[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 26th 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
122/14:29:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 213
9
128/00:24:00
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
5
Coasting Arc #1 (Orbit 3031)
---------------------------------------
Vector Time (GMT): 2018/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 818571
90 A = 6786696
53 meter
Y = 6276822
11 meter E =
0013755
Z = 2434098
05 I = 51
27611
XDOT = -4831
664500 Wp = 93
87183
YDOT = 2698
739052 meter/sec RA = 280
52875 deg
ZDOT = -5309
288434 TA = 58
73809
MA = 58
60342
Ha = 221
337 n
mi
Hp = 214
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2685603
36 X = 736498
32
Y = 20593248
40 feet Y = 6285517
16 meter
Z = 7985885
99 Z = 2437874
76
XDOT = -15851
917652 XDOT = -4835
693610
YDOT = 8854
130749 feet/sec YDOT = 2644
685269 meter/sec
ZDOT = -17418
925309 ZDOT = -5332
768993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13307936
12 X = 4056258
93
Y = 15935430
86 feet Y = 4857119
33 meter
Z = 8001849
76 Z = 2438963
81
XDOT = -7330
990874 XDOT = -2234
486018
YDOT = 14963
047881 feet/sec YDOT = 4560
736994 meter/sec
ZDOT = -17524
005314 ZDOT = -5341
316820
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
53706808
00016717 00000-0 10270-3 0 9000
2 25544 51
6361 281
1814 0002773 10
0177 350
1030 15
54167441 30322
Satellite: ISS
Catalog Number: 25544
Epoch time: 18115
53706808 = yrday
fracday
Element set: 900
Inclination: 51
6361 deg
RA of node: 281
1814 deg
Eccentricity:
0002773
Arg of perigee: 10
0177 deg
Mean anomaly: 350
1030 deg
Mean motion: 15
54167441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3032
Checksum: 266
Coasting Arc #2 (Orbit 3046)
---------------------------------------
Vector Time (GMT): 2018/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6224
26 A = 6788931
23 meter
Y = -6733250
47 meter E =
0012839
Z = -817059
48 I = 51
28032
XDOT = 4831
921353 Wp = 35
02362
YDOT = -715
116026 meter/sec RA = 275
52992 deg
ZDOT = 5912
974908 TA = 316
09453
MA = 316
19649
Ha = 221
433 n
mi
Hp = 214
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20420
79 X = 73038
12
Y = -22090716
78 feet Y = -6732876
94 meter
Z = -2680641
33 Z = -816896
82
XDOT = 15852
760345 XDOT = 4810
836526
YDOT = -2346
181188 feet/sec YDOT = -661
199711 meter/sec
ZDOT = 19399
523977 ZDOT = 5936
395710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12216301
74 X = -3723528
77
Y = -18405732
91 feet Y = -5610067
39 meter
Z = -2678990
58 Z = -816556
33
XDOT = 10463
636662 XDOT = 3189
316455
YDOT = -9756
746148 feet/sec YDOT = -2973
856226 meter/sec
ZDOT = 19504
058349 ZDOT = 5944
836985
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
50158000
00016717 00000-0 10270-3 0 9014
2 25544 51
6378 276
3725 0002747 18
2496 341
8754 15
54167622 30479
Satellite: ISS
Catalog Number: 25544
Epoch time: 18116
50158000 = yrday
fracday
Element set: 901
Inclination: 51
6378 deg
RA of node: 276
3725 deg
Eccentricity:
0002747
Arg of perigee: 18
2496 deg
Mean anomaly: 341
8754 deg
Mean motion: 15
54167622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3047
Checksum: 307
Coasting Arc #3 (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 = 2669659
91 A = 6785141
20 meter
Y = -5406972
16 meter E =
0014525
Z = 3093380
09 I = 51
26850
XDOT = 3733
210901 Wp = 72
88843
YDOT = 4627
142968 meter/sec RA = 271
98202 deg
ZDOT = 4851
308445 TA = 322
92214
MA = 323
02240
Ha = 221
518 n
mi
Hp = 214
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8758726
72 X = 2714897
56
Y = -17739409
96 feet Y = -5376865
06 meter
Z = 10148884
80 Z = 3106458
69
XDOT = 12248
067262 XDOT = 3657
626121
YDOT = 15180
915250 feet/sec YDOT = 4668
467963 meter/sec
ZDOT = 15916
366290 ZDOT = 4869
259426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19697027
79 X = 6003654
07
Y = 1492279
68 feet Y = 454846
85 meter
Z = 10207939
06 Z = 3111379
83
XDOT = -9486
762436 XDOT = -2891
565191
YDOT = 15471
236922 feet/sec YDOT = 4715
633014 meter/sec
ZDOT = 15995
782556 ZDOT = 4875
514523
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
27318686
00016717 00000-0 10270-3 0 9028
2 25544 51
6406 272
5302 0003267 17
3894 342
7370 15
54156579 30596
Satellite: ISS
Catalog Number: 25544
Epoch time: 18117
27318686 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 272
5302 deg
Eccentricity:
0003267
Arg of perigee: 17
3894 deg
Mean anomaly: 342
7370 deg
Mean motion: 15
54156579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 318
Coasting Arc #4 (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 = -3254296
84 A = 6781200
25 meter
Y = 4102681
30 meter E =
0010958
Z = -4320073
77 I = 51
25545
XDOT = -3097
619251 Wp = 56
20215
YDOT = -6093
337201 meter/sec RA = 266
97087 deg
ZDOT = -3453
636633 TA = 178
47594
MA = 178
47259
Ha = 221
553 n
mi
Hp = 214
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10676826
90 X = -3278947
33
Y = 13460240
49 feet Y = 4066151
46 meter
Z = -14173470
36 Z = -4335942
32
XDOT = -10162
792818 XDOT = -3012
475482
YDOT = -19991
263782 feet/sec YDOT = -6127
501022 meter/sec
ZDOT = -11330
828848 ZDOT = -3468
476892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16505082
37 X = -5030749
11
Y = -4552849
22 feet Y = -1387708
44 meter
Z = -14244781
11 Z = -4341809
28
XDOT = 14201
772223 XDOT = 4328
700174
YDOT = -15832
190045 feet/sec YDOT = -4825
651526 meter/sec
ZDOT = -11396
185968 ZDOT = -3473
557483
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
23769211
00016717 00000-0 10270-3 0 9030
2 25544 51
6405 267
7225 0003228 18
0257 342
1010 15
54181217 30742
Satellite: ISS
Catalog Number: 25544
Epoch time: 18118
23769211 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 267
7225 deg
Eccentricity:
0003228
Arg of perigee: 18
0257 deg
Mean anomaly: 342
1010 deg
Mean motion: 15
54181217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 276
Coasting Arc #5 (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 = 3753662
28 A = 6778178
46 meter
Y = -2482455
38 meter E =
0005493
Z = 5063880
59 I = 51
24890
XDOT = 2385
572269 Wp = 90
46415
YDOT = 7089
980557 meter/sec RA = 261
94872 deg
ZDOT = 1705
720844 TA = 342
96391
MA = 342
98234
Ha = 221
468 n
mi
Hp = 214
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12315164
96 X = 3756544
70
Y = -8144538
64 feet Y = -2440463
04 meter
Z = 16613781
46 Z = 5082121
99
XDOT = 7826
680672 XDOT = 2297
827232
YDOT = 23261
091065 feet/sec YDOT = 7116
167119 meter/sec
ZDOT = 5596
196994 ZDOT = 1717
095944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12368093
57 X = 3769794
92
Y = 7893454
51 feet Y = 2405924
93 meter
Z = 16695453
55 Z = 5088774
24
XDOT = -17580
953436 XDOT = -5358
674607
YDOT = 15594
018706 feet/sec YDOT = 4753
056902 meter/sec
ZDOT = 5645
980335 ZDOT = 1720
894806
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
26649575
00016717 00000-0 10270-3 0 9045
2 25544 51
6413 262
5931 0003187 22
5307 337
5985 15
54178592 30907
Satellite: ISS
Catalog Number: 25544
Epoch time: 18119
26649575 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 262
5931 deg
Eccentricity:
0003187
Arg of perigee: 22
5307 deg
Mean anomaly: 337
5985 deg
Mean motion: 15
54178592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 326
Coasting Arc #6 (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 = -4194371
33 A = 6777162
33 meter
Y = 706945
72 meter E =
0016390
Z = -5290105
80 I = 51
25142
XDOT = -1550
711614 Wp = 81
01999
YDOT = -7494
553374 meter/sec RA = 256
92115 deg
ZDOT = 231
103389 TA = 191
17972
MA = 191
21618
Ha = 221
619 n
mi
Hp = 213
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13761060
79 X = -4176267
81
Y = 2319375
71 feet Y = 660142
50 meter
Z = -17355990
15 Z = -5310437
03
XDOT = -5087
636530 XDOT = -1467
912821
YDOT = -24588
429706 feet/sec YDOT = -7511
431539 meter/sec
ZDOT = 758
213219 ZDOT = 223
771658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7813730
83 X = -2381625
16
Y = -11425116
18 feet Y = -3482375
41 meter
Z = -17446748
20 Z = -5317768
85
XDOT = 19370
331970 XDOT = 5904
077184
YDOT = -14341
351190 feet/sec YDOT = -4371
243843 meter/sec
ZDOT = 726
503047 ZDOT = 221
438129
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
23099470
00016717 00000-0 10270-3 0 9058
2 25544 51
6414 257
7845 0003313 23
8991 336
2315 15
54201245 31054
Satellite: ISS
Catalog Number: 25544
Epoch time: 18120
23099470 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 257
7845 deg
Eccentricity:
0003313
Arg of perigee: 23
8991 deg
Mean anomaly: 336
2315 deg
Mean motion: 15
54201245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3105
Checksum: 286
Coasting Arc #7 (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 = 4518071
11 A = 6778594
67 meter
Y = 1093320
76 meter E =
0009259
Z = 4929924
87 I = 51
26452
XDOT = 582
691227 Wp = 46
77191
YDOT = 7339
962671 meter/sec RA = 251
89532 deg
ZDOT = -2153
015071 TA = 64
36350
MA = 64
26788
Ha = 221
482 n
mi
Hp = 213
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14823067
95 X = 4481562
06
Y = 3587010
38 feet Y = 1143640
78 meter
Z = 16174294
19 Z = 4951783
85
XDOT = 1911
716625 XDOT = 511
028873
YDOT = 24081
242360 feet/sec YDOT = 7346
078050 meter/sec
ZDOT = -7063
697740 ZDOT = -2150
358518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3151831
84 X = 960678
35
Y = 14815452
03 feet Y = 4515749
78 meter
Z = 16271635
34 Z = 4959594
45
XDOT = -19766
042145 XDOT = -6024
689646
YDOT = 11982
542380 feet/sec YDOT = 3652
278917 meter/sec
ZDOT = -7052
806431 ZDOT = -2149
695400
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
25979021
00016717 00000-0 10270-3 0 9061
2 25544 51
6409 252
6558 0003300 26
1366 333
9953 15
54227269 31215
Satellite: ISS
Catalog Number: 25544
Epoch time: 18121
25979021 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 252
6558 deg
Eccentricity:
0003300
Arg of perigee: 26
1366 deg
Mean anomaly: 333
9953 deg
Mean motion: 15
54227269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 300
Coasting Arc #8 (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 = 4479489
94 A = 6782070
46 meter
Y = 3069384
41 meter E =
0012805
Z = 4056649
95 I = 51
27364
XDOT = -1014
415036 Wp = 66
64784
YDOT = 6566
293234 meter/sec RA = 251
22248 deg
ZDOT = -3833
457477 TA = 63
25323
MA = 63
12225
Ha = 221
544 n
mi
Hp = 213
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14696489
30 X = 4425128
87
Y = 10070158
84 feet Y = 3119173
17 meter
Z = 13309218
98 Z = 4078278
17
XDOT = -3328
133320 XDOT = -1069
144444
YDOT = 21542
956806 feet/sec YDOT = 6554
643370 meter/sec
ZDOT = -12576
960226 ZDOT = -3838
518122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11108521
26 X = 3385877
28
Y = 13835807
33 feet Y = 4217154
07 meter
Z = 13405274
99 Z = 4085927
82
XDOT = -8274
458168 XDOT = -2522
054850
YDOT = 18897
936011 feet/sec YDOT = 5760
090896 meter/sec
ZDOT = -12600
383351 ZDOT = -3840
596845
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
38839001
00016717 00000-0 10270-3 0 9079
2 25544 51
6374 252
0110 0003089 27
5379 332
5937 15
54188640 31235
Satellite: ISS
Catalog Number: 25544
Epoch time: 18121
38839001 = yrday
fracday
Element set: 907
Inclination: 51
6374 deg
RA of node: 252
0110 deg
Eccentricity:
0003089
Arg of perigee: 27
5379 deg
Mean anomaly: 332
5937 deg
Mean motion: 15
54188640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 298
Coasting Arc #9 (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 = -4361211
93 A = 6785835
70 meter
Y = -4401060
25 meter E =
0007621
Z = -2765457
56 I = 51
29755
XDOT = 2129
175156 Wp = 50
11094
YDOT = -5307
872493 meter/sec RA = 246
21423 deg
ZDOT = 5103
562725 TA = 278
40459
MA = 278
49097
Ha = 221
657 n
mi
Hp = 213
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14308438
09 X = -4298240
56
Y = -14439174
05 feet Y = -4449478
15 meter
Z = -9073023
49 Z = -2786490
38
XDOT = 6985
482795 XDOT = 2163
580119
YDOT = -17414
279834 feet/sec YDOT = -5283
870369 meter/sec
ZDOT = 16743
972195 ZDOT = 5113
989121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9818187
18 X = -2992583
45
Y = -17751724
35 feet Y = -5410725
58 meter
Z = -9166263
46 Z = -2793877
10
XDOT = 10028
045885 XDOT = 3056
548386
YDOT = -14192
842699 feet/sec YDOT = -4325
978455 meter/sec
ZDOT = 16791
158578 ZDOT = 5117
945135
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
35288469
00016717 00000-0 10270-3 0 9084
2 25544 51
6371 247
2021 0003071 34
6123 325
5229 15
54190290 31382
Satellite: ISS
Catalog Number: 25544
Epoch time: 18122
35288469 = yrday
fracday
Element set: 908
Inclination: 51
6371 deg
RA of node: 247
2021 deg
Eccentricity:
0003071
Arg of perigee: 34
6123 deg
Mean anomaly: 325
5229 deg
Mean motion: 15
54190290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3138
Checksum: 290
Coasting Arc #10 (Orbit 3141)
---------------------------------------
Vector Time (GMT): 2018/122/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4603525
99 A = 6784811
71 meter
Y = -3847233
27 meter E =
0006911
Z = -3170219
72 I = 51
30128
XDOT = 1536
241692 Wp = 62
56226
YDOT = -5779
050026 meter/sec RA = 244
93049 deg
ZDOT = 4793
577804 TA = 260
66564
MA = 260
74379
Ha = 221
605 n
mi
Hp = 213
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15103431
73 X = -4544763
50
Y = -12622156
38 feet Y = -3898384
40 meter
Z = -10400983
32 Z = -3192439
85
XDOT = 5040
163032 XDOT = 1577
465342
YDOT = -18960
137879 feet/sec YDOT = -5761
640377 meter/sec
ZDOT = 15726
961299 ZDOT = 4801
140401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15716059
48 X = -4790254
93
Y = 11763372
99 feet Y = 3585476
09 meter
Z = -10499593
62 Z = -3200276
13
XDOT = -16478
079122 XDOT = -5022
518516
YDOT = -7979
310654 feet/sec YDOT = -2432
093887 meter/sec
ZDOT = 15761
434703 ZDOT = 4804
085298
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
61008187
00016717 00000-0 10270-3 0 9091
2 25544 51
6409 245
9215 0002894 34
3493 325
7846 15
54187851 31424
Satellite: ISS
Catalog Number: 25544
Epoch time: 18122
61008187 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 245
9215 deg
Eccentricity:
0002894
Arg of perigee: 34
3493 deg
Mean anomaly: 325
7846 deg
Mean motion: 15
54187851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3142
Checksum: 319
Coasting Arc #11 (Orbit 3157)
---------------------------------------
Vector Time (GMT): 2018/123/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4351544
54 A = 6787984
61 meter
Y = 4947802
28 meter E =
0014942
Z = 1607883
62 I = 51
32659
XDOT = -2778
649092 Wp = 105
15018
YDOT = 4310
129244 meter/sec RA = 239
93160 deg
ZDOT = -5702
524457 TA = 57
17296
MA = 57
02918
Ha = 221
732 n
mi
Hp = 213
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14276720
94 X = 4288083
08
Y = 16232947
13 feet Y = 4996109
34 meter
Z = 5275208
73 Z = 1628868
33
XDOT = -9116
302796 XDOT = -2798
939340
YDOT = 14140
843975 feet/sec YDOT = 4278
943286 meter/sec
ZDOT = -18709
069742 ZDOT = -5716
071465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18873162
36 X = 5752539
89
Y = -10495118
65 feet Y = -3198912
16 meter
Z = 5368182
88 Z = 1636222
14
XDOT = 11157
965650 XDOT = 3400
947930
YDOT = 10397
466564 feet/sec YDOT = 3169
147809 meter/sec
ZDOT = -18770
045844 ZDOT = -5721
109973
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
63886932
00016717 00000-0 10270-3 0 9108
2 25544 51
6406 240
7928 0003079 39
9178 320
2201 15
54201537 31582
Satellite: ISS
Catalog Number: 25544
Epoch time: 18123
63886932 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 240
7928 deg
Eccentricity:
0003079
Arg of perigee: 39
9178 deg
Mean anomaly: 320
2201 deg
Mean motion: 15
54201537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3158
Checksum: 304
Coasting Arc #12 (Orbit 3173)
---------------------------------------
Vector Time (GMT): 2018/124/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3837428
93 A = 6789202
86 meter
Y = -5590881
52 meter E =
0015431
Z = 88122
59 I = 51
34710
XDOT = 3999
261671 Wp = 45
35059
YDOT = -2640
544548 meter/sec RA = 234
93983 deg
ZDOT = 5989
502413 TA = 315
60280
MA = 315
72641
Ha = 221
821 n
mi
Hp = 213
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12589989
92 X = -3775053
02
Y = -18342787
16 feet Y = -5633445
54 meter
Z = 289116
10 Z = 69632
68
XDOT = 13120
937241 XDOT = 3999
397522
YDOT = -8663
203897 feet/sec YDOT = -2595
821592 meter/sec
ZDOT = 19650
598469 ZDOT = 6008
929880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20438701
55 X = -6229716
23
Y = 8790094
76 feet Y = 2679220
88 meter
Z = 207335
07 Z = 63195
73
XDOT = -5333
200521 XDOT = -1625
559519
YDOT = -12934
996831 feet/sec YDOT = -3942
587034 meter/sec
ZDOT = 19737
597872 ZDOT = 6016
019831
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 18124
66765384
00016717 00000-0 10270-3 0 9110
2 25544 51
6400 235
6641 0003209 41
2520 318
8875 15
54172627 31748
Satellite: ISS
Catalog Number: 25544
Epoch time: 18124
66765384 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 235
6641 deg
Eccentricity:
0003209
Arg of perigee: 41
2520 deg
Mean anomaly: 318
8875 deg
Mean motion: 15
54172627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3174
Checksum: 302
Coasting Arc #13 (Orbit 3188)
---------------------------------------
Vector Time (GMT): 2018/125/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2988231
57 A = 6787706
84 meter
Y = 5815643
95 meter E =
0007738
Z = -1819820
28 I = 51
36138
XDOT = -5130
829935 Wp = 118
07631
YDOT = 883
312841 meter/sec RA = 229
94925 deg
ZDOT = -5624
141093 TA = 82
00040
MA = 81
91261
Ha = 221
821 n
mi
Hp = 213
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9803909
33 X = 2931817
17
Y = 19080196
68 feet Y = 5848745
07 meter
Z = -5970538
99 Z = -1805441
08
XDOT = -16833
431546 XDOT = -5113
006667
YDOT = 2898
008010 feet/sec YDOT = 826
036302 meter/sec
ZDOT = -18451
906473 ZDOT = -5649
021799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20522512
31 X = 6255261
75
Y = -6304795
32 feet Y = -1921701
61 meter
Z = -5907107
91 Z = -1800486
49
XDOT = -571
644048 XDOT = -174
237106
YDOT = 15463
349975 feet/sec YDOT = 4713
229072 meter/sec
ZDOT = -18563
023298 ZDOT = -5658
009501
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 18125
63213381
00016717 00000-0 10270-3 0 9124
2 25544 51
6392 230
8559 0003122 46
5131 313
6281 15
54212104 31898
Satellite: ISS
Catalog Number: 25544
Epoch time: 18125
63213381 = yrday
fracday
Element set: 912
Inclination: 51
6392 deg
RA of node: 230
8559 deg
Eccentricity:
0003122
Arg of perigee: 46
5131 deg
Mean anomaly: 313
6281 deg
Mean motion: 15
54212104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3189
Checksum: 276
Coasting Arc #14 (Orbit 3204)
---------------------------------------
Vector Time (GMT): 2018/126/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1864109
58 A = 6784403
09 meter
Y = -5607226
53 meter E =
0015242
Z = 3317840
52 I = 51
37282
XDOT = 6042
895095 Wp = 80
89423
YDOT = 762
454423 meter/sec RA = 224
95236 deg
ZDOT = 4667
737125 TA = 317
91288
MA = 318
02984
Ha = 221
847 n
mi
Hp = 213
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6115845
08 X = -1817385
94
Y = -18396412
51 feet Y = -5627811
19 meter
Z = 10885303
55 Z = 3308898
49
XDOT = 19825
771309 XDOT = 6011
246420
YDOT = 2501
490889 feet/sec YDOT = 829
853072 meter/sec
ZDOT = 15314
098178 ZDOT = 4697
014807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19149632
30 X = -5836807
93
Y = 3158366
93 feet Y = 962670
24 meter
Z = 10846090
94 Z = 3305888
52
XDOT = 5862
923542 XDOT = 1787
019095
YDOT = -17671
279598 feet/sec YDOT = -5386
206022 meter/sec
ZDOT = 15444
644445 ZDOT = 4707
527627
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 18126
66090785
00016717 00000-0 10270-3 0 9130
2 25544 51
6396 225
7264 0003206 49
1242 311
0188 15
54227947 32051
Satellite: ISS
Catalog Number: 25544
Epoch time: 18126
66090785 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 225
7264 deg
Eccentricity:
0003206
Arg of perigee: 49
1242 deg
Mean anomaly: 311
0188 deg
Mean motion: 15
54227947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3205
Checksum: 305
Coasting Arc #15 (Orbit 3219)
---------------------------------------
Vector Time (GMT): 2018/127/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 463018
79 A = 6780553
07 meter
Y = 5068818
66 meter E =
0012709
Z = -4492711
11 I = 51
38321
XDOT = -6603
460614 Wp = 65
64893
YDOT = -2215
314672 meter/sec RA = 219
94729 deg
ZDOT = -3181
930794 TA = 172
23260
MA = 172
21290
Ha = 221
931 n
mi
Hp = 213
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1519090
53 X = 428126
83
Y = 16629982
49 feet Y = 5073801
52 meter
Z = -14739865
86 Z = -4490546
48
XDOT = -21664
897026 XDOT = -6562
741335
YDOT = -7268
092757 feet/sec YDOT = -2288
931328 meter/sec
ZDOT = -10439
405491 ZDOT = -3213
909503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16688821
48 X = 5086752
79
Y = 783459
98 feet Y = 238798
60 meter
Z = -14730818
96 Z = -4489953
62
XDOT = -10231
868091 XDOT = -3118
673394
YDOT = 19113
677667 feet/sec YDOT = 5825
848953 meter/sec
ZDOT = -10581
846142 ZDOT = -3225
346704
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 18127
62538204
00016717 00000-0 10270-3 0 9141
2 25544 51
6389 220
9183 0003318 53
1615 306
9841 15
54214162 32204
Satellite: ISS
Catalog Number: 25544
Epoch time: 18127
62538204 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 220
9183 deg
Eccentricity:
0003318
Arg of perigee: 53
1615 deg
Mean anomaly: 306
9841 deg
Mean motion: 15
54214162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3220
Checksum: 289
Coasting Arc #16 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2018/128/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3232436
56 A = 6785939
63 meter
Y = -5287850
13 meter E =
0016729
Z = 2743100
95 I = 51
41249
XDOT = 5654
402557 Wp = 73
28183
YDOT = -785
314072 meter/sec RA = 217
88133 deg
ZDOT = 5127
998518 TA = 317
90247
MA = 318
03087
Ha = 222
017 n
mi
Hp = 213
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10605106
82 X = -3186390
75
Y = -17348589
65 feet Y = -5323740
08 meter
Z = 8999675
03 Z = 2727510
47
XDOT = 18551
189491 XDOT = 5637
854637
YDOT = -2576
489737 feet/sec YDOT = -722
175331 meter/sec
ZDOT = 16824
142119 ZDOT = 5155
425603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20189321
78 X = 6153705
28
Y = 2658814
05 feet Y = 810406
52 meter
Z = 8930733
34 Z = 2722087
52
XDOT = -9432
304957 XDOT = -2874
966551
YDOT = 14464
666259 feet/sec YDOT = 4408
830276 meter/sec
ZDOT = 16946
638659 ZDOT = 5165
335463
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 18128
07546970
00016717 00000-0 10270-3 0 9151
2 25544 51
6397 218
6757 0003576 50
6257 309
5212 15
54214277 32279
Satellite: ISS
Catalog Number: 25544
Epoch time: 18128
07546970 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 218
6757 deg
Eccentricity:
0003576
Arg of perigee: 50
6257 deg
Mean anomaly: 309
5212 deg
Mean motion: 15
54214277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 324
Coasting Arc #17 (Orbit 3241)
---------------------------------------
Vector Time (GMT): 2018/129/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1872545
05 A = 6781983
16 meter
Y = 5089324
45 meter E =
0010530
Z = -4084252
17 I = 51
42717
XDOT = -6604
240050 Wp = 65
61941
YDOT = -637
023163 meter/sec RA = 212
88326 deg
ZDOT = -3825
235242 TA = 164
68987
MA = 164
65799
Ha = 221
911 n
mi
Hp = 213
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6143520
51 X = 1835334
94
Y = 16697258
68 feet Y = 5110056
56 meter
Z = -13399777
47 Z = -4075246
22
XDOT = -21667
454233 XDOT = -6578
044743
YDOT = -2089
971006 feet/sec YDOT = -710
729784 meter/sec
ZDOT = -12549
984390 ZDOT = -3857
252952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16984439
39 X = -5176857
13
Y = -5397184
76 feet Y = -1645061
92 meter
Z = -13360184
99 Z = -4072184
39
XDOT = 14569
255112 XDOT = 4440
708958
YDOT = -14457
176220 feet/sec YDOT = -4406
547312 meter/sec
ZDOT = -12692
813862 ZDOT = -3868
769665
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 18129
03993749
00016717 00000-0 10270-3 0 9169
2 25544 51
6407 213
8677 0003408 51
9279 308
2181 15
54241227 32424
Satellite: ISS
Catalog Number: 25544
Epoch time: 18129
03993749 = yrday
fracday
Element set: 916
Inclination: 51
6407 deg
RA of node: 213
8677 deg
Eccentricity:
0003408
Arg of perigee: 51
9279 deg
Mean anomaly: 308
2181 deg
Mean motion: 15
54241227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3242
Checksum: 317
Coasting Arc #18 (Orbit 3257)
---------------------------------------
Vector Time (GMT): 2018/130/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -280799
61 A = 6778590
26 meter
Y = -4613356
76 meter E =
0008405
Z = 4951910
48 I = 51
44454
XDOT = 7135
534961 Wp = 100
55082
YDOT = 1855
157603 meter/sec RA = 207
87552 deg
ZDOT = 2128
359519 TA = 328
65094
MA = 328
70102
Ha = 221
979 n
mi
Hp = 213
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -921258
55 X = -253244
89
Y = -15135684
92 feet Y = -4616342
83 meter
Z = 16246425
45 Z = 4950613
33
XDOT = 23410
547772 XDOT = 7103
921220
YDOT = 6086
475077 feet/sec YDOT = 1934
775289 meter/sec
ZDOT = 6982
806821 ZDOT = 2162
944990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12689757
99 X = 3867838
24
Y = 8311332
52 feet Y = 2533294
15 meter
Z = 16241176
35 Z = 4950310
55
XDOT = -18345
174201 XDOT = -5591
609097
YDOT = 14033
673133 feet/sec YDOT = 4277
463571 meter/sec
ZDOT = 7136
971406 ZDOT = 2175
348885
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 18130
06870056
00016717 00000-0 10270-3 0 9170
2 25544 51
6412 208
7380 0003512 56
8107 303
3382 15
54239049 32589
Satellite: ISS
Catalog Number: 25544
Epoch time: 18130
06870056 = yrday
fracday
Element set: 917
Inclination: 51
6412 deg
RA of node: 208
7380 deg
Eccentricity:
0003512
Arg of perigee: 56
8107 deg
Mean anomaly: 303
3382 deg
Mean motion: 15
54239049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 293
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