[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 9th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
042/08:58:44
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
042/12:24:48
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
6
043/19:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
6
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
Coasting Arc #1 (Orbit 1865)
---------------------------------------
Vector Time (GMT): 2018/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3494274
82 A = 6789062
28 meter
Y = -5725334
94 meter E =
0016458
Z = 1001337
84 I = 51
31852
XDOT = 3675
281224 Wp = 60
07942
YDOT = 3282
512552 meter/sec RA = 294
53188 deg
ZDOT = 5878
457137 TA = 310
82341
MA = 310
96602
Ha = 222
189 n
mi
Hp = 213
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11464156
23 X = 3553173
47
Y = -18783907
30 feet Y = -5685930
23 meter
Z = 3285229
13 Z = 1018454
71
XDOT = 12058
009265 XDOT = 3609
748120
YDOT = 10769
398136 feet/sec YDOT = 3323
245755 meter/sec
ZDOT = 19286
276697 ZDOT = 5896
150880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20997997
18 X = 6400189
54
Y = -6544762
76 feet Y = -1994843
69 meter
Z = 3362287
42 Z = 1024825
21
XDOT = 1365
626502 XDOT = 416
242958
YDOT = 14436
136220 feet/sec YDOT = 4400
134320 meter/sec
ZDOT = 19364
504288 ZDOT = 5902
300907
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 18040
56232320
00016717 00000-0 10270-3 0 9003
2 25544 51
6421 294
9562 0003081 79
1822 280
9678 15
54068781 18665
Satellite: ISS
Catalog Number: 25544
Epoch time: 18040
56232320 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 294
9562 deg
Eccentricity:
0003081
Arg of perigee: 79
1822 deg
Mean anomaly: 280
9678 deg
Mean motion: 15
54068781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1866
Checksum: 312
Coasting Arc #2 (Orbit 1880)
---------------------------------------
Vector Time (GMT): 2018/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3947777
55 A = 6786587
60 meter
Y = 4863324
98 meter E =
0007512
Z = -2613741
69 I = 51
29731
XDOT = -2666
409906 Wp = 110
58710
YDOT = -4953
099685 meter/sec RA = 289
53615 deg
ZDOT = -5203
550833 TA = 98
98046
MA = 98
89542
Ha = 222
183 n
mi
Hp = 213
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12952026
08 X = -3989171
20
Y = 15955790
61 feet Y = 4818946
74 meter
Z = -8575268
01 Z = -2633018
89
XDOT = -8748
063997 XDOT = -2585
549171
YDOT = -16250
327049 feet/sec YDOT = -4982
465263 meter/sec
ZDOT = -17072
017170 ZDOT = -5216
306638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20157991
87 X = -6144155
92
Y = 3808684
78 feet Y = 1160887
12 meter
Z = -8661797
68 Z = -2640115
93
XDOT = 4220
519205 XDOT = 1286
414254
YDOT = -16506
173862 feet/sec YDOT = -5031
081793 meter/sec
ZDOT = -17128
022444 ZDOT = -5220
621241
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 18041
52688660
00016717 00000-0 10270-3 0 9013
2 25544 51
6419 290
1489 0003003 84
4747 275
6748 15
54054067 18815
Satellite: ISS
Catalog Number: 25544
Epoch time: 18041
52688660 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 290
1489 deg
Eccentricity:
0003003
Arg of perigee: 84
4747 deg
Mean anomaly: 275
6748 deg
Mean motion: 15
54054067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1881
Checksum: 322
Coasting Arc #3 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2018/042/08:58:44
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4450433
48 A = 6779846
07 meter
Y = -1970755
61 meter E =
0010439
Z = 4712691
12 I = 51
26416
XDOT = 304
384005 Wp = 109
15716
YDOT = 7174
310001 meter/sec RA = 285
15538 deg
ZDOT = 2704
425340 TA = 313
93800
MA = 314
02410
Ha = 222
017 n
mi
Hp = 213
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14601159
72 X = 4449248
93
Y = -6465733
62 feet Y = -1920994
36 meter
Z = 15461585
02 Z = 4734306
50
XDOT = 998
635186 XDOT = 210
999894
YDOT = 23537
762471 feet/sec YDOT = 7177
191729 meter/sec
ZDOT = 8872
786550 ZDOT = 2705
676988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7749536
55 X = 2362058
74
Y = 13854644
49 feet Y = 4222895
64 meter
Z = 15558074
99 Z = 4742101
26
XDOT = -22346
639056 XDOT = -6811
255584
YDOT = 2500
426014 feet/sec YDOT = 762
129849 meter/sec
ZDOT = 8877
271525 ZDOT = 2705
792361
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 18042
42714455
00016717 00000-0 10270-3 0 9026
2 25544 51
6398 285
6610 0003053 87
8044 272
3458 15
54104000 18958
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
42714455 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 285
6610 deg
Eccentricity:
0003053
Arg of perigee: 87
8044 deg
Mean anomaly: 272
3458 deg
Mean motion: 15
54104000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 298
Coasting Arc #4 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2018/042/12:24:48
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1017757
32 A = 6785396
93 meter
Y = 5953998
55 meter E =
0016110
Z = 3076100
51 I = 51
28273
XDOT = -4888
968993 Wp = 93
35439
YDOT = 3360
213671 meter/sec RA = 284
39441 deg
ZDOT = -4865
187275 TA = 51
08132
MA = 50
93781
Ha = 222
168 n
mi
Hp = 213
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3339098
83 X = 936160
69
Y = 19534115
98 feet Y = 5964923
62 meter
Z = 10092193
29 Z = 3080846
06
XDOT = -16039
924518 XDOT = -4902
548416
YDOT = 11024
323069 feet/sec YDOT = 3305
465865 meter/sec
ZDOT = -15961
900508 ZDOT = -4888
968746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7943202
83 X = -2421088
22
Y = 18144648
20 feet Y = 5530488
77 meter
Z = 10112413
37 Z = 3082263
59
XDOT = -18045
501356 XDOT = -5500
268813
YDOT = 1094
015505 feet/sec YDOT = 333
455926 meter/sec
ZDOT = -16068
239198 ZDOT = -4897
599307
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 18042
55575296
00016717 00000-0 10270-3 0 9039
2 25544 51
6412 285
0208 0003137 84
9338 275
2173 15
54095595 18975
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
55575296 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 285
0208 deg
Eccentricity:
0003137
Arg of perigee: 84
9338 deg
Mean anomaly: 275
2173 deg
Mean motion: 15
54095595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1897
Checksum: 328
Coasting Arc #5 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2018/043/12:24:48
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -192295
17 A = 6788390
67 meter
Y = -6596500
77 meter E =
0010191
Z = -1579878
21 I = 51
28550
XDOT = 4888
207407 Wp = 50
52680
YDOT = -1502
744049 meter/sec RA = 279
39367 deg
ZDOT = 5710
547351 TA = 292
11254
MA = 292
22071
Ha = 222
138 n
mi
Hp = 213
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -630889
65 X = -110842
98
Y = -21642062
88 feet Y = -6598195
75 meter
Z = -5183327
48 Z = -1580614
33
XDOT = 16037
425877 XDOT = 4876
909997
YDOT = -4930
262627 feet/sec YDOT = -1448
143804 meter/sec
ZDOT = 18735
391572 ZDOT = 5734
264625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11016990
97 X = 3357978
85
Y = -18638106
10 feet Y = -5680894
74 meter
Z = -5185624
56 Z = -1580578
37
XDOT = 14735
699710 XDOT = 4491
441272
YDOT = 3496
510302 feet/sec YDOT = 1065
736340 meter/sec
ZDOT = 18841
164021 ZDOT = 5742
786794
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 18043
52031321
00016717 00000-0 10270-3 0 9044
2 25544 51
6412 280
2128 0002956 87
8977 272
2514 15
54085162 19125
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
52031321 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 280
2128 deg
Eccentricity:
0002956
Arg of perigee: 87
8977 deg
Mean anomaly: 272
2514 deg
Mean motion: 15
54085162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1912
Checksum: 293
Coasting Arc #6 (Orbit 1916)
---------------------------------------
Vector Time (GMT): 2018/043/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3608873
09 A = 6779009
31 meter
Y = 2887406
60 meter E =
0008798
Z = 4952880
25 I = 51
25139
XDOT = -2652
452543 Wp = 71
38352
YDOT = 6893
283186 meter/sec RA = 277
98319 deg
ZDOT = -2080
121174 TA = 38
98813
MA = 38
92473
Ha = 222
161 n
mi
Hp = 213
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11840134
79 X = 3552259
18
Y = 9473118
77 feet Y = 2927447
07 meter
Z = 16249607
13 Z = 4970272
93
XDOT = -8702
272123 XDOT = -2719
234069
YDOT = 22615
758485 feet/sec YDOT = 6863
248193 meter/sec
ZDOT = -6824
544534 ZDOT = -2093
167933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13061712
22 X = 3981209
88
Y = -7537427
22 feet Y = -2297407
82 meter
Z = 16326584
70 Z = 4976343
02
XDOT = 17435
429064 XDOT = 5314
318779
YDOT = 15262
627501 feet/sec YDOT = 4652
048862 meter/sec
ZDOT = -6883
625147 ZDOT = -2098
128945
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 18043
84183497
00016717 00000-0 10270-3 0 9052
2 25544 51
6402 278
6047 0003239 100
0300 260
1218 15
54058089 19178
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
84183497 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 278
6047 deg
Eccentricity:
0003239
Arg of perigee: 100
0300 deg
Mean anomaly: 260
1218 deg
Mean motion: 15
54058089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1917
Checksum: 294
Coasting Arc #7 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2018/044/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3090741
52 A = 6782172
25 meter
Y = -4412320
92 meter E =
0010758
Z = -4131443
80 I = 51
25838
XDOT = 3304
380686 Wp = 107
39282
YDOT = -5810
365572 meter/sec RA = 272
96507 deg
ZDOT = 3738
299562 TA = 201
32650
MA = 201
37137
Ha = 222
187 n
mi
Hp = 213
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10140228
07 X = -3021104
17
Y = -14476118
50 feet Y = -4446494
50 meter
Z = -13554605
63 Z = -4146287
87
XDOT = 10841
143984 XDOT = 3350
949947
YDOT = -19062
879173 feet/sec YDOT = -5773
153197 meter/sec
ZDOT = 12264
762341 ZDOT = 3754
464015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17049847
75 X = -5196793
59
Y = 4461728
52 feet Y = 1359934
85 meter
Z = -13620030
70 Z = -4151385
36
XDOT = -13876
311505 XDOT = -4229
499747
YDOT = -15413
411150 feet/sec YDOT = -4698
007719 meter/sec
ZDOT = 12337
544426 ZDOT = 3760
483541
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 18044
80639156
00016717 00000-0 10270-3 0 9068
2 25544 51
6399 273
7977 0003125 102
6557 257
4945 15
54081421 19326
Satellite: ISS
Catalog Number: 25544
Epoch time: 18044
80639156 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 273
7977 deg
Eccentricity:
0003125
Arg of perigee: 102
6557 deg
Mean anomaly: 257
4945 deg
Mean motion: 15
54081421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1932
Checksum: 328
Coasting Arc #8 (Orbit 1947)
---------------------------------------
Vector Time (GMT): 2018/045/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2488708
66 A = 6786010
22 meter
Y = 5623488
76 meter E =
0016516
Z = 2850965
88 I = 51
26966
XDOT = -3889
508260 Wp = 100
79685
YDOT = 4286
125821 meter/sec RA = 267
95582 deg
ZDOT = -5037
174411 TA = 46
57633
MA = 46
43900
Ha = 222
183 n
mi
Hp = 213
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8165054
66 X = 2411792
19
Y = 18449766
28 feet Y = 5650889
29 meter
Z = 9353562
60 Z = 2862867
74
XDOT = -12760
853872 XDOT = -3912
680501
YDOT = 14062
092587 feet/sec YDOT = 4242
500838 meter/sec
ZDOT = -16526
162765 ZDOT = -5056
124310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20086853
11 X = 6122472
83
Y = -1612942
14 feet Y = -491624
77 meter
Z = 9405736
34 Z = 2866868
44
XDOT = 9023
653530 XDOT = 2750
409596
YDOT = 15094
350881 feet/sec YDOT = 4600
758148 meter/sec
ZDOT = -16611
111387 ZDOT = -5063
066751
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 18045
83525220
00016717 00000-0 10270-3 0 9079
2 25544 51
6392 268
6691 0003224 108
1875 251
9628 15
54071770 19489
Satellite: ISS
Catalog Number: 25544
Epoch time: 18045
83525220 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 268
6691 deg
Eccentricity:
0003224
Arg of perigee: 108
1875 deg
Mean anomaly: 251
9628 deg
Mean motion: 15
54071770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1948
Checksum: 322
Coasting Arc #9 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2018/046/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1852481
07 A = 6788726
88 meter
Y = -6394589
67 meter E =
0010297
Z = -1315166
13 I = 51
28211
XDOT = 4377
837727 Wp = 54
23130
YDOT = -2452
259436 meter/sec RA = 262
95600 deg
ZDOT = 5794
847488 TA = 291
38657
MA = 291
49640
Ha = 222
169 n
mi
Hp = 213
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6077693
81 X = -1774449
14
Y = -20979624
91 feet Y = -6414869
18 meter
Z = -4314849
50 Z = -1323974
64
XDOT = 14362
984667 XDOT = 4376
786591
YDOT = -8045
470590 feet/sec YDOT = -2403
308920 meter/sec
ZDOT = 19011
966825 ZDOT = 5816
110581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21820650
41 X = -6650934
24
Y = -781091
70 feet Y = -238076
75 meter
Z = -4353166
80 Z = -1326845
24
XDOT = -3270
212278 XDOT = -996
760702
YDOT = -14442
508673 feet/sec YDOT = -4402
076643 meter/sec
ZDOT = 19106
946651 ZDOT = 5823
797339
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 18046
79980584
00016717 00000-0 10270-3 0 9084
2 25544 51
6403 263
8613 0003108 107
6566 252
4926 15
54077055 19631
Satellite: ISS
Catalog Number: 25544
Epoch time: 18046
79980584 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 263
8613 deg
Eccentricity:
0003108
Arg of perigee: 107
6566 deg
Mean anomaly: 252
4926 deg
Mean motion: 15
54077055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 329
Coasting Arc #10 (Orbit 1978)
---------------------------------------
Vector Time (GMT): 2018/047/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1094834
89 A = 6789367
04 meter
Y = 6682350
59 meter E =
0014210
Z = -402998
23 I = 51
28874
XDOT = -4797
409801 Wp = 132
30654
YDOT = 434
850830 meter/sec RA = 257
96134 deg
ZDOT = -5967
254783 TA = 52
05994
MA = 51
93161
Ha = 222
153 n
mi
Hp = 213
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3591977
97 X = 1021987
17
Y = 21923722
41 feet Y = 6694186
44 meter
Z = -1322172
68 Z = -397857
53
XDOT = -15739
533467 XDOT = -4772
930781
YDOT = 1426
675951 feet/sec YDOT = 381
339259 meter/sec
ZDOT = -19577
607556 ZDOT = -5990
498962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22010634
74 X = 6708841
47
Y = 3023489
56 feet Y = 921559
62 meter
Z = -1300199
92 Z = -396300
94
XDOT = -3020
299382 XDOT = -920
587251
YDOT = 13731
244553 feet/sec YDOT = 4185
283340 meter/sec
ZDOT = -19681
126975 ZDOT = -5998
807502
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
82866112
00016717 00000-0 10270-3 0 9090
2 25544 51
6396 258
7324 0003176 112
4494 247
6995 15
54092476 19796
Satellite: ISS
Catalog Number: 25544
Epoch time: 18047
82866112 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 258
7324 deg
Eccentricity:
0003176
Arg of perigee: 112
4494 deg
Mean anomaly: 247
6995 deg
Mean motion: 15
54092476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1979
Checksum: 350
Coasting Arc #11 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2018/048/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4192912
30 A = 6782582
65 meter
Y = 3535843
04 meter E =
0013667
Z = 3979366
82 I = 51
26767
XDOT = -1633
760551 Wp = 83
89020
YDOT = 6381
246378 meter/sec RA = 255
72716 deg
ZDOT = -3935
479237 TA = 47
27556
MA = 47
16059
Ha = 222
021 n
mi
Hp = 213
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13756273
94 X = 4133732
69
Y = 11600534
92 feet Y = 3582400
54 meter
Z = 13055665
43 Z = 3999590
02
XDOT = -5360
106796 XDOT = -1685
879902
YDOT = 20935
847697 feet/sec YDOT = 6362
684769 meter/sec
ZDOT = -12911
677286 ZDOT = -3943
542466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17563781
52 X = -5353440
61
Y = 3602091
79 feet Y = 1097917
58 meter
Z = 13145204
32 Z = 4006658
28
XDOT = -12960
228197 XDOT = -3950
277554
YDOT = -15785
133650 feet/sec YDOT = -4811
308736 meter/sec
ZDOT = -12948
427115 ZDOT = -3946
680585
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
27878499
00016717 00000-0 10270-3 0 9103
2 25544 51
6379 256
4914 0003019 102
4577 257
6913 15
54104604 19860
Satellite: ISS
Catalog Number: 25544
Epoch time: 18048
27878499 = yrday
fracday
Element set: 910
Inclination: 51
6379 deg
RA of node: 256
4914 deg
Eccentricity:
0003019
Arg of perigee: 102
4577 deg
Mean anomaly: 257
6913 deg
Mean motion: 15
54104604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 337
Coasting Arc #12 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2018/049/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3965554
67 A = 6786317
33 meter
Y = -4807433
43 meter E =
0007134
Z = -2689828
47 I = 51
28877
XDOT = 2614
761219 Wp = 75
51935
YDOT = -5032
452764 meter/sec RA = 250
72015 deg
ZDOT = 5152
695838 TA = 253
95965
MA = 254
03822
Ha = 222
099 n
mi
Hp = 213
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13010349
98 X = -3898436
41
Y = -15772419
40 feet Y = -4851403
98 meter
Z = -8824896
55 Z = -2708927
88
XDOT = 8578
612924 XDOT = 2645
812542
YDOT = -16510
671798 feet/sec YDOT = -5003
038570 meter/sec
ZDOT = 16905
170071 ZDOT = 5165
473115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20393099
69 X = 6215816
79
Y = -814540
27 feet Y = -248271
87 meter
Z = -8909277
67 Z = -2715547
83
XDOT = 7999
910174 XDOT = 2438
372621
YDOT = 15224
994508 feet/sec YDOT = 4640
578326 meter/sec
ZDOT = 16962
709403 ZDOT = 5170
233826
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
24333529
00016717 00000-0 10270-3 0 9112
2 25544 51
6376 251
6835 0002979 107
0946 253
0533 15
54088002 20011
Satellite: ISS
Catalog Number: 25544
Epoch time: 18049
24333529 = yrday
fracday
Element set: 911
Inclination: 51
6376 deg
RA of node: 251
6835 deg
Eccentricity:
0002979
Arg of perigee: 107
0946 deg
Mean anomaly: 253
0533 deg
Mean motion: 15
54088002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 297
Coasting Arc #13 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2018/050/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3518158
50 A = 6788912
39 meter
Y = 5695715
46 meter E =
0016549
Z = 1080343
73 I = 51
31073
XDOT = -3630
505850 Wp = 120
94654
YDOT = 3365
127591 meter/sec RA = 245
72239 deg
ZDOT = -5860
118301 TA = 47
27643
MA = 47
13723
Ha = 222
069 n
mi
Hp = 213
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11542514
78 X = 3448958
34
Y = 18686730
51 feet Y = 5734671
12 meter
Z = 3544434
82 Z = 1097264
79
XDOT = -11911
108432 XDOT = -3639
400872
YDOT = 11040
444853 feet/sec YDOT = 3324
478434 meter/sec
ZDOT = -19226
109910 ZDOT = -5877
775715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21885277
99 X = -6670632
73
Y = -1709934
50 feet Y = -521188
04 meter
Z = 3619018
38 Z = 1103076
80
XDOT = -2095
976707 XDOT = -638
853700
YDOT = -14430
159352 feet/sec YDOT = -4398
312570 meter/sec
ZDOT = -19305
146759 ZDOT = -5884
208732
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
27218655
00016717 00000-0 10270-3 0 9120
2 25544 51
6390 246
5542 0002965 110
5712 249
5758 15
54095796 20174
Satellite: ISS
Catalog Number: 25544
Epoch time: 18050
27218655 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 246
5542 deg
Eccentricity:
0002965
Arg of perigee: 110
5712 deg
Mean anomaly: 249
5758 deg
Mean motion: 15
54095796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2017
Checksum: 318
Coasting Arc #14 (Orbit 2032)
---------------------------------------
Vector Time (GMT): 2018/051/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2877489
87 A = 6789282
34 meter
Y = -6113766
90 meter E =
0014747
Z = 598535
09 I = 51
32611
XDOT = 4581
164736 Wp = 61
52138
YDOT = -1563
585214 meter/sec RA = 240
73001 deg
ZDOT = 5947
932670 TA = 304
96783
MA = 305
10623
Ha = 222
073 n
mi
Hp = 213
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9440583
56 X = -2811817
55
Y = -20058290
36 feet Y = -6145577
71 meter
Z = 1963697
79 Z = 584717
53
XDOT = 15030
068033 XDOT = 4569
417111
YDOT = -5129
872750 feet/sec YDOT = -1512
420568 meter/sec
ZDOT = 19514
214795 ZDOT = 5970
157736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21844147
57 X = 6658096
18
Y = 3811517
76 feet Y = 1161750
61 meter
Z = 1902968
39 Z = 580024
76
XDOT = -4102
957583 XDOT = -1250
581471
YDOT = 13544
711028 feet/sec YDOT = 4128
427921 meter/sec
ZDOT = 19613
351909 ZDOT = 5978
149662
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
30103505
00016717 00000-0 10270-3 0 9133
2 25544 51
6387 241
4255 0002957 112
0747 248
0720 15
54096402 20337
Satellite: ISS
Catalog Number: 25544
Epoch time: 18051
30103505 = yrday
fracday
Element set: 913
Inclination: 51
6387 deg
RA of node: 241
4255 deg
Eccentricity:
0002957
Arg of perigee: 112
0747 deg
Mean anomaly: 248
0720 deg
Mean motion: 15
54096402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2033
Checksum: 274
Coasting Arc #15 (Orbit 2047)
---------------------------------------
Vector Time (GMT): 2018/052/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1959046
38 A = 6787248
46 meter
Y = 6090296
46 meter E =
0008804
Z = -2261917
87 I = 51
33735
XDOT = -5419
263446 Wp = 130
15148
YDOT = -260
515294 meter/sec RA = 235
73696 deg
ZDOT = -5414
631320 TA = 75
11917
MA = 75
02168
Ha = 222
042 n
mi
Hp = 213
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6427317
51 X = 1901784
54
Y = 19981287
60 feet Y = 6111883
49 meter
Z = -7420990
40 Z = -2252541
22
XDOT = -17779
735715 XDOT = -5389
646336
YDOT = -854
708970 feet/sec YDOT = -320
952111 meter/sec
ZDOT = -17764
538453 ZDOT = -5440
884024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20171259
54 X = -6148199
91
Y = -5855684
04 feet Y = -1784812
49 meter
Z = -7380014
63 Z = -2249428
46
XDOT = 10195
479743 XDOT = 3107
582226
YDOT = -12665
830573 feet/sec YDOT = -3860
545159 meter/sec
ZDOT = -17881
379588 ZDOT = -5450
244498
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
26557892
00016717 00000-0 10270-3 0 9142
2 25544 51
6397 236
6176 0002929 116
4781 243
6672 15
54104872 20485
Satellite: ISS
Catalog Number: 25544
Epoch time: 18052
26557892 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 236
6176 deg
Eccentricity:
0002929
Arg of perigee: 116
4781 deg
Mean anomaly: 243
6672 deg
Mean motion: 15
54104872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2048
Checksum: 331
Coasting Arc #16 (Orbit 2058)
---------------------------------------
Vector Time (GMT): 2018/052/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -101751
94 A = 6781920
30 meter
Y = 5338181
35 meter E =
0010107
Z = -4191261
47 I = 51
33262
XDOT = -6028
525996 Wp = 84
37061
YDOT = -2985
576806 meter/sec RA = 232
17643 deg
ZDOT = -3662
880695 TA = 147
89342
MA = 147
83183
Ha = 222
042 n
mi
Hp = 213
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -333831
84 X = -141078
59
Y = 17513718
35 feet Y = 5336823
27 meter
Z = -13750857
85 Z = -4191851
69
XDOT = -19778
628596 XDOT = -5976
900215
YDOT = -9795
199495 feet/sec YDOT = -3052
703558 meter/sec
ZDOT = -12017
325114 ZDOT = -3692
039320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12987992
27 X = 3958740
05
Y = -11750029
23 feet Y = -3581408
91 meter
Z = -13754153
39 Z = -4192265
95
XDOT = 5387
741833 XDOT = 1642
183711
YDOT = 20148
339753 feet/sec YDOT = 6141
213957 meter/sec
ZDOT = -12146
769570 ZDOT = -3702
335365
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
97290880
00016717 00000-0 10270-3 0 9152
2 25544 51
6392 233
0912 0003105 121
3785 238
7671 15
54117483 20593
Satellite: ISS
Catalog Number: 25544
Epoch time: 18052
97290880 = yrday
fracday
Element set: 915
Inclination: 51
6392 deg
RA of node: 233
0912 deg
Eccentricity:
0003105
Arg of perigee: 121
3785 deg
Mean anomaly: 238
7671 deg
Mean motion: 15
54117483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2059
Checksum: 309
Coasting Arc #17 (Orbit 2074)
---------------------------------------
Vector Time (GMT): 2018/053/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1403271
15 A = 6778749
48 meter
Y = -4360003
75 meter E =
0009057
Z = 4992231
10 I = 51
34235
XDOT = 6084
844487 Wp = 123
54516
YDOT = 4233
483810 meter/sec RA = 227
16200 deg
ZDOT = 1979
435255 TA = 307
12143
MA = 307
20415
Ha = 222
002 n
mi
Hp = 213
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4603907
98 X = 1427672
17
Y = -14304474
26 feet Y = -4344174
67 meter
Z = 16378710
95 Z = 4999107
18
XDOT = 19963
400549 XDOT = 6027
437314
YDOT = 13889
382580 feet/sec YDOT = 4301
207859 meter/sec
ZDOT = 6494
210154 ZDOT = 2008
853381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13421651
11 X = -4090919
26
Y = 6682190
53 feet Y = 2036731
67 meter
Z = 16409867
03 Z = 5001727
47
XDOT = -3323
712196 XDOT = -1013
067477
YDOT = -23004
963732 feet/sec YDOT = -7011
912946 meter/sec
ZDOT = 6624
671586 ZDOT = 2019
199899
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
00175185
00016717 00000-0 10270-3 0 9169
2 25544 51
6385 227
9618 0003103 122
7891 237
3561 15
54111613 20751
Satellite: ISS
Catalog Number: 25544
Epoch time: 18054
00175185 = yrday
fracday
Element set: 916
Inclination: 51
6385 deg
RA of node: 227
9618 deg
Eccentricity:
0003103
Arg of perigee: 122
7891 deg
Mean anomaly: 237
3561 deg
Mean motion: 15
54111613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2075
Checksum: 294
Coasting Arc #18 (Orbit 2089)
---------------------------------------
Vector Time (GMT): 2018/054/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2784587
61 A = 6777452
70 meter
Y = 3197123
13 meter E =
0017367
Z = -5302554
39 I = 51
36032
XDOT = -5714
689626 Wp = 95
54768
YDOT = -5093
834376 meter/sec RA = 222
14393 deg
ZDOT = -72
110760 TA = 173
77218
MA = 173
75056
Ha = 222
011 n
mi
Hp = 213
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9135786
11 X = -2794375
00
Y = 10489249
10 feet Y = 3165928
99 meter
Z = -17396832
00 Z = -5316104
73
XDOT = -18748
981712 XDOT = -5656
953992
YDOT = -16712
055038 feet/sec YDOT = -5157
417143 meter/sec
ZDOT = -236
583859 ZDOT = -99
729987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13796469
49 X = 4205163
90
Y = -1013689
77 feet Y = -308972
64 meter
Z = -17457564
57 Z = -5321065
68
XDOT = 1321
965667 XDOT = 402
935135
YDOT = 24069
745264 feet/sec YDOT = 7336
458356 meter/sec
ZDOT = -358
949472 ZDOT = -109
407799
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
96629005
00016717 00000-0 10270-3 0 9170
2 25544 51
6379 223
1545 0003020 126
4635 233
6796 15
54098136 20906
Satellite: ISS
Catalog Number: 25544
Epoch time: 18054
96629005 = yrday
fracday
Element set: 917
Inclination: 51
6379 deg
RA of node: 223
1545 deg
Eccentricity:
0003020
Arg of perigee: 126
4635 deg
Mean anomaly: 233
6796 deg
Mean motion: 15
54098136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2090
Checksum: 310
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