[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 11th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 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
069/22:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
5
072/21:25:54
220 -0
5 0
7 0
7
N/A 0
4 -0
1 220
9
000/00:01:48
441 0
2 0
0 215
0
073/06:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
0
077/07:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 215
2
080/17:44:26
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
082/19:41:05
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
Coasting Arc #1 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2018/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5842587
46 A = 6788935
71 meter
Y = -3373837
70 meter E =
0015247
Z = 678118
42 I = 51
81686
XDOT = 2910
283200 Wp = 134
97426
YDOT = 3823
421969 meter/sec RA = 154
52919 deg
ZDOT = -5980
541478 TA = 37
71627
MA = 37
60948
Ha = 221
257 n
mi
Hp = 214
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19168594
04 X = 5876586
49
Y = -11069021
31 feet Y = -3308311
71 meter
Z = 2224797
95 Z = 706582
29
XDOT = 9548
173229 XDOT = 2896
362442
YDOT = 12544
035332 feet/sec YDOT = 3855
888449 meter/sec
ZDOT = -19621
199075 ZDOT = -5966
438561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21234770
64 X = 6472358
09
Y = -6201605
88 feet Y = -1890249
47 meter
Z = 2352138
71 Z = 716931
88
XDOT = 5968
433956 XDOT = 1819
178670
YDOT = 12934
038761 feet/sec YDOT = 3942
295014 meter/sec
ZDOT = -19558
734632 ZDOT = -5961
502316
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 18068
53357280
00016717 00000-0 10270-3 0 9003
2 25544 51
6397 155
5133 0002684 172
9694 187
1496 15
54190241 23018
Satellite: ISS
Catalog Number: 25544
Epoch time: 18068
53357280 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 155
5133 deg
Eccentricity:
0002684
Arg of perigee: 172
9694 deg
Mean anomaly: 187
1496 deg
Mean motion: 15
54190241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 315
Coasting Arc #2 (Orbit 2316)
---------------------------------------
Vector Time (GMT): 2018/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6152171
74 A = 6788707
78 meter
Y = 2660227
32 meter E =
0012437
Z = 1046293
52 I = 51
84583
XDOT = -1048
657655 Wp = 66
32724
YDOT = -4770
124241 meter/sec RA = 149
57181 deg
ZDOT = 5911
462859 TA = 304
98392
MA = 305
10063
Ha = 221
159 n
mi
Hp = 214
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20184290
47 X = -6186544
17
Y = 8727779
91 feet Y = 2591237
39 meter
Z = 3432721
53 Z = 1016325
03
XDOT = -3440
477872 XDOT = -1023
953372
YDOT = -15650
013913 feet/sec YDOT = -4781
712469 meter/sec
ZDOT = 19394
563187 ZDOT = 5906
429264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21635060
80 X = -6594366
53
Y = 4050409
10 feet Y = 1234564
69 meter
Z = 3298731
78 Z = 1005453
45
XDOT = 270
657129 XDOT = 82
496293
YDOT = -14472
528769 feet/sec YDOT = -4411
226769 meter/sec
ZDOT = 19372
659655 ZDOT = 5904
786663
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 18069
56235529
00016717 00000-0 10270-3 0 9019
2 25544 51
6402 150
3841 0002529 177
3254 182
7912 15
54195530 23170
Satellite: ISS
Catalog Number: 25544
Epoch time: 18069
56235529 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 150
3841 deg
Eccentricity:
0002529
Arg of perigee: 177
3254 deg
Mean anomaly: 182
7912 deg
Mean motion: 15
54195530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2317
Checksum: 303
Coasting Arc #3 (Orbit 2322)
---------------------------------------
Vector Time (GMT): 2018/069/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 43134
64 A = 6778617
23 meter
Y = 4616867
92 meter E =
0013378
Z = -4975451
54 I = 51
82430
XDOT = -6936
267701 Wp = 114
63793
YDOT = 2409
304145 meter/sec RA = 147
38008 deg
ZDOT = 2174
686373 TA = 176
54275
MA = 176
53350
Ha = 221
067 n
mi
Hp = 214
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 141517
85 X = 15672
22
Y = 15147204
47 feet Y = 4617196
35 meter
Z = -16323659
89 Z = -4975309
06
XDOT = -22756
783797 XDOT = -6973
257043
YDOT = 7904
541158 feet/sec YDOT = 2331
531379 meter/sec
ZDOT = 7134
797812 ZDOT = 2140
902743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8582152
32 X = 2615840
03
Y = -12482299
14 feet Y = -3804604
78 meter
Z = -16323558
82 Z = -4975420
73
XDOT = 22250
429343 XDOT = 6781
930864
YDOT = 6161
585753 feet/sec YDOT = 1878
051337 meter/sec
ZDOT = 6983
809195 ZDOT = 2128
665043
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 18069
94814857
00016717 00000-0 10270-3 0 9029
2 25544 51
6398 148
4625 0002116 176
0514 184
0656 15
54211567 23235
Satellite: ISS
Catalog Number: 25544
Epoch time: 18069
94814857 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 148
4625 deg
Eccentricity:
0002116
Arg of perigee: 176
0514 deg
Mean anomaly: 184
0656 deg
Mean motion: 15
54211567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2323
Checksum: 318
Coasting Arc #4 (Orbit 2338)
---------------------------------------
Vector Time (GMT): 2018/070/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1505275
47 A = 6782012
83 meter
Y = -5199456
31 meter E =
0010413
Z = 4077187
67 I = 51
86286
XDOT = 6513
100274 Wp = 88
85307
YDOT = -1166
750819 meter/sec RA = 142
40203 deg
ZDOT = -3883
758849 TA = 41
24573
MA = 41
16710
Ha = 221
049 n
mi
Hp = 214
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4938567
81 X = 1543500
75
Y = -17058583
70 feet Y = -5182409
22 meter
Z = 13376599
96 Z = 4084592
94
XDOT = 21368
439220 XDOT = 6544
528142
YDOT = -3827
922633 feet/sec YDOT = -1093
741446 meter/sec
ZDOT = -12741
990973 ZDOT = -3852
044456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13652229
43 X = -4161199
53
Y = 11318131
57 feet Y = 3449766
50 meter
Z = 13410245
56 Z = 4087442
85
XDOT = -19027
703065 XDOT = -5799
643894
YDOT = -7988
310978 feet/sec YDOT = -2434
837186 meter/sec
ZDOT = -12600
358710 ZDOT = -3840
589335
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 18070
97692594
00016717 00000-0 10270-3 0 9037
2 25544 51
6399 143
3342 0002096 177
4823 182
6341 15
54204890 23394
Satellite: ISS
Catalog Number: 25544
Epoch time: 18070
97692594 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 143
3342 deg
Eccentricity:
0002096
Arg of perigee: 177
4823 deg
Mean anomaly: 182
6341 deg
Mean motion: 15
54204890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2339
Checksum: 325
Coasting Arc #5 (Orbit 2353)
---------------------------------------
Vector Time (GMT): 2018/071/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2812322
10 A = 6785757
01 meter
Y = 5524391
40 meter E =
0004002
Z = -2763129
96 I = 51
90147
XDOT = -5655
606787 Wp = 85
36452
YDOT = -300
753857 meter/sec RA = 137
43513 deg
ZDOT = 5161
730635 TA = 243
48134
MA = 243
52238
Ha = 220
949 n
mi
Hp = 214
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9226778
55 X = -2860466
70
Y = 18124643
71 feet Y = 5492672
64 meter
Z = -9065387
01 Z = -2776908
48
XDOT = -18555
140378 XDOT = -5676
895944
YDOT = -986
725252 feet/sec YDOT = -364
117308 meter/sec
ZDOT = 16934
811795 ZDOT = 5134
206384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17644106
58 X = 5377923
69
Y = -10059390
44 feet Y = -3066102
21 meter
Z = -9127516
67 Z = -2782067
08
XDOT = 14291
832618 XDOT = 4356
150582
YDOT = 9833
102262 feet/sec YDOT = 2997
129569 meter/sec
ZDOT = 16812
031570 ZDOT = 5124
307223
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 18071
94140186
00016717 00000-0 10270-3 0 9041
2 25544 51
6404 138
5255 0002080 182
6136 177
5006 15
54227701 23542
Satellite: ISS
Catalog Number: 25544
Epoch time: 18071
94140186 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 138
5255 deg
Eccentricity:
0002080
Arg of perigee: 182
6136 deg
Mean anomaly: 177
5006 deg
Mean motion: 15
54227701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2354
Checksum: 287
Coasting Arc #6 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2018/072/21:26:48
441
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1150084
95 A = 6779062
64 meter
Y = 4488895
60 meter E =
0012239
Z = -4959346
38 I = 51
90017
XDOT = -6110
656333 Wp = 115
66585
YDOT = 4038
461351 meter/sec RA = 132
68176 deg
ZDOT = 2237
423722 TA = 176
13098
MA = 176
12151
Ha = 220
882 n
mi
Hp = 215
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3773244
59 X = 1123892
95
Y = 14727347
76 feet Y = 4501609
68 meter
Z = -16270821
47 Z = -4953823
84
XDOT = -20048
085083 XDOT = -6166
229411
YDOT = 13249
545114 feet/sec YDOT = 3969
817293 meter/sec
ZDOT = 7340
629010 ZDOT = 2207
605340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8282651
50 X = 2524552
18
Y = -12779434
72 feet Y = -3895171
70 meter
Z = -16246707
69 Z = -4951996
50
XDOT = 22392
087298 XDOT = 6825
108208
YDOT = 5346
727826 feet/sec YDOT = 1629
682641 meter/sec
ZDOT = 7207
086654 ZDOT = 2196
720012
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 18072
90587582
00016717 00000-0 10270-3 0 9054
2 25544 51
6402 133
7166 0001988 204
3293 155
7767 15
54091727 23695
Satellite: ISS
Catalog Number: 25544
Epoch time: 18072
90587582 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 133
7166 deg
Eccentricity:
0001988
Arg of perigee: 204
3293 deg
Mean anomaly: 155
7767 deg
Mean motion: 15
54091727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2369
Checksum: 333
Coasting Arc #7 (Orbit 2374)
---------------------------------------
Vector Time (GMT): 2018/073/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -571497
92 A = 6782695
40 meter
Y = 5458529
87 meter E =
0007167
Z = -3993572
36 I = 51
92028
XDOT = -6114
788331 Wp = 127
77939
YDOT = 2290
179317 meter/sec RA = 130
73624 deg
ZDOT = 4005
963434 TA = 183
84955
MA = 183
85507
Ha = 220
942 n
mi
Hp = 215
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1874993
19 X = -613095
84
Y = 17908562
56 feet Y = 5451905
96 meter
Z = -13102271
54 Z = -3996450
09
XDOT = -20061
641505 XDOT = -6159
401839
YDOT = 7513
711671 feet/sec YDOT = 2221
550537 meter/sec
ZDOT = 13142
924652 ZDOT = 3976
151766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17974250
49 X = -5478551
55
Y = -897143
54 feet Y = -273449
35 meter
Z = -13115760
93 Z = -3997683
93
XDOT = -8571
223579 XDOT = -2612
508947
YDOT = -18439
311335 feet/sec YDOT = -5620
302095 meter/sec
ZDOT = 13009
613428 ZDOT = 3965
330173
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 18073
29169710
00016717 00000-0 10270-3 0 9067
2 25544 51
6396 131
7891 0002451 201
5359 158
5691 15
54082806 23750
Satellite: ISS
Catalog Number: 25544
Epoch time: 18073
29169710 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 131
7891 deg
Eccentricity:
0002451
Arg of perigee: 201
5359 deg
Mean anomaly: 158
5691 deg
Mean motion: 15
54082806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2375
Checksum: 321
Coasting Arc #8 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2018/074/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1750105
98 A = 6786447
75 meter
Y = -5986153
97 meter E =
0013325
Z = 2657314
96 I = 51
95334
XDOT = 5561
187816 Wp = 112
84644
YDOT = -706
232693 meter/sec RA = 125
77476 deg
ZDOT = -5237
742060 TA = 37
30273
MA = 37
21026
Ha = 220
935 n
mi
Hp = 215
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5741817
51 X = 1804007
06
Y = -19639612
76 feet Y = -5966281
37 meter
Z = 8718224
92 Z = 2665947
90
XDOT = 18245
366849 XDOT = 5594
113610
YDOT = -2317
036395 feet/sec YDOT = -643
860217 meter/sec
ZDOT = -17184
193110 ZDOT = -5210
648075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19974864
93 X = 6088338
83
Y = 4359106
76 feet Y = 1328655
74 meter
Z = 8757468
96 Z = 2669276
54
XDOT = 3857
811356 XDOT = 1175
860901
YDOT = 16705
871612 feet/sec YDOT = 5091
949667 meter/sec
ZDOT = -17063
187496 ZDOT = -5200
859549
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 18074
32055311
00016717 00000-0 10270-3 0 9074
2 25544 51
6395 126
6604 0002460 202
6634 157
4410 15
54080763 23917
Satellite: ISS
Catalog Number: 25544
Epoch time: 18074
32055311 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 126
6604 deg
Eccentricity:
0002460
Arg of perigee: 202
6634 deg
Mean anomaly: 157
4410 deg
Mean motion: 15
54080763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 285
Coasting Arc #9 (Orbit 2405)
---------------------------------------
Vector Time (GMT): 2018/075/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2686414
17 A = 6788923
91 meter
Y = 6138668
07 meter E =
0007194
Z = -1072461
28 I = 51
98015
XDOT = -4758
440191 Wp = 42
16449
YDOT = -1053
579501 meter/sec RA = 120
82377 deg
ZDOT = 5916
977499 TA = 306
26292
MA = 306
32937
Ha = 220
832 n
mi
Hp = 215
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8813694
79 X = -2749649
38
Y = 20139987
10 feet Y = 6108273
02 meter
Z = -3518573
74 Z = -1085665
21
XDOT = -15611
680416 XDOT = -4775
046335
YDOT = -3456
625659 feet/sec YDOT = -1106
883694 meter/sec
ZDOT = 19412
655838 ZDOT = 5893
822743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20806741
02 X = -6341894
66
Y = -7067979
63 feet Y = -2154320
19 meter
Z = -3578246
74 Z = -1090649
61
XDOT = 1605
782609 XDOT = 489
442539
YDOT = -14456
798640 feet/sec YDOT = -4406
432225 meter/sec
ZDOT = 19309
435957 ZDOT = 5885
516080
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 18075
28510316
00016717 00000-0 10270-3 0 9082
2 25544 51
6395 121
8528 0002356 207
1579 152
9451 15
54092861 24065
Satellite: ISS
Catalog Number: 25544
Epoch time: 18075
28510316 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 121
8528 deg
Eccentricity:
0002356
Arg of perigee: 207
1579 deg
Mean anomaly: 152
9451 deg
Mean motion: 15
54092861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2406
Checksum: 311
Coasting Arc #10 (Orbit 2421)
---------------------------------------
Vector Time (GMT): 2018/076/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3397675
78 A = 6789212
90 meter
Y = -5833956
71 meter E =
0011669
Z = -653665
00 I = 51
99719
XDOT = 3809
993176 Wp = 150
89365
YDOT = 2884
907484 meter/sec RA = 115
87764 deg
ZDOT = -5998
579765 TA = 36
13127
MA = 36
05248
Ha = 220
777 n
mi
Hp = 215
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11147230
24 X = 3465835
28
Y = -19140277
91 feet Y = -5795580
55 meter
Z = -2144570
20 Z = -636994
03
XDOT = 12499
977613 XDOT = 3806
587881
YDOT = 9464
919568 feet/sec YDOT = 2927
493545 meter/sec
ZDOT = -19680
379807 ZDOT = -5980
080990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20170794
70 X = 6148058
22
Y = 9168783
29 feet Y = 2794645
15 meter
Z = -2069448
17 Z = -630767
80
XDOT = -7469
407286 XDOT = -2276
675341
YDOT = 12050
824101 feet/sec YDOT = 3673
091186 meter/sec
ZDOT = -19598
161700 ZDOT = -5973
519686
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 18076
31395425
00016717 00000-0 10270-3 0 9090
2 25544 51
6395 116
7240 0002402 211
8531 148
2476 15
54110558 24228
Satellite: ISS
Catalog Number: 25544
Epoch time: 18076
31395425 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 116
7240 deg
Eccentricity:
0002402
Arg of perigee: 211
8531 deg
Mean anomaly: 148
2476 deg
Mean motion: 15
54110558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2422
Checksum: 292
Coasting Arc #11 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/077/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3857058
15 A = 6787187
85 meter
Y = 5089582
58 meter E =
0012149
Z = 2284365
43 I = 52
00465
XDOT = -2811
365055 Wp = 78
67236
YDOT = -4591
718430 meter/sec RA = 110
92981 deg
ZDOT = 5461
323480 TA = 306
63011
MA = 306
74177
Ha = 220
727 n
mi
Hp = 215
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12654390
26 X = -3924780
78
Y = 16698105
58 feet Y = 5046071
97 meter
Z = 7494637
24 Z = 2265464
04
XDOT = -9223
638631 XDOT = -2786
338380
YDOT = -15064
693011 feet/sec YDOT = -4623
016323 meter/sec
ZDOT = 17917
727954 ZDOT = 5447
728359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18083204
83 X = -5511760
83
Y = -10640717
25 feet Y = -3243290
62 meter
Z = 7409638
99 Z = 2258457
96
XDOT = 13077
565595 XDOT = 3986
041993
YDOT = -9738
103548 feet/sec YDOT = -2968
173961 meter/sec
ZDOT = 17857
610971 ZDOT = 5442
999824
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 18077
34280180
00016717 00000-0 10270-3 0 9107
2 25544 51
6403 111
5952 0002272 214
0349 146
0658 15
54122277 24384
Satellite: ISS
Catalog Number: 25544
Epoch time: 18077
34280180 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 111
5952 deg
Eccentricity:
0002272
Arg of perigee: 214
0349 deg
Mean anomaly: 146
0658 deg
Mean motion: 15
54122277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 285
Coasting Arc #12 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/077/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2748460
72 A = 6778952
43 meter
Y = 3719421
95 meter E =
0011748
Z = -4967265
00 I = 51
97799
XDOT = -4143
098573 Wp = 116
47663
YDOT = 6042
980913 meter/sec RA = 110
65829 deg
ZDOT = 2231
443783 TA = 175
23425
MA = 175
22306
Ha = 220
637 n
mi
Hp = 215
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9017259
59 X = 2730793
12
Y = 12202827
92 feet Y = 3750057
62 meter
Z = -16296801
18 Z = -4953957
44
XDOT = -13592
843086 XDOT = -4221
204038
YDOT = 19826
052865 feet/sec YDOT = 5996
213543 meter/sec
ZDOT = 7321
009788 ZDOT = 2211
127557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7444587
63 X = -2269110
31
Y = 13293446
23 feet Y = 4051842
41 meter
Z = -16237860
41 Z = -4949299
85
XDOT = -22688
326080 XDOT = -6915
401789
YDOT = -3870
906170 feet/sec YDOT = -1179
852201 meter/sec
ZDOT = 7229
577662 ZDOT = 2203
575271
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 18077
34280162
00016717 00000-0 10270-3 0 9118
2 25544 51
6404 111
5968 0002219 216
9050 143
1951 15
54132886 24384
Satellite: ISS
Catalog Number: 25544
Epoch time: 18077
34280162 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 111
5968 deg
Eccentricity:
0002219
Arg of perigee: 216
9050 deg
Mean anomaly: 143
1951 deg
Mean motion: 15
54132886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 296
Coasting Arc #13 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2018/078/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1883423
28 A = 6782349
36 meter
Y = -5075987
75 meter E =
0009008
Z = 4077762
44 I = 51
99940
XDOT = 4519
073198 Wp = 85
77995
YDOT = -4817
179548 meter/sec RA = 105
69012 deg
ZDOT = -3901
119391 TA = 44
44887
MA = 44
37662
Ha = 220
685 n
mi
Hp = 215
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6179210
23 X = -1846329
85
Y = -16653503
12 feet Y = -5096841
51 meter
Z = 13378485
68 Z = 4068704
22
XDOT = 14826
355638 XDOT = 4591
553927
YDOT = -15804
394844 feet/sec YDOT = -4766
239442 meter/sec
ZDOT = -12798
948134 ZDOT = -3878
990591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12455561
60 X = 3796455
17
Y = -12706062
68 feet Y = -3872807
90 meter
Z = 13338689
62 Z = 4065632
60
XDOT = 19692
990161 XDOT = 6002
423401
YDOT = 5945
105314 feet/sec YDOT = 1812
068100 meter/sec
ZDOT = -12699
564201 ZDOT = -3870
827168
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 18078
37164787
00016717 00000-0 10270-3 0 9127
2 25544 51
6399 106
4679 0002156 221
4364 138
6625 15
54116088 24549
Satellite: ISS
Catalog Number: 25544
Epoch time: 18078
37164787 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 106
4679 deg
Eccentricity:
0002156
Arg of perigee: 221
4364 deg
Mean anomaly: 138
6625 deg
Mean motion: 15
54116088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 330
Coasting Arc #14 (Orbit 2468)
---------------------------------------
Vector Time (GMT): 2018/079/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1058686
57 A = 6786140
05 meter
Y = 6096730
34 meter E =
0002551
Z = -2786530
78 I = 52
01943
XDOT = -4699
101227 Wp = 68
40897
YDOT = 3170
930406 meter/sec RA = 100
73280 deg
ZDOT = 5157
132357 TA = 260
19673
MA = 260
22554
Ha = 220
526 n
mi
Hp = 215
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3473381
13 X = 1003968
14
Y = 20002396
14 feet Y = 6108263
00 meter
Z = -9142161
36 Z = -2781521
71
XDOT = -15416
998777 XDOT = -4759
260907
YDOT = 10403
314980 feet/sec YDOT = 3118
046106 meter/sec
ZDOT = 16919
725582 ZDOT = 5134
159156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16442621
05 X = -5011710
89
Y = 11924535
14 feet Y = 3634598
31 meter
Z = -9120582
04 Z = -2779953
41
XDOT = -15277
994129 XDOT = -4656
732611
YDOT = -8216
026140 feet/sec YDOT = -2504
244768 meter/sec
ZDOT = 16816
769080 ZDOT = 5125
751216
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 18079
33618868
00016717 00000-0 10270-3 0 9139
2 25544 51
6396 101
6600 0002267 228
9332 131
1625 15
54097806 24697
Satellite: ISS
Catalog Number: 25544
Epoch time: 18079
33618868 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 101
6600 deg
Eccentricity:
0002267
Arg of perigee: 228
9332 deg
Mean anomaly: 131
1625 deg
Mean motion: 15
54097806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2469
Checksum: 320
Coasting Arc #15 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2018/080/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -251200
49 A = 6788770
35 meter
Y = -6672996
69 meter E =
0013183
Z = 1182213
68 I = 52
03381
XDOT = 4749
469372 Wp = 130
80366
YDOT = -1229
555020 meter/sec RA = 95
78493 deg
ZDOT = -5896
627588 TA = 36
42134
MA = 36
33172
Ha = 220
523 n
mi
Hp = 215
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -824148
59 X = -182305
16
Y = -21893033
77 feet Y = -6675420
44 meter
Z = 3878653
79 Z = 1181161
49
XDOT = 15582
248597 XDOT = 4791
508468
YDOT = -4033
973164 feet/sec YDOT = -1176
208776 meter/sec
ZDOT = -19345
891037 ZDOT = -5873
453949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19136256
77 X = 5832731
06
Y = -10668527
70 feet Y = -3251767
24 meter
Z = 3874828
70 Z = 1181047
79
XDOT = 9932
070434 XDOT = 3027
295068
YDOT = 10785
395832 feet/sec YDOT = 3287
388650 meter/sec
ZDOT = -19242
282108 ZDOT = -5865
047586
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
36502991
00016717 00000-0 10270-3 0 9144
2 25544 51
6399 96
5312 0002098 230
8064 129
2903 15
54118305 24851
Satellite: ISS
Catalog Number: 25544
Epoch time: 18080
36502991 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 96
5312 deg
Eccentricity:
0002098
Arg of perigee: 230
8064 deg
Mean anomaly: 129
2903 deg
Mean motion: 15
54118305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 309
Coasting Arc #16 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2018/080/17:44:26
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3595858
57 A = 6779476
41 meter
Y = 3095363
66 meter E =
0010452
Z = -4852417
59 I = 52
00342
XDOT = -2433
075373 Wp = 115
10817
YDOT = 6805
227633 meter/sec RA = 93
75103 deg
ZDOT = 2537
998237 TA = 179
75555
MA = 179
75504
Ha = 220
476 n
mi
Hp = 215
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11797436
26 X = 3584548
75
Y = 10155392
57 feet Y = 3135511
29 meter
Z = -15920005
20 Z = -4834977
84
XDOT = -7982
530751 XDOT = -2521
320776
YDOT = 22326
862312 feet/sec YDOT = 6777
526156 meter/sec
ZDOT = 8326
765869 ZDOT = 2525
964115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11261822
80 X = 3432603
59
Y = -10860142
75 feet Y = -3310171
51 meter
Z = -15842560
18 Z = -4828812
34
XDOT = 20649
704344 XDOT = 6294
029884
YDOT = 9345
992956 feet/sec YDOT = 2848
658653 meter/sec
ZDOT = 8272
147559 ZDOT = 2521
350576
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
75084546
00016717 00000-0 10270-3 0 9159
2 25544 51
6392 94
6090 0001767 240
7335 119
3641 15
54123229 24916
Satellite: ISS
Catalog Number: 25544
Epoch time: 18080
75084546 = yrday
fracday
Element set: 915
Inclination: 51
6392 deg
RA of node: 94
6090 deg
Eccentricity:
0001767
Arg of perigee: 240
7335 deg
Mean anomaly: 119
3641 deg
Mean motion: 15
54123229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 309
Coasting Arc #17 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2018/081/17:44:26
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3126837
95 A = 6783042
72 meter
Y = -4596448
07 meter E =
0009610
Z = 3879015
73 I = 52
01647
XDOT = 3125
223966 Wp = 84
79880
YDOT = -5640
216572 meter/sec RA = 88
78687 deg
ZDOT = -4154
509105 TA = 48
64816
MA = 48
56553
Ha = 220
538 n
mi
Hp = 215
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10258654
68 X = -3094049
12
Y = -15080210
20 feet Y = -4631230
88 meter
Z = 12726429
57 Z = 3863906
57
XDOT = 10253
359470 XDOT = 3208
242638
YDOT = -18504
647547 feet/sec YDOT = -5604
804314 meter/sec
ZDOT = -13630
279215 ZDOT = -4139
125693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15857918
46 X = -4833493
55
Y = 9103614
53 feet Y = 2774781
71 meter
Z = 12659595
95 Z = 3858644
85
XDOT = -16955
575014 XDOT = -5168
059264
YDOT = -10633
336262 feet/sec YDOT = -3241
040893 meter/sec
ZDOT = -13560
845080 ZDOT = -4133
345580
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
77968359
00016717 00000-0 10270-3 0 9166
2 25544 51
6393 89
4812 0001788 244
7793 115
3174 15
54117737 25078
Satellite: ISS
Catalog Number: 25544
Epoch time: 18081
77968359 = yrday
fracday
Element set: 916
Inclination: 51
6393 deg
RA of node: 89
4812 deg
Eccentricity:
0001788
Arg of perigee: 244
7793 deg
Mean anomaly: 115
3174 deg
Mean motion: 15
54117737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 348
Coasting Arc #18 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2018/082/17:44:26
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2601435
58 A = 6786655
95 meter
Y = 5736568
73 meter E =
0003598
Z = -2523960
50 I = 52
02768
XDOT = -3746
339587 Wp = 39
45478
YDOT = 4040
214138 meter/sec RA = 83
83158 deg
ZDOT = 5328
294318 TA = 292
39173
MA = 292
42985
Ha = 220
391 n
mi
Hp = 215
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8534893
64 X = 2549354
46
Y = 18820763
56 feet Y = 5765368
41 meter
Z = -8280710
32 Z = -2511450
47
XDOT = -12291
140378 XDOT = -3817
122012
YDOT = 13255
295728 feet/sec YDOT = 3997
924561 meter/sec
ZDOT = 17481
280571 ZDOT = 5309
923697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19322396
25 X = 5889466
38
Y = -7390499
34 feet Y = -2252624
20 meter
Z = -8225645
06 Z = -2507176
61
XDOT = 11912
429982 XDOT = 3630
908659
YDOT = 11805
328393 feet/sec YDOT = 3598
264094 meter/sec
ZDOT = 17398
712086 ZDOT = 5303
127444
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
74421717
00016717 00000-0 10270-3 0 9177
2 25544 51
6400 84
6728 0001868 249
1434 110
9518 15
54130222 25224
Satellite: ISS
Catalog Number: 25544
Epoch time: 18082
74421717 = yrday
fracday
Element set: 917
Inclination: 51
6400 deg
RA of node: 84
6728 deg
Eccentricity:
0001868
Arg of perigee: 249
1434 deg
Mean anomaly: 110
9518 deg
Mean motion: 15
54130222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 295
Coasting Arc #19 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2018/082/19:41:05
000
Vector Time (MET): N/A
Weight (LBS) : 919827
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3447410
75 A = 6779448
38 meter
Y = 3236747
45 meter E =
0006140
Z = 4855749
49 I = 52
00465
XDOT = -2744
827861 Wp = 133
08039
YDOT = -6705
507504 meter/sec RA = 83
47096 deg
ZDOT = 2514
948750 TA = 292
29855
MA = 292
36364
Ha = 220
514 n
mi
Hp = 215
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11310402
72 X = -3506935
42
Y = 10619250
15 feet Y = 3197863
61 meter
Z = 15930936
65 Z = 4838858
37
XDOT = -9005
340752 XDOT = -2681
857364
YDOT = -21999
696534 feet/sec YDOT = -6735
849810 meter/sec
ZDOT = 8251
144192 ZDOT = 2501
768674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14514458
45 X = 4424006
94
Y = 5695197
74 feet Y = 1735896
27 meter
Z = 15855082
61 Z = 4832629
18
XDOT = -15496
754785 XDOT = -4723
410859
YDOT = 16628
923913 feet/sec YDOT = 5068
496009 meter/sec
ZDOT = 8193
221192 ZDOT = 2497
293819
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
87282105
00016717 00000-0 10270-3 0 9188
2 25544 51
6415 84
0324 0001841 249
8865 110
2090 15
54117644 25245
Satellite: ISS
Catalog Number: 25544
Epoch time: 18082
87282105 = yrday
fracday
Element set: 918
Inclination: 51
6415 deg
RA of node: 84
0324 deg
Eccentricity:
0001841
Arg of perigee: 249
8865 deg
Mean anomaly: 110
2090 deg
Mean motion: 15
54117644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 297
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