[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 18th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
263/18:05:08
491 0
1 0
8 0
9
N/A -0
8 0
1 222
0
000/00:00:16
983 0
2 -0
0 215
2
267/01:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 215
7
268/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 215
7
271/01:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 216
1
274/09:07:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 216
3
Coasting Arc #1 (Orbit 1286)
---------------------------------------
Vector Time (GMT): 2018/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4301935
67 A = 6778552
45 meter
Y = -722051
28 meter E =
0007970
Z = 5185765
58 I = 51
24343
XDOT = -117
151688 Wp = 145
96942
YDOT = 7583
753222 meter/sec RA = 277
85044 deg
ZDOT = 1145
770630 TA = 292
94556
MA = 293
02965
Ha = 222
248 n
mi
Hp = 214
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14113962
16 X = 4284500
37
Y = -2368934
64 feet Y = -674041
26 meter
Z = 17013666
62 Z = 5206620
61
XDOT = -384
355931 XDOT = -207
512170
YDOT = 24881
080126 feet/sec YDOT = 7581
937975 meter/sec
ZDOT = 3759
089995 ZDOT = 1144
981676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14143292
58 X = -4310875
58
Y = 1260509
80 feet Y = 384203
39 meter
Z = 17107279
76 Z = 5214298
87
XDOT = 2454
628456 XDOT = 748
170753
YDOT = -23740
955904 feet/sec YDOT = -7236
243360 meter/sec
ZDOT = 3754
641495 ZDOT = 1144
414728
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 18260
55021177
00016717 00000-0 10270-3 0 9002
2 25544 51
6388 278
4263 0004600 165
1486 194
9802 15
53864325 12879
Satellite: ISS
Catalog Number: 25544
Epoch time: 18260
55021177 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 278
4263 deg
Eccentricity:
0004600
Arg of perigee: 165
1486 deg
Mean anomaly: 194
9802 deg
Mean motion: 15
53864325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1287
Checksum: 315
Coasting Arc #2 (Orbit 1301)
---------------------------------------
Vector Time (GMT): 2018/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4177477
93 A = 6778350
09 meter
Y = -996995
31 meter E =
0016328
Z = -5257960
55 I = 51
23944
XDOT = 929
975385 Wp = 111
06347
YDOT = -7568
047931 meter/sec RA = 272
82605 deg
ZDOT = 692
139263 TA = 165
61725
MA = 165
57072
Ha = 222
261 n
mi
Hp = 214
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13705636
27 X = -4140478
40
Y = -3270982
00 feet Y = -1043504
18 meter
Z = -17250526
75 Z = -5278163
35
XDOT = 3051
100343 XDOT = 1011
172235
YDOT = -24829
553580 feet/sec YDOT = -7557
194264 meter/sec
ZDOT = 2270
798108 ZDOT = 696
854381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13364110
15 X = 4073380
77
Y = 4100518
26 feet Y = 1249837
97 meter
Z = -17341014
15 Z = -5285541
11
XDOT = -4255
687428 XDOT = -1297
133528
YDOT = 23621
612913 feet/sec YDOT = 7199
867616 meter/sec
ZDOT = 2292
835440 ZDOT = 698
856242
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 18261
51490912
00016717 00000-0 10270-3 0 9017
2 25544 51
6392 273
6198 0004548 171
4134 188
7097 15
53844200 13024
Satellite: ISS
Catalog Number: 25544
Epoch time: 18261
51490912 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 273
6198 deg
Eccentricity:
0004548
Arg of perigee: 171
4134 deg
Mean anomaly: 188
7097 deg
Mean motion: 15
53844200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1302
Checksum: 305
Coasting Arc #3 (Orbit 1317)
---------------------------------------
Vector Time (GMT): 2018/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3969557
69 A = 6780086
41 meter
Y = 2639454
58 meter E =
0006668
Z = 4815267
28 I = 51
24431
XDOT = -1707
060234 Wp = 97
47838
YDOT = 7063
150952 meter/sec RA = 267
80284 deg
ZDOT = -2462
284748 TA = 16
83440
MA = 16
81229
Ha = 221
992 n
mi
Hp = 214
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13023483
24 X = 3916357
59
Y = 8659627
87 feet Y = 2683547
76 meter
Z = 15798120
98 Z = 4834420
58
XDOT = -5600
591320 XDOT = -1773
955031
YDOT = 23173
067428 feet/sec YDOT = 7043
687239 meter/sec
ZDOT = -8078
362033 ZDOT = -2470
739935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12522552
45 X = -3816873
99
Y = -9223560
31 feet Y = -2811341
18 meter
Z = 15883718
47 Z = 4841357
39
XDOT = 5893
450658 XDOT = 1796
323761
YDOT = -21991
369446 feet/sec YDOT = -6702
969407 meter/sec
ZDOT = -8117
097075 ZDOT = -2474
091189
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 18262
54391578
00016717 00000-0 10270-3 0 9020
2 25544 51
6383 268
4917 0004442 173
9947 186
1260 15
53882821 13189
Satellite: ISS
Catalog Number: 25544
Epoch time: 18262
54391578 = yrday
fracday
Element set: 902
Inclination: 51
6383 deg
RA of node: 268
4917 deg
Eccentricity:
0004442
Arg of perigee: 173
9947 deg
Mean anomaly: 186
1260 deg
Mean motion: 15
53882821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1318
Checksum: 333
Coasting Arc #4 (Orbit 1332)
---------------------------------------
Vector Time (GMT): 2018/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3704357
39 A = 6783493
45 meter
Y = -4107919
89 meter E =
0009190
Z = -3937399
16 I = 51
25689
XDOT = 2464
839379 Wp = 133
22942
YDOT = -6051
574495 meter/sec RA = 262
78776 deg
ZDOT = 3994
435022 TA = 178
73957
MA = 178
73725
Ha = 222
100 n
mi
Hp = 214
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12153403
51 X = -3639020
44
Y = -13477427
46 feet Y = -4148979
55 meter
Z = -12917976
23 Z = -3955234
57
XDOT = 8086
743370 XDOT = 2512
923794
YDOT = -19854
247030 feet/sec YDOT = -6023
741806 meter/sec
ZDOT = 13105
101777 ZDOT = 4006
525532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11698532
91 X = 3565712
83
Y = 13799618
90 feet Y = 4206123
84 meter
Z = -12997508
36 Z = -3961640
55
XDOT = -7526
864812 XDOT = -2294
188395
YDOT = 18776
746764 feet/sec YDOT = 5723
152414 meter/sec
ZDOT = 13160
010648 ZDOT = 4011
171245
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 18263
50860825
00016717 00000-0 10270-3 0 9034
2 25544 51
6375 263
6853 0004337 176
6302 183
4880 15
53851833 13338
Satellite: ISS
Catalog Number: 25544
Epoch time: 18263
50860825 = yrday
fracday
Element set: 903
Inclination: 51
6375 deg
RA of node: 263
6853 deg
Eccentricity:
0004337
Arg of perigee: 176
6302 deg
Mean anomaly: 183
4880 deg
Mean motion: 15
53851833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1333
Checksum: 316
Coasting Arc #5 (Orbit 1336)
---------------------------------------
Vector Time (GMT): 2018/263/18:05:16
983
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4272565
97 A = 6780223
06 meter
Y = -1929449
21 meter E =
0013425
Z = -4910683
85 I = 51
24775
XDOT = 724
315495 Wp = 123
55807
YDOT = -7289
211366 meter/sec RA = 261
52512 deg
ZDOT = 2230
935413 TA = 168
39457
MA = 168
36360
Ha = 221
982 n
mi
Hp = 215
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14017604
89 X = -4226819
38
Y = -6330213
96 feet Y = -1976972
60 meter
Z = -16111167
49 Z = -4931327
15
XDOT = 2376
363172 XDOT = 794
934985
YDOT = -23914
735452 feet/sec YDOT = -7280
716540 meter/sec
ZDOT = 7319
341907 ZDOT = 2234
625947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6326068
62 X = 1928185
71
Y = -13912609
00 feet Y = -4240563
22 meter
Z = -16203540
97 Z = -4938839
29
XDOT = 22900
568889 XDOT = 6980
093397
YDOT = 1857
204424 feet/sec YDOT = 566
075908 meter/sec
ZDOT = 7336
710086 ZDOT = 2236
229234
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 18263
76586051
00016717 00000-0 10270-3 0 9049
2 25544 51
6396 262
4037 0004001 188
3029 171
8058 15
53714318 13374
Satellite: ISS
Catalog Number: 25544
Epoch time: 18263
76586051 = yrday
fracday
Element set: 904
Inclination: 51
6396 deg
RA of node: 262
4037 deg
Eccentricity:
0004001
Arg of perigee: 188
3029 deg
Mean anomaly: 171
8058 deg
Mean motion: 15
53714318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1337
Checksum: 307
Coasting Arc #6 (Orbit 1352)
---------------------------------------
Vector Time (GMT): 2018/264/18:05:16
983
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4197780
11 A = 6783290
61 meter
Y = 3388239
58 meter E =
0009391
Z = 4103257
77 I = 51
26349
XDOT = -1552
516890 Wp = 99
02169
YDOT = 6497
981883 meter/sec RA = 256
51070 deg
ZDOT = -3771
428992 TA = 30
07156
MA = 30
01767
Ha = 221
772 n
mi
Hp = 215
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13772244
47 X = 4139648
51
Y = 11116271
59 feet Y = 3434857
41 meter
Z = 13462131
79 Z = 4123507
54
XDOT = -5093
559351 XDOT = -1606
744202
YDOT = 21318
838200 feet/sec YDOT = 6480
317012 meter/sec
ZDOT = -12373
454697 ZDOT = -3779
102854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10874945
13 X = -3314683
28
Y = 13875808
70 feet Y = 4229346
49 meter
Z = 13552590
35 Z = 4130829
54
XDOT = -20390
920811 XDOT = -6215
152663
YDOT = -3842
552133 feet/sec YDOT = -1171
209890 meter/sec
ZDOT = -12408
583851 ZDOT = -3782
136358
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 18264
79496759
00016717 00000-0 10270-3 0 9059
2 25544 51
6391 257
2776 0004041 192
2790 167
8264 15
53714264 13536
Satellite: ISS
Catalog Number: 25544
Epoch time: 18264
79496759 = yrday
fracday
Element set: 905
Inclination: 51
6391 deg
RA of node: 257
2776 deg
Eccentricity:
0004041
Arg of perigee: 192
2790 deg
Mean anomaly: 167
8264 deg
Mean motion: 15
53714264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1353
Checksum: 339
Coasting Arc #7 (Orbit 1367)
---------------------------------------
Vector Time (GMT): 2018/265/18:05:16
983
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4030910
21 A = 6786712
24 meter
Y = -4598595
54 meter E =
0003713
Z = -2948925
97 I = 51
28520
XDOT = 2422
440179 Wp = 125
55316
YDOT = -5306
598007 meter/sec RA = 251
50340 deg
ZDOT = 4966
236250 TA = 200
62001
MA = 200
63500
Ha = 221
744 n
mi
Hp = 215
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13224771
03 X = -3964863
56
Y = -15087255
69 feet Y = -4643303
00 meter
Z = -9674953
96 Z = -2968345
77
XDOT = 7947
638382 XDOT = 2457
476693
YDOT = -17410
098448 feet/sec YDOT = -5279
312161 meter/sec
ZDOT = 16293
426016 ZDOT = 4978
089264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14621124
88 X = 4456518
86
Y = -13676950
33 feet Y = -4168734
46 meter
Z = -9761573
85 Z = -2975327
71
XDOT = 16673
692004 XDOT = 5082
141323
YDOT = 6162
732033 feet/sec YDOT = 1878
400724 meter/sec
ZDOT = 16347
158056 ZDOT = 4982
613775
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 18265
75975081
00016717 00000-0 10270-3 0 9067
2 25544 51
6403 252
4700 0004022 197
2033 162
8984 15
53738412 13689
Satellite: ISS
Catalog Number: 25544
Epoch time: 18265
75975081 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 252
4700 deg
Eccentricity:
0004022
Arg of perigee: 197
2033 deg
Mean anomaly: 162
8984 deg
Mean motion: 15
53738412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1368
Checksum: 310
Coasting Arc #8 (Orbit 1383)
---------------------------------------
Vector Time (GMT): 2018/266/18:05:16
983
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3698955
49 A = 6789589
64 meter
Y = 5479164
45 meter E =
0015056
Z = 1508267
12 I = 51
30533
XDOT = -3341
578448 Wp = 133
40353
YDOT = 3842
647001 meter/sec RA = 246
50676 deg
ZDOT = -5738
365716 TA = 30
03801
MA = 29
95174
Ha = 221
711 n
mi
Hp = 215
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12135680
73 X = 3630084
66
Y = 17976261
31 feet Y = 5520143
84 meter
Z = 4948382
93 Z = 1526067
42
XDOT = -10963
183884 XDOT = -3356
425674
YDOT = 12607
109582 feet/sec YDOT = 3805
195440 meter/sec
ZDOT = -18826
659174 ZDOT = -5754
634475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17323421
59 X = -5280178
90
Y = 13020326
04 feet Y = 3968595
38 meter
Z = 5027662
02 Z = 1532431
38
XDOT = -12202
451605 XDOT = -3719
307249
YDOT = -8904
826453 feet/sec YDOT = -2714
191103 meter/sec
ZDOT = -18900
035728 ZDOT = -5760
730890
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 18266
78885204
00016717 00000-0 10270-3 0 9079
2 25544 51
6398 247
3434 0004051 199
0968 161
0033 15
53698030 13843
Satellite: ISS
Catalog Number: 25544
Epoch time: 18266
78885204 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 247
3434 deg
Eccentricity:
0004051
Arg of perigee: 199
0968 deg
Mean anomaly: 161
0033 deg
Mean motion: 15
53698030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1384
Checksum: 326
Coasting Arc #9 (Orbit 1388)
---------------------------------------
Vector Time (GMT): 2018/267/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3935183
83 A = 6778570
43 meter
Y = -1589588
29 meter E =
0003920
Z = 5284499
27 I = 51
27051
XDOT = 3097
431714 Wp = 164
77429
YDOT = 7013
008079 meter/sec RA = 244
96735 deg
ZDOT = -200
707738 TA = 287
12673
MA = 287
16966
Ha = 221
687 n
mi
Hp = 215
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12910708
11 X = 3926997
23
Y = -5215184
68 feet Y = -1545627
45 meter
Z = 17337596
04 Z = 5303595
37
XDOT = 10162
177538 XDOT = 3019
755035
YDOT = 23008
556689 feet/sec YDOT = 7047
211368 meter/sec
ZDOT = -658
489954 ZDOT = -185
851004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9487514
55 X = 2891794
43
Y = -10044312
95 feet Y = -3061506
59 meter
Z = 17423421
50 Z = 5310658
87
XDOT = 18049
013578 XDOT = 5501
339339
YDOT = 16041
446670 feet/sec YDOT = 4889
432945 meter/sec
ZDOT = -592
568204 ZDOT = -180
614789
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 18267
11044558
00016717 00000-0 10270-3 0 9087
2 25544 51
6375 245
7354 0004365 198
6947 161
4046 15
53712062 13896
Satellite: ISS
Catalog Number: 25544
Epoch time: 18267
11044558 = yrday
fracday
Element set: 908
Inclination: 51
6375 deg
RA of node: 245
7354 deg
Eccentricity:
0004365
Arg of perigee: 198
6947 deg
Mean anomaly: 161
4046 deg
Mean motion: 15
53712062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1389
Checksum: 327
Coasting Arc #10 (Orbit 1403)
---------------------------------------
Vector Time (GMT): 2018/268/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4586156
39 A = 6779739
08 meter
Y = 81404
01 meter E =
0013033
Z = -5004098
41 I = 51
29040
XDOT = -2265
244883 Wp = 124
50100
YDOT = -7048
476446 meter/sec RA = 239
94810 deg
ZDOT = 1957
800851 TA = 164
64343
MA = 164
60384
Ha = 221
661 n
mi
Hp = 215
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15046444
87 X = -4562418
42
Y = 267073
53 feet Y = 30250
51 meter
Z = -16417645
70 Z = -5026318
84
XDOT = -7431
905784 XDOT = -2195
768520
YDOT = -23124
922724 feet/sec YDOT = -7073
419268 meter/sec
ZDOT = 6423
231140 ZDOT = 1946
966674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13373466
31 X = -4076232
53
Y = 6658375
82 feet Y = 2029472
95 meter
Z = -16517334
89 Z = -5034483
67
XDOT = -16200
091480 XDOT = -4937
787883
YDOT = -16693
918041 feet/sec YDOT = -5088
306219 meter/sec
ZDOT = 6375
339923 ZDOT = 1943
203608
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 18268
07522354
00016717 00000-0 10270-3 0 9099
2 25544 51
6382 240
9294 0004460 202
7537 157
3419 15
53741230 14047
Satellite: ISS
Catalog Number: 25544
Epoch time: 18268
07522354 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 240
9294 deg
Eccentricity:
0004460
Arg of perigee: 202
7537 deg
Mean anomaly: 157
3419 deg
Mean motion: 15
53741230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1404
Checksum: 300
Coasting Arc #11 (Orbit 1409)
---------------------------------------
Vector Time (GMT): 2018/268/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4424905
93 A = 6789551
19 meter
Y = -4952138
78 meter E =
0004672
Z = -1405966
31 I = 51
32824
XDOT = 2838
345480 Wp = 50
23809
YDOT = -4169
729596 meter/sec RA = 237
97334 deg
ZDOT = 5769
555286 TA = 294
37804
MA = 294
42680
Ha = 221
575 n
mi
Hp = 215
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14517407
90 X = -4362371
37
Y = -16247174
46 feet Y = -5001271
67 meter
Z = -4612750
37 Z = -1427308
60
XDOT = 9312
157086 XDOT = 2856
735942
YDOT = -13680
215209 feet/sec YDOT = -4137
885677 meter/sec
ZDOT = 18928
987159 ZDOT = 5783
388284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10903181
09 X = 3323289
60
Y = 18840346
95 feet Y = 5742537
75 meter
Z = -4707997
98 Z = -1434997
78
XDOT = -10387
607557 XDOT = -3166
142783
YDOT = 10744
573442 feet/sec YDOT = 3274
945985 meter/sec
ZDOT = 18991
460435 ZDOT = 5788
597141
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 18268
46113360
00016717 00000-0 10270-3 0 9107
2 25544 51
6365 239
0106 0004045 203
2983 156
7987 15
53750191 14105
Satellite: ISS
Catalog Number: 25544
Epoch time: 18268
46113360 = yrday
fracday
Element set: 910
Inclination: 51
6365 deg
RA of node: 239
0106 deg
Eccentricity:
0004045
Arg of perigee: 203
2983 deg
Mean anomaly: 156
7987 deg
Mean motion: 15
53750191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1410
Checksum: 296
Coasting Arc #12 (Orbit 1425)
---------------------------------------
Vector Time (GMT): 2018/269/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3966073
82 A = 6790438
89 meter
Y = 5499177
67 meter E =
0013375
Z = -180109
51 I = 51
35053
XDOT = -3976
953808 Wp = 152
06484
YDOT = 2678
431742 meter/sec RA = 232
98315 deg
ZDOT = -5987
192596 TA = 29
88370
MA = 29
80740
Ha = 221
387 n
mi
Hp = 215
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13012053
22 X = 3905160
61
Y = 18041921
47 feet Y = 5543188
45 meter
Z = -590910
48 Z = -160992
11
XDOT = -13047
748713 XDOT = -3977
526241
YDOT = 8787
505716 feet/sec YDOT = 2633
954746 meter/sec
ZDOT = -19643
020328 ZDOT = -6006
513196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9447954
96 X = -2879736
67
Y = -20140855
60 feet Y = -6138932
79 meter
Z = -505684
96 Z = -154132
78
XDOT = 12852
285203 XDOT = 3917
376530
YDOT = -5552
069028 feet/sec YDOT = -1692
270640 meter/sec
ZDOT = -19729
962093 ZDOT = -6013
692446
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 18269
49022624
00016717 00000-0 10270-3 0 9114
2 25544 51
6375 233
8824 0003835 209
8868 150
2065 15
53744223 14267
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
49022624 = yrday
fracday
Element set: 911
Inclination: 51
6375 deg
RA of node: 233
8824 deg
Eccentricity:
0003835
Arg of perigee: 209
8868 deg
Mean anomaly: 150
2065 deg
Mean motion: 15
53744223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1426
Checksum: 315
Coasting Arc #13 (Orbit 1441)
---------------------------------------
Vector Time (GMT): 2018/270/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3269182
25 A = 6789097
82 meter
Y = -5690044
24 meter E =
0010640
Z = 1724662
75 I = 51
36671
XDOT = 5036
066879 Wp = 76
16188
YDOT = -1169
319622 meter/sec RA = 227
99540 deg
ZDOT = 5661
312473 TA = 302
82733
MA = 302
92974
Ha = 221
277 n
mi
Hp = 215
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10725663
55 X = -3213689
25
Y = -18668124
16 feet Y = -5726292
04 meter
Z = 5658342
36 Z = 1708917
38
XDOT = 16522
529129 XDOT = 5021
268156
YDOT = -3836
350467 feet/sec YDOT = -1113
084941 meter/sec
ZDOT = 18573
859820 ZDOT = 5685
740490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7467154
26 X = 2275988
62
Y = 20213080
11 feet Y = 6160946
82 meter
Z = 5588251
62 Z = 1703299
09
XDOT = -15336
265714 XDOT = -4674
493790
YDOT = 475
404849 feet/sec YDOT = 144
903398 meter/sec
ZDOT = 18683
572040 ZDOT = 5694
752758
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 18270
51931450
00016717 00000-0 10270-3 0 9126
2 25544 51
6371 228
7561 0004099 213
5233 146
5661 15
53785930 14423
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
51931450 = yrday
fracday
Element set: 912
Inclination: 51
6371 deg
RA of node: 228
7561 deg
Eccentricity:
0004099
Arg of perigee: 213
5233 deg
Mean anomaly: 146
5661 deg
Mean motion: 15
53785930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1442
Checksum: 303
Coasting Arc #14 (Orbit 1450)
---------------------------------------
Vector Time (GMT): 2018/271/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -414235
56 A = 6782643
79 meter
Y = -5250721
27 meter E =
0009579
Z = 4271576
57 I = 51
36087
XDOT = 6371
397604 Wp = 133
19269
YDOT = 2384
062486 meter/sec RA = 225
07402 deg
ZDOT = 3536
949284 TA = 280
55513
MA = 280
66303
Ha = 221
308 n
mi
Hp = 216
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1359040
54 X = -376239
16
Y = -17226775
80 feet Y = -5255140
65 meter
Z = 14014358
82 Z = 4269657
15
XDOT = 20903
535446 XDOT = 6327
083895
YDOT = 7821
727315 feet/sec YDOT = 2455
064462 meter/sec
ZDOT = 11604
164316 ZDOT = 3567
791960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7667375
20 X = -2337015
96
Y = -15493459
05 feet Y = -4722406
32 meter
Z = 14006253
35 Z = 4269106
02
XDOT = 21113
919299 XDOT = 6435
522602
YDOT = 200
376827 feet/sec YDOT = 61
074857 meter/sec
ZDOT = 11742
319294 ZDOT = 3579
058921
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 18271
09817780
00016717 00000-0 10270-3 0 9130
2 25544 51
6398 225
8682 0004420 214
4489 145
6377 15
53771206 14510
Satellite: ISS
Catalog Number: 25544
Epoch time: 18271
09817780 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 225
8682 deg
Eccentricity:
0004420
Arg of perigee: 214
4489 deg
Mean anomaly: 145
6377 deg
Mean motion: 15
53771206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1451
Checksum: 324
Coasting Arc #15 (Orbit 1465)
---------------------------------------
Vector Time (GMT): 2018/272/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -899014
52 A = 6779767
09 meter
Y = 4480830
78 meter E =
0009704
Z = -5016268
72 I = 51
37607
XDOT = -6543
668731 Wp = 91
25621
YDOT = -3479
515498 meter/sec RA = 220
06594 deg
ZDOT = -1938
821761 TA = 159
86105
MA = 159
82274
Ha = 221
180 n
mi
Hp = 216
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2949522
70 X = -924686
77
Y = 14700888
38 feet Y = 4470633
42 meter
Z = -16457574
55 Z = -5020698
63
XDOT = -21468
729434 XDOT = -6494
855536
YDOT = -11415
733260 feet/sec YDOT = -3552
418570 meter/sec
ZDOT = -6360
963782 ZDOT = -1970
490357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3000609
22 X = 914585
69
Y = 14667765
50 feet Y = 4470734
93 meter
Z = -16477881
01 Z = -5022458
13
XDOT = -23094
071690 XDOT = -7039
073051
YDOT = -2568
072668 feet/sec YDOT = -782
748549 meter/sec
ZDOT = -6502
734914 ZDOT = -1982
033602
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 18272
06294604
00016717 00000-0 10270-3 0 9143
2 25544 51
6406 221
0624 0004356 218
5774 141
5068 15
53745433 14665
Satellite: ISS
Catalog Number: 25544
Epoch time: 18272
06294604 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 221
0624 deg
Eccentricity:
0004356
Arg of perigee: 218
5774 deg
Mean anomaly: 141
5068 deg
Mean motion: 15
53745433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1466
Checksum: 302
Coasting Arc #16 (Orbit 1481)
---------------------------------------
Vector Time (GMT): 2018/273/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2261158
46 A = 6778342
14 meter
Y = -3577644
34 meter E =
0003599
Z = 5295174
74 I = 51
39794
XDOT = 6356
013245 Wp = 187
57186
YDOT = 4285
747281 meter/sec RA = 215
05317 deg
ZDOT = 177
985196 TA = 260
70579
MA = 260
74649
Ha = 220
946 n
mi
Hp = 216
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7418498
90 X = 2275275
01
Y = -11737678
27 feet Y = -3552279
24 meter
Z = 17372620
54 Z = 5306193
36
XDOT = 20853
061829 XDOT = 6306
751861
YDOT = 14060
850658 feet/sec YDOT = 4356
549204 meter/sec
ZDOT = 583
940933 ZDOT = 208
741126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2021490
16 X = 616150
20
Y = -13674370
74 feet Y = -4167948
20 meter
Z = 17422408
67 Z = 5310350
16
XDOT = 23727
725503 XDOT = 7232
210733
YDOT = 4441
548928 feet/sec YDOT = 1353
784113 meter/sec
ZDOT = 721
558221 ZDOT = 219
930946
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 18273
09202570
00016717 00000-0 10270-3 0 9159
2 25544 51
6407 215
9350 0004256 222
9331 137
1490 15
53792622 14821
Satellite: ISS
Catalog Number: 25544
Epoch time: 18273
09202570 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 215
9350 deg
Eccentricity:
0004256
Arg of perigee: 222
9331 deg
Mean anomaly: 137
1490 deg
Mean motion: 15
53792622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1482
Checksum: 294
Coasting Arc #17 (Orbit 1496)
---------------------------------------
Vector Time (GMT): 2018/274/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3620813
08 A = 6779176
31 meter
Y = 2614136
88 meter E =
0011813
Z = -5110644
23 I = 51
42795
XDOT = -5743
861367 Wp = 119
49669
YDOT = -4804
379978 meter/sec RA = 210
04323 deg
ZDOT = 1609
069290 TA = 166
10706
MA = 166
07453
Ha = 220
928 n
mi
Hp = 216
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11879307
99 X = -3624950
79
Y = 8576564
56 feet Y = 2573623
07 meter
Z = -16767205
48 Z = -5128243
31
XDOT = -18844
689524 XDOT = -5697
526684
YDOT = -15762
401501 feet/sec YDOT = -4868
352675 meter/sec
ZDOT = 5279
098719 ZDOT = 1581
279947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7159005
42 X = -2182064
85
Y = 12679141
72 feet Y = 3864602
40 meter
Z = -16846441
89 Z = -5134795
49
XDOT = -22787
667390 XDOT = -6945
681020
YDOT = -6004
957366 feet/sec YDOT = -1830
311005 meter/sec
ZDOT = 5154
824130 ZDOT = 1571
190395
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 18274
05678714
00016717 00000-0 10270-3 0 9164
2 25544 51
6402 211
1298 0004179 225
3568 134
7244 15
53784767 14975
Satellite: ISS
Catalog Number: 25544
Epoch time: 18274
05678714 = yrday
fracday
Element set: 916
Inclination: 51
6402 deg
RA of node: 211
1298 deg
Eccentricity:
0004179
Arg of perigee: 225
3568 deg
Mean anomaly: 134
7244 deg
Mean motion: 15
53784767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1497
Checksum: 333
Coasting Arc #18 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2018/274/09:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5492662
83 A = 6789873
23 meter
Y = -3860377
05 meter E =
0009538
Z = 985814
89 I = 51
46972
XDOT = 3488
029840 Wp = 58
86446
YDOT = -3448
563566 meter/sec RA = 208
38563 deg
ZDOT = 5892
455436 TA = 311
83840
MA = 311
91979
Ha = 220
838 n
mi
Hp = 216
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18020547
35 X = -5453875
43
Y = -12665279
04 feet Y = -3921582
90 meter
Z = 3234300
82 Z = 959227
45
XDOT = 11443
667454 XDOT = 3497
710568
YDOT = -11314
184928 feet/sec YDOT = -3409
503631 meter/sec
ZDOT = 19332
202875 ZDOT = 5909
422956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7892890
60 X = 2405753
06
Y = 20581718
80 feet Y = 6273307
89 meter
Z = 3115325
18 Z = 949551
11
XDOT = -14202
978956 XDOT = -4329
067986
YDOT = 2489
612734 feet/sec YDOT = 758
833961 meter/sec
ZDOT = 19408
685816 ZDOT = 5915
767437
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 18274
44268873
00016717 00000-0 10270-3 0 9179
2 25544 51
6365 209
2096 0004011 227
8824 132
1988 15
53810278 15036
Satellite: ISS
Catalog Number: 25544
Epoch time: 18274
44268873 = yrday
fracday
Element set: 917
Inclination: 51
6365 deg
RA of node: 209
2096 deg
Eccentricity:
0004011
Arg of perigee: 227
8824 deg
Mean anomaly: 132
1988 deg
Mean motion: 15
53810278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 319
Coasting Arc #19 (Orbit 1517)
---------------------------------------
Vector Time (GMT): 2018/275/09:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4700432
54 A = 6787779
88 meter
Y = 4204013
17 meter E =
0005834
Z = -2502629
42 I = 51
49278
XDOT = -4986
860580 Wp = 171
24961
YDOT = 2429
715147 meter/sec RA = 203
40277 deg
ZDOT = -5292
053703 TA = 36
87428
MA = 36
83417
Ha = 220
767 n
mi
Hp = 216
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15421366
59 X = 4665229
31
Y = 13792694
11 feet Y = 4256379
74 meter
Z = -8210726
46 Z = -2479881
79
XDOT = -16361
091141 XDOT = -4987
953448
YDOT = 7971
506387 feet/sec YDOT = 2373
942314 meter/sec
ZDOT = -17362
380914 ZDOT = -5316
281108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5479584
72 X = -1670177
42
Y = -19992280
17 feet Y = -6093647
00 meter
Z = -8108999
46 Z = -2471623
04
XDOT = 16508
813767 XDOT = 5031
886436
YDOT = 2551
882286 feet/sec YDOT = 777
813721 meter/sec
ZDOT = -17471
368107 ZDOT = -5325
272999
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 18275
40744614
00016717 00000-0 10270-3 0 9189
2 25544 51
6373 204
4021 0003802 234
8901 125
1895 15
53770074 15185
Satellite: ISS
Catalog Number: 25544
Epoch time: 18275
40744614 = yrday
fracday
Element set: 918
Inclination: 51
6373 deg
RA of node: 204
4021 deg
Eccentricity:
0003802
Arg of perigee: 234
8901 deg
Mean anomaly: 125
1895 deg
Mean motion: 15
53770074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1518
Checksum: 298
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