[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 20th 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) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
117/05:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
2
121/08:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 2924)
---------------------------------------
Vector Time (GMT): 2018/108/14:46:24
552
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -690100
51 A = 6782256
57 meter
Y = 5342219
57 meter E =
0010741
Z = 4116113
34 I = 51
36758
XDOT = -6346
412931 Wp = 63
49713
YDOT = 2090
638444 meter/sec RA = 315
00162 deg
ZDOT = -3765
085953 TA = 65
49303
MA = 65
38107
Ha = 221
048 n
mi
Hp = 214
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2264109
30 X = -769781
67
Y = 17526967
09 feet Y = 5334056
98 meter
Z = 13504308
86 Z = 4112567
33
XDOT = -20821
564734 XDOT = -6351
030190
YDOT = 6859
050012 feet/sec YDOT = 2019
642567 meter/sec
ZDOT = -12352
644203 ZDOT = -3795
926481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15277293
39 X = 4656519
02
Y = 8909199
55 feet Y = 2715524
02 meter
Z = 13487683
05 Z = 4111045
79
XDOT = -989
961142 XDOT = -301
740156
YDOT = 20668
328803 feet/sec YDOT = 6299
706619 meter/sec
ZDOT = -12490
478798 ZDOT = -3807
097938
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 18108
65679891
00016717 00000-0 10270-3 0 9006
2 25544 51
6366 315
4809 0002370 346
0422 14
0664 15
54095255 29252
Satellite: ISS
Catalog Number: 25544
Epoch time: 18108
65679891 = yrday
fracday
Element set: 900
Inclination: 51
6366 deg
RA of node: 315
4809 deg
Eccentricity:
0002370
Arg of perigee: 346
0422 deg
Mean anomaly: 14
0664 deg
Mean motion: 15
54095255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2925
Checksum: 312
Coasting Arc #2 (Orbit 2939)
---------------------------------------
Vector Time (GMT): 2018/109/14:46:24
552
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1924673
76 A = 6785901
54 meter
Y = -5845665
53 meter E =
0005904
Z = -2855777
34 I = 51
35983
XDOT = 5742
831021 Wp = 39
40277
YDOT = -569
061334 meter/sec RA = 309
99881 deg
ZDOT = 5045
497960 TA = 287
98921
MA = 288
05356
Ha = 221
079 n
mi
Hp = 214
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6314546
47 X = 2003770
63
Y = -19178692
70 feet Y = -5823700
26 meter
Z = -9369348
22 Z = -2846235
64
XDOT = 18841
309125 XDOT = 5724
258830
YDOT = -1866
999128 feet/sec YDOT = -504
944863 meter/sec
ZDOT = 16553
470998 ZDOT = 5073
349992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15481452
84 X = -4718746
82
Y = -12993549
93 feet Y = -3960434
02 meter
Z = -9325916
31 Z = -2842539
29
XDOT = 4218
715413 XDOT = 1285
864458
YDOT = -16972
482566 feet/sec YDOT = -5173
212686 meter/sec
ZDOT = 16677
746212 ZDOT = 5083
377046
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 18109
62133489
00016717 00000-0 10270-3 0 9013
2 25544 51
6389 310
6722 0002373 351
7291 8
3822 15
54127879 29405
Satellite: ISS
Catalog Number: 25544
Epoch time: 18109
62133489 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 310
6722 deg
Eccentricity:
0002373
Arg of perigee: 351
7291 deg
Mean anomaly: 8
3822 deg
Mean motion: 15
54127879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2940
Checksum: 312
Coasting Arc #3 (Orbit 2955)
---------------------------------------
Vector Time (GMT): 2018/110/14:46:24
552
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2950030
68 A = 6788643
23 meter
Y = 5976275
82 meter E =
0012424
Z = 1265098
96 I = 51
34777
XDOT = -4863
387448 Wp = 111
73467
YDOT = -1161
192697 meter/sec RA = 305
00415 deg
ZDOT = -5813
768379 TA = 54
44969
MA = 54
33393
Ha = 221
118 n
mi
Hp = 214
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9678578
34 X = -3022785
03
Y = 19607204
12 feet Y = 5942879
74 meter
Z = 4150587
13 Z = 1250591
90
XDOT = -15955
995564 XDOT = -4821
800652
YDOT = -3809
687327 feet/sec YDOT = -1215
345862 meter/sec
ZDOT = -19074
043239 ZDOT = -5837
292320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14930159
32 X = 4550712
56
Y = 15992117
01 feet Y = 4874397
26 meter
Z = 4085002
06 Z = 1245108
63
XDOT = -7978
232464 XDOT = -2431
765255
YDOT = 12382
795299 feet/sec YDOT = 3774
276007 meter/sec
ZDOT = -19178
759477 ZDOT = -5845
685888
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 18110
65016918
00016717 00000-0 10270-3 0 9026
2 25544 51
6379 305
5429 0002498 354
8967 5
2160 15
54138821 29560
Satellite: ISS
Catalog Number: 25544
Epoch time: 18110
65016918 = yrday
fracday
Element set: 902
Inclination: 51
6379 deg
RA of node: 305
5429 deg
Eccentricity:
0002498
Arg of perigee: 354
8967 deg
Mean anomaly: 5
2160 deg
Mean motion: 15
54138821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2956
Checksum: 320
Coasting Arc #4 (Orbit 2971)
---------------------------------------
Vector Time (GMT): 2018/111/14:46:24
552
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3675075
71 A = 6789207
78 meter
Y = -5683469
66 meter E =
0014503
Z = 424072
10 I = 51
33280
XDOT = 3825
807034 Wp = 42
50474
YDOT = 2927
449240 meter/sec RA = 300
01379 deg
ZDOT = 5969
821447 TA = 322
08907
MA = 322
19109
Ha = 221
146 n
mi
Hp = 214
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12057335
01 X = 3736296
75
Y = -18646554
00 feet Y = -5642030
13 meter
Z = 1391312
67 Z = 442073
11
XDOT = 12551
860349 XDOT = 3763
788694
YDOT = 9604
492258 feet/sec YDOT = 2969
885208 meter/sec
ZDOT = 19586
028369 ZDOT = 5988
255434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13510477
14 X = -4117993
43
Y = -17615562
07 feet Y = -5369223
32 meter
Z = 1472424
89 Z = 448795
11
XDOT = 11938
692807 XDOT = 3638
913568
YDOT = -7484
273543 feet/sec YDOT = -2281
206576 meter/sec
ZDOT = 19667
789141 ZDOT = 5994
742130
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 18111
67900196
00016717 00000-0 10270-3 0 9030
2 25544 51
6390 300
4147 0002347
1457 359
9696 15
54142372 29729
Satellite: ISS
Catalog Number: 25544
Epoch time: 18111
67900196 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 300
4147 deg
Eccentricity:
0002347
Arg of perigee:
1457 deg
Mean anomaly: 359
9696 deg
Mean motion: 15
54142372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2972
Checksum: 303
Coasting Arc #5 (Orbit 2986)
---------------------------------------
Vector Time (GMT): 2018/112/14:46:24
552
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4161065
64 A = 6787339
61 meter
Y = 4932029
72 meter E =
0004872
Z = -2103682
84 I = 51
31125
XDOT = -2699
231120 Wp = 117
34591
YDOT = -4614
346067 meter/sec RA = 295
01978 deg
ZDOT = -5491
175746 TA = 86
05070
MA = 85
99501
Ha = 221
198 n
mi
Hp = 214
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13651790
16 X = -4205689
06
Y = 16181199
85 feet Y = 4885248
32 meter
Z = -6901846
57 Z = -2124004
29
XDOT = -8855
745145 XDOT = -2620
758297
YDOT = -15138
930666 feet/sec YDOT = -4644
091943 meter/sec
ZDOT = -18015
668458 ZDOT = -5504
097139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10976830
88 X = 3345738
05
Y = 18067723
55 feet Y = 5507042
14 meter
Z = -6993185
18 Z = -2131522
84
XDOT = -15822
226371 XDOT = -4822
614598
YDOT = 2632
589517 feet/sec YDOT = 802
413285 meter/sec
ZDOT = -18072
608059 ZDOT = -5508
530936
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 18112
64352984
00016717 00000-0 10270-3 0 9045
2 25544 51
6391 295
6062 0002487 2
4656 357
6509 15
54149037 29871
Satellite: ISS
Catalog Number: 25544
Epoch time: 18112
64352984 = yrday
fracday
Element set: 904
Inclination: 51
6391 deg
RA of node: 295
6062 deg
Eccentricity:
0002487
Arg of perigee: 2
4656 deg
Mean anomaly: 357
6509 deg
Mean motion: 15
54149037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2987
Checksum: 330
Coasting Arc #6 (Orbit 3002)
---------------------------------------
Vector Time (GMT): 2018/113/14:46:24
552
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4386700
35 A = 6783824
86 meter
Y = -3769600
12 meter E =
0012427
Z = 3532517
90 I = 51
28763
XDOT = 1596
933736 Wp = 81
17434
YDOT = 6041
391289 meter/sec RA = 290
01747 deg
ZDOT = 4452
207466 TA = 320
73767
MA = 320
82773
Ha = 221
102 n
mi
Hp = 214
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14392061
51 X = 4411367
88
Y = -12367454
47 feet Y = -3720407
04 meter
Z = 11589625
66 Z = 3553886
97
XDOT = 5239
283911 XDOT = 1507
632051
YDOT = 19820
837563 feet/sec YDOT = 6058
750051 meter/sec
ZDOT = 14606
979874 ZDOT = 4459
747841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7436580
19 X = -2266669
64
Y = -17394026
31 feet Y = -5301699
22 meter
Z = 11685457
26 Z = 3561727
37
XDOT = 19179
281137 XDOT = 5845
844891
YDOT = 1660
539297 feet/sec YDOT = 506
132378 meter/sec
ZDOT = 14639
730515 ZDOT = 4462
189861
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 18113
67235474
00016717 00000-0 10270-3 0 9054
2 25544 51
6400 290
4775 0002457 5
3120 354
8058 15
54169966 30032
Satellite: ISS
Catalog Number: 25544
Epoch time: 18113
67235474 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 290
4775 deg
Eccentricity:
0002457
Arg of perigee: 5
3120 deg
Mean anomaly: 354
8058 deg
Mean motion: 15
54169966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3003
Checksum: 300
Coasting Arc #7 (Orbit 3017)
---------------------------------------
Vector Time (GMT): 2018/114/14:46:24
552
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4437689
14 A = 6780167
21 meter
Y = 2253322
17 meter E =
0011852
Z = -4616181
33 I = 51
26408
XDOT = -538
857720 Wp = 59
45894
YDOT = -7056
658930 meter/sec RA = 285
00454 deg
ZDOT = -2926
302282 TA = 181
20846
MA = 181
21133
Ha = 221
328 n
mi
Hp = 214
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14559347
59 X = -4440133
57
Y = 7392789
26 feet Y = 2203683
05 meter
Z = -15144951
87 Z = -4637744
14
XDOT = -1767
905906 XDOT = -445
693724
YDOT = -23151
768142 feet/sec YDOT = -7062
163996 meter/sec
ZDOT = -9600
729272 ZDOT = -2928
693349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2928001
27 X = 892454
79
Y = 15972580
52 feet Y = 4868442
54 meter
Z = -15241423
25 Z = -4645585
81
XDOT = -21502
020133 XDOT = -6553
815737
YDOT = -5229
717221 feet/sec YDOT = -1594
017809 meter/sec
ZDOT = -9610
389768 ZDOT = -2929
246801
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 18114
63687758
00016717 00000-0 10270-3 0 9068
2 25544 51
6392 285
6701 0002511 9
5724 350
5476 15
54139803 30184
Satellite: ISS
Catalog Number: 25544
Epoch time: 18114
63687758 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 285
6701 deg
Eccentricity:
0002511
Arg of perigee: 9
5724 deg
Mean anomaly: 350
5476 deg
Mean motion: 15
54139803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3018
Checksum: 316
Coasting Arc #8 (Orbit 3033)
---------------------------------------
Vector Time (GMT): 2018/115/14:46:24
552
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4321737
60 A = 6777586
02 meter
Y = -511631
21 meter E =
0003666
Z = 5192583
62 I = 51
24885
XDOT = -432
240439 Wp = 83
97445
YDOT = 7579
181716 meter/sec RA = 279
98062 deg
ZDOT = 1106
238833 TA = 355
36859
MA = 355
37198
Ha = 221
116 n
mi
Hp = 214
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14178929
13 X = 4301914
66
Y = -1678580
10 feet Y = -463413
15 meter
Z = 17036035
49 Z = 5213529
09
XDOT = -1418
111676 XDOT = -522
334340
YDOT = 24866
081746 feet/sec YDOT = 7573
844415 meter/sec
ZDOT = 3629
392496 ZDOT = 1103
919950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2192412
34 X = 668247
28
Y = -13994982
53 feet Y = -4265670
67 meter
Z = 17129505
54 Z = 5221073
29
XDOT = 22527
423036 XDOT = 6866
358541
YDOT = 7958
596988 feet/sec YDOT = 2425
780362 meter/sec
ZDOT = 3617
995271 ZDOT = 1102
764959
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 18115
66569664
00016717 00000-0 10270-3 0 9078
2 25544 51
6397 280
5407 0002517 10
5920 349
5285 15
54183833 30348
Satellite: ISS
Catalog Number: 25544
Epoch time: 18115
66569664 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 280
5407 deg
Eccentricity:
0002517
Arg of perigee: 10
5920 deg
Mean anomaly: 349
5285 deg
Mean motion: 15
54183833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3034
Checksum: 320
Coasting Arc #9 (Orbit 3048)
---------------------------------------
Vector Time (GMT): 2018/116/14:46:24
552
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4110258
19 A = 6777450
16 meter
Y = -1305280
07 meter E =
0015264
Z = -5241508
15 I = 51
24426
XDOT = 1321
417588 Wp = 86
61436
YDOT = -7496
401796 meter/sec RA = 274
95373 deg
ZDOT = 833
582791 TA = 191
39271
MA = 191
42730
Ha = 221
401 n
mi
Hp = 214
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13485099
04 X = -4069896
02
Y = -4282414
93 feet Y = -1351018
43 meter
Z = -17196549
06 Z = -5261376
41
XDOT = 4335
359542 XDOT = 1401
097050
YDOT = -24594
494081 feet/sec YDOT = -7481
179231 meter/sec
ZDOT = 2734
851675 ZDOT = 840
195788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7540239
66 X = -2298265
05
Y = 11844114
37 feet Y = 3610086
06 meter
Z = -17284964
96 Z = -5268457
32
XDOT = -21826
828564 XDOT = -6652
817346
YDOT = -9874
031635 feet/sec YDOT = -3009
604842 meter/sec
ZDOT = 2765
368269 ZDOT = 842
884248
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 18116
63021334
00016717 00000-0 10270-3 0 9084
2 25544 51
6404 275
7332 0002661 18
0594 342
0653 15
54177131 30497
Satellite: ISS
Catalog Number: 25544
Epoch time: 18116
63021334 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 275
7332 deg
Eccentricity:
0002661
Arg of perigee: 18
0594 deg
Mean anomaly: 342
0653 deg
Mean motion: 15
54177131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3049
Checksum: 285
Coasting Arc #10 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2018/117/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2658220
31 A = 6785205
01 meter
Y = -5421204
07 meter E =
0014549
Z = 3078430
16 I = 51
26897
XDOT = 3743
600302 Wp = 72
83411
YDOT = 4605
813104 meter/sec RA = 271
98313 deg
ZDOT = 4863
524046 TA = 322
77626
MA = 322
87702
Ha = 221
525 n
mi
Hp = 214
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8721195
23 X = 2703690
58
Y = -17786102
61 feet Y = -5391223
61 meter
Z = 10099836
49 Z = 3091453
76
XDOT = 12282
153223 XDOT = 3668
193928
YDOT = 15110
935382 feet/sec YDOT = 4647
255279 meter/sec
ZDOT = 15956
443719 ZDOT = 4881
525929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19726593
69 X = 6012665
76
Y = 1440407
30 feet Y = 439036
15 meter
Z = 10158647
42 Z = 3096355
73
XDOT = -9413
015597 XDOT = -2869
087154
YDOT = 15474
534639 feet/sec YDOT = 4716
638158 meter/sec
ZDOT = 16036
089866 ZDOT = 4887
800191
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 18117
27322284
00016717 00000-0 10270-3 0 9094
2 25544 51
6408 272
5310 0003231 17
5937 342
5327 15
54148304 30595
Satellite: ISS
Catalog Number: 25544
Epoch time: 18117
27322284 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 272
5310 deg
Eccentricity:
0003231
Arg of perigee: 17
5937 deg
Mean anomaly: 342
5327 deg
Mean motion: 15
54148304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 293
Coasting Arc #11 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2018/118/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3243399
23 A = 6781268
84 meter
Y = 4124085
71 meter E =
0010868
Z = -4307881
58 I = 51
25593
XDOT = -3112
078765 Wp = 56
30302
YDOT = -6074
927466 meter/sec RA = 266
97220 deg
ZDOT = -3473
084524 TA = 178
14688
MA = 178
14285
Ha = 221
559 n
mi
Hp = 214
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10641073
60 X = -3268349
11
Y = 13530464
93 feet Y = 4087676
06 meter
Z = -14133469
77 Z = -4323697
93
XDOT = -10210
232170 XDOT = -3027
045316
YDOT = -19930
864391 feet/sec YDOT = -6109
253602 meter/sec
ZDOT = -11394
634264 ZDOT = -3487
995292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16556115
64 X = -5046304
05
Y = -4492958
26 feet Y = -1369453
68 meter
Z = -14204550
58 Z = -4329547
02
XDOT = 14132
259611 XDOT = 4307
512729
YDOT = -15848
463570 feet/sec YDOT = -4830
611696 meter/sec
ZDOT = -11460
308260 ZDOT = -3493
101958
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 18118
23773312
00016717 00000-0 10270-3 0 9105
2 25544 51
6408 267
7234 0003191 18
1885 341
9382 15
54173076 30745
Satellite: ISS
Catalog Number: 25544
Epoch time: 18118
23773312 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 267
7234 deg
Eccentricity:
0003191
Arg of perigee: 18
1885 deg
Mean anomaly: 341
9382 deg
Mean motion: 15
54173076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 304
Coasting Arc #12 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2018/119/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3744189
95 A = 6778231
27 meter
Y = -2510518
45 meter E =
0005546
Z = 5057103
62 I = 51
24933
XDOT = 2404
436189 Wp = 91
14587
YDOT = 7077
341276 meter/sec RA = 261
95027 deg
ZDOT = 1731
473060 TA = 342
02424
MA = 342
04385
Ha = 221
474 n
mi
Hp = 214
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12284087
76 X = 3747419
80
Y = -8236609
09 feet Y = -2468630
09 meter
Z = 16591547
31 Z = 5075299
85
XDOT = 7888
570175 XDOT = 2316
705994
YDOT = 23219
623610 feet/sec YDOT = 7103
738872 meter/sec
ZDOT = 5680
685894 ZDOT = 1742
939833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12439920
30 X = 3791687
71
Y = 7828072
16 feet Y = 2385996
39 meter
Z = 16673021
71 Z = 5081937
02
XDOT = -17523
076585 XDOT = -5341
033743
YDOT = 15628
227010 feet/sec YDOT = 4763
483593 meter/sec
ZDOT = 5730
879696 ZDOT = 1746
772131
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 18119
26654190
00016717 00000-0 10270-3 0 9112
2 25544 51
6415 262
5941 0003152 22
7256 337
4035 15
54170658 30907
Satellite: ISS
Catalog Number: 25544
Epoch time: 18119
26654190 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 262
5941 deg
Eccentricity:
0003152
Arg of perigee: 22
7256 deg
Mean anomaly: 337
4035 deg
Mean motion: 15
54170658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 293
Coasting Arc #13 (Orbit 3104)
---------------------------------------
Vector Time (GMT): 2018/120/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4187538
02 A = 6777178
89 meter
Y = 739603
50 meter E =
0016395
Z = -5291089
18 I = 51
25174
XDOT = -1573
848094 Wp = 80
93934
YDOT = -7490
558821 meter/sec RA = 256
92285 deg
ZDOT = 201
614054 TA = 190
97756
MA = 191
01338
Ha = 221
622 n
mi
Hp = 213
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13738641
79 X = -4169795
42
Y = 2426520
66 feet Y = 692874
68 meter
Z = -17359216
46 Z = -5311388
10
XDOT = -5163
543614 XDOT = -1490
949002
YDOT = -24575
324216 feet/sec YDOT = -7507
695153 meter/sec
ZDOT = 661
463431 ZDOT = 194
170175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7901664
02 X = -2408427
19
Y = -11359914
27 feet Y = -3462501
87 meter
Z = -17449834
68 Z = -5318709
61
XDOT = 19331
705235 XDOT = 5892
303756
YDOT = -14397
824427 feet/sec YDOT = -4388
456885 meter/sec
ZDOT = 629
252628 ZDOT = 191
796201
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 18120
23104544
00016717 00000-0 10270-3 0 9125
2 25544 51
6416 257
7855 0003278 24
0397 336
0909 15
54194158 31051
Satellite: ISS
Catalog Number: 25544
Epoch time: 18120
23104544 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 257
7855 deg
Eccentricity:
0003278
Arg of perigee: 24
0397 deg
Mean anomaly: 336
0909 deg
Mean motion: 15
54194158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3105
Checksum: 300
Coasting Arc #14 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2018/121/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4515183
42 A = 6778572
19 meter
Y = 1058357
25 meter E =
0009156
Z = 4940172
56 I = 51
26471
XDOT = 610
096310 Wp = 46
66903
YDOT = 7346
527510 meter/sec RA = 251
89708 deg
ZDOT = -2122
826789 TA = 64
15623
MA = 64
06183
Ha = 221
484 n
mi
Hp = 213
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14813593
88 X = 4479015
77
Y = 3472300
69 feet Y = 1108646
89 meter
Z = 16207915
21 Z = 4962018
34
XDOT = 2001
628314 XDOT = 538
211867
YDOT = 24102
780544 feet/sec YDOT = 7352
948109 meter/sec
ZDOT = -6964
654819 ZDOT = -2120
037648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3250973
08 X = 990896
60
Y = 14756947
90 feet Y = 4497917
72 meter
Z = 16305202
05 Z = 4969825
58
XDOT = -19750
995466 XDOT = -6020
103418
YDOT = 12065
077651 feet/sec YDOT = 3677
435668 meter/sec
ZDOT = -6953
173075 ZDOT = -2119
327153
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 18121
25984561
00016717 00000-0 10270-3 0 9134
2 25544 51
6411 252
6568 0003262 26
2700 333
8617 15
54220146 31212
Satellite: ISS
Catalog Number: 25544
Epoch time: 18121
25984561 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 252
6568 deg
Eccentricity:
0003262
Arg of perigee: 26
2700 deg
Mean anomaly: 333
8617 deg
Mean motion: 15
54220146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 280
Coasting Arc #15 (Orbit 3122)
---------------------------------------
Vector Time (GMT): 2018/121/08:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4484236
07 A = 6782027
05 meter
Y = 3037758
76 meter E =
0012733
Z = 4075116
10 I = 51
27375
XDOT = -986
902130 Wp = 66
41535
YDOT = 6585
095203 meter/sec RA = 251
22409 deg
ZDOT = -3808
328936 TA = 63
17255
MA = 63
04239
Ha = 221
546 n
mi
Hp = 213
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14712060
60 X = 4430138
59
Y = 9966400
14 feet Y = 3087602
06 meter
Z = 13369803
48 Z = 4096768
02
XDOT = -3237
867881 XDOT = -1041
965896
YDOT = 21604
643054 feet/sec YDOT = 6573
751137 meter/sec
ZDOT = -12494
517506 ZDOT = -3813
256743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11152794
37 X = 3399371
72
Y = 13740755
19 feet Y = 4188182
18 meter
Z = 13465969
27 Z = 4104427
43
XDOT = -8213
118557 XDOT = -2503
358536
YDOT = 18979
527953 feet/sec YDOT = 5784
960120 meter/sec
ZDOT = -12517
350660 ZDOT = -3815
288481
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 18121
38844599
00016717 00000-0 10270-3 0 9145
2 25544 51
6377 252
0120 0003053 27
7054 332
4261 15
54181421 31231
Satellite: ISS
Catalog Number: 25544
Epoch time: 18121
38844599 = yrday
fracday
Element set: 914
Inclination: 51
6377 deg
RA of node: 252
0120 deg
Eccentricity:
0003053
Arg of perigee: 27
7054 deg
Mean anomaly: 332
4261 deg
Mean motion: 15
54181421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 280
Coasting Arc #16 (Orbit 3137)
---------------------------------------
Vector Time (GMT): 2018/122/08:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4372079
48 A = 6785790
80 meter
Y = -4373599
25 meter E =
0007536
Z = -2791893
58 I = 51
29767
XDOT = 2100
359302 Wp = 50
90694
YDOT = -5336
834616 meter/sec RA = 246
21574 deg
ZDOT = 5085
120167 TA = 277
27294
MA = 277
35860
Ha = 221
659 n
mi
Hp = 213
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14344092
79 X = -4309285
96
Y = -14349078
90 feet Y = -4422139
67 meter
Z = -9159755
84 Z = -2812979
63
XDOT = 6890
942592 XDOT = 2135
179855
YDOT = -17509
299920 feet/sec YDOT = -5313
152406 meter/sec
ZDOT = 16683
465114 ZDOT = 5095
407591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9876297
54 X = -3010295
49
Y = -17674460
31 feet Y = -5387175
50 meter
Z = -9253236
73 Z = -2820386
56
XDOT = 9968
708185 XDOT = 3038
462255
YDOT = -14305
525654 feet/sec YDOT = -4360
324219 meter/sec
ZDOT = 16730
035414 ZDOT = 5099
314794
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 18122
35294476
00016717 00000-0 10270-3 0 9157
2 25544 51
6374 247
2032 0003036 34
7975 325
3376 15
54184069 31382
Satellite: ISS
Catalog Number: 25544
Epoch time: 18122
35294476 = yrday
fracday
Element set: 915
Inclination: 51
6374 deg
RA of node: 247
2032 deg
Eccentricity:
0003036
Arg of perigee: 34
7975 deg
Mean anomaly: 325
3376 deg
Mean motion: 15
54184069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3138
Checksum: 313
Coasting Arc #17 (Orbit 3153)
---------------------------------------
Vector Time (GMT): 2018/123/08:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4005329
47 A = 6788405
72 meter
Y = 5348418
92 meter E =
0014193
Z = 1168444
48 I = 51
32144
XDOT = -3276
708992 Wp = 109
00191
YDOT = 3740
859283 meter/sec RA = 241
21824 deg
ZDOT = -5837
375242 TA = 58
25097
MA = 58
11274
Ha = 221
664 n
mi
Hp = 213
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13140844
71 X = 3939548
53
Y = 17547306
17 feet Y = 5392841
42 meter
Z = 3833479
26 Z = 1187741
75
XDOT = -10750
357586 XDOT = -3289
941427
YDOT = 12273
160377 feet/sec YDOT = 3704
143131 meter/sec
ZDOT = -19151
493577 ZDOT = -5853
324593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8238331
55 X = 2511043
46
Y = 20299203
37 feet Y = 6187197
19 meter
Z = 3918871
36 Z = 1194471
99
XDOT = -11907
200912 XDOT = -3629
314838
YDOT = 8576
870755 feet/sec YDOT = 2614
230206 meter/sec
ZDOT = -19223
112498 ZDOT = -5859
204689
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 18123
38173554
00016717 00000-0 10270-3 0 9165
2 25544 51
6377 242
0739 0003228 33
9453 326
1905 15
54238687 31548
Satellite: ISS
Catalog Number: 25544
Epoch time: 18123
38173554 = yrday
fracday
Element set: 916
Inclination: 51
6377 deg
RA of node: 242
0739 deg
Eccentricity:
0003228
Arg of perigee: 33
9453 deg
Mean anomaly: 326
1905 deg
Mean motion: 15
54238687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3154
Checksum: 317
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