[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 8th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
159/13:01:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 214
3
164/10:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
7
172/07:16:17
060 0
9 1
0 1
0
N/A 0
1 -0
1 220
4
000/00:02:34
120 0
3 -0
0 215
9
Coasting Arc #1 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2018/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907993
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2426941
58 A = 6778437
92 meter
Y = -3814477
21 meter E =
0013333
Z = -5061977
21 I = 51
96105
XDOT = 4813
523706 Wp = 89
11773
YDOT = 5632
039883 meter/sec RA = 61
30499 deg
ZDOT = -1940
433145 TA = 162
14027
MA = 162
09337
Ha = 221
500 n
mi
Hp = 214
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7962406
74 X = 2494004
32
Y = -12514689
02 feet Y = -3786962
08 meter
Z = -16607536
77 Z = -5050025
32
XDOT = 15792
400609 XDOT = 4759
612609
YDOT = 18477
821139 feet/sec YDOT = 5685
566752 meter/sec
ZDOT = -6366
250475 ZDOT = -1917
181010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10181433
59 X = -3103300
96
Y = -10869647
36 feet Y = -3313068
52 meter
Z = -16553453
30 Z = -5045492
57
XDOT = 20976
459670 XDOT = 6393
624908
YDOT = -10131
387058 feet/sec YDOT = -3088
046775 meter/sec
ZDOT = -6263
037406 ZDOT = -1908
973801
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 18159
51941492
00016717 00000-0 10270-3 0 9006
2 25544 51
6421 61
9290 0003129 166
3168 193
8070 15
54170133 37169
Satellite: ISS
Catalog Number: 25544
Epoch time: 18159
51941492 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 61
9290 deg
Eccentricity:
0003129
Arg of perigee: 166
3168 deg
Mean anomaly: 193
8070 deg
Mean motion: 15
54170133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 299
Coasting Arc #2 (Orbit 3716)
---------------------------------------
Vector Time (GMT): 2018/159/13:01:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4899799
60 A = 6781871
74 meter
Y = -2101188
46 meter E =
0010710
Z = 4182283
63 I = 51
97199
XDOT = -343
191798 Wp = 91
96842
YDOT = -6684
176500 meter/sec RA = 61
05533 deg
ZDOT = -3752
312252 TA = 36
44389
MA = 36
37103
Ha = 221
572 n
mi
Hp = 214
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16075458
02 X = -4896254
85
Y = -6893662
92 feet Y = -2155961
93 meter
Z = 13721402
98 Z = 4158490
36
XDOT = -1125
957344 XDOT = -250
195114
YDOT = -21929
712926 feet/sec YDOT = -6687
494011 meter/sec
ZDOT = -12310
735736 ZDOT = -3753
754067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6541347
65 X = -1993802
76
Y = 16311230
46 feet Y = 4971663
04 meter
Z = 13615225
68 Z = 4149920
79
XDOT = -20713
550548 XDOT = -6313
490207
YDOT = 1995
468810 feet/sec YDOT = 608
218893 meter/sec
ZDOT = -12316
161919 ZDOT = -3753
966153
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 18159
58371548
00016717 00000-0 10270-3 0 9013
2 25544 51
6423 61
6091 0003038 167
5854 192
5374 15
54177604 37175
Satellite: ISS
Catalog Number: 25544
Epoch time: 18159
58371548 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 61
6091 deg
Eccentricity:
0003038
Arg of perigee: 167
5854 deg
Mean anomaly: 192
5374 deg
Mean motion: 15
54177604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3717
Checksum: 322
Coasting Arc #3 (Orbit 3731)
---------------------------------------
Vector Time (GMT): 2018/160/13:01:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5067194
88 A = 6785725
05 meter
Y = 3447613
91 meter E =
0004678
Z = -2917837
98 I = 51
96752
XDOT = -952
352199 Wp = 101
47699
YDOT = 5675
523303 meter/sec RA = 56
09381 deg
ZDOT = 5058
061088 TA = 225
44802
MA = 225
48623
Ha = 221
406 n
mi
Hp = 214
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16624655
13 X = 5042439
58
Y = 11311069
26 feet Y = 3504140
64 meter
Z = -9572959
24 Z = -2893282
84
XDOT = -3124
515088 XDOT = -1040
316319
YDOT = 18620
483276 feet/sec YDOT = 5664
381129 meter/sec
ZDOT = 16594
688609 ZDOT = 5053
221727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10653960
06 X = 3247327
03
Y = -17114164
07 feet Y = -5216397
21 meter
Z = -9463589
06 Z = -2884501
95
XDOT = 17485
349381 XDOT = 5329
534491
YDOT = 1732
070680 feet/sec YDOT = 527
935143 meter/sec
ZDOT = 16572
143881 ZDOT = 5051
189455
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 18160
54823249
00016717 00000-0 10270-3 0 9022
2 25544 51
6420 56
8007 0003022 171
6684 188
4520 15
54154455 37328
Satellite: ISS
Catalog Number: 25544
Epoch time: 18160
54823249 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 56
8007 deg
Eccentricity:
0003022
Arg of perigee: 171
6684 deg
Mean anomaly: 188
4520 deg
Mean motion: 15
54154455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3732
Checksum: 294
Coasting Arc #4 (Orbit 3747)
---------------------------------------
Vector Time (GMT): 2018/161/13:01:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4925192
48 A = 6788640
86 meter
Y = -4468989
64 meter E =
0015892
Z = 1318155
27 I = 51
95772
XDOT = 2374
316463 Wp = 129
84992
YDOT = -4354
221691 meter/sec RA = 51
14174 deg
ZDOT = -5854
122501 TA = 35
85791
MA = 35
75134
Ha = 221
477 n
mi
Hp = 214
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16158767
97 X = -4881255
94
Y = -14662039
51 feet Y = -4523821
02 meter
Z = 4324656
39 Z = 1294336
30
XDOT = 7789
752174 XDOT = 2451
266696
YDOT = -14285
504235 feet/sec YDOT = -4327
239541 meter/sec
ZDOT = -19206
438650 ZDOT = -5842
402330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13732164
77 X = -4185563
82
Y = 16982744
45 feet Y = 5176340
51 meter
Z = 4218753
30 Z = 1285876
00
XDOT = -13469
583062 XDOT = -4105
528917
YDOT = -6102
837617 feet/sec YDOT = -1860
144906 meter/sec
ZDOT = -19153
293549 ZDOT = -5837
923874
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 18161
57705007
00016717 00000-0 10270-3 0 9038
2 25544 51
6420 51
6727 0003205 174
4355 185
6834 15
54125669 37488
Satellite: ISS
Catalog Number: 25544
Epoch time: 18161
57705007 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 51
6727 deg
Eccentricity:
0003205
Arg of perigee: 174
4355 deg
Mean anomaly: 185
6834 deg
Mean motion: 15
54125669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3748
Checksum: 310
Coasting Arc #5 (Orbit 3763)
---------------------------------------
Vector Time (GMT): 2018/162/13:01:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4465518
35 A = 6789092
09 meter
Y = 5093640
75 meter E =
0011009
Z = 387563
25 I = 51
93880
XDOT = -3791
792315 Wp = 61
02580
YDOT = 2856
726159 meter/sec RA = 46
19179 deg
ZDOT = 6020
311779 TA = 303
13452
MA = 303
24012
Ha = 221
192 n
mi
Hp = 214
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14650650
74 X = 4406345
37
Y = 16711419
78 feet Y = 5143246
34 meter
Z = 1271532
97 Z = 409112
44
XDOT = -12440
263500 XDOT = -3852
699088
YDOT = 9372
461151 feet/sec YDOT = 2813
982369 meter/sec
ZDOT = 19751
679064 ZDOT = 6001
744762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15595398
69 X = 4753477
52
Y = -15825432
54 feet Y = -4823591
84 meter
Z = 1367164
57 Z = 416711
76
XDOT = 9114
703441 XDOT = 2778
161609
YDOT = 10713
950675 feet/sec YDOT = 3265
612166 meter/sec
ZDOT = 19668
120680 ZDOT = 5994
843183
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 18162
60586087
00016717 00000-0 10270-3 0 9049
2 25544 51
6424 46
5434 0003050 182
1638 177
9502 15
54184764 37643
Satellite: ISS
Catalog Number: 25544
Epoch time: 18162
60586087 = yrday
fracday
Element set: 904
Inclination: 51
6424 deg
RA of node: 46
5434 deg
Eccentricity:
0003050
Arg of perigee: 182
1638 deg
Mean anomaly: 177
9502 deg
Mean motion: 15
54184764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3764
Checksum: 316
Coasting Arc #6 (Orbit 3778)
---------------------------------------
Vector Time (GMT): 2018/163/13:01:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3615699
14 A = 6787411
67 meter
Y = -5346355
23 meter E =
0008754
Z = -2088080
09 I = 51
90836
XDOT = 5122
206194 Wp = 153
22174
YDOT = -1300
841199 meter/sec RA = 41
23930 deg
ZDOT = -5555
512905 TA = 49
80191
MA = 49
72532
Ha = 221
160 n
mi
Hp = 214
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11862529
98 X = -3545503
09
Y = -17540535
54 feet Y = -5386395
65 meter
Z = -6850656
46 Z = -2105474
46
XDOT = 16805
138432 XDOT = 5163
357938
YDOT = -4267
851703 feet/sec YDOT = -1243
330194 meter/sec
ZDOT = -18226
748377 ZDOT = -5530
530951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16402183
91 X = -4999385
66
Y = 13352815
28 feet Y = 4069938
10 meter
Z = -6927639
25 Z = -2111544
44
XDOT = -4806
764002 XDOT = -1465
101668
YDOT = -15274
649915 feet/sec YDOT = -4655
713294 meter/sec
ZDOT = -18114
726332 ZDOT = -5521
368586
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 18163
57037175
00016717 00000-0 10270-3 0 9056
2 25544 51
6416 41
7351 0003058 186
4750 173
6364 15
54136723 37796
Satellite: ISS
Catalog Number: 25544
Epoch time: 18163
57037175 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 41
7351 deg
Eccentricity:
0003058
Arg of perigee: 186
4750 deg
Mean anomaly: 173
6364 deg
Mean motion: 15
54136723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3779
Checksum: 316
Coasting Arc #7 (Orbit 3792)
---------------------------------------
Vector Time (GMT): 2018/164/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3026566
66 A = 6777329
69 meter
Y = -2948016
94 meter E =
0014837
Z = -5311820
32 I = 51
85222
XDOT = 5835
387236 Wp = 106
04251
YDOT = 4923
719508 meter/sec RA = 36
67908 deg
ZDOT = 589
633583 TA = 169
59164
MA = 169
56089
Ha = 221
085 n
mi
Hp = 214
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9929680
64 X = 3085109
49
Y = -9671971
60 feet Y = -2913843
53 meter
Z = -17427232
02 Z = -5296976
50
XDOT = 19144
971246 XDOT = 5777
031004
YDOT = 16153
935393 feet/sec YDOT = 4988
648434 meter/sec
ZDOT = 1934
493384 ZDOT = 617
839241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4483143
19 X = -1366462
04
Y = -13205112
44 feet Y = -4024918
27 meter
Z = -17360312
23 Z = -5291423
17
XDOT = 21793
859430 XDOT = 6642
768354
YDOT = -10118
512447 feet/sec YDOT = -3084
122594 meter/sec
ZDOT = 2059
923852 ZDOT = 627
864790
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 18164
47057994
00016717 00000-0 10270-3 0 9068
2 25544 51
6420 37
2480 0002976 187
5366 172
5742 15
54182980 37937
Satellite: ISS
Catalog Number: 25544
Epoch time: 18164
47057994 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 37
2480 deg
Eccentricity:
0002976
Arg of perigee: 187
5366 deg
Mean anomaly: 172
5742 deg
Mean motion: 15
54182980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3793
Checksum: 339
Coasting Arc #8 (Orbit 3808)
---------------------------------------
Vector Time (GMT): 2018/165/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4378926
42 A = 6779178
07 meter
Y = 1780786
22 meter E =
0005540
Z = 4854687
07 I = 51
83200
XDOT = -4924
117615 Wp = 82
08566
YDOT = -5333
456117 meter/sec RA = 31
69504 deg
ZDOT = -2481
983134 TA = 32
23099
MA = 32
19715
Ha = 221
020 n
mi
Hp = 214
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14366556
51 X = -4422095
78
Y = 5842474
47 feet Y = 1731575
77 meter
Z = 15927451
02 Z = 4833311
18
XDOT = -16155
241518 XDOT = -4852
055280
YDOT = -17498
215608 feet/sec YDOT = -5388
117607 meter/sec
ZDOT = -8142
989285 ZDOT = -2505
728822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -597371
75 X = -182078
91
Y = 15595621
24 feet Y = 4753545
35 meter
Z = 15831484
30 Z = 4825436
41
XDOT = -21421
715475 XDOT = -6529
338877
YDOT = 7563
192540 feet/sec YDOT = 2305
261086 meter/sec
ZDOT = -8248
384176 ZDOT = -2514
107497
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 18165
49938532
00016717 00000-0 10270-3 0 9078
2 25544 51
6424 32
1195 0002937 195
0575 165
0491 15
54217941 38093
Satellite: ISS
Catalog Number: 25544
Epoch time: 18165
49938532 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 32
1195 deg
Eccentricity:
0002937
Arg of perigee: 195
0575 deg
Mean anomaly: 165
0491 deg
Mean motion: 15
54217941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3809
Checksum: 325
Coasting Arc #9 (Orbit 3823)
---------------------------------------
Vector Time (GMT): 2018/166/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5513774
86 A = 6782861
52 meter
Y = -661236
60 meter E =
0006811
Z = -3902671
79 I = 51
81489
XDOT = 3553
731744 Wp = 129
68224
YDOT = 5403
681687 meter/sec RA = 26
71589 deg
ZDOT = 4105
753223 TA = 183
30444
MA = 183
30894
Ha = 220
886 n
mi
Hp = 214
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18089812
53 X = 5539716
25
Y = -2169411
41 feet Y = -599432
01 meter
Z = -12804041
30 Z = -3875824
98
XDOT = 11659
224883 XDOT = 3473
098660
YDOT = 17728
614460 feet/sec YDOT = 5442
970367 meter/sec
ZDOT = 13470
318973 ZDOT = 4122
821109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5163763
23 X = 1573915
03
Y = -17559857
52 feet Y = -5352244
57 meter
Z = -12683772
71 Z = -3866013
92
XDOT = 19573
142455 XDOT = 5965
893820
YDOT = -4027
305878 feet/sec YDOT = -1227
522832 meter/sec
ZDOT = 13545
810171 ZDOT = 4128
762940
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 18166
46388993
00016717 00000-0 10270-3 0 9087
2 25544 51
6420 27
3105 0002885 198
2187 161
8863 15
54176032 38241
Satellite: ISS
Catalog Number: 25544
Epoch time: 18166
46388993 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 27
3105 deg
Eccentricity:
0002885
Arg of perigee: 198
2187 deg
Mean anomaly: 161
8863 deg
Mean motion: 15
54176032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3824
Checksum: 332
Coasting Arc #10 (Orbit 3839)
---------------------------------------
Vector Time (GMT): 2018/167/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6283400
48 A = 6786585
22 meter
Y = -373983
82 meter E =
0013832
Z = 2516577
16 I = 51
79673
XDOT = -1822
887838 Wp = 116
20141
YDOT = -5227
747540 meter/sec RA = 21
74600 deg
ZDOT = -5311
654247 TA = 35
60740
MA = 35
51519
Ha = 220
948 n
mi
Hp = 214
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20614830
97 X = -6290975
60
Y = -1226981
03 feet Y = -444291
90 meter
Z = 8256486
76 Z = 2486036
36
XDOT = -5980
603144 XDOT = -1738
493248
YDOT = -17151
402691 feet/sec YDOT = -5247
659561 meter/sec
ZDOT = -17426
687162 ZDOT = -5320
305030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8948769
73 X = -2727585
01
Y = 18671736
21 feet Y = 5691145
20 meter
Z = 8119858
30 Z = 2474932
81
XDOT = -16735
562636 XDOT = -5100
999491
YDOT = -401
826793 feet/sec YDOT = -122
476807 meter/sec
ZDOT = -17464
533284 ZDOT = -5323
189745
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 18167
49269290
00016717 00000-0 10270-3 0 9090
2 25544 51
6413 22
1816 0002799 198
6894 161
4156 15
54179400 38409
Satellite: ISS
Catalog Number: 25544
Epoch time: 18167
49269290 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 22
1816 deg
Eccentricity:
0002799
Arg of perigee: 198
6894 deg
Mean anomaly: 161
4156 deg
Mean motion: 15
54179400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3840
Checksum: 333
Coasting Arc #11 (Orbit 3854)
---------------------------------------
Vector Time (GMT): 2018/168/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6608078
95 A = 6788847
28 meter
Y = 1261110
73 meter E =
0007383
Z = -889418
46 I = 51
77335
XDOT = -130
289164 Wp = 44
13718
YDOT = 4846
196972 meter/sec RA = 16
78214 deg
ZDOT = 5938
247141 TA = 306
25833
MA = 306
32653
Ha = 220
736 n
mi
Hp = 214
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21680049
05 X = 6597806
02
Y = 4137502
38 feet Y = 1334949
51 meter
Z = -2918039
58 Z = -857343
80
XDOT = -427
457887 XDOT = -213
315554
YDOT = 15899
596366 feet/sec YDOT = 4844
274905 meter/sec
ZDOT = 19482
438128 ZDOT = 5937
413292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11712590
20 X = 3569997
49
Y = -18728980
01 feet Y = -5708593
11 meter
Z = -2774697
54 Z = -845727
81
XDOT = 13255
221569 XDOT = 4040
191534
YDOT = 5421
593556 feet/sec YDOT = 1652
501716 meter/sec
ZDOT = 19477
898361 ZDOT = 5936
863420
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 18168
45719316
00016717 00000-0 10270-3 0 9108
2 25544 51
6412 17
3728 0002890 205
9370 154
1638 15
54188349 38551
Satellite: ISS
Catalog Number: 25544
Epoch time: 18168
45719316 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 17
3728 deg
Eccentricity:
0002890
Arg of perigee: 205
9370 deg
Mean anomaly: 154
1638 deg
Mean motion: 15
54188349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3855
Checksum: 323
Coasting Arc #12 (Orbit 3870)
---------------------------------------
Vector Time (GMT): 2018/169/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6412316
62 A = 6788907
16 meter
Y = -2035609
42 meter E =
0011387
Z = -861047
48 I = 51
74182
XDOT = 2168
972901 Wp = 154
65866
YDOT = -4334
750853 meter/sec RA = 11
81972 deg
ZDOT = -5943
834270 TA = 34
64538
MA = 34
57125
Ha = 220
645 n
mi
Hp = 215
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21037784
18 X = -6384894
83
Y = -6678508
60 feet Y = -2107162
94 meter
Z = -2824958
91 Z = -892129
61
XDOT = 7116
052826 XDOT = 2246
155786
YDOT = -14221
623534 feet/sec YDOT = -4310
063634 meter/sec
ZDOT = -19500
768604 ZDOT = -5933
111317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13537874
25 X = -4126344
07
Y = 17410156
04 feet Y = 5306615
56 meter
Z = -2963724
08 Z = -903343
10
XDOT = -9568
853442 XDOT = -2916
586529
YDOT = -10731
112709 feet/sec YDOT = -3270
843154 meter/sec
ZDOT = -19452
058392 ZDOT = -5928
987398
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 18169
48599189
00016717 00000-0 10270-3 0 9117
2 25544 51
6416 12
2434 0002979 210
7960 149
3019 15
54154608 38718
Satellite: ISS
Catalog Number: 25544
Epoch time: 18169
48599189 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 12
2434 deg
Eccentricity:
0002979
Arg of perigee: 210
7960 deg
Mean anomaly: 149
3019 deg
Mean motion: 15
54154608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3871
Checksum: 329
Coasting Arc #13 (Orbit 3886)
---------------------------------------
Vector Time (GMT): 2018/170/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5716611
40 A = 6786419
78 meter
Y = 2667578
04 meter E =
0011632
Z = 2490152
02 I = 51
70012
XDOT = -4069
679724 Wp = 84
51435
YDOT = 3739
732915 meter/sec RA = 6
85113 deg
ZDOT = 5316
247136 TA = 303
38119
MA = 303
49244
Ha = 220
491 n
mi
Hp = 215
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18755286
74 X = 5674261
19
Y = 8751896
45 feet Y = 2731268
08 meter
Z = 8169790
08 Z = 2517818
52
XDOT = -13351
967600 XDOT = -4137
019291
YDOT = 12269
464945 feet/sec YDOT = 3693
845893 meter/sec
ZDOT = 17441
755694 ZDOT = 5296
315025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14429851
73 X = 4398218
81
Y = -14768373
87 feet Y = -4501400
35 meter
Z = 8293157
09 Z = 2527754
28
XDOT = 6066
484335 XDOT = 1849
064425
YDOT = 15708
176390 feet/sec YDOT = 4787
852164 meter/sec
ZDOT = 17351
937150 ZDOT = 5288
870443
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 18170
51478726
00016717 00000-0 10270-3 0 9127
2 25544 51
6403 7
1136 0002884 215
7162 144
3798 15
54198346 38873
Satellite: ISS
Catalog Number: 25544
Epoch time: 18170
51478726 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 7
1136 deg
Eccentricity:
0002884
Arg of perigee: 215
7162 deg
Mean anomaly: 144
3798 deg
Mean motion: 15
54198346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3887
Checksum: 324
Coasting Arc #14 (Orbit 3901)
---------------------------------------
Vector Time (GMT): 2018/171/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923033
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4539602
97 A = 6782692
04 meter
Y = -3219690
42 meter E =
0004420
Z = -3880391
55 I = 51
65384
XDOT = 5690
419137 Wp = 95
35255
YDOT = -3070
205248 meter/sec RA = 1
87262 deg
ZDOT = -4114
110670 TA = 131
47109
MA = 131
43313
Ha = 220
422 n
mi
Hp = 215
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14893710
54 X = -4484413
31
Y = -10563288
77 feet Y = -3270146
45 meter
Z = -12730943
42 Z = -3902309
52
XDOT = 18669
354123 XDOT = 5744
312175
YDOT = -10072
851864 feet/sec YDOT = -3006
269346 meter/sec
ZDOT = -13497
738417 ZDOT = -4086
338101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14674145
36 X = -4472679
51
Y = 10750905
83 feet Y = 3276876
10 meter
Z = -12828487
25 Z = -3910122
92
XDOT = -2901
827845 XDOT = -884
477127
YDOT = -19900
759105 feet/sec YDOT = -6065
751375 meter/sec
ZDOT = -13372
954341 ZDOT = -4076
076483
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 18171
47928338
00016717 00000-0 10270-3 0 9133
2 25544 51
6394 2
3056 0002927 219
8389 140
2549 15
54182358 39027
Satellite: ISS
Catalog Number: 25544
Epoch time: 18171
47928338 = yrday
fracday
Element set: 913
Inclination: 51
6394 deg
RA of node: 2
3056 deg
Eccentricity:
0002927
Arg of perigee: 219
8389 deg
Mean anomaly: 140
2549 deg
Mean motion: 15
54182358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3902
Checksum: 324
Coasting Arc #15 (Orbit 3914)
---------------------------------------
Vector Time (GMT): 2018/172/07:17:34
120
Vector Time (MET): N/A
Weight (LBS) : 922932
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2842858
39 A = 6780113
22 meter
Y = -3901050
93 meter E =
0009544
Z = -4770417
84 I = 51
61824
XDOT = 6951
572465 Wp = 123
97007
YDOT = 1814
947944 meter/sec RA = 357
59869 deg
ZDOT = 2657
100256 TA = 172
30070
MA = 172
28604
Ha = 220
411 n
mi
Hp = 215
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9326963
22 X = 2909441
86
Y = -12798723
52 feet Y = -3868887
40 meter
Z = -15650977
16 Z = -4756446
88
XDOT = 22806
996277 XDOT = 6917
853797
YDOT = 5954
553622 feet/sec YDOT = 1892
496445 meter/sec
ZDOT = 8717
520524 ZDOT = 2690
786799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5024204
80 X = 1531377
62
Y = -15084095
12 feet Y = -4597632
19 meter
Z = -15587818
74 Z = -4751167
15
XDOT = 22376
632790 XDOT = 6820
397674
YDOT = -1715
635478 feet/sec YDOT = -522
925694 meter/sec
ZDOT = 8867
948857 ZDOT = 2702
950811
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 18172
31517934
00016717 00000-0 10270-3 0 9144
2 25544 51
6424 358
1392 0003189 235
2016 124
8837 15
54012376 39150
Satellite: ISS
Catalog Number: 25544
Epoch time: 18172
31517934 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 358
1392 deg
Eccentricity:
0003189
Arg of perigee: 235
2016 deg
Mean anomaly: 124
8837 deg
Mean motion: 15
54012376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3915
Checksum: 308
Coasting Arc #16 (Orbit 3930)
---------------------------------------
Vector Time (GMT): 2018/173/07:17:34
120
Vector Time (MET): N/A
Weight (LBS) : 922932
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4323328
98 A = 6783643
51 meter
Y = 3591046
10 meter E =
0008934
Z = 3790926
98 I = 51
59683
XDOT = -5860
381816 Wp = 91
22660
YDOT = -2603
737831 meter/sec RA = 352
60823 deg
ZDOT = -4208
576992 TA = 43
24707
MA = 43
17697
Ha = 220
451 n
mi
Hp = 215
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14184150
21 X = -4381578
08
Y = 11781647
30 feet Y = 3542373
59 meter
Z = 12437424
47 Z = 3769784
59
XDOT = -19226
974462 XDOT = -5810
387475
YDOT = -8542
446953 feet/sec YDOT = -2668
992711 meter/sec
ZDOT = -13807
667295 ZDOT = -4236
923567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9668125
86 X = -2946844
76
Y = 15776038
93 feet Y = 4808536
67 meter
Z = 12342236
26 Z = 3761913
61
XDOT = -19721
885286 XDOT = -6011
230635
YDOT = -1163
397409 feet/sec YDOT = -354
603530 meter/sec
ZDOT = -13934
062272 ZDOT = -4247
102181
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 18173
34409082
00016717 00000-0 10270-3 0 9153
2 25544 51
6421 353
0115 0003013 238
8134 121
2723 15
54018920 39314
Satellite: ISS
Catalog Number: 25544
Epoch time: 18173
34409082 = yrday
fracday
Element set: 915
Inclination: 51
6421 deg
RA of node: 353
0115 deg
Eccentricity:
0003013
Arg of perigee: 238
8134 deg
Mean anomaly: 121
2723 deg
Mean motion: 15
54018920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3931
Checksum: 271
Coasting Arc #17 (Orbit 3945)
---------------------------------------
Vector Time (GMT): 2018/174/07:17:34
120
Vector Time (MET): N/A
Weight (LBS) : 922932
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5465350
20 A = 6787154
63 meter
Y = -3189689
71 meter E =
0002683
Z = -2450911
82 I = 51
57574
XDOT = 4355
931736 Wp = 27
13052
YDOT = 3372
339643 meter/sec RA = 347
62456 deg
ZDOT = 5329
177564 TA = 305
41740
MA = 305
44245
Ha = 220
264 n
mi
Hp = 215
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17930938
98 X = 5512517
27
Y = -10464861
25 feet Y = -3128308
39 meter
Z = -8041049
28 Z = -2424248
75
XDOT = 14291
114620 XDOT = 4292
011150
YDOT = 11064
106441 feet/sec YDOT = 3420
692674 meter/sec
ZDOT = 17484
178361 ZDOT = 5350
182370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13339236
72 X = 4065799
35
Y = -15969006
44 feet Y = -4867353
16 meter
Z = -7921235
04 Z = -2414392
44
XDOT = 15933
511559 XDOT = 4856
534323
YDOT = 4598
095666 feet/sec YDOT = 1401
499559 meter/sec
ZDOT = 17577
591964 ZDOT = 5357
650031
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 18174
30869337
00016717 00000-0 10270-3 0 9164
2 25544 51
6417 348
2037 0003138 243
6039 116
4792 15
54025443 39460
Satellite: ISS
Catalog Number: 25544
Epoch time: 18174
30869337 = yrday
fracday
Element set: 916
Inclination: 51
6417 deg
RA of node: 348
2037 deg
Eccentricity:
0003138
Arg of perigee: 243
6039 deg
Mean anomaly: 116
4792 deg
Mean motion: 15
54025443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3946
Checksum: 318
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