[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 22nd 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
265/17:52:27
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
4
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
270/11:54:38
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
0
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
277/07:57:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 216
4
Coasting Arc #1 (Orbit 1348)
---------------------------------------
Vector Time (GMT): 2018/264/12:03:24
619
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2611787
56 A = 6789418
99 meter
Y = 6053002
01 meter E =
0015531
Z = 1585388
86 I = 51
27943
XDOT = -3985
690604 Wp = 131
38446
YDOT = 3222
079650 meter/sec RA = 257
77713 deg
ZDOT = -5709
455164 TA = 31
17658
MA = 31
08453
Ha = 221
866 n
mi
Hp = 215
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8568856
82 X = 2536206
15
Y = 19858930
48 feet Y = 6081786
37 meter
Z = 5201407
01 Z = 1597891
86
XDOT = -13076
412742 XDOT = -3993
691162
YDOT = 10571
127462 feet/sec YDOT = 3177
463659 meter/sec
ZDOT = -18731
808280 ZDOT = -5728
835897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8635066
37 X = -2631968
23
Y = -19815612
68 feet Y = -6039798
75 meter
Z = 5256822
70 Z = 1602279
56
XDOT = 11452
645850 XDOT = 3490
766455
YDOT = -10005
877893 feet/sec YDOT = -3049
791582 meter/sec
ZDOT = -18819
091228 ZDOT = -5736
059006
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
53769407
00016717 00000-0 10270-3 0 9009
2 25544 51
6363 258
5570 0004017 190
7069 169
3998 15
53724827 13498
Satellite: ISS
Catalog Number: 25544
Epoch time: 18264
53769407 = yrday
fracday
Element set: 900
Inclination: 51
6363 deg
RA of node: 258
5570 deg
Eccentricity:
0004017
Arg of perigee: 190
7069 deg
Mean anomaly: 169
3998 deg
Mean motion: 15
53724827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1349
Checksum: 341
Coasting Arc #2 (Orbit 1363)
---------------------------------------
Vector Time (GMT): 2018/265/12:03:24
619
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2043523
60 A = 6790383
79 meter
Y = -6472449
76 meter E =
0008689
Z = -45284
96 I = 51
29136
XDOT = 4560
729810 Wp = 60
69593
YDOT = -1475
672249 meter/sec RA = 252
78407 deg
ZDOT = 5980
981892 TA = 298
81420
MA = 298
90141
Ha = 221
871 n
mi
Hp = 215
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6704473
77 X = -1970775
02
Y = -21235071
40 feet Y = -6494895
10 meter
Z = -148572
69 Z = -55034
28
XDOT = 14963
024310 XDOT = 4547
839854
YDOT = -4841
444386 feet/sec YDOT = -1424
742452 meter/sec
ZDOT = 19622
644004 ZDOT = 6003
105112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7175015
08 X = 2186944
60
Y = 21080387
65 feet Y = 6425302
16 meter
Z = -191610
75 Z = -58402
96
XDOT = -13183
460285 XDOT = -4018
318695
YDOT = 4646
228827 feet/sec YDOT = 1416
170547 meter/sec
ZDOT = 19722
036314 ZDOT = 6011
276669
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
50248361
00016717 00000-0 10270-3 0 9019
2 25544 51
6365 253
7509 0004301 192
3770 167
7277 15
53763701 13645
Satellite: ISS
Catalog Number: 25544
Epoch time: 18265
50248361 = yrday
fracday
Element set: 901
Inclination: 51
6365 deg
RA of node: 253
7509 deg
Eccentricity:
0004301
Arg of perigee: 192
3770 deg
Mean anomaly: 167
7277 deg
Mean motion: 15
53763701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1364
Checksum: 308
Coasting Arc #3 (Orbit 1367)
---------------------------------------
Vector Time (GMT): 2018/265/17:52:27
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4241523
68 A = 6778654
20 meter
Y = 627631
02 meter E =
0014322
Z = -5262428
74 I = 51
25795
XDOT = -1909
028233 Wp = 110
90184
YDOT = -7386
971378 meter/sec RA = 251
56571 deg
ZDOT = 654
091967 TA = 165
40609
MA = 165
36470
Ha = 221
722 n
mi
Hp = 215
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13915760
11 X = -4222664
74
Y = 2059156
87 feet Y = 580304
23 meter
Z = -17265186
17 Z = -5282986
80
XDOT = -6263
215988 XDOT = -1829
460411
YDOT = -24235
470401 feet/sec YDOT = -7407
874494 meter/sec
ZDOT = 2145
971019 ZDOT = 645
012649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1762658
05 X = -537258
17
Y = -13841477
85 feet Y = -4218882
45 meter
Z = -17357467
76 Z = -5290556
17
XDOT = 23354
535348 XDOT = 7118
462374
YDOT = -5629
717593 feet/sec YDOT = -1715
937922 meter/sec
ZDOT = 2106
030997 ZDOT = 641
918248
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
75976082
00016717 00000-0 10270-3 0 9025
2 25544 51
6403 252
4695 0003990 197
6950 162
4064 15
53730364 13680
Satellite: ISS
Catalog Number: 25544
Epoch time: 18265
75976082 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 252
4695 deg
Eccentricity:
0003990
Arg of perigee: 197
6950 deg
Mean anomaly: 162
4064 deg
Mean motion: 15
53730364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1368
Checksum: 329
Coasting Arc #4 (Orbit 1383)
---------------------------------------
Vector Time (GMT): 2018/266/17:52:27
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4641142
07 A = 6780281
76 meter
Y = 921211
45 meter E =
0004350
Z = 4852455
04 I = 51
27492
XDOT = 1053
885512 Wp = 91
37056
YDOT = 7216
533103 meter/sec RA = 246
54604 deg
ZDOT = -2376
261908 TA = 22
03536
MA = 22
01666
Ha = 221
406 n
mi
Hp = 215
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15226844
08 X = 4606925
22
Y = 3022347
28 feet Y = 972921
19 meter
Z = 15920128
09 Z = 4874916
89
XDOT = 3457
629632 XDOT = 984
652539
YDOT = 23676
289709 feet/sec YDOT = 7227
930989 meter/sec
ZDOT = -7796
134868 ZDOT = -2371
311526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3086362
40 X = -940723
26
Y = 15107960
45 feet Y = 4604906
35 meter
Z = 16020790
87 Z = 4883137
06
XDOT = -22588
432095 XDOT = -6884
954103
YDOT = 3635
943690 feet/sec YDOT = 1108
235637 meter/sec
ZDOT = -7774
677938 ZDOT = -2369
721836
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
78886499
00016717 00000-0 10270-3 0 9032
2 25544 51
6400 247
3426 0003904 202
7723 157
3257 15
53758719 13842
Satellite: ISS
Catalog Number: 25544
Epoch time: 18266
78886499 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 247
3426 deg
Eccentricity:
0003904
Arg of perigee: 202
7723 deg
Mean anomaly: 157
3257 deg
Mean motion: 15
53758719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1384
Checksum: 338
Coasting Arc #5 (Orbit 1388)
---------------------------------------
Vector Time (GMT): 2018/267/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3930788
96 A = 6778592
38 meter
Y = -1599581
99 meter E =
0003906
Z = 5284816
99 I = 51
27058
XDOT = 3104
625626 Wp = 165
22205
YDOT = 7010
048129 meter/sec RA = 244
96685 deg
ZDOT = -191
101846 TA = 286
58695
MA = 286
62985
Ha = 221
685 n
mi
Hp = 215
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12896289
24 X = 3922712
89
Y = -5247972
39 feet Y = -1555669
68 meter
Z = 17338638
41 Z = 5303892
00
XDOT = 10185
779614 XDOT = 3026
934852
YDOT = 22998
845567 feet/sec YDOT = 7044
331787 meter/sec
ZDOT = -626
974562 ZDOT = -176
210201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9460806
77 X = 2883653
90
Y = -10068183
83 feet Y = -3068782
43 meter
Z = 17424370
34 Z = 5310948
08
XDOT = 18064
544706 XDOT = 5506
073226
YDOT = 16024
870380 feet/sec YDOT = 4884
380492 meter/sec
ZDOT = -560
895898 ZDOT = -170
961070
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
11046221
00016717 00000-0 10270-3 0 9042
2 25544 51
6376 245
7349 0004351 199
1875 160
9114 15
53704150 13891
Satellite: ISS
Catalog Number: 25544
Epoch time: 18267
11046221 = yrday
fracday
Element set: 904
Inclination: 51
6376 deg
RA of node: 245
7349 deg
Eccentricity:
0004351
Arg of perigee: 199
1875 deg
Mean anomaly: 160
9114 deg
Mean motion: 15
53704150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1389
Checksum: 307
Coasting Arc #6 (Orbit 1403)
---------------------------------------
Vector Time (GMT): 2018/268/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4581836
91 A = 6779749
15 meter
Y = 94841
55 meter E =
0013011
Z = -5007812
60 I = 51
29042
XDOT = -2276
387671 Wp = 124
35773
YDOT = -7048
250068 meter/sec RA = 239
94769 deg
ZDOT = 1945
691549 TA = 164
66377
MA = 164
62430
Ha = 221
660 n
mi
Hp = 215
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15032273
34 X = -4558231
48
Y = 311159
93 feet Y = 43735
61 meter
Z = -16429831
35 Z = -5030012
37
XDOT = -7468
463488 XDOT = -2206
854191
YDOT = -23124
180012 feet/sec YDOT = -7073
317178 meter/sec
ZDOT = 6383
502458 ZDOT = 1934
803383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13341653
71 X = -4066536
05
Y = 6692059
93 feet Y = 2039739
87 meter
Z = -16529429
23 Z = -5038170
03
XDOT = -16230
088783 XDOT = -4946
931061
YDOT = -16679
975099 feet/sec YDOT = -5084
056410 meter/sec
ZDOT = 6335
369020 ZDOT = 1931
020477
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
07524550
00016717 00000-0 10270-3 0 9055
2 25544 51
6383 240
9290 0004445 203
2275 156
8677 15
53732375 14042
Satellite: ISS
Catalog Number: 25544
Epoch time: 18268
07524550 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 240
9290 deg
Eccentricity:
0004445
Arg of perigee: 203
2275 deg
Mean anomaly: 156
8677 deg
Mean motion: 15
53732375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1404
Checksum: 311
Coasting Arc #7 (Orbit 1419)
---------------------------------------
Vector Time (GMT): 2018/269/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5097450
12 A = 6782703
45 meter
Y = 1309641
07 meter E =
0007456
Z = 4271466
65 I = 51
31879
XDOT = 1243
754618 Wp = 98
02542
YDOT = 6694
661835 meter/sec RA = 234
93384 deg
ZDOT = -3532
581904 TA = 28
14583
MA = 28
10555
Ha = 221
484 n
mi
Hp = 215
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16723917
73 X = 5061677
76
Y = 4296722
67 feet Y = 1366444
82 meter
Z = 14013998
20 Z = 4296141
48
XDOT = 4080
559771 XDOT = 1185
960200
YDOT = 21964
113632 feet/sec YDOT = 6708
246768 meter/sec
ZDOT = -11589
835643 ZDOT = -3526
681336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16804869
77 X = 5122124
31
Y = -3554772
10 feet Y = -1083494
54 meter
Z = 14124565
22 Z = 4305167
48
XDOT = 13240
820104 XDOT = 4035
801968
YDOT = 16590
848270 feet/sec YDOT = 5056
890553 meter/sec
ZDOT = -11564
027306 ZDOT = -3524
715523
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
10434642
00016717 00000-0 10270-3 0 9063
2 25544 51
6396 235
8012 0004407 206
1875 153
9055 15
53701778 14206
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
10434642 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 235
8012 deg
Eccentricity:
0004407
Arg of perigee: 206
1875 deg
Mean anomaly: 153
9055 deg
Mean motion: 15
53701778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1420
Checksum: 303
Coasting Arc #8 (Orbit 1434)
---------------------------------------
Vector Time (GMT): 2018/270/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5442755
13 A = 6786196
99 meter
Y = -2534128
95 meter E =
0003595
Z = -3168624
50 I = 51
35084
XDOT = -11
533151 Wp = 141
97722
YDOT = -5973
393265 meter/sec RA = 229
93101 deg
ZDOT = 4797
208412 TA = 181
32114
MA = 181
32209
Ha = 221
444 n
mi
Hp = 215
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17856808
16 X = -5398621
56
Y = -8314071
37 feet Y = -2594747
22 meter
Z = -10395749
68 Z = -3194956
39
XDOT = -37
838423 XDOT = 31
961218
YDOT = -19597
746933 feet/sec YDOT = -5973
278484 meter/sec
ZDOT = 15738
872744 ZDOT = 4797
258727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19618049
13 X = -5979581
37
Y = 810256
42 feet Y = 246966
16 meter
Z = -10513639
94 Z = -3204557
46
XDOT = -9091
573993 XDOT = -2771
111753
YDOT = -15898
973708 feet/sec YDOT = -4846
007186 meter/sec
ZDOT = 15739
681205 ZDOT = 4797
454831
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
06912444
00016717 00000-0 10270-3 0 9072
2 25544 51
6399 230
9951 0004274 212
0098 148
0796 15
53709750 14353
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
06912444 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 230
9951 deg
Eccentricity:
0004274
Arg of perigee: 212
0098 deg
Mean anomaly: 148
0796 deg
Mean motion: 15
53709750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1435
Checksum: 319
Coasting Arc #9 (Orbit 1441)
---------------------------------------
Vector Time (GMT): 2018/270/11:54:38
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 399521
86 A = 6783242
58 meter
Y = 5365315
99 meter E =
0004946
Z = -4134933
71 I = 51
34820
XDOT = -6233
260003 Wp = 97
43171
YDOT = -2418
183460 meter/sec RA = 227
81385 deg
ZDOT = -3744
484351 TA = 133
85539
MA = 133
81451
Ha = 221
251 n
mi
Hp = 216
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1310767
27 X = 359581
35
Y = 17602742
75 feet Y = 5369559
94 meter
Z = -13566055
47 Z = -4133090
54
XDOT = -20450
328095 XDOT = -6187
566925
YDOT = -7933
672770 feet/sec YDOT = -2487
633029 meter/sec
ZDOT = -12285
053646 ZDOT = -3774
652571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2626899
90 X = -800679
09
Y = -17460934
74 feet Y = -5322092
91 meter
Z = -13558306
65 Z = -4132571
87
XDOT = 19599
375869 XDOT = 5973
889765
YDOT = 6684
132719 feet/sec YDOT = 2037
323653 meter/sec
ZDOT = -12420
172060 ZDOT = -3785
668444
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
51935405
00016717 00000-0 10270-3 0 9085
2 25544 51
6378 228
7550 0003823 215
8494 144
2402 15
53733689 14428
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
51935405 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 228
7550 deg
Eccentricity:
0003823
Arg of perigee: 215
8494 deg
Mean anomaly: 144
2402 deg
Mean motion: 15
53733689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1442
Checksum: 317
Coasting Arc #10 (Orbit 1450)
---------------------------------------
Vector Time (GMT): 2018/271/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -436902
57 A = 6782721
60 meter
Y = -5259159
87 meter E =
0009562
Z = 4259007
05 I = 51
36109
XDOT = 6369
470199 Wp = 132
74452
YDOT = 2360
170503 meter/sec RA = 225
07382 deg
ZDOT = 3556
349800 TA = 280
77312
MA = 280
88075
Ha = 221
309 n
mi
Hp = 216
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1433407
37 X = -398749
06
Y = -17254461
52 feet Y = -5263831
85 meter
Z = 13973120
24 Z = 4256977
90
XDOT = 20897
211939 XDOT = 6325
329561
YDOT = 7743
341546 feet/sec YDOT = 2431
151896 meter/sec
ZDOT = 11667
814305 ZDOT = 3587
183537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7746458
47 X = -2361120
54
Y = -15492051
49 feet Y = -4721977
30 meter
Z = 13964523
26 Z = 4256386
69
XDOT = 21079
004522 XDOT = 6424
880578
YDOT = 135
695764 feet/sec YDOT = 41
360069 meter/sec
ZDOT = 11805
931476 ZDOT = 3598
447914
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
09821932
00016717 00000-0 10270-3 0 9099
2 25544 51
6399 225
8678 0004404 214
9521 145
1342 15
53760303 14513
Satellite: ISS
Catalog Number: 25544
Epoch time: 18271
09821932 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 225
8678 deg
Eccentricity:
0004404
Arg of perigee: 214
9521 deg
Mean anomaly: 145
1342 deg
Mean motion: 15
53760303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1451
Checksum: 306
Coasting Arc #11 (Orbit 1465)
---------------------------------------
Vector Time (GMT): 2018/272/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -871412
36 A = 6779838
44 meter
Y = 4495456
96 meter E =
0009618
Z = -5008073
91 I = 51
37626
XDOT = -6548
419710 Wp = 90
90100
YDOT = -3455
433130 meter/sec RA = 220
06596 deg
ZDOT = -1965
733758 TA = 159
94357
MA = 159
90574
Ha = 221
184 n
mi
Hp = 216
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2858964
44 X = -897290
02
Y = 14748874
55 feet Y = 4485567
12 meter
Z = -16430688
69 Z = -5012370
23
XDOT = -21484
316635 XDOT = -6499
744731
YDOT = -11336
722866 feet/sec YDOT = -3528
390106 meter/sec
ZDOT = -6449
257736 ZDOT = -1997
425771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3102470
84 X = 945633
11
Y = 14677520
83 feet Y = 4473708
35 meter
Z = -16450397
13 Z = -5014081
05
XDOT = -23076
989492 XDOT = -7033
866397
YDOT = -2496
769183 feet/sec YDOT = -761
015247 meter/sec
ZDOT = -6591
136247 ZDOT = -2008
978328
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
06299481
00016717 00000-0 10270-3 0 9107
2 25544 51
6407 221
0621 0004340 219
0970 140
9869 15
53733140 14664
Satellite: ISS
Catalog Number: 25544
Epoch time: 18272
06299481 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 221
0621 deg
Eccentricity:
0004340
Arg of perigee: 219
0970 deg
Mean anomaly: 140
9869 deg
Mean motion: 15
53733140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1466
Checksum: 295
Coasting Arc #12 (Orbit 1481)
---------------------------------------
Vector Time (GMT): 2018/273/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2229978
93 A = 6778385
27 meter
Y = -3598617
49 meter E =
0003627
Z = 5294265
18 I = 51
39803
XDOT = 6370
055903 Wp = 187
63633
YDOT = 4263
248687 meter/sec RA = 215
05340 deg
ZDOT = 211
195379 TA = 260
32347
MA = 260
36444
Ha = 220
951 n
mi
Hp = 216
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7316203
83 X = 2244336
73
Y = -11806487
84 feet Y = -3573599
71 meter
Z = 17369636
42 Z = 5305132
93
XDOT = 20899
133541 XDOT = 6320
883740
YDOT = 13987
036374 feet/sec YDOT = 4334
208146 meter/sec
ZDOT = 692
898225 ZDOT = 242
019742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1900268
79 X = 579201
93
Y = -13696729
86 feet Y = -4174763
26 meter
Z = 17418749
45 Z = 5309234
83
XDOT = 23738
276686 XDOT = 7235
426734
YDOT = 4364
625636 feet/sec YDOT = 1330
337894 meter/sec
ZDOT = 830
824760 ZDOT = 253
235387
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
09208285
00016717 00000-0 10270-3 0 9114
2 25544 51
6408 215
9348 0004240 223
4724 136
6094 15
53779625 14826
Satellite: ISS
Catalog Number: 25544
Epoch time: 18273
09208285 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 215
9348 deg
Eccentricity:
0004240
Arg of perigee: 223
4724 deg
Mean anomaly: 136
6094 deg
Mean motion: 15
53779625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1482
Checksum: 314
Coasting Arc #13 (Orbit 1496)
---------------------------------------
Vector Time (GMT): 2018/274/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3588162
37 A = 6779179
67 meter
Y = 2641350
21 meter E =
0011817
Z = -5119687
70 I = 51
42789
XDOT = -5769
860654 Wp = 118
96344
YDOT = -4785
410259 meter/sec RA = 210
04356 deg
ZDOT = 1572
099722 TA = 166
27325
MA = 166
24109
Ha = 220
933 n
mi
Hp = 216
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11772186
26 X = -3592562
89
Y = 8665847
15 feet Y = 2601200
06 meter
Z = -16796875
67 Z = -5137128
82
XDOT = -18929
989022 XDOT = -5723
556582
YDOT = -15700
164891 feet/sec YDOT = -4849
673871 meter/sec
ZDOT = 5157
807486 ZDOT = 1544
184006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7024348
06 X = -2141021
29
Y = 12715955
62 feet Y = 3875823
27 meter
Z = -16875405
63 Z = -5143623
64
XDOT = -22836
112555 XDOT = -6960
447107
YDOT = -5923
142646 feet/sec YDOT = -1805
373878 meter/sec
ZDOT = 5032
963912 ZDOT = 1534
047400
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
05685279
00016717 00000-0 10270-3 0 9124
2 25544 51
6403 211
1297 0004158 225
9421 134
1389 15
53770459 14973
Satellite: ISS
Catalog Number: 25544
Epoch time: 18274
05685279 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 211
1297 deg
Eccentricity:
0004158
Arg of perigee: 225
9421 deg
Mean anomaly: 134
1389 deg
Mean motion: 15
53770459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1497
Checksum: 321
Coasting Arc #14 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2018/274/09:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5513248
50 A = 6789943
84 meter
Y = -3839826
67 meter E =
0009514
Z = 950860
35 I = 51
46988
XDOT = 3446
325605 Wp = 58
05470
YDOT = -3477
744816 meter/sec RA = 208
38540 deg
ZDOT = 5899
823403 TA = 312
26434
MA = 312
34498
Ha = 220
845 n
mi
Hp = 216
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18088085
63 X = -5474519
57
Y = -12597856
53 feet Y = -3901263
05 meter
Z = 3119620
56 Z = 924172
76
XDOT = 11306
842535 XDOT = 3456
299955
YDOT = -11409
923937 feet/sec YDOT = -3439
149604 meter/sec
ZDOT = 19356
375994 ZDOT = 5916
589050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7985930
34 X = 2434111
57
Y = 20563088
75 feet Y = 6267629
45 meter
Z = 3000193
49 Z = 914458
98
XDOT = -14144
173849 XDOT = -4311
144189
YDOT = 2638
745494 feet/sec YDOT = 804
289627 meter/sec
ZDOT = 19431
955565 ZDOT = 5922
860056
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
44275797
00016717 00000-0 10270-3 0 9138
2 25544 51
6366 209
2095 0003988 228
4583 131
6228 15
53795519 15038
Satellite: ISS
Catalog Number: 25544
Epoch time: 18274
44275797 = yrday
fracday
Element set: 913
Inclination: 51
6366 deg
RA of node: 209
2095 deg
Eccentricity:
0003988
Arg of perigee: 228
4583 deg
Mean anomaly: 131
6228 deg
Mean motion: 15
53795519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 340
Coasting Arc #15 (Orbit 1517)
---------------------------------------
Vector Time (GMT): 2018/275/09:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4734170
32 A = 6787901
01 meter
Y = 4187441
83 meter E =
0005915
Z = -2466703
00 I = 51
49310
XDOT = -4945
988901 Wp = 171
39555
YDOT = 2466
020444 meter/sec RA = 203
40276 deg
ZDOT = -5313
586305 TA = 36
28924
MA = 36
24914
Ha = 220
777 n
mi
Hp = 216
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15532054
84 X = 4698975
38
Y = 13738326
20 feet Y = 4240185
73 meter
Z = -8092857
60 Z = -2443791
46
XDOT = -16226
997708 XDOT = -4947
386188
YDOT = 8090
618254 feet/sec YDOT = 2410
702963 meter/sec
ZDOT = -17433
025935 ZDOT = -5337
615909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5601371
32 X = -1707297
98
Y = -20006472
30 feet Y = -6097972
76 meter
Z = -7990393
24 Z = -2435471
86
XDOT = 16459
690379 XDOT = 5016
913628
YDOT = 2387
614658 feet/sec YDOT = 727
744948 meter/sec
ZDOT = -17541
128539 ZDOT = -5346
535979
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
40752481
00016717 00000-0 10270-3 0 9146
2 25544 51
6374 204
4021 0003783 235
5576 124
5219 15
53754296 15181
Satellite: ISS
Catalog Number: 25544
Epoch time: 18275
40752481 = yrday
fracday
Element set: 914
Inclination: 51
6374 deg
RA of node: 204
4021 deg
Eccentricity:
0003783
Arg of perigee: 235
5576 deg
Mean anomaly: 124
5219 deg
Mean motion: 15
53754296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1518
Checksum: 311
Coasting Arc #16 (Orbit 1533)
---------------------------------------
Vector Time (GMT): 2018/276/09:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3625087
22 A = 6784463
22 meter
Y = -4342362
19 meter E =
0008836
Z = 3741507
59 I = 51
51296
XDOT = 6200
167797 Wp = 111
15555
YDOT = -1500
628258 meter/sec RA = 198
41620 deg
ZDOT = 4254
382222 TA = 293
65745
MA = 293
75017
Ha = 220
612 n
mi
Hp = 216
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11893330
78 X = -3594434
66
Y = -14246595
12 feet Y = -4382728
88 meter
Z = 12275287
37 Z = 3723972
72
XDOT = 20341
757863 XDOT = 6195
821773
YDOT = -4923
321056 feet/sec YDOT = -1431
317798 meter/sec
ZDOT = 13957
946922 ZDOT = 4284
490155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2612800
62 X = 796381
63
Y = 18425714
72 feet Y = 5616157
85 meter
Z = 12196957
80 Z = 3717632
74
XDOT = -18438
893939 XDOT = -5620
174873
YDOT = -6738
989027 feet/sec YDOT = -2054
043855 meter/sec
ZDOT = 14093
265060 ZDOT = 4295
627190
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 18276
43660152
00016717 00000-0 10270-3 0 9154
2 25544 51
6377 199
2755 0003917 239
7645 120
3120 15
53787714 15345
Satellite: ISS
Catalog Number: 25544
Epoch time: 18276
43660152 = yrday
fracday
Element set: 915
Inclination: 51
6377 deg
RA of node: 199
2755 deg
Eccentricity:
0003917
Arg of perigee: 239
7645 deg
Mean anomaly: 120
3120 deg
Mean motion: 15
53787714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 323
Coasting Arc #17 (Orbit 1547)
---------------------------------------
Vector Time (GMT): 2018/277/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6210762
08 A = 6787324
35 meter
Y = 663922
01 meter E =
0001300
Z = -2654887
91 I = 51
55161
XDOT = -2747
149315 Wp = 35
44628
YDOT = -4913
850353 meter/sec RA = 193
62118 deg
ZDOT = 5200
078072 TA = 294
58829
MA = 294
60183
Ha = 220
553 n
mi
Hp = 216
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20376516
02 X = -6204828
57
Y = 2178221
81 feet Y = 594501
98 meter
Z = -8710262
16 Z = -2685043
34
XDOT = -9012
957071 XDOT = -2717
256408
YDOT = -16121
556275 feet/sec YDOT = -4944
403432 meter/sec
ZDOT = 17060
623597 ZDOT = 5186
806234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15084191
63 X = 4597661
61
Y = 13785349
64 feet Y = 4201774
57 meter
Z = -8845734
59 Z = -2696179
90
XDOT = -5033
575596 XDOT = -1534
233842
YDOT = 16412
479737 feet/sec YDOT = 5002
523824 meter/sec
ZDOT = 17001
473032 ZDOT = 5182
048980
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 18277
33704292
00016717 00000-0 10270-3 0 9169
2 25544 51
6366 194
7893 0003707 243
0096 117
0679 15
53757861 15488
Satellite: ISS
Catalog Number: 25544
Epoch time: 18277
33704292 = yrday
fracday
Element set: 916
Inclination: 51
6366 deg
RA of node: 194
7893 deg
Eccentricity:
0003707
Arg of perigee: 243
0096 deg
Mean anomaly: 117
0679 deg
Mean motion: 15
53757861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1548
Checksum: 341
Coasting Arc #18 (Orbit 1563)
---------------------------------------
Vector Time (GMT): 2018/278/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6682531
59 A = 6789728
98 meter
Y = 86744
74 meter E =
0011820
Z = 1158709
64 I = 51
59304
XDOT = 958
633972 Wp = 137
08783
YDOT = 4848
767899 meter/sec RA = 188
64419 deg
ZDOT = -5864
882500 TA = 30
32044
MA = 30
25211
Ha = 220
358 n
mi
Hp = 216
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21924316
24 X = 6675436
52
Y = 284595
61 feet Y = 161433
87 meter
Z = 3801540
81 Z = 1191153
88
XDOT = 3145
124580 XDOT = 932
831018
YDOT = 15908
031165 feet/sec YDOT = 4859
343258 meter/sec
ZDOT = -19241
740487 ZDOT = -5860
288846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14568528
84 X = -4440487
59
Y = -16351929
40 feet Y = -4984068
08 meter
Z = 3947242
35 Z = 1203119
47
XDOT = 8336
769281 XDOT = 2541
047277
YDOT = -12087
892101 feet/sec YDOT = -3684
389512 meter/sec
ZDOT = -19221
544556 ZDOT = -5858
726781
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 18278
36611453
00016717 00000-0 10270-3 0 9170
2 25544 51
6374 189
6615 0003786 249
0913 110
9834 15
53780819 15645
Satellite: ISS
Catalog Number: 25544
Epoch time: 18278
36611453 = yrday
fracday
Element set: 917
Inclination: 51
6374 deg
RA of node: 189
6615 deg
Eccentricity:
0003786
Arg of perigee: 249
0913 deg
Mean anomaly: 110
9834 deg
Mean motion: 15
53780819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 339
Coasting Arc #19 (Orbit 1579)
---------------------------------------
Vector Time (GMT): 2018/279/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6727764
54 A = 6790208
12 meter
Y = -770264
42 meter E =
0009319
Z = 426319
29 I = 51
62839
XDOT = 921
466526 Wp = 41
12594
YDOT = -4694
740118 meter/sec RA = 183
67415 deg
ZDOT = 5991
711309 TA = 323
47080
MA = 323
53432
Ha = 220
304 n
mi
Hp = 216
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22072718
30 X = -6720722
05
Y = -2527114
25 feet Y = -845459
54 meter
Z = 1398685
33 Z = 393655
22
XDOT = 3023
184141 XDOT = 944
791253
YDOT = -15402
690677 feet/sec YDOT = -4684
304608 meter/sec
ZDOT = 19657
845501 ZDOT = 5996
244622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13345162
92 X = 4067605
66
Y = 17773197
34 feet Y = 5417270
55 meter
Z = 1252039
72 Z = 381621
71
XDOT = -11877
021184 XDOT = -3620
116057
YDOT = 7514
234479 feet/sec YDOT = 2290
338669 meter/sec
ZDOT = 19678
623268 ZDOT = 5998
044372
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 18279
39518044
00016717 00000-0 10270-3 0 9187
2 25544 51
6381 184
5346 0003818 250
6963 109
3777 15
53805301 15807
Satellite: ISS
Catalog Number: 25544
Epoch time: 18279
39518044 = yrday
fracday
Element set: 918
Inclination: 51
6381 deg
RA of node: 184
5346 deg
Eccentricity:
0003818
Arg of perigee: 250
6963 deg
Mean anomaly: 109
3777 deg
Mean motion: 15
53805301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 328
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