[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 24th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 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
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
280/14:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
6
Coasting Arc #1 (Orbit 1395)
---------------------------------------
Vector Time (GMT): 2018/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1582667
07 A = 6788928
46 meter
Y = -6331513
01 meter E =
0011311
Z = 1856206
36 I = 51
31050
XDOT = 5222
132804 Wp = 81
18092
YDOT = 345
237677 meter/sec RA = 242
79935 deg
ZDOT = 5602
561677 TA = 299
33600
MA = 299
44895
Ha = 221
589 n
mi
Hp = 215
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5192477
27 X = -1520765
21
Y = -20772680
48 feet Y = -6348865
14 meter
Z = 6089915
89 Z = 1848669
45
XDOT = 17132
981641 XDOT = 5190
669763
YDOT = 1132
669545 feet/sec YDOT = 403
459982 meter/sec
ZDOT = 18381
107865 ZDOT = 5627
852600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6095808
15 X = 1858002
32
Y = 20535579
48 feet Y = 6259244
62 meter
Z = 6056752
33 Z = 1846098
11
XDOT = -15545
440882 XDOT = -4738
250381
YDOT = -867
106358 feet/sec YDOT = -264
294018 meter/sec
ZDOT = 18494
524980 ZDOT = 5637
131214
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
56068992
00016717 00000-0 10270-3 0 9006
2 25544 51
6363 243
4961 0004165 202
7876 157
3092 15
53770437 13961
Satellite: ISS
Catalog Number: 25544
Epoch time: 18267
56068992 = yrday
fracday
Element set: 900
Inclination: 51
6363 deg
RA of node: 243
4961 deg
Eccentricity:
0004165
Arg of perigee: 202
7876 deg
Mean anomaly: 157
3092 deg
Mean motion: 15
53770437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1396
Checksum: 331
Coasting Arc #2 (Orbit 1410)
---------------------------------------
Vector Time (GMT): 2018/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 652463
49 A = 6786020
96 meter
Y = 5919930
72 meter E =
0004970
Z = -3250324
44 I = 51
31750
XDOT = -5707
106598 Wp = 145
88160
YDOT = -1961
755256 meter/sec RA = 237
80116 deg
ZDOT = -4726
207583 TA = 71
97407
MA = 71
91992
Ha = 221
487 n
mi
Hp = 215
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2140628
23 X = 602005
16
Y = 19422344
90 feet Y = 5926944
48 meter
Z = -10663794
09 Z = -3247278
29
XDOT = -18724
103012 XDOT = -5661
787946
YDOT = -6436
204907 feet/sec YDOT = -2025
323298 meter/sec
ZDOT = -15505
930391 ZDOT = -4753
820602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3352412
34 X = -1021815
28
Y = -19257459
60 feet Y = -5869673
69 meter
Z = -10650720
93 Z = -3246339
74
XDOT = 17563
390034 XDOT = 5353
321282
YDOT = 5573
027963 feet/sec YDOT = 1698
658923 meter/sec
ZDOT = -15629
608669 ZDOT = -4763
904722
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
52547184
00016717 00000-0 10270-3 0 9019
2 25544 51
6373 238
6885 0003885 206
9748 153
1203 15
53729445 14114
Satellite: ISS
Catalog Number: 25544
Epoch time: 18268
52547184 = yrday
fracday
Element set: 901
Inclination: 51
6373 deg
RA of node: 238
6885 deg
Eccentricity:
0003885
Arg of perigee: 206
9748 deg
Mean anomaly: 153
1203 deg
Mean motion: 15
53729445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1411
Checksum: 327
Coasting Arc #3 (Orbit 1426)
---------------------------------------
Vector Time (GMT): 2018/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 401568
61 A = 6782413
49 meter
Y = -5203111
52 meter E =
0009518
Z = 4329990
07 I = 51
32520
XDOT = 5987
347604 Wp = 132
60233
YDOT = 3333
812328 meter/sec RA = 232
79718 deg
ZDOT = 3439
620039 TA = 282
27346
MA = 282
38001
Ha = 221
305 n
mi
Hp = 215
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1317482
30 X = 438688
35
Y = -17070575
85 feet Y = -5198412
82 meter
Z = 14206004
17 Z = 4332031
57
XDOT = 19643
528884 XDOT = 5932
914940
YDOT = 10937
704488 feet/sec YDOT = 3400
463075 meter/sec
ZDOT = 11284
842649 ZDOT = 3468
572210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 79642
57 X = 24275
06
Y = 17113127
19 feet Y = 5216081
17 meter
Z = 14215674
75 Z = 4332937
66
XDOT = -19095
899948 XDOT = -5820
430304
YDOT = -9423
350343 feet/sec YDOT = -2872
237185 meter/sec
ZDOT = 11414
403586 ZDOT = 3479
110213
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
55456552
00016717 00000-0 10270-3 0 9022
2 25544 51
6381 233
5620 0004020 212
6473 147
4431 15
53769975 14273
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
55456552 = yrday
fracday
Element set: 902
Inclination: 51
6381 deg
RA of node: 233
5620 deg
Eccentricity:
0004020
Arg of perigee: 212
6473 deg
Mean anomaly: 147
4431 deg
Mean motion: 15
53769975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1427
Checksum: 309
Coasting Arc #4 (Orbit 1441)
---------------------------------------
Vector Time (GMT): 2018/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1596041
48 A = 6779674
85 meter
Y = 4248754
76 meter E =
0010427
Z = -5045397
01 I = 51
33628
XDOT = -5984
556507 Wp = 89
99410
YDOT = -4417
346572 meter/sec RA = 227
78476 deg
ZDOT = -1830
024687 TA = 162
20806
MA = 162
17152
Ha = 221
238 n
mi
Hp = 215
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5236356
56 X = -1618925
36
Y = 13939484
11 feet Y = 4230778
20 meter
Z = -16553139
80 Z = -5053206
20
XDOT = -19634
371741 XDOT = -5925
826293
YDOT = -14492
606865 feet/sec YDOT = -4483
941858 meter/sec
ZDOT = -6004
018001 ZDOT = -1858
952887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3804156
99 X = 1159507
05
Y = -14355563
02 feet Y = -4375575
61 meter
Z = -16588588
98 Z = -5056201
92
XDOT = 19813
254522 XDOT = 6039
079978
YDOT = 12325
422284 feet/sec YDOT = 3756
788712 meter/sec
ZDOT = -6133
378997 ZDOT = -1869
453918
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
51934197
00016717 00000-0 10270-3 0 9037
2 25544 51
6378 228
7548 0003820 216
0740 144
0155 15
53728444 14425
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
51934197 = yrday
fracday
Element set: 903
Inclination: 51
6378 deg
RA of node: 228
7548 deg
Eccentricity:
0003820
Arg of perigee: 216
0740 deg
Mean anomaly: 144
0155 deg
Mean motion: 15
53728444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1442
Checksum: 306
Coasting Arc #5 (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 = -429139
33 A = 6782689
31 meter
Y = -5256230
77 meter E =
0009551
Z = 4263320
76 I = 51
36103
XDOT = 6370
194550 Wp = 132
59644
YDOT = 2368
347475 meter/sec RA = 225
07342 deg
ZDOT = 3549
707591 TA = 281
00045
MA = 281
10787
Ha = 221
297 n
mi
Hp = 216
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1407937
44 X = -391040
11
Y = -17244851
61 feet Y = -5260816
24 meter
Z = 13987272
82 Z = 4261329
18
XDOT = 20899
588418 XDOT = 6325
994686
YDOT = 7770
168881 feet/sec YDOT = 2439
336636 meter/sec
ZDOT = 11646
022280 ZDOT = 3580
544701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7719326
51 X = -2352850
72
Y = -15492414
59 feet Y = -4722087
97 meter
Z = 13978844
17 Z = 4260751
70
XDOT = 21091
160203 XDOT = 6428
585630
YDOT = 157
750037 feet/sec YDOT = 48
082211 meter/sec
ZDOT = 11784
153802 ZDOT = 3591
810079
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
09820506
00016717 00000-0 10270-3 0 9040
2 25544 51
6399 225
8677 0004357 214
9086 145
1782 15
53765930 14514
Satellite: ISS
Catalog Number: 25544
Epoch time: 18271
09820506 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 225
8677 deg
Eccentricity:
0004357
Arg of perigee: 214
9086 deg
Mean anomaly: 145
1782 deg
Mean motion: 15
53765930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1451
Checksum: 328
Coasting Arc #6 (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 = -881468
67 A = 6779808
05 meter
Y = 4490142
99 meter E =
0009673
Z = -5011100
27 I = 51
37621
XDOT = -6546
701366 Wp = 90
74375
YDOT = -3464
197945 meter/sec RA = 220
06548 deg
ZDOT = -1955
874084 TA = 160
20050
MA = 160
16292
Ha = 221
172 n
mi
Hp = 216
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2891957
57 X = -907271
46
Y = 14731440
25 feet Y = 4480141
11 meter
Z = -16440617
67 Z = -5015445
26
XDOT = -21478
679023 XDOT = -6497
976398
YDOT = -11365
478822 feet/sec YDOT = -3537
135425 meter/sec
ZDOT = -6416
909724 ZDOT = -1987
557628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3065378
93 X = 934327
50
Y = 14674011
15 feet Y = 4472638
60 meter
Z = -16460543
99 Z = -5017173
81
XDOT = -23083
237596 XDOT = -7035
770819
YDOT = -2522
704705 feet/sec YDOT = -768
920394 meter/sec
ZDOT = -6558
749394 ZDOT = -1999
106815
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
06297694
00016717 00000-0 10270-3 0 9055
2 25544 51
6408 221
0619 0004293 219
0583 141
0259 15
53739102 14668
Satellite: ISS
Catalog Number: 25544
Epoch time: 18272
06297694 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 221
0619 deg
Eccentricity:
0004293
Arg of perigee: 219
0583 deg
Mean anomaly: 141
0259 deg
Mean motion: 15
53739102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1466
Checksum: 307
Coasting Arc #7 (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 = 2241932
26 A = 6778365
44 meter
Y = -3590574
58 meter E =
0003566
Z = 5294617
93 I = 51
39801
XDOT = 6364
749318 Wp = 187
28068
YDOT = 4271
852333 meter/sec RA = 215
05283 deg
ZDOT = 198
459935 TA = 260
80129
MA = 260
84163
Ha = 220
940 n
mi
Hp = 216
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7355420
80 X = 2256197
52
Y = -11780100
32 feet Y = -3565423
65 meter
Z = 17370793
73 Z = 5305543
52
XDOT = 20881
723484 XDOT = 6315
543204
YDOT = 14015
263559 feet/sec YDOT = 4342
752259 meter/sec
ZDOT = 651
115271 ZDOT = 229
258437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1946744
63 X = 593367
76
Y = -13688150
71 feet Y = -4172148
34 meter
Z = 17420165
58 Z = 5309666
47
XDOT = 23734
435540 XDOT = 7234
255952
YDOT = 4393
949743 feet/sec YDOT = 1339
275882 meter/sec
ZDOT = 788
924934 ZDOT = 240
464320
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
09206101
00016717 00000-0 10270-3 0 9063
2 25544 51
6408 215
9345 0004193 223
4394 136
6429 15
53785689 14822
Satellite: ISS
Catalog Number: 25544
Epoch time: 18273
09206101 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 215
9345 deg
Eccentricity:
0004193
Arg of perigee: 223
4394 deg
Mean anomaly: 136
6429 deg
Mean motion: 15
53785689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1482
Checksum: 319
Coasting Arc #8 (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 = -3600921
41 A = 6779175
97 meter
Y = 2630760
52 meter E =
0011819
Z = -5116187
04 I = 51
42793
XDOT = -5759
739169 Wp = 118
90556
YDOT = -4792
805558 meter/sec RA = 210
04294 deg
ZDOT = 1586
583586 TA = 166
47458
MA = 166
44287
Ha = 220
925 n
mi
Hp = 216
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11814046
62 X = -3605219
57
Y = 8631104
06 feet Y = 2590468
26 meter
Z = -16785390
55 Z = -5133689
88
XDOT = -18896
782052 XDOT = -5713
423509
YDOT = -15724
427685 feet/sec YDOT = -4856
955920 meter/sec
ZDOT = 5205
326725 ZDOT = 1558
717066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7076907
41 X = -2157041
38
Y = 12701702
49 feet Y = 3871478
92 meter
Z = -16864196
59 Z = -5140207
12
XDOT = -22817
263166 XDOT = -6954
701813
YDOT = -5955
013230 feet/sec YDOT = -1815
088033 meter/sec
ZDOT = 5080
704652 ZDOT = 1548
598778
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
05682709
00016717 00000-0 10270-3 0 9073
2 25544 51
6404 211
1294 0004112 225
8823 134
1991 15
53776825 14978
Satellite: ISS
Catalog Number: 25544
Epoch time: 18274
05682709 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 211
1294 deg
Eccentricity:
0004112
Arg of perigee: 225
8823 deg
Mean anomaly: 134
1991 deg
Mean motion: 15
53776825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1497
Checksum: 315
Coasting Arc #9 (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 = -5505169
37 A = 6789914
26 meter
Y = -3847877
80 meter E =
0009574
Z = 964635
48 I = 51
46984
XDOT = 3462
780056 Wp = 58
23920
YDOT = -3466
299599 meter/sec RA = 208
38500 deg
ZDOT = 5896
981677 TA = 312
23109
MA = 312
31229
Ha = 220
837 n
mi
Hp = 216
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18061579
28 X = -5466417
92
Y = -12624271
01 feet Y = -3909223
71 meter
Z = 3164814
56 Z = 937987
19
XDOT = 11360
826956 XDOT = 3472
639004
YDOT = -11372
374013 feet/sec YDOT = -3427
521028 meter/sec
ZDOT = 19347
052747 ZDOT = 5913
826975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7949442
56 X = 2422990
09
Y = 20570362
54 feet Y = 6269846
50 meter
Z = 3045564
65 Z = 928288
11
XDOT = -14167
504973 XDOT = -4318
255516
YDOT = 2580
075476 feet/sec YDOT = 786
407005 meter/sec
ZDOT = 19422
988755 ZDOT = 5920
126972
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
44273069
00016717 00000-0 10270-3 0 9082
2 25544 51
6366 209
2092 0003943 228
4247 131
6567 15
53801997 15037
Satellite: ISS
Catalog Number: 25544
Epoch time: 18274
44273069 = yrday
fracday
Element set: 908
Inclination: 51
6366 deg
RA of node: 209
2092 deg
Eccentricity:
0003943
Arg of perigee: 228
4247 deg
Mean anomaly: 131
6567 deg
Mean motion: 15
53801997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 323
Coasting Arc #10 (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 = 4720789
25 A = 6787851
65 meter
Y = 4194071
48 meter E =
0005845
Z = -2481084
67 I = 51
49300
XDOT = -4962
295299 Wp = 170
94318
YDOT = 2451
568156 meter/sec RA = 203
40227 deg
ZDOT = -5304
998666 TA = 36
91700
MA = 36
87678
Ha = 220
771 n
mi
Hp = 216
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15488153
70 X = 4685591
03
Y = 13760077
04 feet Y = 4246665
73 meter
Z = -8140041
56 Z = -2458238
14
XDOT = -16280
496387 XDOT = -4963
571479
YDOT = 8043
202611 feet/sec YDOT = 2396
069003 meter/sec
ZDOT = -17404
851265 ZDOT = -5329
107186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5552968
80 X = -1692544
89
Y = -20001002
24 feet Y = -6096305
48 meter
Z = -8037869
66 Z = -2449942
67
XDOT = 16479
332484 XDOT = 5022
900541
YDOT = 2453
076489 feet/sec YDOT = 747
697714 meter/sec
ZDOT = -17513
306797 ZDOT = -5338
055912
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
40749348
00016717 00000-0 10270-3 0 9098
2 25544 51
6375 204
4018 0003737 235
5510 124
5289 15
53760957 15183
Satellite: ISS
Catalog Number: 25544
Epoch time: 18275
40749348 = yrday
fracday
Element set: 909
Inclination: 51
6375 deg
RA of node: 204
4018 deg
Eccentricity:
0003737
Arg of perigee: 235
5510 deg
Mean anomaly: 124
5289 deg
Mean motion: 15
53760957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1518
Checksum: 325
Coasting Arc #11 (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 = -3605982
63 A = 6784401
42 meter
Y = -4346896
60 meter E =
0008845
Z = 3754555
87 I = 51
51282
XDOT = 6214
411394 Wp = 111
30450
YDOT = -1483
599556 meter/sec RA = 198
41558 deg
ZDOT = 4239
624649 TA = 293
70805
MA = 293
80083
Ha = 220
607 n
mi
Hp = 216
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11830651
68 X = -3575344
17
Y = -14261471
78 feet Y = -4387049
73 meter
Z = 12318096
69 Z = 3737113
77
XDOT = 20388
488827 XDOT = 6209
945577
YDOT = -4867
452611 feet/sec YDOT = -1414
130484 meter/sec
ZDOT = 13909
529689 ZDOT = 4269
801481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2551999
06 X = 777849
31
Y = 18405287
22 feet Y = 5609931
54 meter
Z = 12240184
06 Z = 3730808
10
XDOT = -18450
708413 XDOT = -5623
775924
YDOT = -6806
861408 feet/sec YDOT = -2074
731357 meter/sec
ZDOT = 14045
155610 ZDOT = 4280
963430
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
43656570
00016717 00000-0 10270-3 0 9108
2 25544 51
6377 199
2752 0003872 239
7586 120
3184 15
53794622 15342
Satellite: ISS
Catalog Number: 25544
Epoch time: 18276
43656570 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 199
2752 deg
Eccentricity:
0003872
Arg of perigee: 239
7586 deg
Mean anomaly: 120
3184 deg
Mean motion: 15
53794622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 334
Coasting Arc #12 (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 = -6220156
14 A = 6787343
56 meter
Y = 647039
80 meter E =
0001391
Z = -2636947
09 I = 51
55174
XDOT = -2719
853419 Wp = 34
64921
YDOT = -4916
717197 meter/sec RA = 193
62060 deg
ZDOT = 5211
755791 TA = 295
60830
MA = 295
62267
Ha = 220
550 n
mi
Hp = 216
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20407336
41 X = -6214120
29
Y = 2122833
97 feet Y = 577515
29 meter
Z = -8651401
23 Z = -2667147
91
XDOT = -8923
403607 XDOT = -2689
987208
YDOT = -16130
961931 feet/sec YDOT = -4946
965183 meter/sec
ZDOT = 17098
936323 ZDOT = 5198
616483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15063349
62 X = 4591308
96
Y = 13845408
68 feet Y = 4220080
57 meter
Z = -8787075
93 Z = -2678300
74
XDOT = -5095
364402 XDOT = -1553
067070
YDOT = 16353
303111 feet/sec YDOT = 4984
486788 meter/sec
ZDOT = 17040
381137 ZDOT = 5193
908171
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
33700302
00016717 00000-0 10270-3 0 9112
2 25544 51
6366 194
7890 0003662 242
9831 117
0948 15
53765216 15482
Satellite: ISS
Catalog Number: 25544
Epoch time: 18277
33700302 = yrday
fracday
Element set: 911
Inclination: 51
6366 deg
RA of node: 194
7890 deg
Eccentricity:
0003662
Arg of perigee: 242
9831 deg
Mean anomaly: 117
0948 deg
Mean motion: 15
53765216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1548
Checksum: 318
Coasting Arc #13 (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 = 6686158
20 A = 6789730
37 meter
Y = 105429
20 meter E =
0011837
Z = 1136022
52 I = 51
59312
XDOT = 925
663230 Wp = 137
20357
YDOT = 4848
289174 meter/sec RA = 188
64366 deg
ZDOT = -5870
571629 TA = 30
45518
MA = 30
38648
Ha = 220
359 n
mi
Hp = 216
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21936214
57 X = 6678964
12
Y = 345896
32 feet Y = 180158
33 meter
Z = 3727108
00 Z = 1168484
13
XDOT = 3036
952853 XDOT = 899
895714
YDOT = 15906
460546 feet/sec YDOT = 4858
496030 meter/sec
ZDOT = -19260
405607 ZDOT = -5866
138050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14531660
70 X = -4429250
18
Y = -16402441
28 feet Y = -4999464
10 meter
Z = 3872885
89 Z = 1180455
62
XDOT = 8404
842702 XDOT = 2561
796056
YDOT = -12009
789490 feet/sec YDOT = -3660
583837 meter/sec
ZDOT = -19240
928539 ZDOT = -5864
635019
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
36606982
00016717 00000-0 10270-3 0 9126
2 25544 51
6374 189
6611 0003741 249
1008 110
9745 15
53788213 15645
Satellite: ISS
Catalog Number: 25544
Epoch time: 18278
36606982 = yrday
fracday
Element set: 912
Inclination: 51
6374 deg
RA of node: 189
6611 deg
Eccentricity:
0003741
Arg of perigee: 249
1008 deg
Mean anomaly: 110
9745 deg
Mean motion: 15
53788213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 325
Coasting Arc #14 (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 = -6723724
57 A = 6790176
76 meter
Y = -790237
83 meter E =
0009387
Z = 451900
65 I = 51
62836
XDOT = 958
160516 Wp = 41
64710
YDOT = -4690
503209 meter/sec RA = 183
67360 deg
ZDOT = 5989
326456 TA = 323
22615
MA = 323
29051
Ha = 220
303 n
mi
Hp = 216
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22059463
82 X = -6716583
29
Y = -2592643
80 feet Y = -865387
21 meter
Z = 1482613
67 Z = 419256
44
XDOT = 3143
571248 XDOT = 981
446722
YDOT = -15388
790055 feet/sec YDOT = -4679
657576 meter/sec
ZDOT = 19650
021181 ZDOT = 5994
037923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13288850
64 X = 4050441
67
Y = 17809022
55 feet Y = 5428190
07 meter
Z = 1336059
05 Z = 407230
80
XDOT = -11947
110407 XDOT = -3641
479252
YDOT = 7421
322122 feet/sec YDOT = 2262
018983 meter/sec
ZDOT = 19671
598766 ZDOT = 5995
903304
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
39513070
00016717 00000-0 10270-3 0 9136
2 25544 51
6381 184
5342 0003775 250
6766 109
3978 15
53813160 15801
Satellite: ISS
Catalog Number: 25544
Epoch time: 18279
39513070 = yrday
fracday
Element set: 913
Inclination: 51
6381 deg
RA of node: 184
5342 deg
Eccentricity:
0003775
Arg of perigee: 250
6766 deg
Mean anomaly: 109
3978 deg
Mean motion: 15
53813160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 321
Coasting Arc #15 (Orbit 1594)
---------------------------------------
Vector Time (GMT): 2018/280/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6310696
61 A = 6788639
50 meter
Y = 1457095
03 meter E =
0006024
Z = -2022098
35 I = 51
65643
XDOT = -2810
900461 Wp = 173
69794
YDOT = 4464
712389 meter/sec RA = 178
70399 deg
ZDOT = -5562
656526 TA = 28
63470
MA = 28
60164
Ha = 220
286 n
mi
Hp = 216
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20704385
20 X = 6303756
30
Y = 4780495
49 feet Y = 1527626
57 meter
Z = -6634180
95 Z = -1991459
99
XDOT = -9222
114372 XDOT = -2833
596559
YDOT = 14648
006524 feet/sec YDOT = 4433
151391 meter/sec
ZDOT = -18250
185452 ZDOT = -5576
366651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11106380
28 X = -3385224
71
Y = -18165311
21 feet Y = -5536786
86 meter
Z = -6496679
65 Z = -1980187
96
XDOT = 15506
320252 XDOT = 4726
326413
YDOT = -2940
350003 feet/sec YDOT = -896
218681 meter/sec
ZDOT = -18312
165049 ZDOT = -5581
547907
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 18280
35987390
00016717 00000-0 10270-3 0 9145
2 25544 51
6385 179
7274 0003729 258
2812 101
7922 15
53793426 15953
Satellite: ISS
Catalog Number: 25544
Epoch time: 18280
35987390 = yrday
fracday
Element set: 914
Inclination: 51
6385 deg
RA of node: 179
7274 deg
Eccentricity:
0003729
Arg of perigee: 258
2812 deg
Mean anomaly: 101
7922 deg
Mean motion: 15
53793426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 342
Coasting Arc #16 (Orbit 1598)
---------------------------------------
Vector Time (GMT): 2018/280/14:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6397513
41 A = 6789181
19 meter
Y = 1584125
41 meter E =
0005621
Z = -1615352
39 I = 51
66889
XDOT = -2537
983658 Wp = 9
75929
YDOT = -4414
703779 meter/sec RA = 177
26589 deg
ZDOT = 5730
514810 TA = 332
57494
MA = 332
60459
Ha = 220
129 n
mi
Hp = 216
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20989217
21 X = -6406905
46
Y = 5197261
83 feet Y = 1512531
26 meter
Z = -5299712
55 Z = -1646452
54
XDOT = -8326
718037 XDOT = -2516
264637
YDOT = -14483
936282 feet/sec YDOT = -4442
963146 meter/sec
ZDOT = 18800
901607 ZDOT = 5718
239349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7295716
41 X = 2223734
36
Y = -20318204
53 feet Y = -6192988
74 meter
Z = -5439559
68 Z = -1657977
79
XDOT = 15256
861719 XDOT = 4650
291452
YDOT = 466
765989 feet/sec YDOT = 142
270273 meter/sec
ZDOT = 18746
145922 ZDOT = 5713
825277
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 18280
61713673
00016717 00000-0 10270-3 0 9156
2 25544 51
6397 178
4465 0003935 261
1588 98
9119 15
53777626 15999
Satellite: ISS
Catalog Number: 25544
Epoch time: 18280
61713673 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 178
4465 deg
Eccentricity:
0003935
Arg of perigee: 261
1588 deg
Mean anomaly: 98
9119 deg
Mean motion: 15
53777626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1599
Checksum: 359
Coasting Arc #17 (Orbit 1614)
---------------------------------------
Vector Time (GMT): 2018/281/14:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6721015
31 A = 6790358
63 meter
Y = -923572
60 meter E =
0010233
Z = 18773
28 I = 51
70615
XDOT = 667
050559 Wp = 152
16796
YDOT = 4705
208822 meter/sec RA = 172
30086 deg
ZDOT = -6018
602811 TA = 27
63003
MA = 27
57568
Ha = 220
148 n
mi
Hp = 216
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22050575
16 X = 6730752
24
Y = -3030093
82 feet Y = -848359
09 meter
Z = 61592
12 Z = 51445
83
XDOT = 2188
486086 XDOT = 643
621618
YDOT = 15437
036819 feet/sec YDOT = 4712
536503 meter/sec
ZDOT = -19746
072215 ZDOT = -6015
419954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9360731
52 X = -2853150
97
Y = 20192730
80 feet Y = 6154744
35 meter
Z = 208458
63 Z = 63538
19
XDOT = -12770
484962 XDOT = -3892
443816
YDOT = -5703
152936 feet/sec YDOT = -1738
321015 meter/sec
ZDOT = -19732
186742 ZDOT = -6014
370519
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 18281
64619158
00016717 00000-0 10270-3 0 9164
2 25544 51
6402 173
3199 0003999 262
4142 97
6556 15
53774087 16152
Satellite: ISS
Catalog Number: 25544
Epoch time: 18281
64619158 = yrday
fracday
Element set: 916
Inclination: 51
6402 deg
RA of node: 173
3199 deg
Eccentricity:
0003999
Arg of perigee: 262
4142 deg
Mean anomaly: 97
6556 deg
Mean motion: 15
53774087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1615
Checksum: 340
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