[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 25th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14678 7446 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
207/16:11:39
616 -1
1 1
3 1
3
N/A -0
4 -0
1 222
1
000/00:03:19
233 0
7 -0
1 215
2
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
7
000/00:00:00
000 0
0 0
0 214
4
Coasting Arc #1 (Orbit 446)
---------------------------------------
Vector Time (GMT): 2018/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5482656
14 A = 6786446
87 meter
Y = 2865656
84 meter E =
0004307
Z = -2796073
63 I = 51
59602
XDOT = -4463
667327 Wp = 63
63813
YDOT = 3559
886848 meter/sec RA = 186
60047 deg
ZDOT = -5108
303503 TA = 148
06805
MA = 148
04194
Ha = 221
746 n
mi
Hp = 214
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17987717
01 X = 5463785
74
Y = 9401761
28 feet Y = 2926862
48 meter
Z = -9173469
90 Z = -2769486
72
XDOT = -14644
577844 XDOT = -4478
330164
YDOT = 11679
418793 feet/sec YDOT = 3509
889605 meter/sec
ZDOT = -16759
525928 ZDOT = -5130
021340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1687557
58 X = -514367
55
Y = -20279772
87 feet Y = -6181274
77 meter
Z = -9054644
66 Z = -2759855
69
XDOT = 16154
958270 XDOT = 4924
031281
YDOT = 6175
924717 feet/sec YDOT = 1882
421854 meter/sec
ZDOT = -16857
245158 ZDOT = -5138
088324
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 18206
52660406
00016717 00000-0 10270-3 0 9003
2 25544 51
6358 187
6223 0004463 357
2113 2
9014 15
54009256 4476
Satellite: ISS
Catalog Number: 25544
Epoch time: 18206
52660406 = yrday
fracday
Element set: 900
Inclination: 51
6358 deg
RA of node: 187
6223 deg
Eccentricity:
0004463
Arg of perigee: 357
2113 deg
Mean anomaly: 2
9014 deg
Mean motion: 15
54009256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 447
Checksum: 283
Coasting Arc #2 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2018/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4283113
15 A = 6782694
01 meter
Y = -3335109
19 meter E =
0010605
Z = 4056050
55 I = 51
61646
XDOT = 5946
077059 Wp = 78
71799
YDOT = -2907
854744 meter/sec RA = 181
61739 deg
ZDOT = 3881
374808 TA = 331
06360
MA = 331
12236
Ha = 221
772 n
mi
Hp = 214
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14052208
49 X = -4265202
50
Y = -10941959
30 feet Y = -3382906
19 meter
Z = 13307252
46 Z = 4035288
22
XDOT = 19508
126834 XDOT = 5959
298252
YDOT = -9540
205852 feet/sec YDOT = -2841
288071 meter/sec
ZDOT = 12734
169318 ZDOT = 3910
290072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1394640
72 X = -425086
49
Y = 17824261
08 feet Y = 5432834
78 meter
Z = 13214563
88 Z = 4027799
07
XDOT = -17328
656523 XDOT = -5281
774508
YDOT = -10909
146976 feet/sec YDOT = -3325
107998 meter/sec
ZDOT = 12864
088434 ZDOT = 3920
974155
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 18207
55551361
00016717 00000-0 10270-3 0 9017
2 25544 51
6356 182
4947 0004358 357
9551 2
1583 15
54041163 4630
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
55551361 = yrday
fracday
Element set: 901
Inclination: 51
6356 deg
RA of node: 182
4947 deg
Eccentricity:
0004358
Arg of perigee: 357
9551 deg
Mean anomaly: 2
1583 deg
Mean motion: 15
54041163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 301
Coasting Arc #3 (Orbit 464)
---------------------------------------
Vector Time (GMT): 2018/207/16:13:19
233
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4794175
66 A = 6784140
42 meter
Y = 2944907
46 meter E =
0006271
Z = -3791902
37 I = 51
62810
XDOT = -5419
582510 Wp = 55
11078
YDOT = -3404
232994 meter/sec RA = 180
68964 deg
ZDOT = 4216
706737 TA = 259
42203
MA = 259
49268
Ha = 222
051 n
mi
Hp = 215
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15728922
78 X = -4808331
41
Y = 9661769
87 feet Y = 2891216
90 meter
Z = -12440624
59 Z = -3815224
46
XDOT = -17780
782514 XDOT = -5401
594792
YDOT = -11168
743418 feet/sec YDOT = -3464
738350 meter/sec
ZDOT = 13834
339687 ZDOT = 4190
424135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14399997
50 X = 4389119
24
Y = -11435423
36 feet Y = -3485517
04 meter
Z = -12545481
80 Z = -3823862
85
XDOT = 18228
674140 XDOT = 5556
099878
YDOT = 7936
101329 feet/sec YDOT = 2418
923685 meter/sec
ZDOT = 13716
913081 ZDOT = 4180
915107
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 18207
68412896
00016717 00000-0 10270-3 0 9021
2 25544 51
6387 181
8536 0005209 350
5334 9
5719 15
53781200 4651
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
68412896 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 181
8536 deg
Eccentricity:
0005209
Arg of perigee: 350
5334 deg
Mean anomaly: 9
5719 deg
Mean motion: 15
53781200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 465
Checksum: 316
Coasting Arc #4 (Orbit 480)
---------------------------------------
Vector Time (GMT): 2018/208/16:13:19
233
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5828548
61 A = 6787675
46 meter
Y = -2415090
69 meter E =
0012822
Z = 2495330
60 I = 51
67323
XDOT = 3906
145329 Wp = 82
39726
YDOT = 3915
764312 meter/sec RA = 175
71254 deg
ZDOT = -5309
008340 TA = 69
64434
MA = 69
50663
Ha = 222
197 n
mi
Hp = 215
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19122534
81 X = 5843000
89
Y = -7923525
88 feet Y = -2349831
24 meter
Z = 8186780
17 Z = 2523677
96
XDOT = 12815
437430 XDOT = 3887
855676
YDOT = 12846
995773 feet/sec YDOT = 3959
343720 meter/sec
ZDOT = -17418
006366 ZDOT = -5290
078126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17825941
11 X = -5433346
85
Y = 10420565
85 feet Y = 3176188
47 meter
Z = 8314120
55 Z = 2534143
94
XDOT = -13784
232267 XDOT = -4201
433995
YDOT = -9685
724257 feet/sec YDOT = -2952
208754 meter/sec
ZDOT = -17333
574672 ZDOT = -5283
273560
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
71319792
00016717 00000-0 10270-3 0 9038
2 25544 51
6392 176
7268 0005177 353
8799 6
2290 15
53762294 4815
Satellite: ISS
Catalog Number: 25544
Epoch time: 18208
71319792 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 176
7268 deg
Eccentricity:
0005177
Arg of perigee: 353
8799 deg
Mean anomaly: 6
2290 deg
Mean motion: 15
53762294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 481
Checksum: 337
Coasting Arc #5 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2018/209/16:13:19
233
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6446283
16 A = 6789860
12 meter
Y = 1853231
53 meter E =
0014060
Z = -1003703
74 I = 51
71475
XDOT = -2172
222446 Wp = 24
47556
YDOT = -4375
682200 meter/sec RA = 170
74413 deg
ZDOT = 5913
968261 TA = 324
65671
MA = 324
74983
Ha = 222
261 n
mi
Hp = 215
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21149222
96 X = -6461652
05
Y = 6080155
94 feet Y = 1781058
88 meter
Z = -3292991
29 Z = -1035054
06
XDOT = -7126
714061 XDOT = -2151
857217
YDOT = -14355
912731 feet/sec YDOT = -4399
860037 meter/sec
ZDOT = 19402
783007 ZDOT = 5903
465748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19959087
36 X = 6083529
83
Y = -9216610
40 feet Y = -2809222
85 meter
Z = -3433750
75 Z = -1046607
23
XDOT = 8678
236022 XDOT = 2645
126339
YDOT = 11631
208845 feet/sec YDOT = 3545
192456 meter/sec
ZDOT = 19356
171748 ZDOT = 5899
761149
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
67794618
00016717 00000-0 10270-3 0 9049
2 25544 51
6404 171
9195 0005323 357
1977 2
9145 15
53786124 4969
Satellite: ISS
Catalog Number: 25544
Epoch time: 18209
67794618 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 171
9195 deg
Eccentricity:
0005323
Arg of perigee: 357
1977 deg
Mean anomaly: 2
9145 deg
Mean motion: 15
53786124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 332
Coasting Arc #6 (Orbit 498)
---------------------------------------
Vector Time (GMT): 2018/209/20:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5441530
44 A = 6784997
63 meter
Y = 1909095
49 meter E =
0007628
Z = -3584902
18 I = 51
70021
XDOT = -4459
102012 Wp = 40
56548
YDOT = 4358
793346 meter/sec RA = 169
92977 deg
ZDOT = -4446
927300 TA = 181
71368
MA = 181
71629
Ha = 222
318 n
mi
Hp = 215
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17852790
15 X = 5437191
16
Y = 6263436
64 feet Y = 1969922
42 meter
Z = -11761490
09 Z = -3558480
11
XDOT = -14629
599778 XDOT = -4485
911490
YDOT = 14300
503103 feet/sec YDOT = 4308
778983 meter/sec
ZDOT = -14589
656497 ZDOT = -4468
652412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11967499
80 X = -3647693
94
Y = 14747863
61 feet Y = 4495148
83 meter
Z = -11643232
86 Z = -3548857
38
XDOT = -7454
019059 XDOT = -2271
985009
YDOT = -17645
210441 feet/sec YDOT = -5378
260143 meter/sec
ZDOT = -14687
536354 ZDOT = -4476
761081
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
87089428
00016717 00000-0 10270-3 0 9058
2 25544 51
6368 170
9564 0005337 357
3187 2
7936 15
53785238 4991
Satellite: ISS
Catalog Number: 25544
Epoch time: 18209
87089428 = yrday
fracday
Element set: 905
Inclination: 51
6368 deg
RA of node: 170
9564 deg
Eccentricity:
0005337
Arg of perigee: 357
3187 deg
Mean anomaly: 2
7936 deg
Mean motion: 15
53785238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 353
Coasting Arc #7 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2018/210/20:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4254714
01 A = 6781577
79 meter
Y = -2603928
21 meter E =
0008168
Z = 4586412
96 I = 51
72081
XDOT = 5764
386879 Wp = 77
19311
YDOT = -4042
224578 meter/sec RA = 164
94955 deg
ZDOT = 3049
726301 TA = 342
37189
MA = 342
40022
Ha = 222
531 n
mi
Hp = 214
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13959035
47 X = -4247557
84
Y = -8543071
56 feet Y = -2651467
58 meter
Z = 15047286
61 Z = 4565762
74
XDOT = 18912
030442 XDOT = 5794
346094
YDOT = -13261
891659 feet/sec YDOT = -3977
595858 meter/sec
ZDOT = 10005
663718 ZDOT = 3077
799648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12620508
82 X = 3846731
09
Y = -10551360
49 feet Y = -3216054
68 meter
Z = 14954969
95 Z = 4558274
84
XDOT = 5703
269527 XDOT = 1738
356552
YDOT = 21195
374566 feet/sec YDOT = 6460
350168 meter/sec
ZDOT = 10131
986244 ZDOT = 3088
229407
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
89995907
00016717 00000-0 10270-3 0 9061
2 25544 51
6367 165
8288 0005309
1957 359
9196 15
53759424 5155
Satellite: ISS
Catalog Number: 25544
Epoch time: 18210
89995907 = yrday
fracday
Element set: 906
Inclination: 51
6367 deg
RA of node: 165
8288 deg
Eccentricity:
0005309
Arg of perigee:
1957 deg
Mean anomaly: 359
9196 deg
Mean motion: 15
53759424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 350
Coasting Arc #8 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2018/211/20:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2852885
26 A = 6779011
12 meter
Y = 3317079
77 meter E =
0016026
Z = -5191840
21 I = 51
74420
XDOT = -6636
497473 Wp = 61
58822
YDOT = 3565
507554 meter/sec RA = 159
96328 deg
ZDOT = -1364
471796 TA = 195
26970
MA = 195
31812
Ha = 222
463 n
mi
Hp = 214
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9359859
77 X = 2840799
44
Y = 10882807
66 feet Y = 3348915
30 meter
Z = -17033596
50 Z = -5178011
41
XDOT = -21773
285672 XDOT = -6669
246977
YDOT = 11697
859430 feet/sec YDOT = 3491
110583 meter/sec
ZDOT = -4476
613505 ZDOT = -1396
788374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13259785
49 X = -4041582
62
Y = 5684833
37 feet Y = 1732737
21 meter
Z = -16971937
00 Z = -5173046
40
XDOT = -4061
604850 XDOT = -1237
977158
YDOT = -23313
892964 feet/sec YDOT = -7106
074575 meter/sec
ZDOT = -4621
927913 ZDOT = -1408
763628
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
86470393
00016717 00000-0 10270-3 0 9077
2 25544 51
6367 161
0215 0005177 4
9879 355
1324 15
53788304 5308
Satellite: ISS
Catalog Number: 25544
Epoch time: 18211
86470393 = yrday
fracday
Element set: 907
Inclination: 51
6367 deg
RA of node: 161
0215 deg
Eccentricity:
0005177
Arg of perigee: 4
9879 deg
Mean anomaly: 355
1324 deg
Mean motion: 15
53788304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 309
Coasting Arc #9 (Orbit 545)
---------------------------------------
Vector Time (GMT): 2018/212/20:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1308014
14 A = 6778487
00 meter
Y = -4003874
07 meter E =
0006828
Z = 5308389
69 I = 51
77321
XDOT = 7080
666578 Wp = 29
73350
YDOT = -2915
712574 meter/sec RA = 154
97498 deg
ZDOT = -448
439010 TA = 64
56972
MA = 64
49907
Ha = 222
638 n
mi
Hp = 214
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4291384
96 X = -1288929
40
Y = -13136069
79 feet Y = -4018394
58 meter
Z = 17415976
69 Z = 5302082
20
XDOT = 23230
533393 XDOT = 7114
922877
YDOT = -9565
986134 feet/sec YDOT = -2836
340118 meter/sec
ZDOT = -1471
256594 ZDOT = -413
961044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13848222
37 X = 4220938
18
Y = -410621
52 feet Y = -125157
44 meter
Z = 17388119
09 Z = 5299898
70
XDOT = 2389
472270 XDOT = 728
311148
YDOT = 24005
050172 feet/sec YDOT = 7316
739292 meter/sec
ZDOT = -1316
302454 ZDOT = -401
208988
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
89376326
00016717 00000-0 10270-3 0 9083
2 25544 51
6370 155
8936 0005215 9
2885 350
8363 15
53755443 5461
Satellite: ISS
Catalog Number: 25544
Epoch time: 18212
89376326 = yrday
fracday
Element set: 908
Inclination: 51
6370 deg
RA of node: 155
8936 deg
Eccentricity:
0005215
Arg of perigee: 9
2885 deg
Mean anomaly: 350
8363 deg
Mean motion: 15
53755443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 546
Checksum: 328
Coasting Arc #10 (Orbit 547)
---------------------------------------
Vector Time (GMT): 2018/212/23:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1338877
35 A = 6781094
47 meter
Y = -4726139
24 meter E =
0011682
Z = 4671622
67 I = 51
78859
XDOT = 7051
058451 Wp = 44
97322
YDOT = -870
271379 meter/sec RA = 154
29493 deg
ZDOT = -2888
769909 TA = 73
73563
MA = 73
60716
Ha = 222
517 n
mi
Hp = 214
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4392642
21 X = 1368934
94
Y = -15505706
17 feet Y = -4710999
01 meter
Z = 15326846
04 Z = 4678199
29
XDOT = 23133
393867 XDOT = 7074
297900
YDOT = -2855
221060 feet/sec YDOT = -791
291578 meter/sec
ZDOT = -9477
591564 ZDOT = -2854
462470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15488033
31 X = 4720752
55
Y = -4349975
90 feet Y = -1325872
65 meter
Z = 15356854
26 Z = 4680769
18
XDOT = 14127
977418 XDOT = 4306
207517
YDOT = 17242
794692 feet/sec YDOT = 5255
603822 meter/sec
ZDOT = -9323
621019 ZDOT = -2841
839687
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
02239625
00016717 00000-0 10270-3 0 9090
2 25544 51
6394 155
2515 0004878 11
7068 348
4197 15
53764230 5483
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
02239625 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 155
2515 deg
Eccentricity:
0004878
Arg of perigee: 11
7068 deg
Mean anomaly: 348
4197 deg
Mean motion: 15
53764230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 548
Checksum: 317
Coasting Arc #11 (Orbit 562)
---------------------------------------
Vector Time (GMT): 2018/213/23:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2696104
27 A = 6784436
89 meter
Y = 4996615
53 meter E =
0007716
Z = -3716686
16 I = 51
82904
XDOT = -6322
871509 Wp = 62
50049
YDOT = -202
226324 meter/sec RA = 149
32142 deg
ZDOT = 4325
122260 TA = 253
33873
MA = 253
42345
Ha = 222
555 n
mi
Hp = 214
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8845486
47 X = -2733723
97
Y = 16393095
57 feet Y = 4966255
52 meter
Z = -12193852
24 Z = -3729874
04
XDOT = -20744
329098 XDOT = -6341
149109
YDOT = -663
472190 feet/sec YDOT = -273
035290 meter/sec
ZDOT = 14190
033661 ZDOT = 4294
363967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18542556
02 X = -5651771
07
Y = 1300136
27 feet Y = 396281
54 meter
Z = -12253550
81 Z = -3734882
29
XDOT = -10430
817864 XDOT = -3179
313285
YDOT = -16644
371272 feet/sec YDOT = -5073
204364 meter/sec
ZDOT = 14052
084231 ZDOT = 4283
075274
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
98713515
00016717 00000-0 10270-3 0 9102
2 25544 51
6392 150
4458 0004937 13
2366 346
8915 15
53777568 5633
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
98713515 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 150
4458 deg
Eccentricity:
0004937
Arg of perigee: 13
2366 deg
Mean anomaly: 346
8915 deg
Mean motion: 15
53777568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 563
Checksum: 329
Coasting Arc #12 (Orbit 578)
---------------------------------------
Vector Time (GMT): 2018/214/23:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 944330
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3839974
81 A = 6787862
37 meter
Y = -5057947
64 meter E =
0014724
Z = 2385777
63 I = 51
86863
XDOT = 5259
628893 Wp = 87
23980
YDOT = 1436
226169 meter/sec RA = 144
35765 deg
ZDOT = -5391
303023 TA = 66
20251
MA = 66
04820
Ha = 222
600 n
mi
Hp = 214
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12598342
56 X = 3884660
05
Y = -16594316
41 feet Y = -5014756
57 meter
Z = 7827354
42 Z = 2404539
17
XDOT = 17256
000306 XDOT = 5269
365553
YDOT = 4712
028113 feet/sec YDOT = 1495
097487 meter/sec
ZDOT = -17688
002043 ZDOT = -5365
730161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20753033
13 X = 6325524
50
Y = 1437969
39 feet Y = 438293
07 meter
Z = 7912073
64 Z = 2411600
05
XDOT = 5654
560735 XDOT = 1723
510112
YDOT = 15610
136665 feet/sec YDOT = 4757
969656 meter/sec
ZDOT = -17573
437092 ZDOT = -5356
383626
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
01618847
00016717 00000-0 10270-3 0 9111
2 25544 51
6395 145
3181 0004820 17
8352 342
2969 15
53786423 5794
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
01618847 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 145
3181 deg
Eccentricity:
0004820
Arg of perigee: 17
8352 deg
Mean anomaly: 342
2969 deg
Mean motion: 15
53786423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 579
Checksum: 319
Coasting Arc #13 (Orbit 589)
---------------------------------------
Vector Time (GMT): 2018/215/16:42:42
000
Vector Time (MET): N/A
Weight (LBS) : 919623
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5892315
87 A = 6787806
71 meter
Y = -2298640
82 meter E =
0005715
Z = -2471137
18 I = 51
88757
XDOT = -97
428155 Wp = 75
39458
YDOT = 5486
522841 meter/sec RA = 140
84105 deg
ZDOT = -5344
773575 TA = 132
15563
MA = 132
10707
Ha = 222
759 n
mi
Hp = 214
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19331744
99 X = 5929585
37
Y = -7541472
51 feet Y = -2232540
44 meter
Z = -8107405
45 Z = -2442424
10
XDOT = -319
646179 XDOT = -132
810843
YDOT = 18000
403021 feet/sec YDOT = 5485
235597 meter/sec
ZDOT = -17535
346375 ZDOT = -5345
332677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15145722
27 X = -4616416
15
Y = 14257400
81 feet Y = 4345655
77 meter
Z = -7978334
04 Z = -2431796
21
XDOT = -5517
446138 XDOT = -1681
717583
YDOT = -15658
961991 feet/sec YDOT = -4772
851615 meter/sec
ZDOT = -17538
459753 ZDOT = -5345
722533
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
72365881
00016717 00000-0 10270-3 0 9127
2 25544 51
6398 141
7973 0005398 15
9357 344
1964 15
53789316 5904
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
72365881 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 141
7973 deg
Eccentricity:
0005398
Arg of perigee: 15
9357 deg
Mean anomaly: 344
1964 deg
Mean motion: 15
53789316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 590
Checksum: 345
Coasting Arc #14 (Orbit 595)
---------------------------------------
Vector Time (GMT): 2018/216/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919623
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3697655
66 A = 6788594
80 meter
Y = 5324684
43 meter E =
0011695
Z = -1998918
01 I = 51
90078
XDOT = -5046
941059 Wp = 31
34621
YDOT = -1412
629418 meter/sec RA = 138
76851 deg
ZDOT = 5597
432860 TA = 306
66445
MA = 306
77190
Ha = 222
746 n
mi
Hp = 214
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12131416
20 X = -3747213
31
Y = 17469437
11 feet Y = 5283057
64 meter
Z = -6558129
94 Z = -2017000
05
XDOT = -16558
205574 XDOT = -5057
958735
YDOT = -4634
610951 feet/sec YDOT = -1469
129540 meter/sec
ZDOT = 18364
281036 ZDOT = 5572
889949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15006189
50 X = -4573886
56
Y = 15036232
06 feet Y = 4583043
53 meter
Z = -6639846
58 Z = -2023825
24
XDOT = -14491
128221 XDOT = -4416
895882
YDOT = -6436
160692 feet/sec YDOT = -1961
741779 meter/sec
ZDOT = 18254
324322 ZDOT = 5563
918053
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
10955199
00016717 00000-0 10270-3 0 9138
2 25544 51
6398 139
8729 0005231 18
9892 341
1455 15
53782517 5968
Satellite: ISS
Catalog Number: 25544
Epoch time: 18216
10955199 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 139
8729 deg
Eccentricity:
0005231
Arg of perigee: 18
9892 deg
Mean anomaly: 341
1455 deg
Mean motion: 15
53782517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 596
Checksum: 340
Coasting Arc #15 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2018/217/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919623
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4456870
26 A = 6790132
45 meter
Y = -5102668
63 meter E =
0012513
Z = 404816
73 I = 51
92988
XDOT = 3808
594886 Wp = 106
46079
YDOT = 2837
332381 meter/sec RA = 133
81770 deg
ZDOT = -6016
597299 TA = 69
19414
MA = 69
06015
Ha = 222
845 n
mi
Hp = 214
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14622277
75 X = 4511632
09
Y = -16741038
81 feet Y = -5052522
65 meter
Z = 1328138
89 Z = 426599
35
XDOT = 12495
390045 XDOT = 3805
809278
YDOT = 9308
833270 feet/sec YDOT = 2879
907382 meter/sec
ZDOT = -19739
492451 ZDOT = -5998
103226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17120478
93 X = 5218321
98
Y = -14166572
48 feet Y = -4317971
29 meter
Z = 1426452
01 Z = 434782
57
XDOT = 9927
776175 XDOT = 3025
986178
YDOT = 9972
350273 feet/sec YDOT = 3039
572363 meter/sec
ZDOT = -19656
828634 ZDOT = -5991
401368
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
13859829
00016717 00000-0 10270-3 0 9146
2 25544 51
6393 134
7457 0005317 24
6995 335
4411 15
53823931 6121
Satellite: ISS
Catalog Number: 25544
Epoch time: 18217
13859829 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 134
7457 deg
Eccentricity:
0005317
Arg of perigee: 24
6995 deg
Mean anomaly: 335
4411 deg
Mean motion: 15
53823931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 321
Coasting Arc #16 (Orbit 627)
---------------------------------------
Vector Time (GMT): 2018/218/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919623
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4870195
60 A = 6789792
34 meter
Y = 4565439
99 meter E =
0018573
Z = 1184126
40 I = 51
94996
XDOT = -2516
400839 Wp = 49
64727
YDOT = -4224
871967 meter/sec RA = 128
86933 deg
ZDOT = 5890
585331 TA = 323
16724
MA = 323
29469
Ha = 223
033 n
mi
Hp = 214
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15978332
03 X = -4926637
48
Y = 14978477
66 feet Y = 4510662
44 meter
Z = 3884929
14 Z = 1160332
00
XDOT = -8255
908263 XDOT = -2497
583309
YDOT = -13861
128502 feet/sec YDOT = -4252
907218 meter/sec
ZDOT = 19326
067358 ZDOT = 5878
407069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17996278
68 X = -5485265
74
Y = 12514712
58 feet Y = 3814484
39 meter
Z = 3777629
50 Z = 1151421
47
XDOT = -5385
438226 XDOT = -1641
481571
YDOT = -13611
379814 feet/sec YDOT = -4148
748567 meter/sec
ZDOT = 19271
900802 ZDOT = 5874
075365
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
16764261
00016717 00000-0 10270-3 0 9156
2 25544 51
6389 129
6183 0005404 28
2732 331
8713 15
53778416 6280
Satellite: ISS
Catalog Number: 25544
Epoch time: 18218
16764261 = yrday
fracday
Element set: 915
Inclination: 51
6389 deg
RA of node: 129
6183 deg
Eccentricity:
0005404
Arg of perigee: 28
2732 deg
Mean anomaly: 331
8713 deg
Mean motion: 15
53778416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 628
Checksum: 320
Coasting Arc #17 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2018/219/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919623
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025947
01 A = 6787158
62 meter
Y = -3675675
97 meter E =
0007169
Z = -2709401
00 I = 51
96282
XDOT = 1214
464692 Wp = 76
19550
YDOT = 5488
534253 meter/sec RA = 123
91819 deg
ZDOT = -5202
982316 TA = 134
24144
MA = 134
18256
Ha = 223
004 n
mi
Hp = 213
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16489327
46 X = 5079836
63
Y = -12059304
36 feet Y = -3619170
85 meter
Z = -8889110
88 Z = -2684856
27
XDOT = 3984
464211 XDOT = 1178
273254
YDOT = 18007
002144 feet/sec YDOT = 5501
913250 meter/sec
ZDOT = -17070
151957 ZDOT = -5197
170428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17947028
83 X = 5470254
39
Y = -9858127
04 feet Y = -3004757
12 meter
Z = -8778526
16 Z = -2675694
77
XDOT = 1056
258491 XDOT = 321
947588
YDOT = 17071
844679 feet/sec YDOT = 5203
498258 meter/sec
ZDOT = -17044
706438 ZDOT = -5195
226522
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
13236485
00016717 00000-0 10270-3 0 9167
2 25544 51
6401 124
8110 0005421 32
5912 327
5574 15
53830980 6438
Satellite: ISS
Catalog Number: 25544
Epoch time: 18219
13236485 = yrday
fracday
Element set: 916
Inclination: 51
6401 deg
RA of node: 124
8110 deg
Eccentricity:
0005421
Arg of perigee: 32
5912 deg
Mean anomaly: 327
5574 deg
Mean motion: 15
53830980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 289
Coasting Arc #18 (Orbit 658)
---------------------------------------
Vector Time (GMT): 2018/220/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919623
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4909361
16 A = 6783678
24 meter
Y = 2490511
68 meter E =
0014430
Z = 3949867
50 I = 51
96837
XDOT = -27
334196 Wp = 79
94889
YDOT = -6511
799826 meter/sec RA = 118
96118 deg
ZDOT = 4061
800887 TA = 327
79294
MA = 327
88099
Ha = 223
204 n
mi
Hp = 213
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16106827
97 X = -4956032
01
Y = 8170970
08 feet Y = 2435350
55 meter
Z = 12958882
87 Z = 3925906
66
XDOT = -89
679122 XDOT = 25
754739
YDOT = -21364
172659 feet/sec YDOT = -6511
808979 meter/sec
ZDOT = 13326
118397 ZDOT = 4061
796537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16993562
74 X = -5179637
92
Y = 6340104
56 feet Y = 1932463
87 meter
Z = 12851039
02 Z = 3916996
69
XDOT = 2636
563949 XDOT = 803
624692
YDOT = -20013
777700 feet/sec YDOT = -6100
199443 meter/sec
ZDOT = 13326
867642 ZDOT = 4062
029257
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
16139908
00016717 00000-0 10270-3 0 9175
2 25544 51
6397 119
6841 0005470 36
3603 323
7920 15
53831088 6598
Satellite: ISS
Catalog Number: 25544
Epoch time: 18220
16139908 = yrday
fracday
Element set: 917
Inclination: 51
6397 deg
RA of node: 119
6841 deg
Eccentricity:
0005470
Arg of perigee: 36
3603 deg
Mean anomaly: 323
7920 deg
Mean motion: 15
53831088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 659
Checksum: 317
Coasting Arc #19 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2018/221/02:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 919623
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4627021
92 A = 6780371
00 meter
Y = -1050164
34 meter E =
0016355
Z = -4859167
67 I = 51
97321
XDOT = -1025
798395 Wp = 62
01532
YDOT = 7154
241114 meter/sec RA = 113
99589 deg
ZDOT = -2521
971939 TA = 183
25534
MA = 183
26599
Ha = 223
104 n
mi
Hp = 213
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15180518
11 X = 4662024
12
Y = -3445421
06 feet Y = -998225
71 meter
Z = -15942151
16 Z = -4836606
66
XDOT = -3365
480300 XDOT = -1093
472661
YDOT = 23471
919664 feet/sec YDOT = 7142
391726 meter/sec
ZDOT = -8274
186150 ZDOT = -2527
118653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15540218
05 X = 4736658
46
Y = -2010871
01 feet Y = -612913
48 meter
Z = -15840746
85 Z = -4828259
64
XDOT = -5624
437472 XDOT = -1714
328542
YDOT = 21928
751384 feet/sec YDOT = 6683
883422 meter/sec
ZDOT = -8298
145391 ZDOT = -2529
274715
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
12611709
00016717 00000-0 10270-3 0 9187
2 25544 51
6406 114
8775 0005396 39
6633 320
4914 15
53822846 6744
Satellite: ISS
Catalog Number: 25544
Epoch time: 18221
12611709 = yrday
fracday
Element set: 918
Inclination: 51
6406 deg
RA of node: 114
8775 deg
Eccentricity:
0005396
Arg of perigee: 39
6633 deg
Mean anomaly: 320
4914 deg
Mean motion: 15
53822846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 315
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