[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 30th 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 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 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
187/05:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 216
1
191/20:25:31
000 0
0 0
2 0
2
N/A -0
2 0
0 220
1
000/00:00:58
000 0
0 -0
0 216
0
193/18:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
9
Coasting Arc #1 (Orbit 42)
---------------------------------------
Vector Time (GMT): 2018/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922867
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1958919
95 A = 6778276
64 meter
Y = 3873260
44 meter E =
0000324
Z = 5206367
67 I = 51
36295
XDOT = -6082
675956 Wp = 355
98465
YDOT = 4540
852002 meter/sec RA = 316
67149 deg
ZDOT = -1089
204467 TA = 104
49405
MA = 104
49046
Ha = 220
209 n
mi
Hp = 216
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6426902
74 X = 1890172
96
Y = 12707547
37 feet Y = 3894781
21 meter
Z = 17081258
76 Z = 5215716
98
XDOT = -19956
285944 XDOT = -6127
710206
YDOT = 14897
808405 feet/sec YDOT = 4472
579699 meter/sec
ZDOT = -3573
505468 ZDOT = -1118
860368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11892919
13 X = 3624961
75
Y = -7741843
82 feet Y = -2359713
99 meter
Z = 17122458
03 Z = 5218925
21
XDOT = 16539
480227 XDOT = 5041
233573
YDOT = 17207
026514 feet/sec YDOT = 5244
701682 meter/sec
ZDOT = -3706
889694 ZDOT = -1129
859979
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 18180
54630952
00016717 00000-0 10270-3 0 9009
2 25544 51
6394 317
1056 0003726 240
9850 119
0930 15
53954593 438
Satellite: ISS
Catalog Number: 25544
Epoch time: 18180
54630952 = yrday
fracday
Element set: 900
Inclination: 51
6394 deg
RA of node: 317
1056 deg
Eccentricity:
0003726
Arg of perigee: 240
9850 deg
Mean anomaly: 119
0930 deg
Mean motion: 15
53954593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 43
Checksum: 301
Coasting Arc #2 (Orbit 57)
---------------------------------------
Vector Time (GMT): 2018/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922867
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -623035
90 A = 6780541
95 meter
Y = -4899373
76 meter E =
0008173
Z = -4653786
80 I = 51
34800
XDOT = 6181
776901 Wp = 128
66790
YDOT = -3505
618554 meter/sec RA = 311
65754 deg
ZDOT = 2861
415631 TA = 169
91243
MA = 169
89601
Ha = 220
107 n
mi
Hp = 216
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2044081
04 X = -545598
09
Y = -16074060
90 feet Y = -4905907
30 meter
Z = -15268329
40 Z = -4656625
91
XDOT = 20281
420278 XDOT = 6206
619171
YDOT = -11501
373208 feet/sec YDOT = -3436
351187 meter/sec
ZDOT = 9387
846559 ZDOT = 2891
504018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15674933
02 X = -4777719
58
Y = 4060287
06 feet Y = 1237575
50 meter
Z = -15280252
87 Z = -4657421
07
XDOT = -13787
552428 XDOT = -4202
445980
YDOT = -17369
479717 feet/sec YDOT = -5294
217418 meter/sec
ZDOT = 9522
991224 ZDOT = 2902
607725
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 18181
51092619
00016717 00000-0 10270-3 0 9010
2 25544 51
6399 312
2990 0003888 245
5666 114
5081 15
53992481 582
Satellite: ISS
Catalog Number: 25544
Epoch time: 18181
51092619 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 312
2990 deg
Eccentricity:
0003888
Arg of perigee: 245
5666 deg
Mean anomaly: 114
5081 deg
Mean motion: 15
53992481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 58
Checksum: 326
Coasting Arc #3 (Orbit 73)
---------------------------------------
Vector Time (GMT): 2018/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922867
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -619680
00 A = 6784204
10 meter
Y = 5694494
95 meter E =
0008370
Z = 3627368
28 I = 51
33967
XDOT = -5937
238632 Wp = 93
73762
YDOT = 2136
502432 meter/sec RA = 306
64916 deg
ZDOT = -4360
134883 TA = 43
01521
MA = 42
94980
Ha = 220
062 n
mi
Hp = 216
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2033070
87 X = -700930
96
Y = 18682726
21 feet Y = 5687110
47 meter
Z = 11900814
55 Z = 3624161
55
XDOT = -19479
129369 XDOT = -5939
509373
YDOT = 7009
522416 feet/sec YDOT = 2070
096027 meter/sec
ZDOT = -14304
904471 ZDOT = -4388
980777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18789206
30 X = 5726950
08
Y = -711125
69 feet Y = -216751
11 meter
Z = 11885581
60 Z = 3622725
27
XDOT = 9781
513651 XDOT = 2981
405361
YDOT = 16744
971182 feet/sec YDOT = 5103
867216 meter/sec
ZDOT = -14434
268446 ZDOT = -4399
565022
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 18182
53984819
00016717 00000-0 10270-3 0 9026
2 25544 51
6407 307
1705 0003820 248
8796 111
1949 15
53976578 748
Satellite: ISS
Catalog Number: 25544
Epoch time: 18182
53984819 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 307
1705 deg
Eccentricity:
0003820
Arg of perigee: 248
8796 deg
Mean anomaly: 111
1949 deg
Mean motion: 15
53976578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 74
Checksum: 338
Coasting Arc #4 (Orbit 88)
---------------------------------------
Vector Time (GMT): 2018/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1686913
30 A = 6787609
99 meter
Y = -6174023
85 meter E =
0003502
Z = -2253970
22 I = 51
33245
XDOT = 5400
533301 Wp = 7
95984
YDOT = -500
386151 meter/sec RA = 301
65004 deg
ZDOT = 5416
922704 TA = 326
86231
MA = 326
88424
Ha = 219
959 n
mi
Hp = 216
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5534492
47 X = 1766776
01
Y = -20255983
77 feet Y = -6154712
82 meter
Z = -7394915
42 Z = -2245582
65
XDOT = 17718
285107 XDOT = 5379
415182
YDOT = -1641
686847 feet/sec YDOT = -440
112385 meter/sec
ZDOT = 17772
056117 ZDOT = 5443
104923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20904113
31 X = -6371573
74
Y = -2126256
07 feet Y = -648082
85 meter
Z = -7356448
96 Z = -2242245
64
XDOT = -4708
120992 XDOT = -1435
035278
YDOT = -15555
551599 feet/sec YDOT = -4741
332127 meter/sec
ZDOT = 17889
247326 ZDOT = 5452
642585
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 18183
50445754
00016717 00000-0 10270-3 0 9035
2 25544 51
6408 302
3635 0003745 256
0704 104
0033 15
53985710 893
Satellite: ISS
Catalog Number: 25544
Epoch time: 18183
50445754 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 302
3635 deg
Eccentricity:
0003745
Arg of perigee: 256
0704 deg
Mean anomaly: 104
0033 deg
Mean motion: 15
53985710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 89
Checksum: 292
Coasting Arc #5 (Orbit 104)
---------------------------------------
Vector Time (GMT): 2018/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2565143
16 A = 6789538
16 meter
Y = 6246794
73 meter E =
0011128
Z = 637278
33 I = 51
32181
XDOT = -4668
146107 Wp = 143
60900
YDOT = -1306
007955 meter/sec RA = 296
65728 deg
ZDOT = -5943
459768 TA = 29
47874
MA = 29
41603
Ha = 219
872 n
mi
Hp = 216
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8415824
03 X = -2637901
42
Y = 20494733
37 feet Y = 6217702
65 meter
Z = 2090808
15 Z = 624641
83
XDOT = -15315
439983 XDOT = -4624
325187
YDOT = -4284
803002 feet/sec YDOT = -1357
964751 meter/sec
ZDOT = -19499
539921 ZDOT = -5966
029431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21694809
27 X = 6612577
87
Y = 4520225
84 feet Y = 1377764
83 meter
Z = 2033341
55 Z = 619762
51
XDOT = -1093
501246 XDOT = -333
299180
YDOT = 14132
867758 feet/sec YDOT = 4307
698093 meter/sec
ZDOT = -19600
296520 ZDOT = -5974
170379
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 18184
53337196
00016717 00000-0 10270-3 0 9040
2 25544 51
6400 297
2358 0003813 257
3679 102
7047 15
54001166 1054
Satellite: ISS
Catalog Number: 25544
Epoch time: 18184
53337196 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 297
2358 deg
Eccentricity:
0003813
Arg of perigee: 257
3679 deg
Mean anomaly: 102
7047 deg
Mean motion: 15
54001166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 105
Checksum: 298
Coasting Arc #6 (Orbit 120)
---------------------------------------
Vector Time (GMT): 2018/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3219934
06 A = 6789196
28 meter
Y = -5881874
06 meter E =
0010419
Z = 1025046
96 I = 51
30812
XDOT = 3820
721952 Wp = 46
81285
YDOT = 3120
229727 meter/sec RA = 291
66524 deg
ZDOT = 5871
695583 TA = 324
35022
MA = 324
41976
Ha = 219
825 n
mi
Hp = 216
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10564088
11 X = 3280488
39
Y = -19297487
06 feet Y = -5845528
05 meter
Z = 3363014
96 Z = 1040834
66
XDOT = 12535
177007 XDOT = 3757
025410
YDOT = 10236
974171 feet/sec YDOT = 3162
598986 meter/sec
ZDOT = 19264
093119 ZDOT = 5890
100723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21019750
13 X = -6406819
84
Y = -6455780
90 feet Y = -1967722
02 meter
Z = 3434506
03 Z = 1046837
44
XDOT = 7070
422085 XDOT = 2155
064651
YDOT = -12676
232436 feet/sec YDOT = -3863
715646 meter/sec
ZDOT = 19345
954497 ZDOT = 5896
646931
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 18185
56228196
00016717 00000-0 10270-3 0 9054
2 25544 51
6411 292
1077 0003721 263
7056 96
3673 15
54015203 1214
Satellite: ISS
Catalog Number: 25544
Epoch time: 18185
56228196 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 292
1077 deg
Eccentricity:
0003721
Arg of perigee: 263
7056 deg
Mean anomaly: 96
3673 deg
Mean motion: 15
54015203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 121
Checksum: 292
Coasting Arc #7 (Orbit 135)
---------------------------------------
Vector Time (GMT): 2018/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3694785
25 A = 6786720
01 meter
Y = 5059141
95 meter E =
0003183
Z = -2605602
52 I = 51
28819
XDOT = -2916
595089 Wp = 174
57511
YDOT = -4810
205212 meter/sec RA = 286
66884 deg
ZDOT = -5207
544375 TA = 34
90701
MA = 34
88614
Ha = 219
775 n
mi
Hp = 216
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12121998
84 X = -3738426
81
Y = 16598234
76 feet Y = 5017580
53 meter
Z = -8548564
69 Z = -2623655
94
XDOT = -9568
881524 XDOT = -2837
293959
YDOT = -15781
513163 feet/sec YDOT = -4842
376738 meter/sec
ZDOT = -17085
119342 ZDOT = -5221
519896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18823896
14 X = 5737523
54
Y = 8167330
98 feet Y = 2489402
48 meter
Z = -8630055
04 Z = -2630440
78
XDOT = -12753
634826 XDOT = -3887
307895
YDOT = 11288
403962 feet/sec YDOT = 3440
705528 meter/sec
ZDOT = -17146
927073 ZDOT = -5226
383372
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 18186
52688123
00016717 00000-0 10270-3 0 9062
2 25544 51
6406 287
3004 0003745 267
3375 92
7349 15
54016427 1369
Satellite: ISS
Catalog Number: 25544
Epoch time: 18186
52688123 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 287
3004 deg
Eccentricity:
0003745
Arg of perigee: 267
3375 deg
Mean anomaly: 92
7349 deg
Mean motion: 15
54016427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 136
Checksum: 315
Coasting Arc #8 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2018/187/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2052373
69 A = 6783029
79 meter
Y = -5134733
81 meter E =
0003018
Z = -3931776
48 I = 51
26590
XDOT = 4407
465692 Wp = 119
38085
YDOT = -4825
592417 meter/sec RA = 282
98683 deg
ZDOT = 4002
211693 TA = 192
64305
MA = 192
65062
Ha = 219
773 n
mi
Hp = 216
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6733509
47 X = -1975704
74
Y = -16846239
54 feet Y = -5157255
84 meter
Z = -12899529
14 Z = -3941560
39
XDOT = 14460
189277 XDOT = 4441
658681
YDOT = -15831
996120 feet/sec YDOT = -4776
114262 meter/sec
ZDOT = 13130
615790 ZDOT = 4023
704159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7956054
67 X = -2425005
46
Y = -16270384
32 feet Y = -4959213
14 meter
Z = -12942549
07 Z = -3944888
96
XDOT = 11892
826041 XDOT = 3624
933377
YDOT = -16335
192697 feet/sec YDOT = -4978
966734 meter/sec
ZDOT = 13227
446261 ZDOT = 4031
725620
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 18187
23425148
00016717 00000-0 10270-3 0 9078
2 25544 51
6371 283
7757 0003792 276
4977 83
5743 15
54026951 1477
Satellite: ISS
Catalog Number: 25544
Epoch time: 18187
23425148 = yrday
fracday
Element set: 907
Inclination: 51
6371 deg
RA of node: 283
7757 deg
Eccentricity:
0003792
Arg of perigee: 276
4977 deg
Mean anomaly: 83
5743 deg
Mean motion: 15
54026951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 147
Checksum: 339
Coasting Arc #9 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2018/188/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1259651
64 A = 6786595
38 meter
Y = 6129043
14 meter E =
0009534
Z = 2616574
18 I = 51
27260
XDOT = -4655
062083 Wp = 103
00972
YDOT = 3181
667129 meter/sec RA = 277
97993 deg
ZDOT = -5197
777580 TA = 47
35141
MA = 47
27109
Ha = 219
691 n
mi
Hp = 216
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4132715
35 X = 1178311
46
Y = 20108409
24 feet Y = 6142674
38 meter
Z = 8584560
96 Z = 2622496
15
XDOT = -15272
513395 XDOT = -4665
046375
YDOT = 10438
540451 feet/sec YDOT = 3129
555686 meter/sec
ZDOT = -17053
076049 ZDOT = -5220
414161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5987691
37 X = 1825048
33
Y = 19624845
77 feet Y = 5981652
99 meter
Z = 8610175
71 Z = 2624381
56
XDOT = -12655
871855 XDOT = -3857
509741
YDOT = 11407
857804 feet/sec YDOT = 3477
115059 meter/sec
ZDOT = -17154
780410 ZDOT = -5228
777069
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 18188
26315142
00016717 00000-0 10270-3 0 9085
2 25544 51
6379 278
6471 0004060 282
2466 77
8231 15
54064836 1638
Satellite: ISS
Catalog Number: 25544
Epoch time: 18188
26315142 = yrday
fracday
Element set: 908
Inclination: 51
6379 deg
RA of node: 278
6471 deg
Eccentricity:
0004060
Arg of perigee: 282
2466 deg
Mean anomaly: 77
8231 deg
Mean motion: 15
54064836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 163
Checksum: 317
Coasting Arc #10 (Orbit 177)
---------------------------------------
Vector Time (GMT): 2018/189/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -498643
39 A = 6789136
77 meter
Y = -6682825
69 meter E =
0008717
Z = -1054371
31 I = 51
27650
XDOT = 4774
149836 Wp = 15
05481
YDOT = -1278
247642 meter/sec RA = 272
98025 deg
ZDOT = 5863
170730 TA = 333
45401
MA = 333
49863
Ha = 219
844 n
mi
Hp = 216
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1635969
13 X = -418755
56
Y = -21925281
14 feet Y = -6687955
07 meter
Z = -3459223
47 Z = -1056600
26
XDOT = 15663
221247 XDOT = 4759
608544
YDOT = -4193
725860 feet/sec YDOT = -1224
941760 meter/sec
ZDOT = 19236
124443 ZDOT = 5886
326434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4082961
02 X = -1244486
52
Y = -21602343
04 feet Y = -6584394
16 meter
Z = -3468253
10 Z = -1057123
55
XDOT = 13386
113354 XDOT = 4080
087350
YDOT = -5624
972925 feet/sec YDOT = -1714
491747 meter/sec
ZDOT = 19339
879425 ZDOT = 5894
795249
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 18189
22774509
00016717 00000-0 10270-3 0 9099
2 25544 51
6372 273
8382 0003794 283
8159 76
2571 15
54031019 1781
Satellite: ISS
Catalog Number: 25544
Epoch time: 18189
22774509 = yrday
fracday
Element set: 909
Inclination: 51
6372 deg
RA of node: 273
8382 deg
Eccentricity:
0003794
Arg of perigee: 283
8159 deg
Mean anomaly: 76
2571 deg
Mean motion: 15
54031019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 178
Checksum: 334
Coasting Arc #11 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2018/190/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -272590
88 A = 6789302
48 meter
Y = 6749698
65 meter E =
0007567
Z = -635640
43 I = 51
27669
XDOT = -4791
052832 Wp = 152
92186
YDOT = -749
496758 meter/sec RA = 267
98569 deg
ZDOT = -5938
680303 TA = 33
97479
MA = 33
92635
Ha = 219
931 n
mi
Hp = 216
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -894327
04 X = -344960
00
Y = 22144680
59 feet Y = 6746245
79 meter
Z = -2085434
48 Z = -637139
48
XDOT = -15718
677270 XDOT = -4753
468695
YDOT = -2458
978864 feet/sec YDOT = -802
862697 meter/sec
ZDOT = -19483
859262 ZDOT = -5961
862396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2010198
98 X = 612708
65
Y = 22070656
06 feet Y = 6727135
97 meter
Z = -2093078
53 Z = -637970
34
XDOT = -14167
395608 XDOT = -4318
222181
YDOT = -556
492017 feet/sec YDOT = -169
618767 meter/sec
ZDOT = -19587
452726 ZDOT = -5970
255591
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 18190
25663964
00016717 00000-0 10270-3 0 9108
2 25544 51
6370 268
7098 0003776 291
6383 68
4367 15
54077679 1948
Satellite: ISS
Catalog Number: 25544
Epoch time: 18190
25663964 = yrday
fracday
Element set: 910
Inclination: 51
6370 deg
RA of node: 268
7098 deg
Eccentricity:
0003776
Arg of perigee: 291
6383 deg
Mean anomaly: 68
4367 deg
Mean motion: 15
54077679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 194
Checksum: 350
Coasting Arc #12 (Orbit 209)
---------------------------------------
Vector Time (GMT): 2018/191/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 947574
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1034688
08 A = 6787445
90 meter
Y = -6315693
60 meter E =
0011233
Z = 2241896
17 I = 51
27145
XDOT = 4710
134090 Wp = 60
09677
YDOT = 2700
285812 meter/sec RA = 262
98818 deg
ZDOT = 5418
251354 TA = 324
97717
MA = 325
05100
Ha = 219
959 n
mi
Hp = 216
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3394645
93 X = 1094345
07
Y = -20720779
52 feet Y = -6303789
78 meter
Z = 7355302
40 Z = 2247066
27
XDOT = 15453
195833 XDOT = 4653
269724
YDOT = 8859
205419 feet/sec YDOT = 2752
639020 meter/sec
ZDOT = 17776
415205 ZDOT = 5440
993811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 258615
82 X = 78826
10
Y = -20986992
91 feet Y = -6396835
44 meter
Z = 7379298
41 Z = 2249210
16
XDOT = 14942
055012 XDOT = 4554
338368
YDOT = 6487
368052 feet/sec YDOT = 1977
349782 meter/sec
ZDOT = 17877
782380 ZDOT = 5449
148069
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 18191
28553428
00016717 00000-0 10270-3 0 9116
2 25544 51
6362 263
5810 0003656 290
5108 69
5652 15
54039370 2108
Satellite: ISS
Catalog Number: 25544
Epoch time: 18191
28553428 = yrday
fracday
Element set: 911
Inclination: 51
6362 deg
RA of node: 263
5810 deg
Eccentricity:
0003656
Arg of perigee: 290
5108 deg
Mean anomaly: 69
5652 deg
Mean motion: 15
54039370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 210
Checksum: 298
Coasting Arc #13 (Orbit 218)
---------------------------------------
Vector Time (GMT): 2018/191/20:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 947556
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4346389
17 A = 6778841
13 meter
Y = -1340974
71 meter E =
0009273
Z = -5034620
46 I = 51
24777
XDOT = 165
152189 Wp = 98
16705
YDOT = -7435
224992 meter/sec RA = 259
82197 deg
ZDOT = 1839
425187 TA = 189
75501
MA = 189
77302
Ha = 220
091 n
mi
Hp = 216
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14259806
99 X = -4306615
56
Y = -4399523
33 feet Y = -1389355
84 meter
Z = -16517783
65 Z = -5055637
24
XDOT = 541
837890 XDOT = 239
347723
YDOT = -24393
782783 feet/sec YDOT = -7432
963588 meter/sec
ZDOT = 6034
859536 ZDOT = 1840
406455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11825744
08 X = 3604486
79
Y = -8929769
40 feet Y = -2721793
71 meter
Z = -16611624
64 Z = -5063223
19
XDOT = 18873
928173 XDOT = 5752
773307
YDOT = 13768
290977 feet/sec YDOT = 4196
575090 meter/sec
ZDOT = 6040
262428 ZDOT = 1841
071988
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 18191
86428632
00016717 00000-0 10270-3 0 9129
2 25544 51
6387 260
6999 0003994 297
0944 62
9801 15
54002786 2199
Satellite: ISS
Catalog Number: 25544
Epoch time: 18191
86428632 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 260
6999 deg
Eccentricity:
0003994
Arg of perigee: 297
0944 deg
Mean anomaly: 62
9801 deg
Mean motion: 15
54002786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 219
Checksum: 342
Coasting Arc #14 (Orbit 234)
---------------------------------------
Vector Time (GMT): 2018/192/20:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 947556
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4353775
48 A = 6781837
71 meter
Y = 2967174
19 meter E =
0007828
Z = 4268156
25 I = 51
26500
XDOT = -1108
858998 Wp = 49
55360
YDOT = 6716
624128 meter/sec RA = 254
80310 deg
ZDOT = -3528
943035 TA = 76
64675
MA = 76
55949
Ha = 220
165 n
mi
Hp = 216
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14284040
29 X = 4299539
88
Y = 9734823
45 feet Y = 3015557
14 meter
Z = 14003137
29 Z = 4289173
96
XDOT = -3637
988837 XDOT = -1166
742138
YDOT = 22036
168399 feet/sec YDOT = 6703
901049 meter/sec
ZDOT = -11577
897097 ZDOT = -3534
468900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16080889
32 X = -4901455
07
Y = 6129790
36 feet Y = 1868360
10 meter
Z = 14096776
84 Z = 4296697
58
XDOT = -15647
000250 XDOT = -4769
205676
YDOT = -14294
007391 feet/sec YDOT = -4356
813453 meter/sec
ZDOT = -11603
522211 ZDOT = -3536
753570
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 18192
89319967
00016717 00000-0 10270-3 0 9134
2 25544 51
6390 255
5721 0004051 302
3775 57
6986 15
54012628 2355
Satellite: ISS
Catalog Number: 25544
Epoch time: 18192
89319967 = yrday
fracday
Element set: 913
Inclination: 51
6390 deg
RA of node: 255
5721 deg
Eccentricity:
0004051
Arg of perigee: 302
3775 deg
Mean anomaly: 57
6986 deg
Mean motion: 15
54012628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 235
Checksum: 323
Coasting Arc #15 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2018/193/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 947556
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3358435
27 A = 6778375
34 meter
Y = 2871184
07 meter E =
0011466
Z = -5150412
75 I = 51
26014
XDOT = -3562
388892 Wp = 64
79098
YDOT = -6639
906481 meter/sec RA = 250
21177 deg
ZDOT = -1376
211927 TA = 191
87823
MA = 191
90530
Ha = 220
353 n
mi
Hp = 215
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11018488
42 X = -3365274
42
Y = 9419895
25 feet Y = 2833590
34 meter
Z = -16897679
62 Z = -5166742
77
XDOT = -11687
627600 XDOT = -3481
190059
YDOT = -21784
470081 feet/sec YDOT = -6679
289335 meter/sec
ZDOT = -4515
130995 ZDOT = -1393
320393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5036403
91 X = 1535095
91
Y = -13501424
37 feet Y = -4115234
15 meter
Z = -16971130
37 Z = -5172800
54
XDOT = 19709
225748 XDOT = 6007
372008
YDOT = 13132
470399 feet/sec YDOT = 4002
776978 meter/sec
ZDOT = -4590
809965 ZDOT = -1399
278877
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 18193
79349735
00016717 00000-0 10270-3 0 9141
2 25544 51
6370 251
0843 0004012 305
8935 54
1845 15
54001810 2494
Satellite: ISS
Catalog Number: 25544
Epoch time: 18193
79349735 = yrday
fracday
Element set: 914
Inclination: 51
6370 deg
RA of node: 251
0843 deg
Eccentricity:
0004012
Arg of perigee: 305
8935 deg
Mean anomaly: 54
1845 deg
Mean motion: 15
54001810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 299
Coasting Arc #16 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2018/194/18:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 947556
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4079034
32 A = 6777778
34 meter
Y = -1245651
99 meter E =
0003614
Z = 5268393
89 I = 51
27056
XDOT = 2834
333795 Wp = 351
19547
YDOT = 7106
728680 meter/sec RA = 245
18805 deg
ZDOT = -510
703234 TA = 103
72217
MA = 103
68194
Ha = 220
305 n
mi
Hp = 215
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13382658
54 X = 4067069
82
Y = -4086784
75 feet Y = -1200105
08 meter
Z = 17284756
86 Z = 5288178
79
XDOT = 9298
995392 XDOT = 2757
134426
YDOT = 23316
038978 feet/sec YDOT = 7137
992582 meter/sec
ZDOT = -1675
535543 ZDOT = -497
121764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9497977
62 X = -2894983
58
Y = 10124796
24 feet Y = 3086037
90 meter
Z = 17373459
68 Z = 5295430
51
XDOT = -18904
706351 XDOT = -5762
154496
YDOT = -14942
544290 feet/sec YDOT = -4554
487500 meter/sec
ZDOT = -1615
673508 ZDOT = -492
457285
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 18194
82240795
00016717 00000-0 10270-3 0 9153
2 25544 51
6372 245
9568 0004063 309
7025 50
3769 15
54008885 2651
Satellite: ISS
Catalog Number: 25544
Epoch time: 18194
82240795 = yrday
fracday
Element set: 915
Inclination: 51
6372 deg
RA of node: 245
9568 deg
Eccentricity:
0004063
Arg of perigee: 309
7025 deg
Mean anomaly: 50
3769 deg
Mean motion: 15
54008885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 328
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