[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 29th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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
209/20:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 215
1
212/23:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 214
7
215/16:42:42
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 214
5
216/02:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 214
4
222/19:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 213
6
Coasting Arc #1 (Orbit 476)
---------------------------------------
Vector Time (GMT): 2018/208/09:58:42
767
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4713817
25 A = 6784400
78 meter
Y = -3177313
45 meter E =
0012703
Z = 3699103
53 I = 51
65152
XDOT = 5510
377018 Wp = 60
39564
YDOT = 3130
456250 meter/sec RA = 177
00241 deg
ZDOT = -4315
781359 TA = 75
54101
MA = 75
40009
Ha = 222
116 n
mi
Hp = 215
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15465279
69 X = 4731028
59
Y = -10424256
71 feet Y = -3124504
38 meter
Z = 12136166
43 Z = 3722042
66
XDOT = 18078
664757 XDOT = 5495
925207
YDOT = 10270
525754 feet/sec YDOT = 3191
996674 meter/sec
ZDOT = -14159
387660 ZDOT = -4289
049230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11429597
32 X = -3483741
26
Y = -14652280
77 feet Y = -4466015
18 meter
Z = 12239342
83 Z = 3730551
70
XDOT = 7961
691224 XDOT = 2426
723485
YDOT = -17985
350673 feet/sec YDOT = -5481
934885 meter/sec
ZDOT = -14039
900732 ZDOT = -4279
361743
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 18208
45593002
00016717 00000-0 10270-3 0 9004
2 25544 51
6367 178
0070 0005223 353
4037 6
7045 15
53795626 4779
Satellite: ISS
Catalog Number: 25544
Epoch time: 18208
45593002 = yrday
fracday
Element set: 900
Inclination: 51
6367 deg
RA of node: 178
0070 deg
Eccentricity:
0005223
Arg of perigee: 353
4037 deg
Mean anomaly: 6
7045 deg
Mean motion: 15
53795626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 477
Checksum: 297
Coasting Arc #2 (Orbit 491)
---------------------------------------
Vector Time (GMT): 2018/209/09:58:42
767
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5721298
87 A = 6787794
45 meter
Y = 2728681
43 meter E =
0009674
Z = -2416631
08 I = 51
69617
XDOT = -4029
600407 Wp = 24
86619
YDOT = -3713
383099 meter/sec RA = 172
02775 deg
ZDOT = 5363
443119 TA = 308
13571
MA = 308
22287
Ha = 222
276 n
mi
Hp = 214
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18770665
60 X = -5739648
07
Y = 8952366
90 feet Y = 2664599
50 meter
Z = -7928579
66 Z = -2444466
92
XDOT = -13220
473777 XDOT = -4013
829049
YDOT = -12183
015418 feet/sec YDOT = -3758
357090 meter/sec
ZDOT = 17596
598160 ZDOT = 5343
907178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10493859
25 X = 3198528
30
Y = 17898670
31 feet Y = 5455514
71 meter
Z = -8053673
37 Z = -2454759
64
XDOT = -9711
927550 XDOT = -2960
195517
YDOT = 13548
770118 feet/sec YDOT = 4129
665132 meter/sec
ZDOT = 17509
417658 ZDOT = 5336
870502
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 18209
42068379
00016717 00000-0 10270-3 0 9017
2 25544 51
6373 173
2010 0005184 359
4640
6506 15
53776381 4928
Satellite: ISS
Catalog Number: 25544
Epoch time: 18209
42068379 = yrday
fracday
Element set: 901
Inclination: 51
6373 deg
RA of node: 173
2010 deg
Eccentricity:
0005184
Arg of perigee: 359
4640 deg
Mean anomaly:
6506 deg
Mean motion: 15
53776381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 492
Checksum: 299
Coasting Arc #3 (Orbit 498)
---------------------------------------
Vector Time (GMT): 2018/209/20:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5443976
04 A = 6785021
07 meter
Y = 1906713
87 meter E =
0007640
Z = -3582515
49 I = 51
70030
XDOT = -4455
327246 Wp = 40
47228
YDOT = 4360
105804 meter/sec RA = 169
92951 deg
ZDOT = -4449
385115 TA = 181
77189
MA = 181
77460
Ha = 222
335 n
mi
Hp = 215
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17860813
78 X = 5439651
62
Y = 6255622
92 feet Y = 1967568
23 meter
Z = -11753659
74 Z = -3556081
50
XDOT = -14617
215374 XDOT = -4482
139742
YDOT = 14304
809067 feet/sec YDOT = 4310
133636 meter/sec
ZDOT = -14597
720193 ZDOT = -4471
091898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11962849
85 X = -3646276
64
Y = 14758010
89 feet Y = 4498241
72 meter
Z = -11635348
83 Z = -3546454
32
XDOT = -7461
544053 XDOT = -2274
278627
YDOT = -17635
306389 feet/sec YDOT = -5375
241387 meter/sec
ZDOT = -14695
518015 ZDOT = -4479
193891
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 18209
87090061
00016717 00000-0 10270-3 0 9020
2 25544 51
6368 170
9562 0005363 357
3770 2
7353 15
53779676 4998
Satellite: ISS
Catalog Number: 25544
Epoch time: 18209
87090061 = yrday
fracday
Element set: 902
Inclination: 51
6368 deg
RA of node: 170
9562 deg
Eccentricity:
0005363
Arg of perigee: 357
3770 deg
Mean anomaly: 2
7353 deg
Mean motion: 15
53779676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 332
Coasting Arc #4 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2018/210/20:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4259694
82 A = 6781605
73 meter
Y = -2600419
61 meter E =
0008196
Z = 4583789
37 I = 51
72091
XDOT = 5759
670462 Wp = 77
02213
YDOT = -4045
123333 meter/sec RA = 164
94936 deg
ZDOT = 3054
810409 TA = 342
48689
MA = 342
51514
Ha = 222
550 n
mi
Hp = 214
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13975376
70 X = -4252564
77
Y = -8531560
39 feet Y = -2648014
82 meter
Z = 15038679
03 Z = 4563114
89
XDOT = 18896
556635 XDOT = 5789
637747
YDOT = -13271
402010 feet/sec YDOT = -3980
547310 meter/sec
ZDOT = 10022
343862 ZDOT = 3082
860865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12614866
82 X = 3845011
41
Y = -10570486
90 feet Y = -3221884
41 meter
Z = 14946253
21 Z = 4555617
98
XDOT = 5715
902910 XDOT = 1742
207207
YDOT = 21184
102616 feet/sec YDOT = 6456
914477 meter/sec
ZDOT = 10148
564056 ZDOT = 3093
282324
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 18210
89996931
00016717 00000-0 10270-3 0 9036
2 25544 51
6368 165
8286 0005336
2576 359
8578 15
53753366 5154
Satellite: ISS
Catalog Number: 25544
Epoch time: 18210
89996931 = yrday
fracday
Element set: 903
Inclination: 51
6368 deg
RA of node: 165
8286 deg
Eccentricity:
0005336
Arg of perigee:
2576 deg
Mean anomaly: 359
8578 deg
Mean motion: 15
53753366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 344
Coasting Arc #5 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2018/211/20:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2861074
75 A = 6779038
47 meter
Y = 3312685
10 meter E =
0016039
Z = -5190183
26 I = 51
74429
XDOT = -6632
006465 Wp = 61
45588
YDOT = 3570
694367 meter/sec RA = 159
96320 deg
ZDOT = -1372
593960 TA = 195
32242
MA = 195
37104
Ha = 222
483 n
mi
Hp = 214
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9386728
19 X = 2849029
42
Y = 10868389
43 feet Y = 3344612
43 meter
Z = -17028160
32 Z = -5176314
58
XDOT = -21758
551395 XDOT = -6664
774852
YDOT = 11714
876533 feet/sec YDOT = 3496
347512 meter/sec
ZDOT = -4503
261024 ZDOT = -1404
888769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13254278
27 X = -4039904
02
Y = 5714791
44 feet Y = 1741868
43 meter
Z = -16966321
50 Z = -5171334
79
XDOT = -4080
184391 XDOT = -1243
640202
YDOT = -23305
311461 feet/sec YDOT = -7103
458933 meter/sec
ZDOT = -4648
478363 ZDOT = -1416
856205
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 18211
86471823
00016717 00000-0 10270-3 0 9043
2 25544 51
6368 161
0214 0005205 5
0539 355
0665 15
53781523 5308
Satellite: ISS
Catalog Number: 25544
Epoch time: 18211
86471823 = yrday
fracday
Element set: 904
Inclination: 51
6368 deg
RA of node: 161
0214 deg
Eccentricity:
0005205
Arg of perigee: 5
0539 deg
Mean anomaly: 355
0665 deg
Mean motion: 15
53781523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 285
Coasting Arc #6 (Orbit 545)
---------------------------------------
Vector Time (GMT): 2018/212/20:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1319472
98 A = 6778505
83 meter
Y = -3999152
33 meter E =
0006836
Z = 5309123
30 I = 51
77327
XDOT = 7077
935299 Wp = 29
74504
YDOT = -2924
009008 meter/sec RA = 154
97498 deg
ZDOT = -437
428572 TA = 64
45321
MA = 64
38254
Ha = 222
660 n
mi
Hp = 214
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4328979
60 X = -1300443
76
Y = -13120578
52 feet Y = -4013801
29 meter
Z = 17418383
52 Z = 5302760
01
XDOT = 23221
572504 XDOT = 7112
231092
YDOT = -9593
205407 feet/sec YDOT = -2844
666875 meter/sec
ZDOT = -1435
133111 ZDOT = -402
963778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13844297
10 X = 4219741
76
Y = -451106
98 feet Y = -137497
41 meter
Z = 17390275
16 Z = 5300555
87
XDOT = 2415
234928 XDOT = 736
163606
YDOT = 24004
419578 feet/sec YDOT = 7316
547087 meter/sec
ZDOT = -1280
237151 ZDOT = -390
216284
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 18212
89378228
00016717 00000-0 10270-3 0 9053
2 25544 51
6370 155
8935 0005244 9
3570 350
7680 15
53747966 5466
Satellite: ISS
Catalog Number: 25544
Epoch time: 18212
89378228 = yrday
fracday
Element set: 905
Inclination: 51
6370 deg
RA of node: 155
8935 deg
Eccentricity:
0005244
Arg of perigee: 9
3570 deg
Mean anomaly: 350
7680 deg
Mean motion: 15
53747966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 546
Checksum: 333
Coasting Arc #7 (Orbit 547)
---------------------------------------
Vector Time (GMT): 2018/212/23:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1327080
69 A = 6781097
50 meter
Y = -4724691
65 meter E =
0011690
Z = 4676464
68 I = 51
78860
XDOT = 7053
890677 Wp = 44
80123
YDOT = -880
398239 meter/sec RA = 154
29490 deg
ZDOT = -2878
744577 TA = 73
79917
MA = 73
67056
Ha = 222
539 n
mi
Hp = 214
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4353939
28 X = 1357099
46
Y = -15500956
84 feet Y = -4709683
55 meter
Z = 15342731
89 Z = 4682983
89
XDOT = 23142
685949 XDOT = 7077
194461
YDOT = -2888
445667 feet/sec YDOT = -801
386407 meter/sec
ZDOT = -9444
700057 ZDOT = -2844
423225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15463889
53 X = 4713393
53
Y = -4380727
61 feet Y = -1335245
78 meter
Z = 15372482
50 Z = 4685532
67
XDOT = 14158
859351 XDOT = 4315
620330
YDOT = 17235
131315 feet/sec YDOT = 5253
268025 meter/sec
ZDOT = -9290
666011 ZDOT = -2831
795000
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 18213
02241590
00016717 00000-0 10270-3 0 9061
2 25544 51
6395 155
2514 0004907 11
7686 348
3581 15
53756696 5485
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
02241590 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 155
2514 deg
Eccentricity:
0004907
Arg of perigee: 11
7686 deg
Mean anomaly: 348
3581 deg
Mean motion: 15
53756696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 548
Checksum: 320
Coasting Arc #8 (Orbit 562)
---------------------------------------
Vector Time (GMT): 2018/213/23:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2682695
16 A = 6784431
79 meter
Y = 4997044
29 meter E =
0007749
Z = -3725853
52 I = 51
82901
XDOT = -6330
120546 Wp = 62
67314
YDOT = -188
726353 meter/sec RA = 149
32141 deg
ZDOT = 4315
054898 TA = 253
02890
MA = 253
11385
Ha = 222
578 n
mi
Hp = 214
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8801493
30 X = -2720276
12
Y = 16394502
26 feet Y = 4966834
45 meter
Z = -12223928
88 Z = -3738976
17
XDOT = -20768
112028 XDOT = -6348
499666
YDOT = -619
180949 feet/sec YDOT = -259
616951 meter/sec
ZDOT = 14157
004259 ZDOT = 4284
261146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18520233
75 X = -5644967
25
Y = 1338301
78 feet Y = 407914
38 meter
Z = -12283334
90 Z = -3743960
48
XDOT = -10478
071474 XDOT = -3193
716185
YDOT = -16642
387607 feet/sec YDOT = -5072
599743 meter/sec
ZDOT = 14018
894306 ZDOT = 4272
958985
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 18213
98715969
00016717 00000-0 10270-3 0 9073
2 25544 51
6393 150
4457 0004967 13
3110 346
8172 15
53769467 5638
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
98715969 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 150
4457 deg
Eccentricity:
0004967
Arg of perigee: 13
3110 deg
Mean anomaly: 346
8172 deg
Mean motion: 15
53769467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 563
Checksum: 335
Coasting Arc #9 (Orbit 578)
---------------------------------------
Vector Time (GMT): 2018/214/23:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944329
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3826365
85 A = 6787860
19 meter
Y = -5061673
94 meter E =
0014749
Z = 2399731
69 I = 51
86861
XDOT = 5272
288479 Wp = 86
94476
YDOT = 1419
468901 meter/sec RA = 144
35762 deg
ZDOT = -5383
349813 TA = 66
32996
MA = 66
17524
Ha = 222
625 n
mi
Hp = 214
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12553693
75 X = 3871025
99
Y = -16606541
81 feet Y = -5018635
20 meter
Z = 7873135
46 Z = 2418427
06
XDOT = 17297
534381 XDOT = 5282
172951
YDOT = 4657
050200 feet/sec YDOT = 1478
482614 meter/sec
ZDOT = -17661
908836 ZDOT = -5357
715097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20738701
48 X = 6321156
21
Y = 1393645
20 feet Y = 424783
06 meter
Z = 7957558
26 Z = 2425463
76
XDOT = 5719
971942 XDOT = 1743
447448
YDOT = 15615
773302 feet/sec YDOT = 4759
687703 meter/sec
ZDOT = -17547
064570 ZDOT = -5348
345281
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 18215
01621872
00016717 00000-0 10270-3 0 9089
2 25544 51
6395 145
3181 0004852 17
9146 342
2176 15
53777416 5793
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
01621872 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 145
3181 deg
Eccentricity:
0004852
Arg of perigee: 17
9146 deg
Mean anomaly: 342
2176 deg
Mean motion: 15
53777416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 579
Checksum: 316
Coasting Arc #10 (Orbit 589)
---------------------------------------
Vector Time (GMT): 2018/215/16:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5892610
36 A = 6787866
98 meter
Y = -2314890
17 meter E =
0005729
Z = -2455326
22 I = 51
88775
XDOT = -75
213149 Wp = 75
72737
YDOT = 5477
792354 meter/sec RA = 140
84106 deg
ZDOT = -5354
063026 TA = 131
63152
MA = 131
58244
Ha = 222
785 n
mi
Hp = 214
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19332711
15 X = 5929984
74
Y = -7594784
03 feet Y = -2248785
91 meter
Z = -8055532
21 Z = -2426611
46
XDOT = -246
762300 XDOT = -110
454738
YDOT = 17971
759693 feet/sec YDOT = 5476
754323 meter/sec
ZDOT = -17565
823575 ZDOT = -5354
513873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15126320
59 X = -4610502
52
Y = 14307056
19 feet Y = 4360790
73 meter
Z = -7926451
45 Z = -2415982
40
XDOT = -5570
847570 XDOT = -1697
994339
YDOT = -15606
428880 feet/sec YDOT = -4756
839523 meter/sec
ZDOT = -17568
450318 ZDOT = -5354
863657
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 18215
72369328
00016717 00000-0 10270-3 0 9093
2 25544 51
6398 141
7974 0005429 16
0328 344
0995 15
53779740 5903
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
72369328 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 141
7974 deg
Eccentricity:
0005429
Arg of perigee: 16
0328 deg
Mean anomaly: 344
0995 deg
Mean motion: 15
53779740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 590
Checksum: 340
Coasting Arc #11 (Orbit 595)
---------------------------------------
Vector Time (GMT): 2018/216/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3681567
90 A = 6788591
26 meter
Y = 5329160
81 meter E =
0011669
Z = -2016734
95 I = 51
90074
XDOT = -5061
936713 Wp = 31
42525
YDOT = -1390
963359 meter/sec RA = 138
76853 deg
ZDOT = 5589
249585 TA = 306
37916
MA = 306
48676
Ha = 222
772 n
mi
Hp = 214
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12078634
83 X = -3731090
26
Y = 17484123
40 feet Y = 5287714
13 meter
Z = -6616584
49 Z = -2034738
76
XDOT = -16607
403914 XDOT = -5073
155800
YDOT = -4563
528080 feet/sec YDOT = -1447
632298 meter/sec
ZDOT = 18337
433021 ZDOT = 5564
633342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14956487
13 X = -4558737
28
Y = 15060150
43 feet Y = 4590333
85 meter
Z = -6697950
62 Z = -2041535
35
XDOT = -14550
281376 XDOT = -4434
925763
YDOT = -6378
573417 feet/sec YDOT = -1944
189178 meter/sec
ZDOT = 18227
144897 ZDOT = 5555
633764
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 18216
10958886
00016717 00000-0 10270-3 0 9101
2 25544 51
6398 139
8729 0005261 19
0875 341
0474 15
53773231 5967
Satellite: ISS
Catalog Number: 25544
Epoch time: 18216
10958886 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 139
8729 deg
Eccentricity:
0005261
Arg of perigee: 19
0875 deg
Mean anomaly: 341
0474 deg
Mean motion: 15
53773231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 596
Checksum: 332
Coasting Arc #12 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2018/217/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4442597
92 A = 6790154
50 meter
Y = -5113286
47 meter E =
0012577
Z = 427353
33 I = 51
92992
XDOT = 3829
861153 Wp = 106
15543
YDOT = 2812
872563 meter/sec RA = 133
81771 deg
ZDOT = -6014
576313 TA = 69
25712
MA = 69
12239
Ha = 222
874 n
mi
Hp = 214
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14575452
48 X = 4497370
07
Y = -16775874
25 feet Y = -5063300
04 meter
Z = 1402077
87 Z = 449066
64
XDOT = 12565
161262 XDOT = 3827
337664
YDOT = 9228
584524 feet/sec YDOT = 2855
686844 meter/sec
ZDOT = -19732
861920 ZDOT = -5995
978301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17079396
71 X = 5205800
12
Y = -14208573
42 feet Y = -4330773
18 meter
Z = 1500081
20 Z = 457224
75
XDOT = 10006
462323 XDOT = 3049
969716
YDOT = 9907
386051 feet/sec YDOT = 3019
771268 meter/sec
ZDOT = -19649
728974 ZDOT = -5989
237391
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 18217
13864196
00016717 00000-0 10270-3 0 9116
2 25544 51
6393 134
7458 0005353 24
7701 335
3708 15
53813452 6123
Satellite: ISS
Catalog Number: 25544
Epoch time: 18217
13864196 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 134
7458 deg
Eccentricity:
0005353
Arg of perigee: 24
7701 deg
Mean anomaly: 335
3708 deg
Mean motion: 15
53813452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 303
Coasting Arc #13 (Orbit 627)
---------------------------------------
Vector Time (GMT): 2018/218/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4859137
35 A = 6789852
15 meter
Y = 4583874
79 meter E =
0018600
Z = 1158338
15 I = 51
95011
XDOT = -2543
645548 Wp = 49
39653
YDOT = -4199
245087 meter/sec RA = 128
86942 deg
ZDOT = 5897
175782 TA = 323
13419
MA = 323
26192
Ha = 223
064 n
mi
Hp = 214
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15942051
67 X = -4915660
92
Y = 15038959
29 feet Y = 4529220
45 meter
Z = 3800322
02 Z = 1134597
27
XDOT = -8345
293793 XDOT = -2525
144573
YDOT = -13777
050809 feet/sec YDOT = -4227
586777 meter/sec
ZDOT = 19347
689574 ZDOT = 5884
864408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17968542
19 X = -5476811
66
Y = 12579867
82 feet Y = 3834343
71 meter
Z = 3693260
44 Z = 1125705
78
XDOT = -5481
401740 XDOT = -1670
731250
YDOT = -13543
110308 feet/sec YDOT = -4127
940022 meter/sec
ZDOT = 19292
922746 ZDOT = 5880
482853
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 18218
16769375
00016717 00000-0 10270-3 0 9124
2 25544 51
6390 129
6185 0005441 28
3422 331
8026 15
53766396 6283
Satellite: ISS
Catalog Number: 25544
Epoch time: 18218
16769375 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 129
6185 deg
Eccentricity:
0005441
Arg of perigee: 28
3422 deg
Mean anomaly: 331
8026 deg
Mean motion: 15
53766396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 628
Checksum: 321
Coasting Arc #14 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2018/219/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5019788
70 A = 6787253
78 meter
Y = -3703334
34 meter E =
0007173
Z = -2683130
97 I = 51
96309
XDOT = 1246
717580 Wp = 76
77449
YDOT = 5464
788224 meter/sec RA = 123
91847 deg
ZDOT = -5220
330194 TA = 133
33626
MA = 133
27645
Ha = 223
037 n
mi
Hp = 213
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16469123
03 X = 5073860
45
Y = -12150047
04 feet Y = -3646897
06 meter
Z = -8802923
13 Z = -2658615
72
XDOT = 4090
280773 XDOT = 1210
873545
YDOT = 17929
095222 feet/sec YDOT = 5478
529838 meter/sec
ZDOT = -17127
067566 ZDOT = -5214
360791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17937957
85 X = 5467489
55
Y = -9950768
29 feet Y = -3032994
17 meter
Z = -8692467
47 Z = -2649464
09
XDOT = 1164
739166 XDOT = 355
012498
YDOT = 17008
728899 feet/sec YDOT = 5184
260568 meter/sec
ZDOT = -17100
912357 ZDOT = -5212
358087
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 18219
13242354
00016717 00000-0 10270-3 0 9136
2 25544 51
6402 124
8112 0005459 32
6690 327
4800 15
53818561 6438
Satellite: ISS
Catalog Number: 25544
Epoch time: 18219
13242354 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 124
8112 deg
Eccentricity:
0005459
Arg of perigee: 32
6690 deg
Mean anomaly: 327
4800 deg
Mean motion: 15
53818561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 288
Coasting Arc #15 (Orbit 658)
---------------------------------------
Vector Time (GMT): 2018/220/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4909111
39 A = 6783797
02 meter
Y = 2528043
25 meter E =
0014564
Z = 3926344
29 I = 51
96870
XDOT = -63
594193 Wp = 79
62156
YDOT = -6493
258030 meter/sec RA = 118
96173 deg
ZDOT = 4091
001152 TA = 327
74535
MA = 327
83433
Ha = 223
240 n
mi
Hp = 213
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16106008
50 X = -4956087
68
Y = 8294105
14 feet Y = 2472883
20 meter
Z = 12881706
99 Z = 3902383
93
XDOT = -208
642367 XDOT = -10
851741
YDOT = -21303
339995 feet/sec YDOT = -6493
674607 meter/sec
ZDOT = 13421
919790 ZDOT = 4090
819825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17005791
03 X = -5183365
11
Y = 6462632
22 feet Y = 1969810
30 meter
Z = 12773860
85 Z = 3893472
79
XDOT = 2519
932516 XDOT = 768
075431
YDOT = -19965
578896 feet/sec YDOT = -6085
508447 meter/sec
ZDOT = 13421
872474 ZDOT = 4090
986730
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 18220
16146647
00016717 00000-0 10270-3 0 9140
2 25544 51
6398 119
6843 0005510 36
4592 323
6935 15
53817162 6596
Satellite: ISS
Catalog Number: 25544
Epoch time: 18220
16146647 = yrday
fracday
Element set: 914
Inclination: 51
6398 deg
RA of node: 119
6843 deg
Eccentricity:
0005510
Arg of perigee: 36
4592 deg
Mean anomaly: 323
6935 deg
Mean motion: 15
53817162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 659
Checksum: 320
Coasting Arc #16 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2018/221/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4633663
14 A = 6780480
56 meter
Y = -1097000
57 meter E =
0016299
Z = -4842566
02 I = 51
97351
XDOT = -987
312712 Wp = 61
78438
YDOT = 7145
254519 meter/sec RA = 113
99677 deg
ZDOT = -2562
420026 TA = 183
06279
MA = 183
07278
Ha = 223
142 n
mi
Hp = 213
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15202306
89 X = 4669107
94
Y = -3599083
25 feet Y = -1044985
20 meter
Z = -15887683
79 Z = -4819971
68
XDOT = -3239
214934 XDOT = -1054
692875
YDOT = 23442
436085 feet/sec YDOT = 7133
837152 meter/sec
ZDOT = -8406
889850 ZDOT = -2567
379080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15575834
52 X = 4747514
36
Y = -2161872
18 feet Y = -658938
64 meter
Z = -15786124
25 Z = -4811610
67
XDOT = -5506
113989 XDOT = -1678
263544
YDOT = 21908
606245 feet/sec YDOT = 6677
743184 meter/sec
ZDOT = -8430
005586 ZDOT = -2569
465703
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 18221
12619317
00016717 00000-0 10270-3 0 9157
2 25544 51
6407 114
8778 0005437 39
7670 320
3881 15
53808520 6741
Satellite: ISS
Catalog Number: 25544
Epoch time: 18221
12619317 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 114
8778 deg
Eccentricity:
0005437
Arg of perigee: 39
7670 deg
Mean anomaly: 320
3881 deg
Mean motion: 15
53808520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 312
Coasting Arc #17 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2018/222/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4204895
31 A = 6778434
35 meter
Y = -488877
36 meter E =
0007134
Z = 5288009
25 I = 51
97902
XDOT = 1878
853991 Wp = 69
79428
YDOT = -7395
748949 meter/sec RA = 109
02558 deg
ZDOT = 811
796787 TA = 12
49719
MA = 12
47951
Ha = 223
372 n
mi
Hp = 213
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13795588
27 X = -4224801
81
Y = -1603928
35 feet Y = -536011
02 meter
Z = 17349111
73 Z = 5267535
41
XDOT = 6164
219132 XDOT = 1957
472467
YDOT = -24264
268205 feet/sec YDOT = -7374
298769 meter/sec
ZDOT = 2663
375284 ZDOT = 821
113919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13748955
48 X = -4190681
63
Y = -2652548
84 feet Y = -808496
89 meter
Z = 17257251
45 Z = 5260010
24
XDOT = 7774
736096 XDOT = 2369
739562
YDOT = -22725
690720 feet/sec YDOT = -6926
790531 meter/sec
ZDOT = 2706
097771 ZDOT = 824
818601
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 18222
15523043
00016717 00000-0 10270-3 0 9162
2 25544 51
6403 109
7506 0005612 43
3908 316
7686 15
53830363 6909
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
15523043 = yrday
fracday
Element set: 916
Inclination: 51
6403 deg
RA of node: 109
7506 deg
Eccentricity:
0005612
Arg of perigee: 43
3908 deg
Mean anomaly: 316
7686 deg
Mean motion: 15
53830363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 295
Coasting Arc #18 (Orbit 700)
---------------------------------------
Vector Time (GMT): 2018/222/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 919622
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4285110
29 A = 6778559
02 meter
Y = 109025
22 meter E =
0007127
Z = 5244937
06 I = 51
98703
XDOT = 1176
410698 Wp = 77
70661
YDOT = -7500
321992 meter/sec RA = 105
51929 deg
ZDOT = 1117
236841 TA = 1
64563
MA = 1
64329
Ha = 223
239 n
mi
Hp = 213
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14058760
80 X = -4311487
47
Y = 357694
30 feet Y = 60958
46 meter
Z = 17207798
75 Z = 5224057
93
XDOT = 3859
615152 XDOT = 1254
767124
YDOT = -24607
355618 feet/sec YDOT = -7486
728481 meter/sec
ZDOT = 3665
475201 ZDOT = 1123
141305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4310349
33 X = 1313794
48
Y = -13506129
65 feet Y = -4116668
32 meter
Z = 17114040
69 Z = 5216359
60
XDOT = 21002
206210 XDOT = 6401
472453
YDOT = 11381
185257 feet/sec YDOT = 3468
985266 meter/sec
ZDOT = 3692
895319 ZDOT = 1125
594493
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 18222
86269158
00016717 00000-0 10270-3 0 9175
2 25544 51
6404 106
2218 0005235 45
7364 314
4218 15
53854344 7019
Satellite: ISS
Catalog Number: 25544
Epoch time: 18222
86269158 = yrday
fracday
Element set: 917
Inclination: 51
6404 deg
RA of node: 106
2218 deg
Eccentricity:
0005235
Arg of perigee: 45
7364 deg
Mean anomaly: 314
4218 deg
Mean motion: 15
53854344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 701
Checksum: 298
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