[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 19th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 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
048/05:42:30
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
6
052/22:48:00
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
7
057/06:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
0
058/23:08:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
0
060/14:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
1
Coasting Arc #1 (Orbit 1973)
---------------------------------------
Vector Time (GMT): 2018/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3630394
26 A = 6784457
79 meter
Y = -4626010
50 meter E =
0007667
Z = -3390931
83 I = 51
26967
XDOT = 2720
703933 Wp = 94
49021
YDOT = -5495
221645 meter/sec RA = 259
42324 deg
ZDOT = 4592
327856 TA = 225
69141
MA = 225
75430
Ha = 222
039 n
mi
Hp = 213
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11910742
33 X = -3561924
19
Y = -15177199
80 feet Y = -4666225
50 meter
Z = -11125104
42 Z = -3408399
92
XDOT = 8926
194007 XDOT = 2759
644219
YDOT = -18028
942406 feet/sec YDOT = -5464
578764 meter/sec
ZDOT = 15066
692442 ZDOT = 4605
638792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1178030
97 X = -359063
84
Y = -19212069
11 feet Y = -5855838
67 meter
Z = -11202221
58 Z = -3414437
14
XDOT = 16074
154441 XDOT = 4899
402274
YDOT = -9789
738538 feet/sec YDOT = -2983
912306 meter/sec
ZDOT = 15126
690987 ZDOT = 4610
615413
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 18047
50713827
00016717 00000-0 10270-3 0 9000
2 25544 51
6386 260
3372 0002835 101
9680 258
1790 15
54104638 19747
Satellite: ISS
Catalog Number: 25544
Epoch time: 18047
50713827 = yrday
fracday
Element set: 900
Inclination: 51
6386 deg
RA of node: 260
3372 deg
Eccentricity:
0002835
Arg of perigee: 101
9680 deg
Mean anomaly: 258
1790 deg
Mean motion: 15
54104638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1974
Checksum: 311
Coasting Arc #2 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2018/048/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4192048
33 A = 6782578
42 meter
Y = 3539330
15 meter E =
0013686
Z = 3977157
58 I = 51
26759
XDOT = -1636
665138 Wp = 83
90872
YDOT = 6378
761327 meter/sec RA = 255
72631 deg
ZDOT = -3938
319803 TA = 47
29322
MA = 47
17805
Ha = 222
019 n
mi
Hp = 213
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13753439
41 X = 4132840
53
Y = 11611975
55 feet Y = 3585877
82 meter
Z = 13048417
26 Z = 3997376
51
XDOT = -5369
636281 XDOT = -1688
742687
YDOT = 20927
694641 feet/sec YDOT = 6360
167470 meter/sec
ZDOT = -12920
996728 ZDOT = -3946
397039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17571066
42 X = -5355661
04
Y = 3592841
36 feet Y = 1095098
05 meter
Z = 13137936
69 Z = 4004443
10
XDOT = -12948
644732 XDOT = -3946
746914
YDOT = -15787
024153 feet/sec YDOT = -4811
884962 meter/sec
ZDOT = -12957
808569 ZDOT = -3949
540052
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 18048
27877848
00016717 00000-0 10270-3 0 9010
2 25544 51
6379 256
4909 0003029 102
3268 257
8224 15
54108637 19868
Satellite: ISS
Catalog Number: 25544
Epoch time: 18048
27877848 = yrday
fracday
Element set: 901
Inclination: 51
6379 deg
RA of node: 256
4909 deg
Eccentricity:
0003029
Arg of perigee: 102
3268 deg
Mean anomaly: 257
8224 deg
Mean motion: 15
54108637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 342
Coasting Arc #3 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2018/049/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3963567
95 A = 6786314
23 meter
Y = -4811316
82 meter E =
0007148
Z = -2685772
07 I = 51
28870
XDOT = 2618
673893 Wp = 75
38964
YDOT = -5027
675207 meter/sec RA = 250
71929 deg
ZDOT = 5155
394773 TA = 254
14018
MA = 254
21898
Ha = 222
096 n
mi
Hp = 213
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13003831
85 X = -3896426
11
Y = -15785160
17 feet Y = -4855265
02 meter
Z = -8811588
17 Z = -2704861
78
XDOT = 8591
449780 XDOT = 2649
658391
YDOT = -16494
997398 feet/sec YDOT = -4998
217632 meter/sec
ZDOT = 16914
024845 ZDOT = 5168
190894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20399381
20 X = 6217731
39
Y = -801726
59 feet Y = -244366
27 meter
Z = -8895925
55 Z = -2711478
11
XDOT = 7980
634413 XDOT = 2432
497369
YDOT = 15225
271599 feet/sec YDOT = 4640
662783 meter/sec
ZDOT = 16971
647421 ZDOT = 5172
958134
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 18049
24332618
00016717 00000-0 10270-3 0 9020
2 25544 51
6375 251
6829 0002989 106
9573 253
1907 15
54092272 20018
Satellite: ISS
Catalog Number: 25544
Epoch time: 18049
24332618 = yrday
fracday
Element set: 902
Inclination: 51
6375 deg
RA of node: 251
6829 deg
Eccentricity:
0002989
Arg of perigee: 106
9573 deg
Mean anomaly: 253
1907 deg
Mean motion: 15
54092272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 312
Coasting Arc #4 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2018/050/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3514476
88 A = 6788904
90 meter
Y = 5699132
95 meter E =
0016551
Z = 1074268
89 I = 51
31065
XDOT = -3635
125011 Wp = 120
97448
YDOT = 3357
643994 meter/sec RA = 245
72151 deg
ZDOT = -5861
545913 TA = 47
31562
MA = 47
17632
Ha = 222
066 n
mi
Hp = 213
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11530435
95 X = 3445268
28
Y = 18697942
76 feet Y = 5738047
39 meter
Z = 3524504
23 Z = 1091172
04
XDOT = -11926
263158 XDOT = -3643
929072
YDOT = 11015
892370 feet/sec YDOT = 3316
943691 meter/sec
ZDOT = -19230
793677 ZDOT = -5879
225544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21887291
90 X = -6671246
57
Y = -1726193
53 feet Y = -526143
79 meter
Z = 3599007
65 Z = 1096977
53
XDOT = -2068
413854 XDOT = -630
452543
YDOT = -14427
756803 feet/sec YDOT = -4397
580273 meter/sec
ZDOT = -19309
928448 ZDOT = -5885
666191
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 18050
27217451
00016717 00000-0 10270-3 0 9033
2 25544 51
6390 246
5536 0002974 110
4349 249
7123 15
54100325 20175
Satellite: ISS
Catalog Number: 25544
Epoch time: 18050
27217451 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 246
5536 deg
Eccentricity:
0002974
Arg of perigee: 110
4349 deg
Mean anomaly: 249
7123 deg
Mean motion: 15
54100325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2017
Checksum: 282
Coasting Arc #5 (Orbit 2032)
---------------------------------------
Vector Time (GMT): 2018/051/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2871652
37 A = 6789264
56 meter
Y = -6115721
98 meter E =
0014772
Z = 606221
27 I = 51
32600
XDOT = 4585
911695 Wp = 61
59597
YDOT = -1553
549094 meter/sec RA = 240
72911 deg
ZDOT = 5946
933400 TA = 304
97698
MA = 305
11560
Ha = 222
070 n
mi
Hp = 213
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9421431
65 X = -2805995
95
Y = -20064704
64 feet Y = -6147467
60 meter
Z = 1988914
94 Z = 592432
03
XDOT = 15045
642043 XDOT = 4574
056344
YDOT = -5096
945848 feet/sec YDOT = -1502
331967 meter/sec
ZDOT = 19510
936351 ZDOT = 5969
181263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21838466
46 X = 6656364
58
Y = 3830734
35 feet Y = 1167607
83 meter
Z = 1928311
84 Z = 587749
45
XDOT = -4137
459134 XDOT = -1261
097544
YDOT = 13538
931503 feet/sec YDOT = 4126
666322 meter/sec
ZDOT = 19610
173663 ZDOT = 5977
180933
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 18051
30101990
00016717 00000-0 10270-3 0 9049
2 25544 51
6387 241
4249 0002966 111
9408 248
2060 15
54101215 20330
Satellite: ISS
Catalog Number: 25544
Epoch time: 18051
30101990 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 241
4249 deg
Eccentricity:
0002966
Arg of perigee: 111
9408 deg
Mean anomaly: 248
2060 deg
Mean motion: 15
54101215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2033
Checksum: 273
Coasting Arc #6 (Orbit 2047)
---------------------------------------
Vector Time (GMT): 2018/052/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1950618
29 A = 6787217
08 meter
Y = 6089838
91 meter E =
0008788
Z = -2270418
14 I = 51
33720
XDOT = -5423
198039 Wp = 129
96763
YDOT = -272
634697 meter/sec RA = 235
73599 deg
ZDOT = -5410
068030 TA = 75
40476
MA = 75
30732
Ha = 222
037 n
mi
Hp = 213
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6399666
29 X = 1893403
48
Y = 19979786
45 feet Y = 6111331
95 meter
Z = -7448878
40 Z = -2261082
31
XDOT = -17792
644485 XDOT = -5393
467280
YDOT = -894
470792 feet/sec YDOT = -333
114878 meter/sec
ZDOT = -17749
567028 ZDOT = -5436
339569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20154598
04 X = -6143121
48
Y = -5877571
72 feet Y = -1791483
86 meter
Z = -7408084
33 Z = -2257984
10
XDOT = 10234
090899 XDOT = 3119
350906
YDOT = -12655
492379 feet/sec YDOT = -3857
394077 meter/sec
ZDOT = -17866
490490 ZDOT = -5445
706301
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 18052
26556069
00016717 00000-0 10270-3 0 9057
2 25544 51
6397 236
6170 0002938 116
3316 243
8139 15
54110040 20486
Satellite: ISS
Catalog Number: 25544
Epoch time: 18052
26556069 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 236
6170 deg
Eccentricity:
0002938
Arg of perigee: 116
3316 deg
Mean anomaly: 243
8139 deg
Mean motion: 15
54110040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2048
Checksum: 297
Coasting Arc #7 (Orbit 2058)
---------------------------------------
Vector Time (GMT): 2018/052/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -112378
26 A = 6781881
75 meter
Y = 5332866
45 meter E =
0010150
Z = -4197748
94 I = 51
33244
XDOT = -6028
339629 Wp = 84
28371
YDOT = -2997
534819 meter/sec RA = 232
17535 deg
ZDOT = -3653
366007 TA = 148
09528
MA = 148
03377
Ha = 222
037 n
mi
Hp = 213
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -368695
07 X = -151613
17
Y = 17496281
01 feet Y = 5331390
05 meter
Z = -13772142
18 Z = -4198390
54
XDOT = -19778
017155 XDOT = -5976
626361
YDOT = -9834
431820 feet/sec YDOT = -3064
658997 meter/sec
ZDOT = -11986
108948 ZDOT = -3682
523514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12998873
27 X = 3962056
57
Y = -11712728
49 feet Y = -3570039
64 meter
Z = -13775665
88 Z = -4198822
96
XDOT = 5361
462322 XDOT = 1634
173716
YDOT = 20173
969254 feet/sec YDOT = 6149
025828 meter/sec
ZDOT = -12115
546930 ZDOT = -3692
818704
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 18052
97288820
00016717 00000-0 10270-3 0 9063
2 25544 51
6391 233
0906 0003114 121
2415 238
9043 15
54122744 20595
Satellite: ISS
Catalog Number: 25544
Epoch time: 18052
97288820 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 233
0906 deg
Eccentricity:
0003114
Arg of perigee: 121
2415 deg
Mean anomaly: 238
9043 deg
Mean motion: 15
54122744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2059
Checksum: 292
Coasting Arc #8 (Orbit 2074)
---------------------------------------
Vector Time (GMT): 2018/053/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1415831
86 A = 6778715
26 meter
Y = -4351214
08 meter E =
0009033
Z = 4996304
01 I = 51
34219
XDOT = 6081
190425 Wp = 123
54921
YDOT = 4244
953791 meter/sec RA = 227
16080 deg
ZDOT = 1966
134721 TA = 307
25228
MA = 307
33463
Ha = 221
997 n
mi
Hp = 213
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4645117
67 X = 1440113
88
Y = -14275636
73 feet Y = -4335245
19 meter
Z = 16392073
51 Z = 5003240
82
XDOT = 19951
412157 XDOT = 6023
719870
YDOT = 13927
013750 feet/sec YDOT = 4312
636623 meter/sec
ZDOT = 6450
573231 ZDOT = 1995
534942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13429398
46 X = -4093280
65
Y = 6632566
44 feet Y = 2021606
25 meter
Z = 16423498
89 Z = 5005882
46
XDOT = -3292
110156 XDOT = -1003
435175
YDOT = -23022
069157 feet/sec YDOT = -7017
126679 meter/sec
ZDOT = 6580
953525 ZDOT = 2005
874634
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 18054
00172765
00016717 00000-0 10270-3 0 9070
2 25544 51
6385 227
9611 0003112 122
6570 237
4883 15
54117250 20758
Satellite: ISS
Catalog Number: 25544
Epoch time: 18054
00172765 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 227
9611 deg
Eccentricity:
0003112
Arg of perigee: 122
6570 deg
Mean anomaly: 237
4883 deg
Mean motion: 15
54117250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2075
Checksum: 292
Coasting Arc #9 (Orbit 2089)
---------------------------------------
Vector Time (GMT): 2018/054/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2798207
28 A = 6777434
72 meter
Y = 3184966
30 meter E =
0017383
Z = -5302692
58 I = 51
36022
XDOT = -5706
292208 Wp = 95
64539
YDOT = -5103
437878 meter/sec RA = 222
14262 deg
ZDOT = -55
937184 TA = 173
82936
MA = 173
80792
Ha = 222
005 n
mi
Hp = 213
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9180470
09 X = -2807857
06
Y = 10449364
49 feet Y = 3153620
62 meter
Z = -17397285
35 Z = -5316308
74
XDOT = -18721
431128 XDOT = -5648
528371
YDOT = -16743
562592 feet/sec YDOT = -5166
926581 meter/sec
ZDOT = -183
520946 ZDOT = -83
515551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13799757
70 X = 4206166
15
Y = -953887
77 feet Y = -290744
99 meter
Z = -17458309
56 Z = -5321292
75
XDOT = 1284
811906 XDOT = 391
610669
YDOT = 24072
477233 feet/sec YDOT = 7337
291060 meter/sec
ZDOT = -305
703432 ZDOT = -93
178406
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 18054
96626230
00016717 00000-0 10270-3 0 9087
2 25544 51
6378 223
1538 0003027 126
3163 233
8270 15
54103954 20903
Satellite: ISS
Catalog Number: 25544
Epoch time: 18054
96626230 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 223
1538 deg
Eccentricity:
0003027
Arg of perigee: 126
3163 deg
Mean anomaly: 233
8270 deg
Mean motion: 15
54103954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2090
Checksum: 294
Coasting Arc #10 (Orbit 2105)
---------------------------------------
Vector Time (GMT): 2018/055/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4100696
62 A = 6778455
57 meter
Y = -1936641
55 meter E =
0006854
Z = 5032445
87 I = 51
38768
XDOT = 4921
592119 Wp = 80
15976
YDOT = 5585
998149 meter/sec RA = 217
12489 deg
ZDOT = -1857
390239 TA = 27
90532
MA = 27
86858
Ha = 221
778 n
mi
Hp = 213
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13453729
06 X = 4097603
27
Y = -6353810
87 feet Y = -1890801
86 meter
Z = 16510649
20 Z = 5052357
91
XDOT = 16146
955771 XDOT = 4867
784290
YDOT = 18326
765581 feet/sec YDOT = 5640
733845 meter/sec
ZDOT = -6093
799996 ZDOT = -1833
614083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14002764
20 X = -4268042
53
Y = -4727821
60 feet Y = -1441040
02 meter
Z = 16599565
44 Z = 5059547
54
XDOT = 789
981350 XDOT = 240
786316
YDOT = -23403
850845 feet/sec YDOT = -7133
493737 meter/sec
ZDOT = -5988
586730 ZDOT = -1825
321235
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 18055
99509739
00016717 00000-0 10270-3 0 9096
2 25544 51
6364 218
0247 0002924 130
3161 229
8248 15
54126299 21061
Satellite: ISS
Catalog Number: 25544
Epoch time: 18055
99509739 = yrday
fracday
Element set: 909
Inclination: 51
6364 deg
RA of node: 218
0247 deg
Eccentricity:
0002924
Arg of perigee: 130
3161 deg
Mean anomaly: 229
8248 deg
Mean motion: 15
54126299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2106
Checksum: 321
Coasting Arc #11 (Orbit 2120)
---------------------------------------
Vector Time (GMT): 2018/056/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5235073
55 A = 6781582
80 meter
Y = 726600
23 meter E =
0011191
Z = -4261119
31 I = 51
42537
XDOT = -3692
625211 Wp = 115
95429
YDOT = -5680
057740 meter/sec RA = 212
11541 deg
ZDOT = 3570
609483 TA = 190
64489
MA = 190
66860
Ha = 221
926 n
mi
Hp = 213
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17175438
14 X = -5222111
62
Y = 2383859
02 feet Y = 668130
35 meter
Z = -13980050
23 Z = -4286517
56
XDOT = -12114
912108 XDOT = -3646
178644
YDOT = -18635
360041 feet/sec YDOT = -5721
091376 meter/sec
ZDOT = 11714
598042 ZDOT = 3552
785347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14096592
19 X = 4296641
30
Y = 9939121
64 feet Y = 3029444
27 meter
Z = -14093268
37 Z = -4295628
20
XDOT = -3115
920436 XDOT = -949
732549
YDOT = 20906
845902 feet/sec YDOT = 6372
406631 meter/sec
ZDOT = 11635
884398 ZDOT = 3546
617565
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 18056
95962793
00016717 00000-0 10270-3 0 9108
2 25544 51
6370 213
2167 0002926 130
7716 229
3690 15
54107593 21217
Satellite: ISS
Catalog Number: 25544
Epoch time: 18056
95962793 = yrday
fracday
Element set: 910
Inclination: 51
6370 deg
RA of node: 213
2167 deg
Eccentricity:
0002926
Arg of perigee: 130
7716 deg
Mean anomaly: 229
3690 deg
Mean motion: 15
54107593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2121
Checksum: 309
Coasting Arc #12 (Orbit 2126)
---------------------------------------
Vector Time (GMT): 2018/057/06:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1745891
54 A = 6781696
13 meter
Y = -4970290
81 meter E =
0012383
Z = 4263764
62 I = 51
43809
XDOT = 6762
125824 Wp = 111
95681
YDOT = 687
274951 meter/sec RA = 210
46244 deg
ZDOT = 3557
209272 TA = 301
61244
MA = 301
73322
Ha = 221
843 n
mi
Hp = 213
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5727990
60 X = -1710893
35
Y = -16306728
39 feet Y = -4989618
71 meter
Z = 13988729
06 Z = 4255369
06
XDOT = 22185
452180 XDOT = 6736
659254
YDOT = 2254
839079 feet/sec YDOT = 762
751440 meter/sec
ZDOT = 11670
634095 ZDOT = 3589
994800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17076912
54 X = 5205042
94
Y = -2850736
61 feet Y = -868904
52 meter
Z = 13951923
41 Z = 4252546
26
XDOT = -6330
449821 XDOT = -1929
521105
YDOT = 20117
420994 feet/sec YDOT = 6131
789919 meter/sec
ZDOT = 11816
595446 ZDOT = 3601
698292
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 18057
34543970
00016717 00000-0 10270-3 0 9115
2 25544 51
6400 211
2941 0002593 131
7528 228
3847 15
54113891 21278
Satellite: ISS
Catalog Number: 25544
Epoch time: 18057
34543970 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 211
2941 deg
Eccentricity:
0002593
Arg of perigee: 131
7528 deg
Mean anomaly: 228
3847 deg
Mean motion: 15
54113891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2127
Checksum: 297
Coasting Arc #13 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2018/058/06:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 127070
17 A = 6778455
53 meter
Y = 4524281
92 meter E =
0014498
Z = -5058865
84 I = 51
45502
XDOT = -7210
483800 Wp = 85
26794
YDOT = -1827
371098 meter/sec RA = 205
45424 deg
ZDOT = -1818
720544 TA = 167
07245
MA = 167
03524
Ha = 221
700 n
mi
Hp = 213
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 416896
89 X = 101041
71
Y = 14843444
61 feet Y = 4525557
08 meter
Z = -16597328
88 Z = -5058312
07
XDOT = -23656
442912 XDOT = -7180
679569
YDOT = -5995
312001 feet/sec YDOT = -1907
837138 meter/sec
ZDOT = -5966
930917 ZDOT = -1853
673260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14735989
38 X = -4491529
56
Y = -1848385
46 feet Y = -563387
89 meter
Z = -16595392
89 Z = -5058275
75
XDOT = 9552
216413 XDOT = 2911
515563
YDOT = -21282
829013 feet/sec YDOT = -6487
006283 meter/sec
ZDOT = -6122
435568 ZDOT = -1866
118361
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 18058
30996507
00016717 00000-0 10270-3 0 9121
2 25544 51
6386 206
4848 0002548 136
4127 223
7227 15
54146829 21425
Satellite: ISS
Catalog Number: 25544
Epoch time: 18058
30996507 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 206
4848 deg
Eccentricity:
0002548
Arg of perigee: 136
4127 deg
Mean anomaly: 223
7227 deg
Mean motion: 15
54146829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 320
Coasting Arc #14 (Orbit 2152)
---------------------------------------
Vector Time (GMT): 2018/058/23:08:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1381340
96 A = 6779726
73 meter
Y = -4636958
26 meter E =
0010269
Z = 4744313
83 I = 51
47733
XDOT = 7164
538064 Wp = 123
89322
YDOT = 611
278250 meter/sec RA = 202
09464 deg
ZDOT = 2673
673850 TA = 299
60232
MA = 299
70460
Ha = 221
735 n
mi
Hp = 213
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4531958
53 X = -1352431
38
Y = -15213117
66 feet Y = -4652243
38 meter
Z = 15565334
08 Z = 4737674
47
XDOT = 23505
702309 XDOT = 7144
183130
YDOT = 2005
506068 feet/sec YDOT = 691
283417 meter/sec
ZDOT = 8771
895834 ZDOT = 2708
426344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5196287
47 X = -1583828
42
Y = 15029287
76 feet Y = 4580926
91 meter
Z = 15536290
67 Z = 4735461
40
XDOT = -16689
563781 XDOT = -5086
979040
YDOT = -15031
346168 feet/sec YDOT = -4581
554312 meter/sec
ZDOT = 8926
665971 ZDOT = 2720
847788
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 18059
01728430
00016717 00000-0 10270-3 0 9139
2 25544 51
6364 202
9587 0002702 140
7817 219
3531 15
54156018 21530
Satellite: ISS
Catalog Number: 25544
Epoch time: 18059
01728430 = yrday
fracday
Element set: 913
Inclination: 51
6364 deg
RA of node: 202
9587 deg
Eccentricity:
0002702
Arg of perigee: 140
7817 deg
Mean anomaly: 219
3531 deg
Mean motion: 15
54156018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2153
Checksum: 293
Coasting Arc #15 (Orbit 2167)
---------------------------------------
Vector Time (GMT): 2018/059/23:08:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -355262
51 A = 6777592
05 meter
Y = 4271206
68 meter E =
0016101
Z = -5264235
36 I = 51
50192
XDOT = -7440
875350 Wp = 92
12227
YDOT = -1613
419122 meter/sec RA = 197
08605 deg
ZDOT = -809
643189 TA = 170
12844
MA = 170
09678
Ha = 221
733 n
mi
Hp = 213
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1165559
42 X = -377427
65
Y = 14013145
27 feet Y = 4267109
44 meter
Z = -17271113
37 Z = -5266015
31
XDOT = -24412
320702 XDOT = -7418
347922
YDOT = -5293
369823 feet/sec YDOT = -1696
502224 meter/sec
ZDOT = -2656
309675 ZDOT = -845
732606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8904136
84 X = 2713980
91
Y = -10869783
86 feet Y = -3313110
12 meter
Z = -17279533
34 Z = -5266801
76
XDOT = 16143
699437 XDOT = 4920
599588
YDOT = 17688
161291 feet/sec YDOT = 5391
351562 meter/sec
ZDOT = -2816
942795 ZDOT = -858
604164
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 18059
98180861
00016717 00000-0 10270-3 0 9146
2 25544 51
6375 198
1496 0002732 141
6030 218
5318 15
54132114 21688
Satellite: ISS
Catalog Number: 25544
Epoch time: 18059
98180861 = yrday
fracday
Element set: 914
Inclination: 51
6375 deg
RA of node: 198
1496 deg
Eccentricity:
0002732
Arg of perigee: 141
6030 deg
Mean anomaly: 218
5318 deg
Mean motion: 15
54132114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2168
Checksum: 308
Coasting Arc #16 (Orbit 2177)
---------------------------------------
Vector Time (GMT): 2018/060/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3882028
15 A = 6783271
98 meter
Y = 4069572
58 meter E =
0007344
Z = -3797350
68 I = 51
54445
XDOT = -6114
071998 Wp = 100
69278
YDOT = 1920
752963 meter/sec RA = 193
92519 deg
ZDOT = -4200
213215 TA = 124
91549
MA = 124
84646
Ha = 221
725 n
mi
Hp = 214
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12736312
82 X = 3854677
66
Y = 13351616
07 feet Y = 4112830
73 meter
Z = -12458499
61 Z = -3778560
47
XDOT = -20059
291331 XDOT = -6114
694031
YDOT = 6301
682949 feet/sec YDOT = 1852
377252 meter/sec
ZDOT = -13780
227082 ZDOT = -4229
914279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15790070
06 X = 4812813
36
Y = 9655104
66 feet Y = 2942875
90 meter
Z = -12375224
03 Z = -3771968
29
XDOT = -17007
323817 XDOT = -5183
832299
YDOT = 10016
458816 feet/sec YDOT = 3053
016647 meter/sec
ZDOT = -13912
804462 ZDOT = -4240
622800
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 18060
62482204
00016717 00000-0 10270-3 0 9156
2 25544 51
6409 194
9420 0002991 151
6514 208
4802 15
54137933 21783
Satellite: ISS
Catalog Number: 25544
Epoch time: 18060
62482204 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 194
9420 deg
Eccentricity:
0002991
Arg of perigee: 151
6514 deg
Mean anomaly: 208
4802 deg
Mean motion: 15
54137933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2178
Checksum: 303
Coasting Arc #17 (Orbit 2193)
---------------------------------------
Vector Time (GMT): 2018/061/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2337744
94 A = 6779561
26 meter
Y = -4202681
31 meter E =
0010094
Z = 4774374
19 I = 51
56507
XDOT = 7141
934631 Wp = 128
44308
YDOT = -983
551927 meter/sec RA = 188
92986 deg
ZDOT = 2621
323689 TA = 295
64054
MA = 295
74478
Ha = 221
637 n
mi
Hp = 214
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7669766
87 X = -2313766
61
Y = -13788324
52 feet Y = -4228688
87 meter
Z = 15663957
32 Z = 4763077
27
XDOT = 23431
544066 XDOT = 7139
669422
YDOT = -3226
876400 feet/sec YDOT = -903
698217 meter/sec
ZDOT = 8600
143335 ZDOT = 2656
010659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11215079
15 X = -3418356
12
Y = -11168048
07 feet Y = -3404021
05 meter
Z = 15614079
48 Z = 4759171
42
XDOT = 20813
726211 XDOT = 6344
023749
YDOT = -8615
624664 feet/sec YDOT = -2626
042398 meter/sec
ZDOT = 8754
848043 ZDOT = 2668
477684
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 18061
65364095
00016717 00000-0 10270-3 0 9168
2 25544 51
6413 189
8137 0002918 154
6489 205
4808 15
54180435 21945
Satellite: ISS
Catalog Number: 25544
Epoch time: 18061
65364095 = yrday
fracday
Element set: 916
Inclination: 51
6413 deg
RA of node: 189
8137 deg
Eccentricity:
0002918
Arg of perigee: 154
6489 deg
Mean anomaly: 205
4808 deg
Mean motion: 15
54180435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2194
Checksum: 327
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