epoch time: 18090
58895511 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 45
5636 deg
Eccentricity:
0001859
Arg of perigee: 289
0920 deg
Mean anomaly: 71
0031 deg
Mean motion: 15
54174580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2644
Checksum: 309
Coasting Arc #15 (Orbit 2644)
---------------------------------------
Vector Time (GMT): 2018/090/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3395199
87 A = 6787562
50 meter
Y = -5535131
70 meter E =
0005314
Z = -1968429
91 I = 51
92541
XDOT = 5098
413881 Wp = 151
22640
YDOT = -1135
829228 meter/sec RA = 44
73785 deg
ZDOT = -5610
796687 TA = 50
39810
MA = 50
35119
Ha = 220
284 n
mi
Hp = 215
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11139107
17 X = -3323490
56
Y = -18159880
90 feet Y = -5572698
49 meter
Z = -6458103
37 Z = -1984747
70
XDOT = 16727
079661 XDOT = 5137
990476
YDOT = -3726
473846 feet/sec YDOT = -1078
594756 meter/sec
ZDOT = -18408
125613 ZDOT = -5585
934014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21183671
52 X = -6456783
08
Y = -2043922
23 feet Y = -622987
50 meter
Z = -6530124
42 Z = -1990381
92
XDOT = 6995
906553 XDOT = 2132
352317
YDOT = -14162
314286 feet/sec YDOT = -4316
673394 meter/sec
ZDOT = -18296
968934 ZDOT = -5576
916131
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
65325551
00016717 00000-0 10270-3 0 9142
2 25544 51
6420 45
2437 0001892 285
8641 74
2303 15
54157412 26450
Satellite: ISS
Catalog Number: 25544
Epoch time: 18090
65325551 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 45
2437 deg
Eccentricity:
0001892
Arg of perigee: 285
8641 deg
Mean anomaly: 74
2303 deg
Mean motion: 15
54157412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2645
Checksum: 296
Coasting Arc #16 (Orbit 2660)
---------------------------------------
Vector Time (GMT): 2018/091/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2250538
69 A = 6784142
67 meter
Y = 5388297
33 meter E =
0010651
Z = 3443599
83 I = 51
88963
XDOT = -6121
107627 Wp = 86
69183
YDOT = -394
626955 meter/sec RA = 39
77803 deg
ZDOT = 4606
232892 TA = 313
51839
MA = 313
60684
Ha = 220
327 n
mi
Hp = 215
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7383657
11 X = 2173390
71
Y = 17678140
85 feet Y = 5413033
49 meter
Z = 11297899
72 Z = 3454344
16
XDOT = -20082
374105 XDOT = -6138
614669
YDOT = -1294
707857 feet/sec YDOT = -463
174681 meter/sec
ZDOT = 15112
312639 ZDOT = 4576
456013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18602503
85 X = 5670043
17
Y = 4462543
46 feet Y = 1360183
25 meter
Z = 11345049
61 Z = 3457971
12
XDOT = -12570
297855 XDOT = -3831
426786
YDOT = 14221
562151 feet/sec YDOT = 4334
732144 meter/sec
ZDOT = 14979
456373 ZDOT = 4565
738303
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
68205810
00016717 00000-0 10270-3 0 9152
2 25544 51
6416 40
1150 0001831 293
7206 66
3754 15
54167918 26611
Satellite: ISS
Catalog Number: 25544
Epoch time: 18091
68205810 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 40
1150 deg
Eccentricity:
0001831
Arg of perigee: 293
7206 deg
Mean anomaly: 66
3754 deg
Mean motion: 15
54167918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2661
Checksum: 297
Coasting Arc #17 (Orbit 2675)
---------------------------------------
Vector Time (GMT): 2018/092/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -814995
73 A = 6780229
83 meter
Y = -4944269
59 meter E =
0008737
Z = -4576226
46 I = 51
85183
XDOT = 6783
344344 Wp = 59
97121
YDOT = 1750
601840 meter/sec RA = 34
80685 deg
ZDOT = -3099
624945 TA = 179
06525
MA = 179
06362
Ha = 220
243 n
mi
Hp = 215
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2673870
50 X = -737417
88
Y = -16221356
92 feet Y = -4952950
18 meter
Z = -15013866
34 Z = -4579996
49
XDOT = 22255
066746 XDOT = 6778
320969
YDOT = 5743
444358 feet/sec YDOT = 1826
429431 meter/sec
ZDOT = -10169
373180 ZDOT = -3066
685909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14769819
93 X = -4501841
12
Y = -7186895
28 feet Y = -2190565
68 meter
Z = -15029941
51 Z = -4581126
17
XDOT = 16974
204300 XDOT = 5173
737471
YDOT = -13924
586666 feet/sec YDOT = -4244
214016 meter/sec
ZDOT = -10022
619005 ZDOT = -3054
894273
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
64655550
00016717 00000-0 10270-3 0 9160
2 25544 51
6425 35
3077 0002027 295
2599 64
8343 15
54202282 26762
Satellite: ISS
Catalog Number: 25544
Epoch time: 18092
64655550 = yrday
fracday
Element set: 916
Inclination: 51
6425 deg
RA of node: 35
3077 deg
Eccentricity:
0002027
Arg of perigee: 295
2599 deg
Mean anomaly: 64
8343 deg
Mean motion: 15
54202282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2676
Checksum: 316
Coasting Arc #18 (Orbit 2679)
---------------------------------------
Vector Time (GMT): 2018/092/20:30:37
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1765053
34 A = 6777399
34 meter
Y = 3832458
91 meter E =
0001023
Z = 5303011
83 I = 51
83105
XDOT = -6608
462167 Wp = 115
52942
YDOT = -3848
850461 meter/sec RA = 33
64340 deg
ZDOT = 581
467405 TA = 328
93381
MA = 328
93986
Ha = 220
453 n
mi
Hp = 215
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5790857
43 X = -1833537
24
Y = 12573684
10 feet Y = 3812338
52 meter
Z = 17398332
78 Z = 5294270
99
XDOT = -21681
306321 XDOT = -6567
756608
YDOT = -12627
462144 feet/sec YDOT = -3922
523173 meter/sec
ZDOT = 1907
701460 ZDOT = 549
464765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12811057
42 X = 3904810
30
Y = -5374446
47 feet Y = -1638131
28 meter
Z = 17358734
92 Z = 5290942
40
XDOT = 7244
691928 XDOT = 2208
182100
YDOT = 22976
818279 feet/sec YDOT = 7003
334211 meter/sec
ZDOT = 1765
449742 ZDOT = 538
109081
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
90375552
00016717 00000-0 10270-3 0 9171
2 25544 51
6381 34
0207 0001788 290
5728 69
5232 15
54143542 26806
Satellite: ISS
Catalog Number: 25544
Epoch time: 18092
90375552 = yrday
fracday
Element set: 917
Inclination: 51
6381 deg
RA of node: 34
0207 deg
Eccentricity:
0001788
Arg of perigee: 290
5728 deg
Mean anomaly: 69
5232 deg
Mean motion: 15
54143542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2680
Checksum: 311
Coasting Arc #19 (Orbit 2694)
---------------------------------------
Vector Time (GMT): 2018/093/20:30:37
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3320606
38 A = 6777816
78 meter
Y = -2840356
37 meter E =
0012238
Z = -5192004
96 I = 51
80594
XDOT = 6023
455458 Wp = 98
74851
YDOT = 4526
340442 meter/sec RA = 28
65538 deg
ZDOT = 1377
130671 TA = 184
47078
MA = 184
48172
Ha = 220
357 n
mi
Hp = 215
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10894377
89 X = 3377341
51
Y = -9318754
48 feet Y = -2802906
28 meter
Z = -17034137
01 Z = -5175736
40
XDOT = 19761
992971 XDOT = 5965
703567
YDOT = 14850
198302 feet/sec YDOT = 4593
376073 meter/sec
ZDOT = 4518
145247 ZDOT = 1406
250166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14420988
20 X = -4395517
20
Y = -212052
95 feet Y = -64633
74 meter
Z = -16961091
10 Z = -5169740
57
XDOT = -5122
470267 XDOT = -1561
328937
YDOT = -23110
326559 feet/sec YDOT = -7044
027535 meter/sec
ZDOT = 4647
409384 ZDOT = 1416
530380
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
86824719
00016717 00000-0 10270-3 0 9182
2 25544 51
6391 29
2122 0001637 292
9765 67
1215 15
54198288 26957
Satellite: ISS
Catalog Number: 25544
Epoch time: 18093
86824719 = yrday
fracday
Element set: 918
Inclination: 51
6391 deg
RA of node: 29
2122 deg
Eccentricity:
0001637
Arg of perigee: 292
9765 deg
Mean anomaly: 67
1215 deg
Mean motion: 15
54198288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2695
Checksum: 343
Coasting Arc #20 (Orbit 2699)
---------------------------------------
Vector Time (GMT): 2018/094/03:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1350962
95 A = 6777180
84 meter
Y = 3997928
41 meter E =
0000804
Z = 5302347
47 I = 51
79839
XDOT = -6990
607221 Wp = 108
44544
YDOT = -3105
122676 meter/sec RA = 27
25184 deg
ZDOT = 559
812814 TA = 336
22326
MA = 336
22697
Ha = 220
284 n
mi
Hp = 215
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4432293
14 X = -1421324
74
Y = 13116563
01 feet Y = 3982428
01 meter
Z = 17396153
12 Z = 5295613
68
XDOT = -22935
063061 XDOT = -6958
084640
YDOT = -10187
410354 feet/sec YDOT = -3183
114567 meter/sec
ZDOT = 1836
656213 ZDOT = 525
933770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9474911
84 X = -2887953
13
Y = -10147989
21 feet Y = -3093107
11 meter
Z = 17365481
61 Z = 5292998
80
XDOT = 18986
127755 XDOT = 5786
971740
YDOT = -14840
052139 feet/sec YDOT = -4523
247892 meter/sec
ZDOT = 1685
934425 ZDOT = 513
872813
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
18974180
00016717 00000-0 10270-3 0 9197
2 25544 51
6417 27
6123 0001971 292
9724 67
1220 15
54215294 27005
Satellite: ISS
Catalog Number: 25544
Epoch time: 18094
18974180 = yrday
fracday
Element set: 919
Inclination: 51
6417 deg
RA of node: 27
6123 deg
Eccentricity:
0001971
Arg of perigee: 292
9724 deg
Mean anomaly: 67
1220 deg
Mean motion: 15
54215294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2700
Checksum: 306
Coasting Arc #21 (Orbit 2704)
---------------------------------------
Vector Time (GMT): 2018/094/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926561
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1108224
75 A = 6779368
75 meter
Y = 4692558
31 meter E =
0005515
Z = 4762502
22 I = 51
79517
XDOT = -7102
311939 Wp = 116
94691
YDOT = -1062
674594 meter/sec RA = 25
68857 deg
ZDOT = 2694
921818 TA = 306
46925
MA = 306
52006
Ha = 220
239 n
mi
Hp = 215
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3635907
96 X = 1032534
96
Y = 15395532
52 feet Y = 4704528
39 meter
Z = 15625007
28 Z = 4767701
46
XDOT = -23301
548356 XDOT = -7102
991602
YDOT = -3486
465203 feet/sec YDOT = -1142
101136 meter/sec
ZDOT = 8841
607013 ZDOT = 2660
419342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2678954
12 X = 816545
21
Y = 15567998
92 feet Y = 4745126
07 meter
Z = 15647482
71 Z = 4769352
73
XDOT = -21996
659381 XDOT = -6704
581779
YDOT = -4962
879398 feet/sec YDOT = -1512
685640 meter/sec
ZDOT = 8687
789922 ZDOT = 2648
038368
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
51123852
00016717 00000-0 10270-3 0 9208
2 25544 51
6402 26
0105 0002025 301
1624 58
9330 15
54232613 27054
Satellite: ISS
Catalog Number: 25544
Epoch time: 18094
51123852 = yrday
fracday
Element set: 920
Inclination: 51
6402 deg
RA of node: 26
0105 deg
Eccentricity:
0002025
Arg of perigee: 301
1624 deg
Mean anomaly: 58
9330 deg
Mean motion: 15
54232613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2705
Checksum: 256
Coasting Arc #22 (Orbit 2719)
---------------------------------------
Vector Time (GMT): 2018/095/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926561
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 616495
44 A = 6777332
44 meter
Y = -4216637
13 meter E =
0013189
Z = -5281382
39 I = 51
75776
XDOT = 7324
835552 Wp = 77
71076
YDOT = 2085
928681 meter/sec RA = 20
69984 deg
ZDOT = -809
339279 TA = 184
55087
MA = 184
56288
Ha = 220
364 n
mi
Hp = 215
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2022622
83 X = 689255
59
Y = -13834111
33 feet Y = -4209336
54 meter
Z = -17327370
06 Z = -5278210
68
XDOT = 24031
612703 XDOT = 7304
897109
YDOT = 6843
598036 feet/sec YDOT = 2167
728502 meter/sec
ZDOT = -2655
312596 ZDOT = -773
806026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2660036
48 X = 810779
12
Y = -13744490
70 feet Y = -4189320
77 meter
Z = -17312555
38 Z = -5276866
88
XDOT = 22769
614119 XDOT = 6940
178383
YDOT = 7556
278781 feet/sec YDOT = 2303
153773 meter/sec
ZDOT = -2497
064914 ZDOT = -761
105386
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
47572612
00016717 00000-0 10270-3 0 9217
2 25544 51
6401 21
2020 0001998 307
3551 52
7419 15
54202787 27207
Satellite: ISS
Catalog Number: 25544
Epoch time: 18095
47572612 = yrday
fracday
Element set: 921
Inclination: 51
6401 deg
RA of node: 21
2020 deg
Eccentricity:
0001998
Arg of perigee: 307
3551 deg
Mean anomaly: 52
7419 deg
Mean motion: 15
54202787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2720
Checksum: 288
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