[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 29th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 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
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
5
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
283/18:05:00
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
5
284/08:40:17
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
284/14:44:01
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
7
Coasting Arc #1 (Orbit 1458)
---------------------------------------
Vector Time (GMT): 2018/271/13:41:14
982
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5116257
07 A = 6781965
26 meter
Y = -138588
68 meter E =
0005890
Z = 4444789
76 I = 51
37083
XDOT = 3001
400087 Wp = 86
51039
YDOT = 6262
826796 meter/sec RA = 222
39518 deg
ZDOT = -3255
452968 TA = 36
41913
MA = 36
37907
Ha = 220
981 n
mi
Hp = 216
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16785620
32 X = 5095835
73
Y = -454687
26 feet Y = -81488
91 meter
Z = 14582643
57 Z = 4469593
61
XDOT = 9847
113146 XDOT = 2946
957900
YDOT = 20547
332009 feet/sec YDOT = 6296
085830 meter/sec
ZDOT = -10680
619975 ZDOT = -3241
005762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13957383
27 X = -4254210
42
Y = 9159503
72 feet Y = 2791816
73 meter
Z = 14693952
06 Z = 4478716
59
XDOT = -18570
780664 XDOT = -5660
373946
YDOT = -11245
922136 feet/sec YDOT = -3427
757067 meter/sec
ZDOT = -10616
396389 ZDOT = -3235
877619
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
61275032
00016717 00000-0 10270-3 0 9002
2 25544 51
6397 223
3088 0003864 221
1951 138
8911 15
53733677 14598
Satellite: ISS
Catalog Number: 25544
Epoch time: 18271
61275032 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 223
3088 deg
Eccentricity:
0003864
Arg of perigee: 221
1951 deg
Mean anomaly: 138
8911 deg
Mean motion: 15
53733677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1459
Checksum: 314
Coasting Arc #2 (Orbit 1473)
---------------------------------------
Vector Time (GMT): 2018/272/13:41:14
982
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5786572
17 A = 6785426
53 meter
Y = -1004757
09 meter E =
0003559
Z = -3403060
79 I = 51
40810
XDOT = -1677
915020 Wp = 141
69041
YDOT = -5897
436169 meter/sec RA = 217
39351 deg
ZDOT = 4594
203503 TA = 178
41111
MA = 178
40998
Ha = 221
003 n
mi
Hp = 216
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18984816
82 X = -5758376
05
Y = -3296447
15 feet Y = -1069309
14 meter
Z = -11164897
60 Z = -3431101
90
XDOT = -5504
970539 XDOT = -1634
160165
YDOT = -19348
543860 feet/sec YDOT = -5915
954801 meter/sec
ZDOT = 15072
846138 ZDOT = 4586
159324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17693986
15 X = 5393126
98
Y = -7442390
27 feet Y = -2268440
56 meter
Z = -11290635
63 Z = -3441385
74
XDOT = 14627
067287 XDOT = 4458
330109
YDOT = 11961
857964 feet/sec YDOT = 3645
974307 meter/sec
ZDOT = 15037
309707 ZDOT = 4583
371999
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
57752036
00016717 00000-0 10270-3 0 9013
2 25544 51
6401 218
5017 0003801 225
3454 134
7389 15
53745570 14743
Satellite: ISS
Catalog Number: 25544
Epoch time: 18272
57752036 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 218
5017 deg
Eccentricity:
0003801
Arg of perigee: 225
3454 deg
Mean anomaly: 134
7389 deg
Mean motion: 15
53745570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1474
Checksum: 300
Coasting Arc #3 (Orbit 1489)
---------------------------------------
Vector Time (GMT): 2018/273/13:41:14
982
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6156159
63 A = 6788631
52 meter
Y = 1984341
51 meter E =
0012615
Z = 2037176
89 I = 51
44564
XDOT = 127
038969 Wp = 126
28091
YDOT = 5307
387125 meter/sec RA = 212
40367 deg
ZDOT = -5537
003015 TA = 31
12818
MA = 31
05351
Ha = 220
855 n
mi
Hp = 216
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20197374
13 X = 6123616
94
Y = 6510306
80 feet Y = 2053002
11 meter
Z = 6683651
20 Z = 2067002
71
XDOT = 416
794519 XDOT = 94
577129
YDOT = 17412
687419 feet/sec YDOT = 5308
625971 meter/sec
ZDOT = -18166
020391 ZDOT = -5536
465015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20379536
32 X = -6211682
67
Y = 5760887
25 feet Y = 1755918
43 meter
Z = 6817322
57 Z = 2077919
92
XDOT = -9685
015319 XDOT = -2951
992669
YDOT = -12703
042043 feet/sec YDOT = -3871
887215 meter/sec
ZDOT = -18164
107538 ZDOT = -5536
419978
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
60660565
00016717 00000-0 10270-3 0 9024
2 25544 51
6401 213
3752 0003747 228
5745 131
5086 15
53739802 14907
Satellite: ISS
Catalog Number: 25544
Epoch time: 18273
60660565 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 213
3752 deg
Eccentricity:
0003747
Arg of perigee: 228
5745 deg
Mean anomaly: 131
5086 deg
Mean motion: 15
53739802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1490
Checksum: 305
Coasting Arc #4 (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 = -5505644
42 A = 6789918
35 meter
Y = -3847401
95 meter E =
0009567
Z = 963878
59 I = 51
47012
XDOT = 3461
835625 Wp = 58
23932
YDOT = -3466
925847 meter/sec RA = 208
38471 deg
ZDOT = 5897
159209 TA = 312
22261
MA = 312
30376
Ha = 220
839 n
mi
Hp = 216
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18063137
87 X = -5466894
59
Y = -12622709
81 feet Y = -3908753
18 meter
Z = 3162331
33 Z = 937227
99
XDOT = 11357
728429 XDOT = 3471
700783
YDOT = -11374
428632 feet/sec YDOT = -3428
157802 meter/sec
ZDOT = 19347
635201 ZDOT = 5913
999934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7951593
50 X = 2423645
70
Y = 20569928
83 feet Y = 6269714
31 meter
Z = 3043071
00 Z = 927528
04
XDOT = -14166
110569 XDOT = -4317
830501
YDOT = 2583
355513 feet/sec YDOT = 787
406760 meter/sec
ZDOT = 19423
550742 ZDOT = 5920
298266
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
44273224
00016717 00000-0 10270-3 0 9030
2 25544 51
6369 209
2091 0003950 228
4119 131
6695 15
53800797 15034
Satellite: ISS
Catalog Number: 25544
Epoch time: 18274
44273224 = yrday
fracday
Element set: 903
Inclination: 51
6369 deg
RA of node: 209
2091 deg
Eccentricity:
0003950
Arg of perigee: 228
4119 deg
Mean anomaly: 131
6695 deg
Mean motion: 15
53800797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 308
Coasting Arc #5 (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 = 4721741
92 A = 6787856
10 meter
Y = 4193577
97 meter E =
0005853
Z = -2480098
36 I = 51
49328
XDOT = -4961
146979 Wp = 171
00105
YDOT = 2452
571930 meter/sec RA = 203
40202 deg
ZDOT = -5305
616759 TA = 36
84699
MA = 36
80678
Ha = 220
772 n
mi
Hp = 216
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15491279
26 X = 4686544
36
Y = 13758457
91 feet Y = 4246182
88 meter
Z = -8136805
64 Z = -2457247
20
XDOT = -16276
728933 XDOT = -4962
431466
YDOT = 8046
495834 feet/sec YDOT = 2397
085573 meter/sec
ZDOT = -17406
879129 ZDOT = -5329
719721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5556453
92 X = -1693607
16
Y = -20001332
91 feet Y = -6096406
27 meter
Z = -8034612
91 Z = -2448950
01
XDOT = 16477
928039 XDOT = 5022
472466
YDOT = 2448
510471 feet/sec YDOT = 746
305992 meter/sec
ZDOT = -17515
309803 ZDOT = -5338
666428
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
40749567
00016717 00000-0 10270-3 0 9046
2 25544 51
6377 204
4017 0003744 235
5275 124
5524 15
53760144 15180
Satellite: ISS
Catalog Number: 25544
Epoch time: 18275
40749567 = yrday
fracday
Element set: 904
Inclination: 51
6377 deg
RA of node: 204
4017 deg
Eccentricity:
0003744
Arg of perigee: 235
5275 deg
Mean anomaly: 124
5524 deg
Mean motion: 15
53760144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1518
Checksum: 310
Coasting Arc #6 (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 = -3607396
65 A = 6784405
65 meter
Y = -4346537
89 meter E =
0008843
Z = 3753626
75 I = 51
51310
XDOT = 6213
365360 Wp = 111
32267
YDOT = -1484
843070 meter/sec RA = 198
41537 deg
ZDOT = 4240
710749 TA = 293
67541
MA = 293
76819
Ha = 220
608 n
mi
Hp = 216
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11835290
85 X = -3576757
58
Y = -14260294
93 feet Y = -4386706
83 meter
Z = 12315048
39 Z = 3736177
78
XDOT = 20385
056955 XDOT = 6208
908250
YDOT = -4871
532382 feet/sec YDOT = -1415
385647 meter/sec
ZDOT = 13913
093010 ZDOT = 4270
882522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2556540
07 X = 779233
41
Y = 18406735
30 feet Y = 5610372
92 meter
Z = 12237104
89 Z = 3729869
57
XDOT = -18449
832267 XDOT = -5623
508875
YDOT = -6801
902070 feet/sec YDOT = -2073
219751 meter/sec
ZDOT = 14048
696325 ZDOT = 4282
042640
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
43656830
00016717 00000-0 10270-3 0 9051
2 25544 51
6380 199
2751 0003879 239
7293 120
3476 15
53794199 15340
Satellite: ISS
Catalog Number: 25544
Epoch time: 18276
43656830 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 199
2751 deg
Eccentricity:
0003879
Arg of perigee: 239
7293 deg
Mean anomaly: 120
3476 deg
Mean motion: 15
53794199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 345
Coasting Arc #7 (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 = -6219509
05 A = 6787340
99 meter
Y = 648211
38 meter E =
0001379
Z = -2638189
75 I = 51
55201
XDOT = -2721
756563 Wp = 34
69659
YDOT = -4916
486774 meter/sec RA = 193
62041 deg
ZDOT = 5210
974603 TA = 295
54562
MA = 295
55988
Ha = 220
550 n
mi
Hp = 216
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20405213
43 X = -6213480
32
Y = 2126677
76 feet Y = 578694
07 meter
Z = -8655478
18 Z = -2668387
44
XDOT = -8929
647515 XDOT = -2691
888992
YDOT = -16130
205950 feet/sec YDOT = -4946
756035 meter/sec
ZDOT = 17096
373369 ZDOT = 5197
826053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15064806
56 X = 4591753
04
Y = 13841252
67 feet Y = 4218813
81 meter
Z = -8791138
94 Z = -2679539
15
XDOT = -5090
978455 XDOT = -1551
730233
YDOT = 16357
362988 feet/sec YDOT = 4985
724239 meter/sec
ZDOT = 17037
776662 ZDOT = 5193
114327
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
33700578
00016717 00000-0 10270-3 0 9061
2 25544 51
6368 194
7889 0003669 242
9489 117
1289 15
53765131 15483
Satellite: ISS
Catalog Number: 25544
Epoch time: 18277
33700578 = yrday
fracday
Element set: 906
Inclination: 51
6368 deg
RA of node: 194
7889 deg
Eccentricity:
0003669
Arg of perigee: 242
9489 deg
Mean anomaly: 117
1289 deg
Mean motion: 15
53765131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1548
Checksum: 358
Coasting Arc #8 (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 = 6685937
93 A = 6789728
04 meter
Y = 104284
17 meter E =
0011837
Z = 1137395
47 I = 51
59339
XDOT = 927
670829 Wp = 137
22529
YDOT = 4848
292244 meter/sec RA = 188
64349 deg
ZDOT = -5870
257467 TA = 30
41835
MA = 30
34973
Ha = 220
357 n
mi
Hp = 216
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21935491
90 X = 6678750
01
Y = 342139
68 feet Y = 179010
87 meter
Z = 3731612
44 Z = 1169856
03
XDOT = 3043
539464 XDOT = 901
901603
YDOT = 15906
470616 feet/sec YDOT = 4858
521540 meter/sec
ZDOT = -19259
374893 ZDOT = -5865
814140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14533924
71 X = -4429940
25
Y = -16399350
86 feet Y = -4998522
14 meter
Z = 3877385
69 Z = 1181827
16
XDOT = 8400
635141 XDOT = 2560
513591
YDOT = -12014
486559 feet/sec YDOT = -3662
015503 meter/sec
ZDOT = -19239
854044 ZDOT = -5864
307513
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
36607249
00016717 00000-0 10270-3 0 9077
2 25544 51
6377 189
6611 0003749 249
0561 111
0191 15
53788538 15646
Satellite: ISS
Catalog Number: 25544
Epoch time: 18278
36607249 = yrday
fracday
Element set: 907
Inclination: 51
6377 deg
RA of node: 189
6611 deg
Eccentricity:
0003749
Arg of perigee: 249
0561 deg
Mean anomaly: 111
0191 deg
Mean motion: 15
53788538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 337
Coasting Arc #9 (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 = -6723923
20 A = 6790175
11 meter
Y = -789266
64 meter E =
0009377
Z = 450685
70 I = 51
62863
XDOT = 956
396383 Wp = 41
61985
YDOT = -4690
680451 meter/sec RA = 183
67346 deg
ZDOT = 5989
464105 TA = 323
24024
MA = 323
30451
Ha = 220
300 n
mi
Hp = 216
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22060115
48 X = -6716786
87
Y = -2589457
48 feet Y = -864418
27 meter
Z = 1478627
63 Z = 418040
52
XDOT = 3137
783409 XDOT = 979
684033
YDOT = -15389
371557 feet/sec YDOT = -4679
854538 meter/sec
ZDOT = 19650
472785 ZDOT = 5994
167006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13291594
15 X = 4051277
90
Y = 17807286
24 feet Y = 5427660
85 meter
Z = 1332068
54 Z = 406014
49
XDOT = -11943
678369 XDOT = -3640
433167
YDOT = 7425
727111 feet/sec YDOT = 2263
361624 meter/sec
ZDOT = 19672
011909 ZDOT = 5996
029230
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
39513304
00016717 00000-0 10270-3 0 9080
2 25544 51
6384 184
5342 0003783 250
6318 109
4425 15
53813870 15802
Satellite: ISS
Catalog Number: 25544
Epoch time: 18279
39513304 = yrday
fracday
Element set: 908
Inclination: 51
6384 deg
RA of node: 184
5342 deg
Eccentricity:
0003783
Arg of perigee: 250
6318 deg
Mean anomaly: 109
4425 deg
Mean motion: 15
53813870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 316
Coasting Arc #10 (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 = 6311129
25 A = 6788637
74 meter
Y = 1456375
22 meter E =
0006031
Z = -2021236
45 I = 51
65671
XDOT = -2809
642580 Wp = 173
76991
YDOT = 4464
985137 meter/sec RA = 178
70388 deg
ZDOT = -5563
085621 TA = 28
55264
MA = 28
51961
Ha = 220
282 n
mi
Hp = 216
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20705804
64 X = 6304192
78
Y = 4778133
92 feet Y = 1526911
62 meter
Z = -6631353
18 Z = -1990595
98
XDOT = -9217
987466 XDOT = -2832
339737
YDOT = 14648
901369 feet/sec YDOT = 4433
438200 meter/sec
ZDOT = -18251
593245 ZDOT = -5576
789638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11109047
18 X = -3386037
58
Y = -18164659
01 feet Y = -5536588
07 meter
Z = -6493842
33 Z = -1979323
14
XDOT = 15504
112179 XDOT = 4725
653392
YDOT = -2943
736124 feet/sec YDOT = -897
250771 meter/sec
ZDOT = -18313
545428 ZDOT = -5581
968647
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
35987567
00016717 00000-0 10270-3 0 9095
2 25544 51
6387 179
7274 0003737 258
2225 101
8509 15
53794536 15957
Satellite: ISS
Catalog Number: 25544
Epoch time: 18280
35987567 = yrday
fracday
Element set: 909
Inclination: 51
6387 deg
RA of node: 179
7274 deg
Eccentricity:
0003737
Arg of perigee: 258
2225 deg
Mean anomaly: 101
8509 deg
Mean motion: 15
53794536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 356
Coasting Arc #11 (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 = -6397165
32 A = 6789176
56 meter
Y = 1584727
45 meter E =
0005612
Z = -1616134
66 I = 51
66915
XDOT = -2539
104145 Wp = 9
68095
YDOT = -4414
395862 meter/sec RA = 177
26578 deg
ZDOT = 5730
254156 TA = 332
64450
MA = 332
67404
Ha = 220
125 n
mi
Hp = 216
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20988075
19 X = -6406560
33
Y = 5199237
06 feet Y = 1513137
18 meter
Z = -5302279
07 Z = -1647233
13
XDOT = -8330
394177 XDOT = -2517
387219
YDOT = -14482
926057 feet/sec YDOT = -4442
667771 meter/sec
ZDOT = 18800
046442 ZDOT = 5717
973246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7293430
13 X = 2223037
50
Y = -20318335
33 feet Y = -6193028
61 meter
Z = -5442118
69 Z = -1658757
78
XDOT = 15258
047073 XDOT = 4650
652748
YDOT = 463
318252 feet/sec YDOT = 141
219403 meter/sec
ZDOT = 18745
266254 ZDOT = 5713
557154
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
61713831
00016717 00000-0 10270-3 0 9107
2 25544 51
6400 178
4466 0003944 261
0971 98
9735 15
53778837 15999
Satellite: ISS
Catalog Number: 25544
Epoch time: 18280
61713831 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 178
4466 deg
Eccentricity:
0003944
Arg of perigee: 261
0971 deg
Mean anomaly: 98
9735 deg
Mean motion: 15
53778837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1599
Checksum: 340
Coasting Arc #12 (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 = 6720963
63 A = 6790354
17 meter
Y = -923880
89 meter E =
0010234
Z = 19156
85 I = 51
70642
XDOT = 667
595159 Wp = 152
21770
YDOT = 4705
109040 meter/sec RA = 172
30077 deg
ZDOT = -6018
628950 TA = 27
57615
MA = 27
52190
Ha = 220
143 n
mi
Hp = 216
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22050405
61 X = 6730702
15
Y = -3031105
27 feet Y = -848667
95 meter
Z = 62850
56 Z = 51829
16
XDOT = 2190
272831 XDOT = 644
167420
YDOT = 15436
709450 feet/sec YDOT = 4712
442818 meter/sec
ZDOT = -19746
157971 ZDOT = -6015
443444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9359784
31 X = -2852862
26
Y = 20193127
39 feet Y = 6154865
23 meter
Z = 209715
99 Z = 63921
43
XDOT = -12771
145983 XDOT = -3892
645295
YDOT = -5701
541082 feet/sec YDOT = -1737
829722 meter/sec
ZDOT = -19732
260589 ZDOT = -6014
393028
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
64619226
00016717 00000-0 10270-3 0 9115
2 25544 51
6404 173
3200 0004008 262
3560 97
7137 15
53775617 16158
Satellite: ISS
Catalog Number: 25544
Epoch time: 18281
64619226 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 173
3200 deg
Eccentricity:
0004008
Arg of perigee: 262
3560 deg
Mean anomaly: 97
7137 deg
Mean motion: 15
53775617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1615
Checksum: 297
Coasting Arc #13 (Orbit 1630)
---------------------------------------
Vector Time (GMT): 2018/282/14:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6597173
48 A = 6789217
74 meter
Y = 217962
15 meter E =
0010327
Z = 1564050
58 I = 51
73485
XDOT = 1206
411590 Wp = 53
07982
YDOT = -4923
265728 meter/sec RA = 167
33592 deg
ZDOT = 5754
570676 TA = 323
99718
MA = 324
06670
Ha = 220
006 n
mi
Hp = 216
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21644269
95 X = -6606717
95
Y = 715098
92 feet Y = 144134
79 meter
Z = 5131399
54 Z = 1531980
02
XDOT = 3958
043273 XDOT = 1233
422081
YDOT = -16152
446613 feet/sec YDOT = -4909
623104 meter/sec
ZDOT = 18879
825052 ZDOT = 5760
497284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10785694
76 X = 3287479
76
Y = -18817885
61 feet Y = -5735691
53 meter
Z = 4987285
73 Z = 1520124
69
XDOT = 10353
443149 XDOT = 3155
729472
YDOT = 10963
121569 feet/sec YDOT = 3341
559454 meter/sec
ZDOT = 18906
889763 ZDOT = 5762
820000
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 18282
67523939
00016717 00000-0 10270-3 0 9125
2 25544 51
6395 168
1914 0004071 266
8692 93
1994 15
53830839 16313
Satellite: ISS
Catalog Number: 25544
Epoch time: 18282
67523939 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 168
1914 deg
Eccentricity:
0004071
Arg of perigee: 266
8692 deg
Mean anomaly: 93
1994 deg
Mean motion: 15
53830839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1631
Checksum: 342
Coasting Arc #14 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2018/283/14:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6046739
42 A = 6786486
06 meter
Y = 579587
78 meter E =
0001548
Z = -3024407
83 I = 51
75558
XDOT = -2961
487373 Wp = 171
24323
YDOT = 5040
567720 meter/sec RA = 162
36961 deg
ZDOT = -4956
809863 TA = 43
33286
MA = 43
32069
Ha = 220
081 n
mi
Hp = 216
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19838383
93 X = 6054500
19
Y = 1901534
71 feet Y = 647249
71 meter
Z = -9922597
87 Z = -2995015
46
XDOT = -9716
165922 XDOT = -2993
554219
YDOT = 16537
295668 feet/sec YDOT = 5007
270522 meter/sec
ZDOT = -16262
499549 ZDOT = -4971
274432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11803116
34 X = -3597589
86
Y = 16138969
76 feet Y = 4919157
98 meter
Z = -9790575
03 Z = -2984167
27
XDOT = -8129
450824 XDOT = -2477
856611
YDOT = -15846
947256 feet/sec YDOT = -4830
149523 meter/sec
ZDOT = -16327
948416 ZDOT = -4976
758677
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 18283
63997072
00016717 00000-0 10270-3 0 9136
2 25544 51
6376 163
3846 0003977 271
8798 88
1898 15
53808008 16466
Satellite: ISS
Catalog Number: 25544
Epoch time: 18283
63997072 = yrday
fracday
Element set: 913
Inclination: 51
6376 deg
RA of node: 163
3846 deg
Eccentricity:
0003977
Arg of perigee: 271
8798 deg
Mean anomaly: 88
1898 deg
Mean motion: 15
53808008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 366
Coasting Arc #15 (Orbit 1647)
---------------------------------------
Vector Time (GMT): 2018/283/18:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 661054
60 A = 6778360
28 meter
Y = 4185592
39 meter E =
0011077
Z = -5300165
43 I = 51
73343
XDOT = -7384
467719 Wp = 98
13117
YDOT = 1941
665102 meter/sec RA = 161
64383 deg
ZDOT = 611
901685 TA = 177
71099
MA = 177
70591
Ha = 220
140 n
mi
Hp = 216
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2168814
30 X = 639946
97
Y = 13732258
51 feet Y = 4192866
23 meter
Z = -17388994
19 Z = -5297005
86
XDOT = -24227
256297 XDOT = -7408
603487
YDOT = 6370
292330 feet/sec YDOT = 1858
951965 meter/sec
ZDOT = 2007
551461 ZDOT = 575
970926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12161626
85 X = -3706863
86
Y = 6771558
16 feet Y = 2063970
93 meter
Z = -17375172
83 Z = -5295952
68
XDOT = -13661
708383 XDOT = -4164
088715
YDOT = -19796
131127 feet/sec YDOT = -6033
860768 meter/sec
ZDOT = 1845
919240 ZDOT = 562
636184
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 18283
76860304
00016717 00000-0 10270-3 0 9148
2 25544 51
6379 162
7410 0003706 264
4783 95
5940 15
53819541 16487
Satellite: ISS
Catalog Number: 25544
Epoch time: 18283
76860304 = yrday
fracday
Element set: 914
Inclination: 51
6379 deg
RA of node: 162
7410 deg
Eccentricity:
0003706
Arg of perigee: 264
4783 deg
Mean anomaly: 95
5940 deg
Mean motion: 15
53819541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1648
Checksum: 329
Coasting Arc #16 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2018/284/08:40:17
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2793837
20 A = 6778717
14 meter
Y = -3317250
56 meter E =
0002173
Z = 5210577
51 I = 51
75480
XDOT = 6633
513034 Wp = 194
25227
YDOT = -3641
063386 meter/sec RA = 158
63997 deg
ZDOT = 1236
809236 TA = 243
88433
MA = 243
90669
Ha = 220
079 n
mi
Hp = 216
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9166132
55 X = -2781845
94
Y = -10883367
99 feet Y = -3348425
71 meter
Z = 17095070
59 Z = 5197035
12
XDOT = 21763
494205 XDOT = 6667
727496
YDOT = -11945
746016 feet/sec YDOT = -3566
691429 meter/sec
ZDOT = 4057
773085 ZDOT = 1269
116668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2369938
45 X = 722357
24
Y = 14103753
11 feet Y = 4298823
95 meter
Z = 17034513
88 Z = 5192119
83
XDOT = -23756
666550 XDOT = -7241
031964
YDOT = -1092
500708 feet/sec YDOT = -332
994216 meter/sec
ZDOT = 4203
289440 ZDOT = 1281
162621
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 18284
41175392
00016717 00000-0 10270-3 0 9158
2 25544 51
6389 159
5404 0003994 274
1143 85
9552 15
53845595 16583
Satellite: ISS
Catalog Number: 25544
Epoch time: 18284
41175392 = yrday
fracday
Element set: 915
Inclination: 51
6389 deg
RA of node: 159
5404 deg
Eccentricity:
0003994
Arg of perigee: 274
1143 deg
Mean anomaly: 85
9552 deg
Mean motion: 15
53845595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 345
Coasting Arc #17 (Orbit 1661)
---------------------------------------
Vector Time (GMT): 2018/284/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5125793
55 A = 6782926
77 meter
Y = -1446469
44 meter E =
0006317
Z = 4196683
60 I = 51
77441
XDOT = 4457
316475 Wp = 111
04274
YDOT = -5018
969005 meter/sec RA = 157
39606 deg
ZDOT = 3707
531254 TA = 300
94163
MA = 301
00370
Ha = 220
149 n
mi
Hp = 216
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16816907
99 X = -5129623
51
Y = -4745634
66 feet Y = -1503810
71 meter
Z = 13768646
98 Z = 4171774
52
XDOT = 14623
741717 XDOT = 4495
099065
YDOT = -16466
433744 feet/sec YDOT = -4968
912652 meter/sec
ZDOT = 12163
816449 ZDOT = 3729
276001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12506067
11 X = 3811849
26
Y = -12328591
44 feet Y = -3757754
67 meter
Z = 13656837
13 Z = 4162603
96
XDOT = 6185
711874 XDOT = 1885
404979
YDOT = 19882
412854 feet/sec YDOT = 6060
159438 meter/sec
ZDOT = 12261
995217 ZDOT = 3737
456142
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 18284
66901428
00016717 00000-0 10270-3 0 9163
2 25544 51
6371 158
2565 0004100 275
2396 84
8289 15
53803601 16622
Satellite: ISS
Catalog Number: 25544
Epoch time: 18284
66901428 = yrday
fracday
Element set: 916
Inclination: 51
6371 deg
RA of node: 158
2565 deg
Eccentricity:
0004100
Arg of perigee: 275
2396 deg
Mean anomaly: 84
8289 deg
Mean motion: 15
53803601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1662
Checksum: 319
Coasting Arc #18 (Orbit 1676)
---------------------------------------
Vector Time (GMT): 2018/285/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3929843
42 A = 6779779
69 meter
Y = 2381242
70 meter E =
0009021
Z = -4993404
15 I = 51
79368
XDOT = -5589
111424 Wp = 64
53965
YDOT = 4794
931569 meter/sec RA = 152
41524 deg
ZDOT = -2111
266736 TA = 184
92426
MA = 184
93314
Ha = 220
083 n
mi
Hp = 216
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12893187
09 X = 3927179
49
Y = 7812476
03 feet Y = 2425173
75 meter
Z = -16382559
53 Z = -4974320
52
XDOT = -18336
979739 XDOT = -5632
058639
YDOT = 15731
402787 feet/sec YDOT = 4732
189991 meter/sec
ZDOT = -6926
728136 ZDOT = -2138
521890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13101988
02 X = -3993485
95
Y = 7642169
47 feet Y = 2329333
25 meter
Z = -16297007
93 Z = -4967328
02
XDOT = -4437
314051 XDOT = -1352
493323
YDOT = -22646
655731 feet/sec YDOT = -6902
700667 meter/sec
ZDOT = -7049
673101 ZDOT = -2148
740361
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 18285
63373907
00016717 00000-0 10270-3 0 9177
2 25544 51
6366 153
4485 0003923 278
0915 81
9792 15
53821301 16774
Satellite: ISS
Catalog Number: 25544
Epoch time: 18285
63373907 = yrday
fracday
Element set: 917
Inclination: 51
6366 deg
RA of node: 153
4485 deg
Eccentricity:
0003923
Arg of perigee: 278
0915 deg
Mean anomaly: 81
9792 deg
Mean motion: 15
53821301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1677
Checksum: 335
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