[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 5th 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) : 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
012/22:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 214
2
013/10:05:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
3
017/20:15:11
040 0
9 1
1 1
1
N/A 0
5 -0
1 221
6
000/00:00:22
080 -0
3 -0
0 214
4
018/18:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
3
Coasting Arc #1 (Orbit 1320)
---------------------------------------
Vector Time (GMT): 2018/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4419074
87 A = 6778020
34 meter
Y = -558943
08 meter E =
0012912
Z = -5120355
80 I = 51
98066
XDOT = -1079
443908 Wp = 63
89697
YDOT = 7381
195987 meter/sec RA = 108
79830 deg
ZDOT = -1735
204141 TA = 189
37744
MA = 189
40157
Ha = 220
618 n
mi
Hp = 215
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14498277
12 X = 4449868
29
Y = -1833802
76 feet Y = -509353
53 meter
Z = -16799067
58 Z = -5098815
03
XDOT = -3541
482639 XDOT = -1153
473628
YDOT = 24216
522266 feet/sec YDOT = 7368
711066 meter/sec
ZDOT = -5692
926973 ZDOT = -1740
627065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5353919
12 X = 1631874
55
Y = 13715487
99 feet Y = 4180480
74 meter
Z = -16703068
06 Z = -5091095
15
XDOT = -23337
143437 XDOT = -7113
161320
YDOT = 2137
455611 feet/sec YDOT = 651
496470 meter/sec
ZDOT = -5718
175510 ZDOT = -1742
899896
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 18005
51910597
00016717 00000-0 10270-3 0 9008
2 25544 51
6417 109
6597 0003025 333
1597 26
9398 15
54246583 13211
Satellite: ISS
Catalog Number: 25544
Epoch time: 18005
51910597 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 109
6597 deg
Eccentricity:
0003025
Arg of perigee: 333
1597 deg
Mean anomaly: 26
9398 deg
Mean motion: 15
54246583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1321
Checksum: 313
Coasting Arc #2 (Orbit 1336)
---------------------------------------
Vector Time (GMT): 2018/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3983027
76 A = 6776863
52 meter
Y = -1263548
19 meter E =
0003497
Z = 5334287
59 I = 51
98699
XDOT = 2015
739773 Wp = 20
81140
YDOT = -7396
508038 meter/sec RA = 103
82068 deg
ZDOT = -243
680583 TA = 71
51862
MA = 71
48062
Ha = 220
741 n
mi
Hp = 214
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13067676
37 X = -3994513
21
Y = -4145499
33 feet Y = -1308153
52 meter
Z = 17500943
55 Z = 5314911
75
XDOT = 6613
319466 XDOT = 2099
483361
YDOT = -24266
758656 feet/sec YDOT = -7373
498410 meter/sec
ZDOT = -799
476978 ZDOT = -233
685777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 555055
06 X = 169180
78
Y = -13807504
95 feet Y = -4208527
51 meter
Z = 17414852
17 Z = 5308046
94
XDOT = 24146
276488 XDOT = 7359
785074
YDOT = 6
422945 feet/sec YDOT = 1
957714 meter/sec
ZDOT = -753
857468 ZDOT = -229
775756
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 18006
54785134
00016717 00000-0 10270-3 0 9010
2 25544 51
6417 104
5302 0003055 336
9439 23
1576 15
54300266 13371
Satellite: ISS
Catalog Number: 25544
Epoch time: 18006
54785134 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 104
5302 deg
Eccentricity:
0003055
Arg of perigee: 336
9439 deg
Mean anomaly: 23
1576 deg
Mean motion: 15
54300266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1337
Checksum: 285
Coasting Arc #3 (Orbit 1351)
---------------------------------------
Vector Time (GMT): 2018/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3468350
76 A = 6778436
08 meter
Y = 3030769
39 meter E =
0011063
Z = -4982809
20 I = 51
99897
XDOT = -2789
565214 Wp = 92
34922
YDOT = 6789
419443 meter/sec RA = 98
84547 deg
ZDOT = 2191
663186 TA = 198
91946
MA = 198
96059
Ha = 220
782 n
mi
Hp = 214
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11379103
54 X = 3458405
72
Y = 9943469
13 feet Y = 3069499
37 meter
Z = -16347799
22 Z = -4965985
41
XDOT = -9152
116844 XDOT = -2875
924842
YDOT = 22274
998173 feet/sec YDOT = 6757
741700 meter/sec
ZDOT = 7190
496016 ZDOT = 2177
902983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6358502
02 X = -1938071
42
Y = 13796919
83 feet Y = 4205301
16 meter
Z = -16273339
25 Z = -4960113
80
XDOT = -22948
529837 XDOT = -6994
711894
YDOT = -2183
079325 feet/sec YDOT = -665
402578 meter/sec
ZDOT = 7128
187695 ZDOT = 2172
671610
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 18007
51229834
00016717 00000-0 10270-3 0 9029
2 25544 51
6416 99
7222 0003104 343
2537 16
8513 15
54292606 13526
Satellite: ISS
Catalog Number: 25544
Epoch time: 18007
51229834 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 99
7222 deg
Eccentricity:
0003104
Arg of perigee: 343
2537 deg
Mean anomaly: 16
8513 deg
Mean motion: 15
54292606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1352
Checksum: 289
Coasting Arc #4 (Orbit 1367)
---------------------------------------
Vector Time (GMT): 2018/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2869203
21 A = 6781920
46 meter
Y = -4604787
14 meter E =
0011211
Z = 4064666
21 I = 52
01472
XDOT = 3447
873570 Wp = 61
16956
YDOT = -5619
277241 meter/sec RA = 93
87693 deg
ZDOT = -3918
752513 TA = 69
30263
MA = 69
18249
Ha = 220
920 n
mi
Hp = 214
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9413396
35 X = -2837241
86
Y = -15107569
34 feet Y = -4636693
92 meter
Z = 13335519
06 Z = 4050806
23
XDOT = 11311
921161 XDOT = 3529
488689
YDOT = -18435
948955 feet/sec YDOT = -5580
264328 meter/sec
ZDOT = -12856
799582 ZDOT = -3901
805960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11640238
64 X = 3547944
74
Y = -13526979
23 feet Y = -4123023
27 meter
Z = 13274502
94 Z = 4046068
50
XDOT = 19988
471587 XDOT = 6092
486140
YDOT = 4615
187938 feet/sec YDOT = 1406
709284 meter/sec
ZDOT = -12780
466794 ZDOT = -3895
486279
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 18008
54103705
00016717 00000-0 10270-3 0 9032
2 25544 51
6417 94
5927 0003240 348
1782 11
9295 15
54288204 13688
Satellite: ISS
Catalog Number: 25544
Epoch time: 18008
54103705 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 94
5927 deg
Eccentricity:
0003240
Arg of perigee: 348
1782 deg
Mean anomaly: 11
9295 deg
Mean motion: 15
54288204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1368
Checksum: 304
Coasting Arc #5 (Orbit 1382)
---------------------------------------
Vector Time (GMT): 2018/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2237362
39 A = 6785816
89 meter
Y = 5794771
82 meter E =
0006830
Z = -2726127
90 I = 52
02789
XDOT = -3985
315012 Wp = 30
51337
YDOT = 3980
294639 meter/sec RA = 88
92005 deg
ZDOT = 5201
301170 TA = 298
83688
MA = 298
90542
Ha = 220
984 n
mi
Hp = 214
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7340427
78 X = 2185639
43
Y = 19011718
58 feet Y = 5819502
43 meter
Z = -8943989
19 Z = -2715385
07
XDOT = -13075
180487 XDOT = -4054
792604
YDOT = 13058
709447 feet/sec YDOT = 3935
339483 meter/sec
ZDOT = 17064
636386 ZDOT = 5181
773357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15770210
47 X = -4806760
15
Y = 12940836
83 feet Y = 3944367
07 meter
Z = -8897048
39 Z = -2711820
35
XDOT = -15568
015525 XDOT = -4745
131132
YDOT = -7325
653226 feet/sec YDOT = -2232
859103 meter/sec
ZDOT = 16977
049472 ZDOT = 5174
604679
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 18009
50547725
00016717 00000-0 10270-3 0 9044
2 25544 51
6408 89
7847 0003252 349
6267 10
4818 15
54262544 13833
Satellite: ISS
Catalog Number: 25544
Epoch time: 18009
50547725 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 89
7847 deg
Eccentricity:
0003252
Arg of perigee: 349
6267 deg
Mean anomaly: 10
4818 deg
Mean motion: 15
54262544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1383
Checksum: 321
Coasting Arc #6 (Orbit 1398)
---------------------------------------
Vector Time (GMT): 2018/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1516821
72 A = 6788401
53 meter
Y = -6527675
13 meter E =
0011861
Z = 1054699
31 I = 52
03542
XDOT = 4438
257370 Wp = 111
06741
YDOT = -1996
636709 meter/sec RA = 83
97232 deg
ZDOT = -5925
208153 TA = 57
55961
MA = 57
44495
Ha = 221
022 n
mi
Hp = 214
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4976449
21 X = -1448837
92
Y = -21416256
99 feet Y = -6544257
19 meter
Z = 3460299
56 Z = 1047495
98
XDOT = 14561
211845 XDOT = 4489
035877
YDOT = -6550
645372 feet/sec YDOT = -1946
720906 meter/sec
ZDOT = -19439
659296 ZDOT = -5903
525464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18602988
53 X = 5670190
90
Y = -11728761
51 feet Y = -3574926
51 meter
Z = 3429249
85 Z = 1045235
36
XDOT = 10140
973024 XDOT = 3090
968578
YDOT = 10381
408016 feet/sec YDOT = 3164
253163 meter/sec
ZDOT = -19342
777533 ZDOT = -5895
678592
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 18010
53421006
00016717 00000-0 10270-3 0 9053
2 25544 51
6411 84
6555 0003271 355
7475 4
3649 15
54288419 13997
Satellite: ISS
Catalog Number: 25544
Epoch time: 18010
53421006 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 84
6555 deg
Eccentricity:
0003271
Arg of perigee: 355
7475 deg
Mean anomaly: 4
3649 deg
Mean motion: 15
54288419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1399
Checksum: 304
Coasting Arc #7 (Orbit 1414)
---------------------------------------
Vector Time (GMT): 2018/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 742425
87 A = 6788749
98 meter
Y = 6702715
70 meter E =
0015643
Z = 700759
94 I = 52
03218
XDOT = -4786
133471 Wp = 42
28396
YDOT = -103
616705 meter/sec RA = 79
02807 deg
ZDOT = 5995
689228 TA = 325
24943
MA = 325
35151
Ha = 221
234 n
mi
Hp = 214
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2435780
40 X = 664015
21
Y = 21990537
07 feet Y = 6710579
55 meter
Z = 2299081
16 Z = 704176
29
XDOT = -15702
537634 XDOT = -4813
742877
YDOT = -339
949819 feet/sec YDOT = -157
293229 meter/sec
ZDOT = 19670
896416 ZDOT = 5972
372869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19823486
93 X = -6042198
82
Y = 9822468
55 feet Y = 2993888
41 meter
Z = 2313222
55 Z = 705070
23
XDOT = -4400
717407 XDOT = -1341
338666
YDOT = -13540
300156 feet/sec YDOT = -4127
083488 meter/sec
ZDOT = 19567
068097 ZDOT = 5964
042356
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 18011
56293952
00016717 00000-0 10270-3 0 9065
2 25544 51
6415 79
5260 0003512
8164 359
2994 15
54257159 14159
Satellite: ISS
Catalog Number: 25544
Epoch time: 18011
56293952 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 79
5260 deg
Eccentricity:
0003512
Arg of perigee:
8164 deg
Mean anomaly: 359
2994 deg
Mean motion: 15
54257159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1415
Checksum: 308
Coasting Arc #8 (Orbit 1429)
---------------------------------------
Vector Time (GMT): 2018/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 150472
62 A = 6786377
14 meter
Y = -6342260
83 meter E =
0004407
Z = -2413090
49 I = 52
01668
XDOT = 4995
490410 Wp = 95
09753
YDOT = 2166
487731 meter/sec RA = 74
08160 deg
ZDOT = -5391
445404 TA = 111
71416
MA = 111
66723
Ha = 221
216 n
mi
Hp = 214
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 493676
59 X = 233103
77
Y = -20807942
37 feet Y = -6340115
97 meter
Z = -7916963
54 Z = -2412159
27
XDOT = 16389
404231 XDOT = 4997
081553
YDOT = 7107
899379 feet/sec YDOT = 2222
359979 meter/sec
ZDOT = -17688
469172 ZDOT = -5367
175154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19614530
46 X = 5978508
88
Y = -6968955
44 feet Y = -2124137
62 meter
Z = -7911785
45 Z = -2411512
20
XDOT = -1207
961619 XDOT = -368
186701
YDOT = 16526
444213 feet/sec YDOT = 5037
260196 meter/sec
ZDOT = -17580
724875 ZDOT = -5358
604942
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 18012
52736944
00016717 00000-0 10270-3 0 9076
2 25544 51
6407 74
7179 0003401 5
7612 354
3579 15
54294792 14301
Satellite: ISS
Catalog Number: 25544
Epoch time: 18012
52736944 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 74
7179 deg
Eccentricity:
0003401
Arg of perigee: 5
7612 deg
Mean anomaly: 354
3579 deg
Mean motion: 15
54294792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1430
Checksum: 311
Coasting Arc #9 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2018/012/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4439737
55 A = 6781163
25 meter
Y = -2814061
04 meter E =
0011957
Z = 4279737
22 I = 51
99617
XDOT = 767
971411 Wp = 56
80086
YDOT = -6723
354294 meter/sec RA = 71
87710 deg
ZDOT = -3610
493756 TA = 69
94703
MA = 69
81836
Ha = 221
393 n
mi
Hp = 214
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14566068
07 X = -4428728
57
Y = -9232483
72 feet Y = -2863647
97 meter
Z = 14041132
61 Z = 4258197
18
XDOT = 2519
591244 XDOT = 860
634463
YDOT = -22058
248997 feet/sec YDOT = -6714
247946 meter/sec
ZDOT = -11845
451955 ZDOT = -3606
538653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9645296
25 X = -2939886
30
Y = 14389213
48 feet Y = 4385832
27 meter
Z = 13945655
07 Z = 4250635
67
XDOT = -20926
981980 XDOT = -6378
544108
YDOT = -2521
820629 feet/sec YDOT = -768
650928 meter/sec
ZDOT = -11826
737377 ZDOT = -3604
789552
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 18012
97743704
00016717 00000-0 10270-3 0 9088
2 25544 51
6417 72
4762 0003727 6
8095 353
3108 15
54300316 14377
Satellite: ISS
Catalog Number: 25544
Epoch time: 18012
97743704 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 72
4762 deg
Eccentricity:
0003727
Arg of perigee: 6
8095 deg
Mean anomaly: 353
3108 deg
Mean motion: 15
54300316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1437
Checksum: 299
Coasting Arc #10 (Orbit 1443)
---------------------------------------
Vector Time (GMT): 2018/013/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4321863
82 A = 6784028
66 meter
Y = 3978222
10 meter E =
0006133
Z = -3394632
87 I = 52
00078
XDOT = -1710
065781 Wp = 55
94996
YDOT = 5833
480822 meter/sec RA = 69
46869 deg
ZDOT = 4668
535401 TA = 264
63332
MA = 264
70329
Ha = 221
239 n
mi
Hp = 214
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14179343
23 X = 4293546
28
Y = 13051909
79 feet Y = 4026394
06 meter
Z = -11137246
95 Z = -3373707
38
XDOT = -5610
452038 XDOT = -1797
847361
YDOT = 19138
716606 feet/sec YDOT = 5813
866530 meter/sec
ZDOT = 15316
717196 ZDOT = 4660
015783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14614830
77 X = -4454600
42
Y = 12643801
93 feet Y = 3853830
83 meter
Z = -11044699
52 Z = -3366424
41
XDOT = -17427
117036 XDOT = -5311
785273
YDOT = -6825
265945 feet/sec YDOT = -2080
341060 meter/sec
ZDOT = 15277
811743 ZDOT = 4656
677019
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 18013
42750158
00016717 00000-0 10270-3 0 9091
2 25544 51
6418 70
2293 0003260 5
5154 354
6034 15
54297871 14448
Satellite: ISS
Catalog Number: 25544
Epoch time: 18013
42750158 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 70
2293 deg
Eccentricity:
0003260
Arg of perigee: 5
5154 deg
Mean anomaly: 354
6034 deg
Mean motion: 15
54297871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1444
Checksum: 293
Coasting Arc #11 (Orbit 1459)
---------------------------------------
Vector Time (GMT): 2018/014/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4033848
36 A = 6787427
71 meter
Y = -5135889
65 meter E =
0013601
Z = 1832262
22 I = 51
99994
XDOT = 2867
133476 Wp = 99
91457
YDOT = -4288
175116 meter/sec RA = 64
51518 deg
ZDOT = -5674
277020 TA = 60
03761
MA = 59
90265
Ha = 221
316 n
mi
Hp = 214
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13234410
62 X = -3985017
73
Y = -16850031
66 feet Y = -5180726
02 meter
Z = 6011359
01 Z = 1812785
58
XDOT = 9406
605893 XDOT = 2942
434284
YDOT = -14068
815996 feet/sec YDOT = -4255
691386 meter/sec
ZDOT = -18616
394423 ZDOT = -5660
167065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18078462
27 X = 5510315
30
Y = -11544164
20 feet Y = -3518661
25 meter
Z = 5925462
32 Z = 1806080
92
XDOT = 12218
325182 XDOT = 3724
145516
YDOT = 9554
189403 feet/sec YDOT = 2912
116930 meter/sec
ZDOT = -18552
834148 ZDOT = -5654
903848
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 18014
45622150
00016717 00000-0 10270-3 0 9107
2 25544 51
6419 65
1001 0003417 11
4403 348
6827 15
54307599 14606
Satellite: ISS
Catalog Number: 25544
Epoch time: 18014
45622150 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 65
1001 deg
Eccentricity:
0003417
Arg of perigee: 11
4403 deg
Mean anomaly: 348
6827 deg
Mean motion: 15
54307599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1460
Checksum: 277
Coasting Arc #12 (Orbit 1474)
---------------------------------------
Vector Time (GMT): 2018/015/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3503373
53 A = 6788924
08 meter
Y = 5804835
94 meter E =
0015185
Z = -102904
35 I = 51
98908
XDOT = -4001
521699 Wp = 37
66352
YDOT = 2513
647234 meter/sec RA = 59
56759 deg
ZDOT = 6043
349658 TA = 321
23283
MA = 321
34169
Ha = 221
493 n
mi
Hp = 214
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11494007
66 X = 3438701
77
Y = 19044737
34 feet Y = 5843651
47 meter
Z = -337612
71 Z = -86043
03
XDOT = -13128
352030 XDOT = -4058
687596
YDOT = 8246
874127 feet/sec YDOT = 2468
579376 meter/sec
ZDOT = 19827
262656 ZDOT = 6023
773259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19919890
26 X = -6071582
55
Y = 9902361
50 feet Y = 3018239
78 meter
Z = -263483
69 Z = -80309
83
XDOT = -6416
167539 XDOT = -1955
647866
YDOT = -12435
421821 feet/sec YDOT = -3790
316571 meter/sec
ZDOT = 19739
643591 ZDOT = 6016
643366
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 18015
42064349
00016717 00000-0 10270-3 0 9116
2 25544 51
6414 60
2916 0003620 14
3165 345
8090 15
54267441 14753
Satellite: ISS
Catalog Number: 25544
Epoch time: 18015
42064349 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 60
2916 deg
Eccentricity:
0003620
Arg of perigee: 14
3165 deg
Mean anomaly: 345
8090 deg
Mean motion: 15
54267441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1475
Checksum: 283
Coasting Arc #13 (Orbit 1490)
---------------------------------------
Vector Time (GMT): 2018/016/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2662332
66 A = 6787577
16 meter
Y = -6013801
88 meter E =
0006524
Z = -1676410
11 I = 51
96663
XDOT = 5045
207002 Wp = 114
94914
YDOT = -640
960411 meter/sec RA = 54
61967 deg
ZDOT = -5733
152386 TA = 83
32666
MA = 83
25241
Ha = 221
432 n
mi
Hp = 213
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8734687
20 X = -2586743
85
Y = -19730321
13 feet Y = -6043151
15 meter
Z = -5500033
17 Z = -1689159
43
XDOT = 16552
516410 XDOT = 5079
847601
YDOT = -2102
888486 feet/sec YDOT = -584
347358 meter/sec
ZDOT = -18809
555073 ZDOT = -5708
560829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20250784
26 X = 6172439
04
Y = -7407392
87 feet Y = -2257773
35 meter
Z = -5555804
63 Z = -1693409
25
XDOT = 484
218092 XDOT = 147
589674
YDOT = 15300
397056 feet/sec YDOT = 4663
561023 meter/sec
ZDOT = -18699
909675 ZDOT = -5699
732469
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 18016
44935915
00016717 00000-0 10270-3 0 9126
2 25544 51
6405 55
1625 0003479 19
6286 340
5000 15
54311228 14911
Satellite: ISS
Catalog Number: 25544
Epoch time: 18016
44935915 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 55
1625 deg
Eccentricity:
0003479
Arg of perigee: 19
6286 deg
Mean anomaly: 340
5000 deg
Mean motion: 15
54311228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1491
Checksum: 291
Coasting Arc #14 (Orbit 1506)
---------------------------------------
Vector Time (GMT): 2018/017/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1557710
73 A = 6784304
92 meter
Y = 5747293
53 meter E =
0014628
Z = 3234389
87 I = 51
93636
XDOT = -5881
049261 Wp = 74
23201
YDOT = -1116
322794 meter/sec RA = 49
66281 deg
ZDOT = 4801
886627 TA = 323
08572
MA = 323
18631
Ha = 221
494 n
mi
Hp = 213
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5110599
50 X = 1477616
51
Y = 18855949
91 feet Y = 5764264
90 meter
Z = 10611515
32 Z = 3241762
35
XDOT = -19294
781041 XDOT = -5891
453743
YDOT = -3662
476358 feet/sec YDOT = -1182
147173 meter/sec
ZDOT = 15754
221217 ZDOT = 4773
293729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19074283
85 X = -5813841
72
Y = 4142409
83 feet Y = 1262606
52 meter
Z = 10643376
72 Z = 3244101
23
XDOT = 4877
261356 XDOT = 1486
589261
YDOT = -17812
224008 feet/sec YDOT = -5429
165878 meter/sec
ZDOT = 15627
050930 ZDOT = 4763
125123
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 18017
47806998
00016717 00000-0 10270-3 0 9139
2 25544 51
6409 50
0325 0003545 23
0004 337
1307 15
54320500 15070
Satellite: ISS
Catalog Number: 25544
Epoch time: 18017
47806998 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 50
0325 deg
Eccentricity:
0003545
Arg of perigee: 23
0004 deg
Mean anomaly: 337
1307 deg
Mean motion: 15
54320500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1507
Checksum: 273
Coasting Arc #15 (Orbit 1512)
---------------------------------------
Vector Time (GMT): 2018/017/20:15:22
080
Vector Time (MET): N/A
Weight (LBS) : 904547
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1221032
92 A = 6778868
23 meter
Y = -4448952
96 meter E =
0014393
Z = -4980001
99 I = 51
90854
XDOT = 6079
286581 Wp = 62
06350
YDOT = 4112
720608 meter/sec RA = 47
55335 deg
ZDOT = -2181
836215 TA = 186
70101
MA = 186
72028
Ha = 221
579 n
mi
Hp = 214
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4006013
52 X = 1294881
31
Y = -14596302
37 feet Y = -4434885
36 meter
Z = -16338589
21 Z = -4973891
63
XDOT = 19945
165947 XDOT = 6043
443210
YDOT = 13493
177848 feet/sec YDOT = 4180
503057 meter/sec
ZDOT = -7158
255300 ZDOT = -2152
392565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10617634
01 X = -3236254
85
Y = -10829561
43 feet Y = -3300850
33 meter
Z = -16310614
08 Z = -4971475
17
XDOT = 20859
432726 XDOT = 6357
955095
YDOT = -9857
820069 feet/sec YDOT = -3004
663557 meter/sec
ZDOT = -7027
806992 ZDOT = -2142
075571
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 18017
86383812
00016717 00000-0 10270-3 0 9148
2 25544 51
6421 48
1106 0003363 12
7278 347
3959 15
54132319 15137
Satellite: ISS
Catalog Number: 25544
Epoch time: 18017
86383812 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 48
1106 deg
Eccentricity:
0003363
Arg of perigee: 12
7278 deg
Mean anomaly: 347
3959 deg
Mean motion: 15
54132319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1513
Checksum: 299
Coasting Arc #16 (Orbit 1527)
---------------------------------------
Vector Time (GMT): 2018/018/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 904547
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5103094
18 A = 6781079
54 meter
Y = 39837
11 meter E =
0011614
Z = 4460786
82 I = 51
89208
XDOT = -2946
802482 Wp = 55
90726
YDOT = -6264
401290 meter/sec RA = 42
83417 deg
ZDOT = -3302
682369 TA = 67
33049
MA = 67
20772
Ha = 221
806 n
mi
Hp = 214
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16742434
96 X = -5124828
08
Y = 130699
18 feet Y = -17350
87 meter
Z = 14635127
37 Z = 4435945
49
XDOT = -9667
987145 XDOT = -2860
490891
YDOT = -20552
497672 feet/sec YDOT = -6296
871732 meter/sec
ZDOT = -10835
572078 ZDOT = -3316
787223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12764911
32 X = -3890744
97
Y = 10982252
97 feet Y = 3347390
70 meter
Z = 14524473
22 Z = 4427059
44
XDOT = -19804
819622 XDOT = -6036
509021
YDOT = -8552
832252 feet/sec YDOT = -2606
903270 meter/sec
ZDOT = -10897
326370 ZDOT = -3321
505078
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 18018
82838005
00016717 00000-0 10270-3 0 9155
2 25544 51
6402 43
3024 0003375 16
7136 343
4127 15
54105321 15285
Satellite: ISS
Catalog Number: 25544
Epoch time: 18018
82838005 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 43
3024 deg
Eccentricity:
0003375
Arg of perigee: 16
7136 deg
Mean anomaly: 343
4127 deg
Mean motion: 15
54105321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1528
Checksum: 274
Coasting Arc #17 (Orbit 1542)
---------------------------------------
Vector Time (GMT): 2018/019/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 904547
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5793451
55 A = 6784775
72 meter
Y = 1204182
11 meter E =
0006765
Z = -3320370
65 I = 51
88048
XDOT = 1485
385261 Wp = 56
93261
YDOT = 5849
870457 meter/sec RA = 37
86440 deg
ZDOT = 4723
822436 TA = 264
60397
MA = 264
68114
Ha = 221
751 n
mi
Hp = 214
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19007386
96 X = 5795683
75
Y = 3950728
72 feet Y = 1268981
01 meter
Z = -10893604
51 Z = -3292223
21
XDOT = 4873
311223 XDOT = 1396
914673
YDOT = 19192
488376 feet/sec YDOT = 5865
986285 meter/sec
ZDOT = 15498
105106 ZDOT = 4730
823020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16949529
76 X = 5166216
67
Y = -9608003
84 feet Y = -2928519
57 meter
Z = -10768441
81 Z = -3282221
06
XDOT = 15540
561473 XDOT = 4736
763137
YDOT = 10050
661688 feet/sec YDOT = 3063
441683 meter/sec
ZDOT = 15528
283153 ZDOT = 4733
020705
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 18019
79291932
00016717 00000-0 10270-3 0 9165
2 25544 51
6408 38
4938 0003331 18
7509 341
3766 15
54122770 15438
Satellite: ISS
Catalog Number: 25544
Epoch time: 18019
79291932 = yrday
fracday
Element set: 916
Inclination: 51
6408 deg
RA of node: 38
4938 deg
Eccentricity:
0003331
Arg of perigee: 18
7509 deg
Mean anomaly: 341
3766 deg
Mean motion: 15
54122770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1543
Checksum: 317
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