[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 17th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21814 1409 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
320/18:14:08
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
3
321/09:01:23
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
4
322/19:30:01
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
2
323/10:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 213
0
325/21:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
1
331/13:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
9
Coasting Arc #1 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2018/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5220617
29 A = 6782696
72 meter
Y = 1466331
39 meter E =
0014568
Z = 4061078
25 I = 51
50341
XDOT = -4403
639115 Wp = 86
56746
YDOT = 4962
754681 meter/sec RA = 339
13043 deg
ZDOT = 3857
986311 TA = 323
42134
MA = 323
52074
Ha = 222
910 n
mi
Hp = 213
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17128009
50 X = 5184105
53
Y = 4810798
53 feet Y = 1524507
76 meter
Z = 13323747
54 Z = 4086349
87
XDOT = -14447
634893 XDOT = -4477
547043
YDOT = 16282
003546 feet/sec YDOT = 4913
096829 meter/sec
ZDOT = 12657
435405 ZDOT = 3836
415238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13786524
65 X = -4202132
71
Y = 11108967
60 feet Y = 3386013
32 meter
Z = 13437161
81 Z = 4095646
92
XDOT = -4056
225372 XDOT = -1236
337493
YDOT = -20269
551380 feet/sec YDOT = -6178
159261 meter/sec
ZDOT = 12559
737385 ZDOT = 3828
207955
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 18320
55531318
00016717 00000-0 10270-3 0 9002
2 25544 51
6400 339
4281 0005316 53
7842 306
3801 15
53958858 22206
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
55531318 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 339
4281 deg
Eccentricity:
0005316
Arg of perigee: 53
7842 deg
Mean anomaly: 306
3801 deg
Mean motion: 15
53958858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 292
Coasting Arc #2 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2018/320/18:14:08
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4139764
85 A = 6779871
33 meter
Y = 2423058
29 meter E =
0010290
Z = 4782653
39 I = 51
48654
XDOT = -5638
209489 Wp = 91
80997
YDOT = 4519
429364 meter/sec RA = 337
82909 deg
ZDOT = 2585
484296 TA = 332
66053
MA = 332
71464
Ha = 222
736 n
mi
Hp = 213
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13581905
69 X = 4089129
94
Y = 7949666
30 feet Y = 2469068
85 meter
Z = 15691120
05 Z = 4802640
24
XDOT = -18498
062627 XDOT = -5700
887053
YDOT = 14827
524159 feet/sec YDOT = 4456
028508 meter/sec
ZDOT = 8482
560027 ZDOT = 2557
943275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7317625
64 X = 2230412
30
Y = 13831142
71 feet Y = 4215732
30 meter
Z = 15780635
32 Z = 4809937
64
XDOT = -22563
179008 XDOT = -6877
256962
YDOT = 2382
215588 feet/sec YDOT = 726
099311 meter/sec
ZDOT = 8358
087339 ZDOT = 2547
545021
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 18320
81254693
00016717 00000-0 10270-3 0 9010
2 25544 51
6403 338
1474 0005053 51
4587 308
7017 15
53998777 22241
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
81254693 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 338
1474 deg
Eccentricity:
0005053
Arg of perigee: 51
4587 deg
Mean anomaly: 308
7017 deg
Mean motion: 15
53998777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2224
Checksum: 315
Coasting Arc #3 (Orbit 2232)
---------------------------------------
Vector Time (GMT): 2018/321/09:01:23
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1408804
65 A = 6777934
02 meter
Y = -4003915
03 meter E =
0018841
Z = -5300469
24 I = 51
46057
XDOT = 7038
653260 Wp = 83
70600
YDOT = -2983
154240 meter/sec RA = 334
72739 deg
ZDOT = 385
851926 TA = 189
97035
MA = 190
00779
Ha = 222
891 n
mi
Hp = 213
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4622062
48 X = -1338179
78
Y = -13136204
15 feet Y = -4019274
35 meter
Z = -17389990
95 Z = -5307141
30
XDOT = 23092
694421 XDOT = 7069
614302
YDOT = -9787
251442 feet/sec YDOT = -2904
270015 meter/sec
ZDOT = 1265
918392 ZDOT = 420
118952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6896515
08 X = 2102057
80
Y = 12055582
91 feet Y = 3674541
67 meter
Z = -17419417
52 Z = -5309438
46
XDOT = -19952
050383 XDOT = -6081
384957
YDOT = 13450
976250 feet/sec YDOT = 4099
857561 meter/sec
ZDOT = 1420
403180 ZDOT = 432
938889
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 18321
39132369
00016717 00000-0 10270-3 0 9020
2 25544 51
6403 335
2616 0004867 55
1622 304
9987 15
53952654 22338
Satellite: ISS
Catalog Number: 25544
Epoch time: 18321
39132369 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 335
2616 deg
Eccentricity:
0004867
Arg of perigee: 55
1622 deg
Mean anomaly: 304
9987 deg
Mean motion: 15
53952654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2233
Checksum: 312
Coasting Arc #4 (Orbit 2248)
---------------------------------------
Vector Time (GMT): 2018/322/09:01:23
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -202286
21 A = 6779412
58 meter
Y = 4656938
63 meter E =
0011488
Z = 4916363
03 I = 51
43705
XDOT = -7047
835518 Wp = 57
65248
YDOT = 2057
602623 meter/sec RA = 329
71721 deg
ZDOT = -2229
167869 TA = 54
21191
MA = 54
10517
Ha = 222
848 n
mi
Hp = 213
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -663668
68 X = -278227
88
Y = 15278670
04 feet Y = 4654251
92 meter
Z = 16129799
97 Z = 4915195
91
XDOT = -23122
819940 XDOT = -7059
492083
YDOT = 6750
664775 feet/sec YDOT = 1978
723646 meter/sec
ZDOT = -7313
542877 ZDOT = -2263
432724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2376703
19 X = -724419
13
Y = -15113568
31 feet Y = -4606615
62 meter
Z = 16123895
20 Z = 4914563
26
XDOT = 20098
416408 XDOT = 6125
997321
YDOT = -11162
172755 feet/sec YDOT = -3402
230256 meter/sec
ZDOT = -7467
873051 ZDOT = -2276
207706
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 18322
42025504
00016717 00000-0 10270-3 0 9038
2 25544 51
6408 330
1334 0004892 57
9857 302
1770 15
54009723 22490
Satellite: ISS
Catalog Number: 25544
Epoch time: 18322
42025504 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 330
1334 deg
Eccentricity:
0004892
Arg of perigee: 57
9857 deg
Mean anomaly: 302
1770 deg
Mean motion: 15
54009723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2249
Checksum: 292
Coasting Arc #5 (Orbit 2255)
---------------------------------------
Vector Time (GMT): 2018/322/19:30:01
000
Vector Time (MET): N/A
Weight (LBS) : 917475
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5971982
69 A = 6785659
31 meter
Y = -887673
84 meter E =
0017775
Z = 3077270
40 I = 51
44656
XDOT = -1681
974727 Wp = 76
79027
YDOT = 5677
561412 meter/sec RA = 327
57923 deg
ZDOT = 4882
126459 TA = 318
70773
MA = 318
84201
Ha = 222
918 n
mi
Hp = 213
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19593119
06 X = 5966517
01
Y = -2912315
75 feet Y = -820921
53 meter
Z = 10096031
48 Z = 3106267
49
XDOT = -5518
289786 XDOT = -1769
053039
YDOT = 18627
169987 feet/sec YDOT = 5658
265533 meter/sec
ZDOT = 16017
475260 ZDOT = 4873
744334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19728019
92 X = 6013100
47
Y = 724886
53 feet Y = 220945
41 meter
Z = 10226510
58 Z = 3117040
42
XDOT = -8898
354801 XDOT = -2712
218543
YDOT = 15839
430623 feet/sec YDOT = 4827
858454 meter/sec
ZDOT = 15978
994488 ZDOT = 4870
397520
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 18322
87041443
00016717 00000-0 10270-3 0 9048
2 25544 51
6421 327
8914 0005242 57
7622 302
4039 15
53973547 22562
Satellite: ISS
Catalog Number: 25544
Epoch time: 18322
87041443 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 327
8914 deg
Eccentricity:
0005242
Arg of perigee: 57
7622 deg
Mean anomaly: 302
4039 deg
Mean motion: 15
53973547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2256
Checksum: 304
Coasting Arc #6 (Orbit 2264)
---------------------------------------
Vector Time (GMT): 2018/323/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3768550
76 A = 6778514
29 meter
Y = -2348682
92 meter E =
0018772
Z = -5138344
35 I = 51
40472
XDOT = 5335
228533 Wp = 74
06383
YDOT = -5279
243869 meter/sec RA = 324
47692 deg
ZDOT = -1499
391687 TA = 181
41781
MA = 181
42314
Ha = 223
026 n
mi
Hp = 213
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12364011
69 X = -3717047
15
Y = -7705652
64 feet Y = -2390537
51 meter
Z = -16858085
14 Z = -5156525
95
XDOT = 17504
030621 XDOT = 5401
149393
YDOT = -17320
353901 feet/sec YDOT = -5219
213050 meter/sec
ZDOT = -4919
264066 ZDOT = -1473
314338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14473666
28 X = 4411573
48
Y = -87675
26 feet Y = -26723
42 meter
Z = -16939486
40 Z = -5163155
45
XDOT = -5481
893202 XDOT = -1670
881048
YDOT = 22976
861116 feet/sec YDOT = 7003
347268 meter/sec
ZDOT = -4801
300182 ZDOT = -1463
436295
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 18323
44918568
00016717 00000-0 10270-3 0 9054
2 25544 51
6413 325
0058 0005164 62
7428 297
4250 15
53976215 22658
Satellite: ISS
Catalog Number: 25544
Epoch time: 18323
44918568 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 325
0058 deg
Eccentricity:
0005164
Arg of perigee: 62
7428 deg
Mean anomaly: 297
4250 deg
Mean motion: 15
53976215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2265
Checksum: 316
Coasting Arc #7 (Orbit 2280)
---------------------------------------
Vector Time (GMT): 2018/324/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2418591
54 A = 6777786
06 meter
Y = 3483706
46 meter E =
0007966
Z = 5280779
68 I = 51
37415
XDOT = -6015
631068 Wp = 67
93357
YDOT = 4750
343846 meter/sec RA = 319
46131 deg
ZDOT = -375
232837 TA = 25
67447
MA = 25
63494
Ha = 223
001 n
mi
Hp = 213
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7935011
60 X = 2353804
14
Y = 11429483
13 feet Y = 3510390
51 meter
Z = 17325392
66 Z = 5292371
33
XDOT = -19736
322403 XDOT = -6066
480916
YDOT = 15585
117604 feet/sec YDOT = 4682
788564 meter/sec
ZDOT = -1231
078860 ZDOT = -404
578844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12830047
06 X = -3910598
34
Y = -5214987
19 feet Y = -1589528
10 meter
Z = 17377011
41 Z = 5296513
08
XDOT = 7466
310681 XDOT = 2275
731496
YDOT = -22949
670907 feet/sec YDOT = -6995
059693 meter/sec
ZDOT = -1363
649654 ZDOT = -415
640414
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 18324
47811211
00016717 00000-0 10270-3 0 9066
2 25544 51
6394 319
8776 0005321 66
7869 293
3843 15
53995769 22818
Satellite: ISS
Catalog Number: 25544
Epoch time: 18324
47811211 = yrday
fracday
Element set: 906
Inclination: 51
6394 deg
RA of node: 319
8776 deg
Eccentricity:
0005321
Arg of perigee: 66
7869 deg
Mean anomaly: 293
3843 deg
Mean motion: 15
53995769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2281
Checksum: 348
Coasting Arc #8 (Orbit 2295)
---------------------------------------
Vector Time (GMT): 2018/325/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1062395
20 A = 6779474
27 meter
Y = -4546469
20 meter E =
0016624
Z = -4930388
05 I = 51
35632
XDOT = 6241
650958 Wp = 95
00174
YDOT = -3845
084882 meter/sec RA = 314
44542 deg
ZDOT = 2205
752088 TA = 196
61839
MA = 196
67294
Ha = 223
059 n
mi
Hp = 213
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3485548
56 X = -987526
49
Y = -14916237
54 feet Y = -4557930
86 meter
Z = -16175813
80 Z = -4935367
24
XDOT = 20477
857475 XDOT = 6273
469209
YDOT = -12615
107881 feet/sec YDOT = -3775
108572 meter/sec
ZDOT = 7236
719448 ZDOT = 2236
149829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11231314
70 X = 3423304
72
Y = 10382515
33 feet Y = 3164590
67 meter
Z = -16197564
29 Z = -4937017
59
XDOT = -8937
759254 XDOT = -2724
229021
YDOT = 21146
635750 feet/sec YDOT = 6445
494576 meter/sec
ZDOT = 7373
882162 ZDOT = 2247
559283
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 18325
44272689
00016717 00000-0 10270-3 0 9075
2 25544 51
6407 315
0702 0005164 68
3634 291
8069 15
53975063 22967
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
44272689 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 315
0702 deg
Eccentricity:
0005164
Arg of perigee: 68
3634 deg
Mean anomaly: 291
8069 deg
Mean motion: 15
53975063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2296
Checksum: 326
Coasting Arc #9 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2018/325/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4228379
35 A = 6778605
88 meter
Y = 1406422
16 meter E =
0008735
Z = 5100700
14 I = 51
34123
XDOT = -4022
451591 Wp = 95
22654
YDOT = 6341
401731 meter/sec RA = 312
09520 deg
ZDOT = 1582
886820 TA = 339
44087
MA = 339
47600
Ha = 222
917 n
mi
Hp = 213
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13872635
66 X = 4187560
89
Y = 4614245
94 feet Y = 1453478
38 meter
Z = 16734580
51 Z = 5121141
62
XDOT = -13197
019657 XDOT = -4100
752998
YDOT = 20805
123791 feet/sec YDOT = 6295
982001 meter/sec
ZDOT = 5193
198228 ZDOT = 1563
156710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14384502
22 X = 4384396
28
Y = -1936595
96 feet Y = -590274
45 meter
Z = 16826264
07 Z = 5128645
29
XDOT = -2823
315994 XDOT = -860
546715
YDOT = 23461
124874 feet/sec YDOT = 7150
950862 meter/sec
ZDOT = 5103
641593 ZDOT = 1555
589958
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 18325
95718742
00016717 00000-0 10270-3 0 9087
2 25544 51
6394 312
5051 0005124 68
0257 292
1439 15
53969947 23044
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
95718742 = yrday
fracday
Element set: 908
Inclination: 51
6394 deg
RA of node: 312
5051 deg
Eccentricity:
0005124
Arg of perigee: 68
0257 deg
Mean anomaly: 292
1439 deg
Mean motion: 15
53969947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 325
Coasting Arc #10 (Orbit 2318)
---------------------------------------
Vector Time (GMT): 2018/326/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3181407
38 A = 6777748
75 meter
Y = -2821937
07 meter E =
0019708
Z = -5294670
60 I = 51
31534
XDOT = 4796
676634 Wp = 87
09931
YDOT = -5956
933310 meter/sec RA = 307
07410 deg
ZDOT = 294
660745 TA = 185
71638
MA = 185
73891
Ha = 223
019 n
mi
Hp = 212
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10437688
25 X = -3123895
82
Y = -9258323
73 feet Y = -2857191
84 meter
Z = -17370966
54 Z = -5309985
71
XDOT = 15737
128063 XDOT = 4861
500879
YDOT = -19543
744457 feet/sec YDOT = -5902
931106 meter/sec
ZDOT = 966
734728 ZDOT = 318
119007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13412590
47 X = -4088157
57
Y = -3518753
40 feet Y = -1072516
04 meter
Z = -17439414
10 Z = -5315533
42
XDOT = 4802
961392 XDOT = 1463
942632
YDOT = -23594
267254 feet/sec YDOT = -7191
532659 meter/sec
ZDOT = 1072
988694 ZDOT = 327
046954
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 18326
92179673
00016717 00000-0 10270-3 0 9090
2 25544 51
6376 307
6962 0005126 72
4574 287
7138 15
54007852 23194
Satellite: ISS
Catalog Number: 25544
Epoch time: 18326
92179673 = yrday
fracday
Element set: 909
Inclination: 51
6376 deg
RA of node: 307
6962 deg
Eccentricity:
0005126
Arg of perigee: 72
4574 deg
Mean anomaly: 287
7138 deg
Mean motion: 15
54007852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2319
Checksum: 338
Coasting Arc #11 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2018/327/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2055963
12 A = 6779311
67 meter
Y = 4162598
89 meter E =
0011178
Z = 4932848
23 I = 51
30191
XDOT = -5260
988515 Wp = 65
43934
YDOT = 5156
348329 meter/sec RA = 302
05378 deg
ZDOT = -2150
055259 TA = 45
64489
MA = 45
55335
Ha = 222
926 n
mi
Hp = 213
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6745285
83 X = 1985301
20
Y = 13656820
52 feet Y = 4185194
55 meter
Z = 16183885
27 Z = 4942664
39
XDOT = -17260
461006 XDOT = -5307
813139
YDOT = 16917
153309 feet/sec YDOT = 5097
254686 meter/sec
ZDOT = -7053
987071 ZDOT = -2175
725211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12300622
62 X = 3749229
78
Y = 8904534
48 feet Y = 2714102
11 meter
Z = 16227437
22 Z = 4946122
86
XDOT = -6534
421627 XDOT = -1991
691712
YDOT = 22143
340894 feet/sec YDOT = 6749
290304 meter/sec
ZDOT = -7170
067610 ZDOT = -2185
436608
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 18327
95071146
00016717 00000-0 10270-3 0 9102
2 25544 51
6381 302
5679 0004959 76
3374 283
8330 15
53997690 23359
Satellite: ISS
Catalog Number: 25544
Epoch time: 18327
95071146 = yrday
fracday
Element set: 910
Inclination: 51
6381 deg
RA of node: 302
5679 deg
Eccentricity:
0004959
Arg of perigee: 76
3374 deg
Mean anomaly: 283
8330 deg
Mean motion: 15
53997690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 335
Coasting Arc #12 (Orbit 2349)
---------------------------------------
Vector Time (GMT): 2018/328/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -988084
66 A = 6782477
10 meter
Y = -5311719
06 meter E =
0012202
Z = -4111797
28 I = 51
29579
XDOT = 5392
310428 Wp = 97
42900
YDOT = -3916
800935 meter/sec RA = 297
03755 deg
ZDOT = 3772
129478 TA = 211
67157
MA = 211
74504
Ha = 223
015 n
mi
Hp = 212
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3241747
59 X = -908640
75
Y = -17426899
82 feet Y = -5322323
87 meter
Z = -13490148
55 Z = -4116404
76
XDOT = 17691
307178 XDOT = 5417
385034
YDOT = -12850
396770 feet/sec YDOT = -3856
360581 meter/sec
ZDOT = 12375
752882 ZDOT = 3798
384471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11245620
58 X = -3427665
15
Y = -13682178
58 feet Y = -4170328
03 meter
Z = -13510139
88 Z = -4117890
64
XDOT = 8116
008865 XDOT = 2473
759502
YDOT = -18981
646037 feet/sec YDOT = -5785
605712 meter/sec
ZDOT = 12494
292133 ZDOT = 3808
260242
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 18328
91531563
00016717 00000-0 10270-3 0 9114
2 25544 51
6380 297
7589 0005089 80
8042 279
3686 15
54016938 23509
Satellite: ISS
Catalog Number: 25544
Epoch time: 18328
91531563 = yrday
fracday
Element set: 911
Inclination: 51
6380 deg
RA of node: 297
7589 deg
Eccentricity:
0005089
Arg of perigee: 80
8042 deg
Mean anomaly: 279
3686 deg
Mean motion: 15
54016938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2350
Checksum: 337
Coasting Arc #13 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2018/329/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -38052
15 A = 6786183
03 meter
Y = 6156013
25 meter E =
0018176
Z = 2837722
89 I = 51
29422
XDOT = -5297
308824 Wp = 94
89035
YDOT = 2306
553981 meter/sec RA = 292
03118 deg
ZDOT = -5048
296383 TA = 52
66769
MA = 52
50221
Ha = 222
939 n
mi
Hp = 212
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -124843
02 X = -120671
95
Y = 20196893
88 feet Y = 6155125
45 meter
Z = 9310114
48 Z = 2837338
07
XDOT = -17379
622127 XDOT = -5298
185326
YDOT = 7567
434320 feet/sec YDOT = 2247
311467 meter/sec
ZDOT = -16562
652176 ZDOT = -5074
031124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9983563
98 X = 3042990
30
Y = 17558646
40 feet Y = 5351875
42 meter
Z = 9307562
88 Z = 2836945
17
XDOT = -9851
499112 XDOT = -3002
736929
YDOT = 14488
516189 feet/sec YDOT = 4416
099734 meter/sec
ZDOT = -16678
636333 ZDOT = -5083
648354
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 18329
94422111
00016717 00000-0 10270-3 0 9127
2 25544 51
6380 292
6304 0004963 83
2201 276
9516 15
54037670 23660
Satellite: ISS
Catalog Number: 25544
Epoch time: 18329
94422111 = yrday
fracday
Element set: 912
Inclination: 51
6380 deg
RA of node: 292
6304 deg
Eccentricity:
0004963
Arg of perigee: 83
2201 deg
Mean anomaly: 276
9516 deg
Mean motion: 15
54037670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 301
Coasting Arc #14 (Orbit 2380)
---------------------------------------
Vector Time (GMT): 2018/330/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 907769
58 A = 6788899
44 meter
Y = -6592884
29 meter E =
0012718
Z = -1326728
43 I = 51
29102
XDOT = 4998
745631 Wp = 56
23903
YDOT = -467
979016 meter/sec RA = 287
03299 deg
ZDOT = 5792
802128 TA = 289
25120
MA = 289
38875
Ha = 223
065 n
mi
Hp = 212
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2978246
67 X = 987870
20
Y = -21630197
82 feet Y = -6582284
97 meter
Z = -4352783
57 Z = -1322124
92
XDOT = 16400
084090 XDOT = 4975
468545
YDOT = -1535
364225 feet/sec YDOT = -412
210346 meter/sec
ZDOT = 19005
256324 ZDOT = 5817
027945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8611090
89 X = -2624660
50
Y = -20069174
05 feet Y = -6117084
25 meter
Z = -4331224
13 Z = -1320157
12
XDOT = 11671
948313 XDOT = 3557
609846
YDOT = -9099
732995 feet/sec YDOT = -2773
598617 meter/sec
ZDOT = 19114
216864 ZDOT = 5826
013300
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 18330
90882021
00016717 00000-0 10270-3 0 9136
2 25544 51
6372 287
8228 0005192 89
3802 270
7945 15
54020217 23815
Satellite: ISS
Catalog Number: 25544
Epoch time: 18330
90882021 = yrday
fracday
Element set: 913
Inclination: 51
6372 deg
RA of node: 287
8228 deg
Eccentricity:
0005192
Arg of perigee: 89
3802 deg
Mean anomaly: 270
7945 deg
Mean motion: 15
54020217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2381
Checksum: 305
Coasting Arc #15 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2018/331/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1692243
84 A = 6789613
05 meter
Y = -6568413
34 meter E =
0016514
Z = 93406
15 I = 51
28961
XDOT = 4621
590895 Wp = 58
31880
YDOT = 1286
757244 meter/sec RA = 283
81478 deg
ZDOT = 5983
111187 TA = 302
69230
MA = 302
85145
Ha = 223
027 n
mi
Hp = 212
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5551981
10 X = 1765114
18
Y = -21549912
52 feet Y = -6549082
06 meter
Z = 306450
62 Z = 101802
88
XDOT = 15162
699786 XDOT = 4577
795540
YDOT = 4221
644502 feet/sec YDOT = 1338
193618 meter/sec
ZDOT = 19629
629878 ZDOT = 6005
455179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20888661
81 X = 6366864
12
Y = 7672149
96 feet Y = 2338471
31 meter
Z = 345048
60 Z = 105170
81
XDOT = -5142
282281 XDOT = -1567
367639
YDOT = 13012
008969 feet/sec YDOT = 3966
060334 meter/sec
ZDOT = 19729
906078 ZDOT = 6013
675373
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 18331
61619003
00016717 00000-0 10270-3 0 9144
2 25544 51
6393 284
3009 0005140 88
2842 271
8899 15
54029935 23920
Satellite: ISS
Catalog Number: 25544
Epoch time: 18331
61619003 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 284
3009 deg
Eccentricity:
0005140
Arg of perigee: 88
2842 deg
Mean anomaly: 271
8899 deg
Mean motion: 15
54029935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 318
Coasting Arc #16 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2018/332/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2386304
36 A = 6788236
44 meter
Y = 6100522
15 meter E =
0011363
Z = -1774563
02 I = 51
27916
XDOT = -4072
873339 Wp = 120
67351
YDOT = -3223
183521 meter/sec RA = 278
81942 deg
ZDOT = -5636
305484 TA = 78
90735
MA = 78
77959
Ha = 223
014 n
mi
Hp = 212
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7829082
55 X = -2445724
82
Y = 20014836
44 feet Y = 6073504
73 meter
Z = -5822057
17 Z = -1786298
76
XDOT = -13362
445337 XDOT = -4009
149785
YDOT = -10574
749086 feet/sec YDOT = -3268
372479 meter/sec
ZDOT = -18491
815891 ZDOT = -5655
935651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19302168
73 X = -5883301
03
Y = -9417445
79 feet Y = -2870437
48 meter
Z = -5875590
03 Z = -1790879
84
XDOT = 10947
286883 XDOT = 3336
733042
YDOT = -10912
106562 feet/sec YDOT = -3326
010080 meter/sec
ZDOT = -18579
654053 ZDOT = -5663
078555
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 18332
58078083
00016717 00000-0 10270-3 0 9159
2 25544 51
6402 279
4927 0005166 90
3970 269
7774 15
54034865 24072
Satellite: ISS
Catalog Number: 25544
Epoch time: 18332
58078083 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 279
4927 deg
Eccentricity:
0005166
Arg of perigee: 90
3970 deg
Mean anomaly: 269
7774 deg
Mean motion: 15
54034865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 335
Coasting Arc #17 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2018/333/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2938903
88 A = 6785133
60 meter
Y = -5186291
73 meter E =
0017919
Z = 3224975
25 I = 51
26388
XDOT = 3479
771514 Wp = 89
10727
YDOT = 4931
904640 meter/sec RA = 273
81808 deg
ZDOT = 4737
622903 TA = 308
48313
MA = 308
64373
Ha = 222
990 n
mi
Hp = 212
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9642073
11 X = 2981014
73
Y = -17015392
81 feet Y = -5153191
59 meter
Z = 10580627
45 Z = 3239353
47
XDOT = 11416
573209 XDOT = 3401
349989
YDOT = 16180
789500 feet/sec YDOT = 4970
379115 meter/sec
ZDOT = 15543
382227 ZDOT = 4754
336298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16351302
50 X = 4983877
00
Y = 10665004
55 feet Y = 3250693
39 meter
Z = 10645911
33 Z = 3244873
77
XDOT = -16110
326395 XDOT = -4910
427485
YDOT = 9036
437056 feet/sec YDOT = 2754
306015 meter/sec
ZDOT = 15617
907534 ZDOT = 4760
338216
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 18333
60967415
00016717 00000-0 10270-3 0 9160
2 25544 51
6393 274
3651 0005205 94
2230 265
9517 15
54036057 24231
Satellite: ISS
Catalog Number: 25544
Epoch time: 18333
60967415 = yrday
fracday
Element set: 916
Inclination: 51
6393 deg
RA of node: 274
3651 deg
Eccentricity:
0005205
Arg of perigee: 94
2230 deg
Mean anomaly: 265
9517 deg
Mean motion: 15
54036057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 305
Coasting Arc #18 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/334/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3448583
02 A = 6781264
30 meter
Y = 3857910
72 meter E =
0013873
Z = -4396195
84 I = 51
25080
XDOT = -2805
799510 Wp = 79
46457
YDOT = -6297
362498 meter/sec RA = 268
80608 deg
ZDOT = -3331
800800 TA = 156
65389
MA = 156
59083
Ha = 222
974 n
mi
Hp = 212
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11314248
77 X = -3470112
42
Y = 12657187
39 feet Y = 3819226
06 meter
Z = -14423214
70 Z = -4413000
11
XDOT = -9205
378970 XDOT = -2718
987880
YDOT = -20660
638117 feet/sec YDOT = -6328
253375 meter/sec
ZDOT = -10931
104988 ZDOT = -3345
219878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12099389
35 X = -3687893
88
Y = -11816208
51 feet Y = -3601580
35 meter
Z = -14499232
18 Z = -4419365
97
XDOT = 20216
866835 XDOT = 6162
101011
YDOT = -7241
200289 feet/sec YDOT = -2207
117848 meter/sec
ZDOT = -10990
669198 ZDOT = -3349
955971
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 18334
57425848
00016717 00000-0 10270-3 0 9177
2 25544 51
6401 269
5572 0005175 97
3424 262
8317 15
54061210 24383
Satellite: ISS
Catalog Number: 25544
Epoch time: 18334
57425848 = yrday
fracday
Element set: 917
Inclination: 51
6401 deg
RA of node: 269
5572 deg
Eccentricity:
0005175
Arg of perigee: 97
3424 deg
Mean anomaly: 262
8317 deg
Mean motion: 15
54061210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 314
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