[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 20th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 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
172/07:16:36
447 1
2 1
2 1
3
N/A 0
1 -0
1 220
4
000/00:03:12
895 0
4 -0
0 216
0
179/14:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
0
180/09:42:42
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
9
183/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
0
Coasting Arc #1 (Orbit 3871)
---------------------------------------
Vector Time (GMT): 2018/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 531203
90 A = 6777705
68 meter
Y = 4306061
54 meter E =
0005094
Z = 5206143
49 I = 51
70140
XDOT = -7549
904587 Wp = 157
11346
YDOT = -559
408954 meter/sec RA = 11
59749 deg
ZDOT = 1228
050753 TA = 281
08525
MA = 281
14252
Ha = 220
682 n
mi
Hp = 215
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1742794
94 X = 457724
42
Y = 14127498
50 feet Y = 4311590
36 meter
Z = 17080523
27 Z = 5208545
92
XDOT = -24770
028172 XDOT = -7549
053162
YDOT = -1835
331215 feet/sec YDOT = -643
832577 meter/sec
ZDOT = 4029
037904 ZDOT = 1191
378305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14210240
50 X = 4331281
30
Y = -591343
55 feet Y = -180241
52 meter
Z = 17090558
83 Z = 5209202
33
XDOT = -3687
708881 XDOT = -1124
013667
YDOT = 23559
190586 feet/sec YDOT = 7180
841291 meter/sec
ZDOT = 3865
008934 ZDOT = 1178
054723
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 18169
55025789
00016717 00000-0 10270-3 0 9003
2 25544 51
6400 11
9206 0002836 208
9467 151
1529 15
54163973 38720
Satellite: ISS
Catalog Number: 25544
Epoch time: 18169
55025789 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 11
9206 deg
Eccentricity:
0002836
Arg of perigee: 208
9467 deg
Mean anomaly: 151
1529 deg
Mean motion: 15
54163973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3872
Checksum: 317
Coasting Arc #2 (Orbit 3886)
---------------------------------------
Vector Time (GMT): 2018/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1309894
07 A = 6777352
03 meter
Y = -4053548
01 meter E =
0013575
Z = -5282847
06 I = 51
66606
XDOT = 7483
279416 Wp = 106
64358
YDOT = 1453
283492 meter/sec RA = 6
59902 deg
ZDOT = 738
162532 TA = 170
42724
MA = 170
40134
Ha = 220
602 n
mi
Hp = 215
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4297552
73 X = 1380785
68
Y = -13299042
02 feet Y = -4038502
96 meter
Z = -17332175
39 Z = -5276312
32
XDOT = 24551
441655 XDOT = 7462
886656
YDOT = 4767
990460 feet/sec YDOT = 1536
852584 meter/sec
ZDOT = 2421
793085 ZDOT = 774
464039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13032417
88 X = -3972280
97
Y = -5150309
45 feet Y = -1569814
32 meter
Z = -17302259
36 Z = -5273728
65
XDOT = 5759
343759 XDOT = 1755
447978
YDOT = -23278
938921 feet/sec YDOT = -7095
420583 meter/sec
ZDOT = 2584
003419 ZDOT = 787
604242
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 18170
51474717
00016717 00000-0 10270-3 0 9011
2 25544 51
6381 7
1111 0002873 211
4456 148
6526 15
54201159 38871
Satellite: ISS
Catalog Number: 25544
Epoch time: 18170
51474717 = yrday
fracday
Element set: 901
Inclination: 51
6381 deg
RA of node: 7
1111 deg
Eccentricity:
0002873
Arg of perigee: 211
4456 deg
Mean anomaly: 148
6526 deg
Mean motion: 15
54201159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3887
Checksum: 296
Coasting Arc #3 (Orbit 3902)
---------------------------------------
Vector Time (GMT): 2018/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3063417
83 A = 6779521
75 meter
Y = 3699473
45 meter E =
0004997
Z = 4780824
33 I = 51
64078
XDOT = -6841
315158 Wp = 75
51740
YDOT = -2269
161388 meter/sec RA = 1
60254 deg
ZDOT = -2624
293256 TA = 40
36926
MA = 40
33218
Ha = 220
563 n
mi
Hp = 215
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10050583
44 X = -3127781
29
Y = 12137380
08 feet Y = 3664855
88 meter
Z = 15685119
20 Z = 4765787
39
XDOT = -22445
259704 XDOT = -6802
684941
YDOT = -7444
755209 feet/sec YDOT = -2345
449456 meter/sec
ZDOT = -8609
886011 ZDOT = -2657
432225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11735212
50 X = 3576892
77
Y = 10617928
99 feet Y = 3236344
75 meter
Z = 15617219
93 Z = 4760128
64
XDOT = -7534
827313 XDOT = -2296
615365
YDOT = 21226
013115 feet/sec YDOT = 6469
688797 meter/sec
ZDOT = -8757
797949 ZDOT = -2669
376815
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 18171
54353484
00016717 00000-0 10270-3 0 9023
2 25544 51
6387 1
9825 0003002 218
0774 142
0167 15
54192336 39036
Satellite: ISS
Catalog Number: 25544
Epoch time: 18171
54353484 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 1
9825 deg
Eccentricity:
0003002
Arg of perigee: 218
0774 deg
Mean anomaly: 142
0167 deg
Mean motion: 15
54192336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3903
Checksum: 293
Coasting Arc #4 (Orbit 3914)
---------------------------------------
Vector Time (GMT): 2018/172/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3141304
33 A = 6780707
33 meter
Y = -3817595
95 meter E =
0008689
Z = -4649240
50 I = 51
61977
XDOT = 6786
172821 Wp = 126
42842
YDOT = 2028
310894 meter/sec RA = 357
59353 deg
ZDOT = 2918
408439 TA = 172
65505
MA = 172
64231
Ha = 220
400 n
mi
Hp = 215
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10306116
57 X = 3206343
79
Y = -12524921
09 feet Y = -3782103
64 meter
Z = -15253413
72 Z = -4633823
54
XDOT = 22264
346524 XDOT = 6748
811267
YDOT = 6654
563299 feet/sec YDOT = 2103
989390 meter/sec
ZDOT = 9574
830837 ZDOT = 2951
282702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5994768
89 X = 1827205
56
Y = -15141707
62 feet Y = -4615192
48 meter
Z = -15183799
05 Z = -4628021
95
XDOT = 22065
146264 XDOT = 6725
456581
YDOT = -1016
887989 feet/sec YDOT = -309
947459 meter/sec
ZDOT = 9721
589307 ZDOT = 2963
140421
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 18172
31512506
00016717 00000-0 10270-3 0 9032
2 25544 51
6424 358
1382 0003248 238
2382 121
8454 15
53975871 39153
Satellite: ISS
Catalog Number: 25544
Epoch time: 18172
31512506 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 358
1382 deg
Eccentricity:
0003248
Arg of perigee: 238
2382 deg
Mean anomaly: 121
8454 deg
Mean motion: 15
53975871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3915
Checksum: 309
Coasting Arc #5 (Orbit 3930)
---------------------------------------
Vector Time (GMT): 2018/173/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4561587
87 A = 6784323
55 meter
Y = 3479375
21 meter E =
0009355
Z = 3612408
37 I = 51
59859
XDOT = -5624
733563 Wp = 94
57170
YDOT = -2791
029234 meter/sec RA = 352
60485 deg
ZDOT = -4405
309358 TA = 42
59162
MA = 42
51911
Ha = 220
456 n
mi
Hp = 215
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14965839
47 X = -4617703
37
Y = 11415272
99 feet Y = 3428050
27 meter
Z = 11851733
49 Z = 3590113
77
XDOT = -18453
850272 XDOT = -5571
706769
YDOT = -9156
920058 feet/sec YDOT = -2853
631957 meter/sec
ZDOT = -14453
114692 ZDOT = -4432
503888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10478364
48 X = -3193805
49
Y = 15711672
99 feet Y = 4788917
93 meter
Z = 11751408
65 Z = 3581829
36
XDOT = -19198
374469 XDOT = -5851
664538
YDOT = -1880
421642 feet/sec YDOT = -573
152516 meter/sec
ZDOT = -14574
324252 ZDOT = -4442
254032
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 18173
34406036
00016717 00000-0 10270-3 0 9047
2 25544 51
6420 353
0107 0003073 241
5464 118
5380 15
53978367 39314
Satellite: ISS
Catalog Number: 25544
Epoch time: 18173
34406036 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 353
0107 deg
Eccentricity:
0003073
Arg of perigee: 241
5464 deg
Mean anomaly: 118
5380 deg
Mean motion: 15
53978367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3931
Checksum: 295
Coasting Arc #6 (Orbit 3945)
---------------------------------------
Vector Time (GMT): 2018/174/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5632011
88 A = 6787668
78 meter
Y = -3053302
15 meter E =
0003453
Z = -2237809
31 I = 51
57705
XDOT = 4076
020048 Wp = 20
24365
YDOT = 3529
831827 meter/sec RA = 347
62273 deg
ZDOT = 5447
861926 TA = 314
86364
MA = 314
89168
Ha = 220
254 n
mi
Hp = 215
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18477729
27 X = 5676606
30
Y = -10017395
49 feet Y = -2990071
51 meter
Z = -7341894
05 Z = -2210342
88
XDOT = 13372
769185 XDOT = 4009
782636
YDOT = 11580
813082 feet/sec YDOT = 3575
041725 meter/sec
ZDOT = 17873
562749 ZDOT = 5467
501404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13956921
74 X = 4254069
75
Y = -15772620
99 feet Y = -4807494
88 meter
Z = -7218508
32 Z = -2200201
34
XDOT = 15276
175468 XDOT = 4656
178283
YDOT = 5306
339265 feet/sec YDOT = 1617
372208 meter/sec
ZDOT = 17960
842019 ZDOT = 5474
464648
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 18174
30868446
00016717 00000-0 10270-3 0 9052
2 25544 51
6417 348
2029 0003209 246
4933 113
5882 15
53992620 39461
Satellite: ISS
Catalog Number: 25544
Epoch time: 18174
30868446 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 348
2029 deg
Eccentricity:
0003209
Arg of perigee: 246
4933 deg
Mean anomaly: 113
5882 deg
Mean motion: 15
53992620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3946
Checksum: 327
Coasting Arc #7 (Orbit 3961)
---------------------------------------
Vector Time (GMT): 2018/175/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6281994
02 A = 6789712
73 meter
Y = 2481040
96 meter E =
0011827
Z = 622732
71 I = 51
55171
XDOT = -2275
175711 Wp = 142
20174
YDOT = -4250
790703 meter/sec RA = 342
64670 deg
ZDOT = -5964
898753 TA = 31
06606
MA = 30
99618
Ha = 220
263 n
mi
Hp = 216
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20610216
59 X = -6312295
73
Y = 8139898
17 feet Y = 2410621
87 meter
Z = 2043086
31 Z = 592143
56
XDOT = -7464
487240 XDOT = -2198
498671
YDOT = -13946
163723 feet/sec YDOT = -4275
803785 meter/sec
ZDOT = -19569
877800 ZDOT = -5975
765126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16315927
30 X = -4973094
64
Y = 15012377
95 feet Y = 4575772
80 meter
Z = 1905832
19 Z = 580897
65
XDOT = -10765
353991 XDOT = -3281
279896
YDOT = -9186
894219 feet/sec YDOT = -2800
165358 meter/sec
ZDOT = -19617
786011 ZDOT = -5979
501176
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 18175
33761653
00016717 00000-0 10270-3 0 9069
2 25544 51
6419 343
0753 0003253 248
0661 112
0146 15
53948045 39622
Satellite: ISS
Catalog Number: 25544
Epoch time: 18175
33761653 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 343
0753 deg
Eccentricity:
0003253
Arg of perigee: 248
0661 deg
Mean anomaly: 112
0146 deg
Mean motion: 15
53948045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3962
Checksum: 305
Coasting Arc #8 (Orbit 3977)
---------------------------------------
Vector Time (GMT): 2018/176/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6466965
54 A = 6789206
86 meter
Y = -1769118
55 meter E =
0010574
Z = 1032521
98 I = 51
51934
XDOT = 394
393476 Wp = 50
17608
YDOT = 4897
556431 meter/sec RA = 337
66890 deg
ZDOT = 5887
783781 TA = 321
03570
MA = 321
11185
Ha = 220
055 n
mi
Hp = 216
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21217078
55 X = 6481252
21
Y = -5804194
73 feet Y = -1696720
76 meter
Z = 3387539
29 Z = 1063970
78
XDOT = 1293
941849 XDOT = 310
998524
YDOT = 16068
098527 feet/sec YDOT = 4901
499657 meter/sec
ZDOT = 19316
875922 ZDOT = 5889
497779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17461881
73 X = 5322381
55
Y = -13340194
41 feet Y = -4066091
26 meter
Z = 3528515
39 Z = 1075491
49
XDOT = 6144
116652 XDOT = 1872
726755
YDOT = 13181
514190 feet/sec YDOT = 4017
725525 meter/sec
ZDOT = 19323
733987 ZDOT = 5889
874119
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 18176
36654206
00016717 00000-0 10270-3 0 9079
2 25544 51
6418 337
9461 0003297 256
7502 103
3283 15
54002674 39789
Satellite: ISS
Catalog Number: 25544
Epoch time: 18176
36654206 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 337
9461 deg
Eccentricity:
0003297
Arg of perigee: 256
7502 deg
Mean anomaly: 103
3283 deg
Mean motion: 15
54002674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3978
Checksum: 322
Coasting Arc #9 (Orbit 3992)
---------------------------------------
Vector Time (GMT): 2018/177/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6203653
34 A = 6786826
78 meter
Y = 868048
45 meter E =
0003609
Z = -2607172
71 I = 51
47981
XDOT = 1435
191067 Wp = 167
77445
YDOT = -5422
336595 meter/sec RA = 332
68644 deg
ZDOT = -5225
103170 TA = 41
64051
MA = 41
61304
Ha = 220
018 n
mi
Hp = 216
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20353193
37 X = -6200234
75
Y = 2847927
99 feet Y = 798694
46 meter
Z = -8553716
25 Z = -2637299
49
XDOT = 4708
632111 XDOT = 1521
099259
YDOT = -17789
818225 feet/sec YDOT = -5405
806121 meter/sec
ZDOT = -17142
726935 ZDOT = -5217
923716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17561036
14 X = -5352603
81
Y = 10566316
05 feet Y = 3220613
13 meter
Z = -8688625
37 Z = -2648293
01
XDOT = -1757
999294 XDOT = -535
838185
YDOT = -16978
293720 feet/sec YDOT = -5174
983926 meter/sec
ZDOT = -17109
717906 ZDOT = -5215
042018
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 18177
33116060
00016717 00000-0 10270-3 0 9089
2 25544 51
6406 333
1386 0003355 259
6377 100
4397 15
53965950 39932
Satellite: ISS
Catalog Number: 25544
Epoch time: 18177
33116060 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 333
1386 deg
Eccentricity:
0003355
Arg of perigee: 259
6377 deg
Mean anomaly: 100
4397 deg
Mean motion: 15
53965950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3993
Checksum: 325
Coasting Arc #10 (Orbit 4008)
---------------------------------------
Vector Time (GMT): 2018/178/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5541089
32 A = 6783194
49 meter
Y = 177848
24 meter E =
0007925
Z = 3903522
85 I = 51
43912
XDOT = -3047
531037 Wp = 105
17376
YDOT = 5751
701708 meter/sec RA = 327
69303 deg
ZDOT = 4055
022535 TA = 302
23978
MA = 302
31656
Ha = 219
935 n
mi
Hp = 216
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18179426
92 X = 5519727
55
Y = 583491
59 feet Y = 239692
42 meter
Z = 12806833
51 Z = 3930387
63
XDOT = -9998
461408 XDOT = -3131
318753
YDOT = 18870
412429 feet/sec YDOT = 5717
152952 meter/sec
ZDOT = 13303
879709 ZDOT = 4040
016178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16763422
31 X = 5109491
12
Y = -6835785
11 feet Y = -2083547
30 meter
Z = 12926976
62 Z = 3940142
47
XDOT = -2024
124444 XDOT = -616
953131
YDOT = 20120
989467 feet/sec YDOT = 6132
877590 meter/sec
ZDOT = 13235
810585 ZDOT = 4034
275066
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 18178
36008516
00016717 00000-0 10270-3 0 9090
2 25544 51
6408 328
0102 0003274 266
2998 93
7780 15
53974111 40094
Satellite: ISS
Catalog Number: 25544
Epoch time: 18178
36008516 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 328
0102 deg
Eccentricity:
0003274
Arg of perigee: 266
2998 deg
Mean anomaly: 93
7780 deg
Mean motion: 15
53974111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4009
Checksum: 318
Coasting Arc #11 (Orbit 4023)
---------------------------------------
Vector Time (GMT): 2018/179/07:18:12
895
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4565900
92 A = 6779697
42 meter
Y = -1367645
45 meter E =
0008584
Z = -4829631
05 I = 51
39996
XDOT = 4352
686196 Wp = 65
33399
YDOT = -5799
331234 meter/sec RA = 322
68692 deg
ZDOT = -2472
713169 TA = 180
27279
MA = 180
27326
Ha = 219
940 n
mi
Hp = 215
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14979989
90 X = -4526808
53
Y = -4487025
75 feet Y = -1418485
11 meter
Z = -15845246
24 Z = -4851715
77
XDOT = 14280
466523 XDOT = 4429
223474
YDOT = -19026
677276 feet/sec YDOT = -5750
228136 meter/sec
ZDOT = -8112
576014 ZDOT = -2451
384527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15377056
35 X = -4686926
78
Y = 2224025
91 feet Y = 677883
10 meter
Z = -15943812
99 Z = -4859674
20
XDOT = 5103
465543 XDOT = 1555
536297
YDOT = -22182
847026 feet/sec YDOT = -6761
331774 meter/sec
ZDOT = -8016
226424 ZDOT = -2443
345814
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 18179
32469717
00016717 00000-0 10270-3 0 9103
2 25544 51
6405 323
2016 0003402 269
8152 90
2611 15
54002630 40247
Satellite: ISS
Catalog Number: 25544
Epoch time: 18179
32469717 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 323
2016 deg
Eccentricity:
0003402
Arg of perigee: 269
8152 deg
Mean anomaly: 90
2611 deg
Mean motion: 15
54002630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4024
Checksum: 274
Coasting Arc #12 (Orbit 4028)
---------------------------------------
Vector Time (GMT): 2018/179/14:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 24070
95 A = 6780180
97 meter
Y = 4843169
83 meter E =
0004826
Z = 4743034
38 I = 51
39481
XDOT = -6684
288743 Wp = 49
79981
YDOT = 2649
590777 meter/sec RA = 321
15195 deg
ZDOT = -2666
750713 TA = 66
64773
MA = 66
59696
Ha = 220
071 n
mi
Hp = 216
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 78972
93 X = -53127
49
Y = 15889664
79 feet Y = 4843006
57 meter
Z = 15561136
41 Z = 4742964
61
XDOT = -21930
081178 XDOT = -6700
466830
YDOT = 8692
883127 feet/sec YDOT = 2574
752440 meter/sec
ZDOT = -8749
182128 ZDOT = -2699
259303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11683390
36 X = 3561097
38
Y = -10771267
99 feet Y = -3283082
48 meter
Z = 15560039
39 Z = 4742700
00
XDOT = 20445
818706 XDOT = 6231
885542
YDOT = 9304
530679 feet/sec YDOT = 2836
020951 meter/sec
ZDOT = -8895
028135 ZDOT = -2711
204575
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 18179
64623627
00016717 00000-0 10270-3 0 9111
2 25544 51
6418 321
5960 0003149 261
3017 98
7779 15
53992352 40296
Satellite: ISS
Catalog Number: 25544
Epoch time: 18179
64623627 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 321
5960 deg
Eccentricity:
0003149
Arg of perigee: 261
3017 deg
Mean anomaly: 98
7779 deg
Mean motion: 15
53992352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 331
Coasting Arc #13 (Orbit 4040)
---------------------------------------
Vector Time (GMT): 2018/180/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1455356
86 A = 6778600
18 meter
Y = -4221002
76 meter E =
0010593
Z = -5109978
43 I = 51
36541
XDOT = 6278
383348 Wp = 106
41386
YDOT = -4090
330990 meter/sec RA = 317
14880 deg
ZDOT = 1590
427336 TA = 179
00129
MA = 178
99917
Ha = 220
082 n
mi
Hp = 215
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4774792
84 X = -1383226
94
Y = -13848434
27 feet Y = -4236873
44 meter
Z = -16765021
10 Z = -5116873
48
XDOT = 20598
370565 XDOT = 6315
930549
YDOT = -13419
721097 feet/sec YDOT = -4019
912097 meter/sec
ZDOT = 5217
937455 ZDOT = 1621
015800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14427355
66 X = -4397458
01
Y = -2327415
66 feet Y = -709396
29 meter
Z = -16795185
49 Z = -5119172
54
XDOT = -2460
937058 XDOT = -750
093615
YDOT = -23395
403236 feet/sec YDOT = -7130
918906 meter/sec
ZDOT = 5355
421669 ZDOT = 1632
332525
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 18180
41792450
00016717 00000-0 10270-3 0 9120
2 25544 51
6378 317
7496 0003040 266
7031 93
3774 15
54004105 40418
Satellite: ISS
Catalog Number: 25544
Epoch time: 18180
41792450 = yrday
fracday
Element set: 912
Inclination: 51
6378 deg
RA of node: 317
7496 deg
Eccentricity:
0003040
Arg of perigee: 266
7031 deg
Mean anomaly: 93
3774 deg
Mean motion: 15
54004105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4041
Checksum: 292
Coasting Arc #14 (Orbit 4056)
---------------------------------------
Vector Time (GMT): 2018/181/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 95819
92 A = 6781520
77 meter
Y = 5149318
77 meter E =
0006462
Z = 4408814
29 I = 51
35085
XDOT = -6250
870519 Wp = 60
30452
YDOT = 2959
322205 meter/sec RA = 312
13616 deg
ZDOT = -3313
707854 TA = 63
32043
MA = 63
25428
Ha = 220
059 n
mi
Hp = 216
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 314369
81 X = 16816
26
Y = 16894090
45 feet Y = 5149947
89 meter
Z = 14464613
82 Z = 4409088
64
XDOT = -20508
105376 XDOT = -6267
401845
YDOT = 9709
062353 feet/sec YDOT = 2889
328727 meter/sec
ZDOT = -10871
744929 ZDOT = -3344
111768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15180520
57 X = 4627022
67
Y = 7419504
48 feet Y = 2261464
96 meter
Z = 14465024
10 Z = 4408939
35
XDOT = -2
815226 XDOT = -
858081
YDOT = 21510
855685 feet/sec YDOT = 6556
508813 meter/sec
ZDOT = -11008
215132 ZDOT = -3355
303972
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 18181
44684091
00016717 00000-0 10270-3 0 9136
2 25544 51
6373 312
6216 0003165 269
9697 90
1092 15
53977910 40575
Satellite: ISS
Catalog Number: 25544
Epoch time: 18181
44684091 = yrday
fracday
Element set: 913
Inclination: 51
6373 deg
RA of node: 312
6216 deg
Eccentricity:
0003165
Arg of perigee: 269
9697 deg
Mean anomaly: 90
1092 deg
Mean motion: 15
53977910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4057
Checksum: 325
Coasting Arc #15 (Orbit 4071)
---------------------------------------
Vector Time (GMT): 2018/182/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1120966
93 A = 6785110
76 meter
Y = -5831341
06 meter E =
0001721
Z = -3283283
66 I = 51
34382
XDOT = 5862
336649 Wp = 63
84615
YDOT = -1516
914125 meter/sec RA = 307
13055 deg
ZDOT = 4698
308705 TA = 257
86439
MA = 257
88367
Ha = 220
059 n
mi
Hp = 215
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3677713
01 X = 1202039
52
Y = -19131696
40 feet Y = -5818351
88 meter
Z = -10771928
03 Z = -3277642
35
XDOT = 19233
387957 XDOT = 5856
041901
YDOT = -4976
752378 feet/sec YDOT = -1451
393270 meter/sec
ZDOT = 15414
398639 ZDOT = 4726
770036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15593204
43 X = -4752808
71
Y = -11703074
56 feet Y = -3567097
13 meter
Z = -10745782
19 Z = -3275314
41
XDOT = 2994
198024 XDOT = 912
631558
YDOT = -18252
068112 feet/sec YDOT = -5563
230361 meter/sec
ZDOT = 15541
946155 ZDOT = 4737
185188
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 18182
41144642
00016717 00000-0 10270-3 0 9148
2 25544 51
6392 307
8137 0003070 274
2122 85
8680 15
54014967 40727
Satellite: ISS
Catalog Number: 25544
Epoch time: 18182
41144642 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 307
8137 deg
Eccentricity:
0003070
Arg of perigee: 274
2122 deg
Mean anomaly: 85
8680 deg
Mean motion: 15
54014967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4072
Checksum: 299
Coasting Arc #16 (Orbit 4087)
---------------------------------------
Vector Time (GMT): 2018/183/09:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 922905
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2164146
89 A = 6788289
62 meter
Y = 6168157
82 meter E =
0010968
Z = 1809832
57 I = 51
33397
XDOT = -5209
007361 Wp = 118
47671
YDOT = -170
720686 meter/sec RA = 302
13356 deg
ZDOT = -5626
056561 TA = 41
54043
MA = 41
45713
Ha = 220
061 n
mi
Hp = 215
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7100219
47 X = -2241751
18
Y = 20236738
25 feet Y = 6143522
70 meter
Z = 5937770
91 Z = 1799132
30
XDOT = -17089
919163 XDOT = -5179
383129
YDOT = -560
107239 feet/sec YDOT = -228
805083 meter/sec
ZDOT = -18458
190816 ZDOT = -5651
287845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15371837
39 X = 4685336
04
Y = 14974064
00 feet Y = 4564094
71 meter
Z = 5888958
93 Z = 1794954
68
XDOT = -6539
251204 XDOT = -1993
163767
YDOT = 14043
698279 feet/sec YDOT = 4280
519235 meter/sec
ZDOT = -18571
025442 ZDOT = -5660
448555
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 18183
44035543
00016717 00000-0 10270-3 0 9152
2 25544 51
6378 302
6855 0003123 279
2976 80
7823 15
54016861 40887
Satellite: ISS
Catalog Number: 25544
Epoch time: 18183
44035543 = yrday
fracday
Element set: 915
Inclination: 51
6378 deg
RA of node: 302
6855 deg
Eccentricity:
0003123
Arg of perigee: 279
2976 deg
Mean anomaly: 80
7823 deg
Mean motion: 15
54016861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4088
Checksum: 323
Coasting Arc #17 (Orbit 4088)
---------------------------------------
Vector Time (GMT): 2018/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947612
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1590573
45 A = 6787391
87 meter
Y = -6163095
27 meter E =
0004675
Z = -2349674
79 I = 51
33219
XDOT = 5438
171144 Wp = 11
44913
YDOT = -639
641976 meter/sec RA = 301
65310 deg
ZDOT = 5365
371405 TA = 322
22070
MA = 322
25352
Ha = 220
080 n
mi
Hp = 216
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5218416
83 X = 1670785
99
Y = -20220128
84 feet Y = -6144859
61 meter
Z = -7708906
79 Z = -2341754
35
XDOT = 17841
768844 XDOT = 5418
857830
YDOT = -2098
562913 feet/sec YDOT = -578
937220 meter/sec
ZDOT = 17602
924557 ZDOT = 5391
740820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20816410
75 X = -6344842
00
Y = -1822644
38 feet Y = -555542
01 meter
Z = -7672531
49 Z = -2338587
60
XDOT = -5157
254004 XDOT = -1571
931021
YDOT = -15608
591698 feet/sec YDOT = -4757
498750 meter/sec
ZDOT = 17720
974501 ZDOT = 5401
353028
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 18183
50466233
00016717 00000-0 10270-3 0 9164
2 25544 51
6410 302
3659 0003180 279
8010 80
2783 15
53996316 40893
Satellite: ISS
Catalog Number: 25544
Epoch time: 18183
50466233 = yrday
fracday
Element set: 916
Inclination: 51
6410 deg
RA of node: 302
3659 deg
Eccentricity:
0003180
Arg of perigee: 279
8010 deg
Mean anomaly: 80
2783 deg
Mean motion: 15
53996316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4089
Checksum: 311
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