[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 28th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
209/15:41:12
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 212
3
209/22:00:48
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 212
4
212/23:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 212
1
216/02:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
4
219/05:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
3
221/12:26:03
848 -0
5 0
8 0
8
N/A 0
6 -0
0 222
8
000/00:02:03
697 0
0 -0
0 213
0
Coasting Arc #1 (Orbit 2816)
---------------------------------------
Vector Time (GMT): 2017/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4213834
52 A = 6780379
65 meter
Y = 2820371
98 meter E =
0015394
Z = -4515781
43 I = 51
54898
XDOT = -5886
478534 Wp = 98
14095
YDOT = -3731
962337 meter/sec RA = 191
20937 deg
ZDOT = 3169
191625 TA = 203
73045
MA = 203
80152
Ha = 223
112 n
mi
Hp = 212
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13824916
41 X = -4223124
32
Y = 9253188
91 feet Y = 2773198
12 meter
Z = -14815555
88 Z = -4536273
20
XDOT = -19312
593616 XDOT = -5859
703428
YDOT = -12243
970923 feet/sec YDOT = -3797
639266 meter/sec
ZDOT = 10397
610317 ZDOT = 3140
662305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15501714
19 X = 4724922
49
Y = 5808790
46 feet Y = 1770519
33 meter
Z = -14906553
09 Z = -4543517
38
XDOT = 1702
313655 XDOT = 518
865202
YDOT = 21757
413705 feet/sec YDOT = 6631
659697 meter/sec
ZDOT = 10272
005624 ZDOT = 3130
907314
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 17209
51048267
00016717 00000-0 10270-3 0 9009
2 25544 51
6369 192
3365 0006212 77
5017 282
6830 15
54203785 28176
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
51048267 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 192
3365 deg
Eccentricity:
0006212
Arg of perigee: 77
5017 deg
Mean anomaly: 282
6830 deg
Mean motion: 15
54203785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2817
Checksum: 309
Coasting Arc #2 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2017/209/15:41:12
000
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -168188
93 A = 6777194
52 meter
Y = -4271835
80 meter E =
0008745
Z = 5251162
60 I = 51
54597
XDOT = 7595
145359 Wp = 93
14703
YDOT = 729
610724 meter/sec RA = 190
47354 deg
ZDOT = 835
133141 TA = 348
85696
MA = 348
87632
Ha = 222
942 n
mi
Hp = 212
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -551800
96 X = -145914
88
Y = -14015209
31 feet Y = -4273592
12 meter
Z = 17228223
75 Z = 5250399
65
XDOT = 24918
455901 XDOT = 7582
365559
YDOT = 2393
735971 feet/sec YDOT = 814
473335 meter/sec
ZDOT = 2739
938126 ZDOT = 871
996503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 892190
79 X = 271939
75
Y = 14001069
89 feet Y = 4267526
10 meter
Z = 17225455
22 Z = 5250318
75
XDOT = -23914
619260 XDOT = -7289
175951
YDOT = -2054
158131 feet/sec YDOT = -626
107398 meter/sec
ZDOT = 2902
816934 ZDOT = 884
778602
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 17209
70337551
00016717 00000-0 10270-3 0 9018
2 25544 51
6391 191
3754 0005968 77
5082 282
6738 15
54267949 28204
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
70337551 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 191
3754 deg
Eccentricity:
0005968
Arg of perigee: 77
5082 deg
Mean anomaly: 282
6738 deg
Mean motion: 15
54267949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 336
Coasting Arc #3 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2017/209/22:00:48
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3736293
72 A = 6779622
45 meter
Y = -3162965
68 meter E =
0013618
Z = 4681313
60 I = 51
56076
XDOT = 6334
358803 Wp = 70
39139
YDOT = 3287
322634 meter/sec RA = 189
12705 deg
ZDOT = -2823
361592 TA = 47
67902
MA = 47
56371
Ha = 222
873 n
mi
Hp = 212
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12258181
50 X = 3748645
90
Y = -10377184
00 feet Y = -3121114
90 meter
Z = 15358640
40 Z = 4699493
10
XDOT = 20782
017070 XDOT = 6310
842655
YDOT = 10785
179245 feet/sec YDOT = 3358
026286 meter/sec
ZDOT = -9262
997349 ZDOT = -2792
648683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11607224
79 X = 3537882
12
Y = 10987812
24 feet Y = 3349085
17 meter
Z = 15439466
03 Z = 4705949
25
XDOT = -7710
817440 XDOT = -2350
257156
YDOT = 21022
422165 feet/sec YDOT = 6407
634276 meter/sec
ZDOT = -9127
668913 ZDOT = -2782
113485
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 17209
96056611
00016717 00000-0 10270-3 0 9022
2 25544 51
6376 190
0905 0005866 79
2364 280
9449 15
54229126 28249
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
96056611 = yrday
fracday
Element set: 902
Inclination: 51
6376 deg
RA of node: 190
0905 deg
Eccentricity:
0005866
Arg of perigee: 79
2364 deg
Mean anomaly: 280
9449 deg
Mean motion: 15
54229126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 325
Coasting Arc #4 (Orbit 2838)
---------------------------------------
Vector Time (GMT): 2017/210/22:00:48
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5145439
70 A = 6783287
11 meter
Y = 2521041
96 meter E =
0011495
Z = -3640988
36 I = 51
60512
XDOT = -4973
042260 Wp = 92
00799
YDOT = -3839
849309 meter/sec RA = 184
13247 deg
ZDOT = 4380
740927 TA = 224
81120
MA = 224
90409
Ha = 222
993 n
mi
Hp = 212
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16881363
85 X = -5155562
27
Y = 8271135
04 feet Y = 2463445
63 meter
Z = -11945499
87 Z = -3666007
61
XDOT = -16315
755447 XDOT = -4951
013735
YDOT = -12597
930803 feet/sec YDOT = -3895
338162 meter/sec
ZDOT = 14372
509602 ZDOT = 4356
637086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10277080
25 X = -3132454
06
Y = -15655983
65 feet Y = -4771943
82 meter
Z = -12056487
25 Z = -3674817
31
XDOT = 9337
557074 XDOT = 2846
087396
YDOT = -17086
918311 feet/sec YDOT = -5208
092701 meter/sec
ZDOT = 14266
467605 ZDOT = 4348
419326
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 17210
92503196
00016717 00000-0 10270-3 0 9036
2 25544 51
6371 185
2808 0006019 83
6799 276
5039 15
54238919 28396
Satellite: ISS
Catalog Number: 25544
Epoch time: 17210
92503196 = yrday
fracday
Element set: 903
Inclination: 51
6371 deg
RA of node: 185
2808 deg
Eccentricity:
0006019
Arg of perigee: 83
6799 deg
Mean anomaly: 276
5039 deg
Mean motion: 15
54238919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2839
Checksum: 336
Coasting Arc #5 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2017/211/22:00:48
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6170574
00 A = 6786871
70 meter
Y = -1797366
10 meter E =
0019428
Z = 2156053
84 I = 51
64976
XDOT = 3186
579557 Wp = 102
54461
YDOT = 4301
745156 meter/sec RA = 179
15177 deg
ZDOT = -5496
173506 TA = 53
52958
MA = 53
35070
Ha = 222
882 n
mi
Hp = 212
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20244665
36 X = 6179741
05
Y = -5896870
40 feet Y = -1728311
35 meter
Z = 7073667
45 Z = 2186050
55
XDOT = 10454
657338 XDOT = 3164
936973
YDOT = 14113
337126 feet/sec YDOT = 4337
258805 meter/sec
ZDOT = -18032
065307 ZDOT = -5480
746653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8670628
76 X = 2642807
65
Y = 19171378
61 feet Y = 5843436
20 meter
Z = 7206578
02 Z = 2196564
98
XDOT = -11091
574307 XDOT = -3380
711849
YDOT = 11814
842143 feet/sec YDOT = 3601
163885 meter/sec
ZDOT = -17964
448958 ZDOT = -5475
564042
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 17211
95379051
00016717 00000-0 10270-3 0 9042
2 25544 51
6369 180
1512 0005887 85
6852 274
4974 15
54271611 28552
Satellite: ISS
Catalog Number: 25544
Epoch time: 17211
95379051 = yrday
fracday
Element set: 904
Inclination: 51
6369 deg
RA of node: 180
1512 deg
Eccentricity:
0005887
Arg of perigee: 85
6852 deg
Mean anomaly: 274
4974 deg
Mean motion: 15
54271611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 328
Coasting Arc #6 (Orbit 2869)
---------------------------------------
Vector Time (GMT): 2017/212/22:00:48
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6681556
19 A = 6788877
38 meter
Y = 1069825
76 meter E =
0015573
Z = -489718
33 I = 51
68791
XDOT = -1170
985911 Wp = 59
50802
YDOT = -4639
122142 meter/sec RA = 174
18124 deg
ZDOT = 5991
602501 TA = 295
21359
MA = 295
37496
Ha = 223
036 n
mi
Hp = 212
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21921116
10 X = -6690643
88
Y = 3509927
05 feet Y = 995057
27 meter
Z = -1606687
45 Z = -522197
04
XDOT = -3841
817294 XDOT = -1148
127030
YDOT = -15220
217000 feet/sec YDOT = -4652
089330 meter/sec
ZDOT = 19657
488521 ZDOT = 5985
969593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6911595
09 X = -2106654
18
Y = -21085587
52 feet Y = -6426887
08 meter
Z = -1750490
17 Z = -533549
40
XDOT = 12867
206826 XDOT = 3921
924640
YDOT = -5810
240366 feet/sec YDOT = -1770
961264 meter/sec
ZDOT = 19633
230346 ZDOT = 5984
208609
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 17212
91825359
00016717 00000-0 10270-3 0 9057
2 25544 51
6361 175
3425 0006125 92
0364 268
1491 15
54241206 28707
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
91825359 = yrday
fracday
Element set: 905
Inclination: 51
6361 deg
RA of node: 175
3425 deg
Eccentricity:
0006125
Arg of perigee: 92
0364 deg
Mean anomaly: 268
1491 deg
Mean motion: 15
54241206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2870
Checksum: 298
Coasting Arc #7 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2017/212/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2659264
20 A = 6779404
60 meter
Y = 4061349
83 meter E =
0017213
Z = -4748498
85 I = 51
65952
XDOT = -7013
473318 Wp = 103
73935
YDOT = -1414
986893 meter/sec RA = 173
89662 deg
ZDOT = 2721
782543 TA = 193
19497
MA = 193
24005
Ha = 223
085 n
mi
Hp = 212
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8724620
07 X = -2681415
94
Y = 13324638
56 feet Y = 4031488
47 meter
Z = -15579064
46 Z = -4761470
27
XDOT = -23010
083064 XDOT = -7010
350287
YDOT = -4642
345448 feet/sec YDOT = -1493
398965 meter/sec
ZDOT = 8929
732751 ZDOT = 2687
721056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15823544
13 X = -4823016
25
Y = -1213084
20 feet Y = -369748
06 meter
Z = -15637011
08 Z = -4766160
98
XDOT = -7026
612867 XDOT = -2141
711602
YDOT = -21330
383340 feet/sec YDOT = -6501
500842 meter/sec
ZDOT = 8779
279744 ZDOT = 2675
924466
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 17212
98255152
00016717 00000-0 10270-3 0 9063
2 25544 51
6376 175
0218 0006201 93
4558 266
7304 15
54239870 28717
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
98255152 = yrday
fracday
Element set: 906
Inclination: 51
6376 deg
RA of node: 175
0218 deg
Eccentricity:
0006201
Arg of perigee: 93
4558 deg
Mean anomaly: 266
7304 deg
Mean motion: 15
54239870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 314
Coasting Arc #8 (Orbit 2886)
---------------------------------------
Vector Time (GMT): 2017/213/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4231735
24 A = 6783180
08 meter
Y = -3795503
34 meter E =
0017771
Z = 3685924
83 I = 51
70457
XDOT = 5886
787039 Wp = 89
32723
YDOT = 2334
875322 meter/sec RA = 168
90814 deg
ZDOT = -4335
962196 TA = 46
78744
MA = 46
63916
Ha = 223
022 n
mi
Hp = 212
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13883645
80 X = 4255958
79
Y = -12452438
78 feet Y = -3748045
94 meter
Z = 12092929
23 Z = 3706539
75
XDOT = 19313
605772 XDOT = 5881
302124
YDOT = 7660
352106 feet/sec YDOT = 2400
674924 meter/sec
ZDOT = -14225
597756 ZDOT = -4307
379461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17635800
50 X = 5375391
99
Y = 5879660
86 feet Y = 1792120
63 meter
Z = 12184659
14 Z = 3713884
11
XDOT = 3322
844248 XDOT = 1012
802927
YDOT = 19375
355984 feet/sec YDOT = 5905
608504 meter/sec
ZDOT = -14099
490958 ZDOT = -4297
524844
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 17214
01130743
00016717 00000-0 10270-3 0 9078
2 25544 51
6377 169
8912 0006174 97
4264 262
7591 15
54229032 28877
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
01130743 = yrday
fracday
Element set: 907
Inclination: 51
6377 deg
RA of node: 169
8912 deg
Eccentricity:
0006174
Arg of perigee: 97
4264 deg
Mean anomaly: 262
7591 deg
Mean motion: 15
54229032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2887
Checksum: 319
Coasting Arc #9 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2017/214/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5410441
28 A = 6786721
62 meter
Y = 3416334
94 meter E =
0010690
Z = -2265014
57 I = 51
74963
XDOT = -4310
653681 Wp = 73
62906
YDOT = -3229
605120 meter/sec RA = 163
93421 deg
ZDOT = 5449
892062 TA = 261
22592
MA = 261
34700
Ha = 223
041 n
mi
Hp = 212
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17750791
60 X = -5437239
31
Y = 11208447
95 feet Y = 3355682
00 meter
Z = -7431150
16 Z = -2291361
43
XDOT = -14142
564570 XDOT = -4300
691632
YDOT = -10595
817324 feet/sec YDOT = -3277
754391 meter/sec
ZDOT = 17880
223300 ZDOT = 5428
976471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18640784
81 X = -5681711
21
Y = -9564921
28 feet Y = -2915388
00 meter
Z = -7548199
99 Z = -2300691
36
XDOT = 1194
599154 XDOT = 364
113822
YDOT = -16303
865346 feet/sec YDOT = -4969
418157 meter/sec
ZDOT = 17788
147885 ZDOT = 5421
827475
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 17214
97576238
00016717 00000-0 10270-3 0 9087
2 25544 51
6389 165
0830 0006223 99
9829 260
2027 15
54251375 29026
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
97576238 = yrday
fracday
Element set: 908
Inclination: 51
6389 deg
RA of node: 165
0830 deg
Eccentricity:
0006223
Arg of perigee: 99
9829 deg
Mean anomaly: 260
2027 deg
Mean motion: 15
54251375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 327
Coasting Arc #10 (Orbit 2917)
---------------------------------------
Vector Time (GMT): 2017/215/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6143828
16 A = 6788813
29 meter
Y = -2818427
13 meter E =
0018832
Z = 541083
71 I = 51
78687
XDOT = 2431
649425 Wp = 121
35555
YDOT = 4122
048672 meter/sec RA = 158
97039 deg
ZDOT = -5995
348010 TA = 52
81573
MA = 52
64395
Ha = 223
024 n
mi
Hp = 212
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20156916
53 X = 6172259
65
Y = -9246808
18 feet Y = -2749563
73 meter
Z = 1775209
01 Z = 570997
02
XDOT = 7977
852443 XDOT = 2414
496945
YDOT = 13523
781731 feet/sec YDOT = 4149
145486 meter/sec
ZDOT = -19669
776935 ZDOT = -5983
577373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18405980
45 X = 5610142
84
Y = 12350531
81 feet Y = 3764442
10 meter
Z = 1907972
81 Z = 581550
11
XDOT = -6397
457035 XDOT = -1949
944904
YDOT = 12632
795491 feet/sec YDOT = 3850
476066 meter/sec
ZDOT = -19618
281866 ZDOT = -5979
652313
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 17216
00451272
00016717 00000-0 10270-3 0 9094
2 25544 51
6382 159
9535 0006146 104
1410 256
0426 15
54257962 29183
Satellite: ISS
Catalog Number: 25544
Epoch time: 17216
00451272 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 159
9535 deg
Eccentricity:
0006146
Arg of perigee: 104
1410 deg
Mean anomaly: 256
0426 deg
Mean motion: 15
54257962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2918
Checksum: 301
Coasting Arc #11 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2017/216/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 849441
81 A = 6777144
99 meter
Y = 4159482
94 meter E =
0020592
Z = -5300579
50 I = 51
75404
XDOT = -7258
964836 Wp = 97
69466
YDOT = 2331
845253 meter/sec RA = 158
24238 deg
ZDOT = 666
099688 TA = 178
67068
MA = 178
66520
Ha = 222
968 n
mi
Hp = 212
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2786882
57 X = 828613
51
Y = 13646597
57 feet Y = 4168865
84 meter
Z = -17390352
69 Z = -5296503
57
XDOT = -23815
501429 XDOT = -7287
736189
YDOT = 7650
410936 feet/sec YDOT = 2250
509665 meter/sec
ZDOT = 2185
366431 ZDOT = 630
768615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1580112
87 X = 481618
40
Y = 13860227
99 feet Y = 4224597
49 meter
Z = -17372910
80 Z = -5295263
21
XDOT = -23441
944571 XDOT = -7145
104705
YDOT = 5217
233909 feet/sec YDOT = 1590
212896 meter/sec
ZDOT = 2028
695889 ZDOT = 618
346507
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 17216
13310544
00016717 00000-0 10270-3 0 9106
2 25544 51
6400 159
3154 0005963 103
3530 256
8288 15
54246723 29205
Satellite: ISS
Catalog Number: 25544
Epoch time: 17216
13310544 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 159
3154 deg
Eccentricity:
0005963
Arg of perigee: 103
3530 deg
Mean anomaly: 256
8288 deg
Mean motion: 15
54246723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 285
Coasting Arc #12 (Orbit 2935)
---------------------------------------
Vector Time (GMT): 2017/217/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 896284
45 A = 6778997
94 meter
Y = -4687270
36 meter E =
0012084
Z = 4805086
76 I = 51
79188
XDOT = 7108
207208 Wp = 81
49867
YDOT = -1301
268145 meter/sec RA = 153
25229 deg
ZDOT = -2587
950655 TA = 33
94920
MA = 33
87193
Ha = 222
834 n
mi
Hp = 212
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2940565
77 X = 925291
75
Y = -15378183
60 feet Y = -4677085
58 meter
Z = 15764720
33 Z = 4809510
75
XDOT = 23320
889790 XDOT = 7134
800830
YDOT = -4269
252443 feet/sec YDOT = -1221
630501 meter/sec
ZDOT = -8490
651755 ZDOT = -2553
357225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4038120
19 X = 1230819
03
Y = -15105964
86 feet Y = -4604298
09 meter
Z = 15784969
94 Z = 4811258
84
XDOT = 22537
914987 XDOT = 6869
556488
YDOT = -2712
275097 feet/sec YDOT = -826
701450 meter/sec
ZDOT = -8337
369952 ZDOT = -2541
230362
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 17217
16185157
00016717 00000-0 10270-3 0 9111
2 25544 51
6411 154
1857 0005862 106
9229 253
2559 15
54295458 29360
Satellite: ISS
Catalog Number: 25544
Epoch time: 17217
16185157 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 154
1857 deg
Eccentricity:
0005862
Arg of perigee: 106
9229 deg
Mean anomaly: 253
2559 deg
Mean motion: 15
54295458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 325
Coasting Arc #13 (Orbit 2950)
---------------------------------------
Vector Time (GMT): 2017/218/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2458658
52 A = 6782637
86 meter
Y = 5048136
19 meter E =
0012247
Z = -3817849
96 I = 51
83229
XDOT = -6395
946679 Wp = 107
40925
YDOT = 63
460440 meter/sec RA = 148
27360 deg
ZDOT = 4210
401175 TA = 206
93346
MA = 206
99707
Ha = 222
904 n
mi
Hp = 212
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8066464
97 X = -2496380
49
Y = 16562126
59 feet Y = 5020431
06 meter
Z = -12525754
47 Z = -3829884
53
XDOT = -20984
077030 XDOT = -6416
632634
YDOT = 208
203544 feet/sec YDOT = -8
179239 meter/sec
ZDOT = 13813
652148 ZDOT = 4179
281988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8987770
84 X = -2739472
55
Y = 16038590
74 feet Y = 4888562
46 meter
Z = -12579745
69 Z = -3834306
49
XDOT = -19877
523120 XDOT = -6058
669047
YDOT = -431
835073 feet/sec YDOT = -131
623330 meter/sec
ZDOT = 13675
904130 ZDOT = 4168
415579
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 17218
12630014
00016717 00000-0 10270-3 0 9126
2 25544 51
6406 149
3779 0006070 109
7245 250
4563 15
54289360 29510
Satellite: ISS
Catalog Number: 25544
Epoch time: 17218
12630014 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 149
3779 deg
Eccentricity:
0006070
Arg of perigee: 109
7245 deg
Mean anomaly: 250
4563 deg
Mean motion: 15
54289360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2951
Checksum: 300
Coasting Arc #14 (Orbit 2966)
---------------------------------------
Vector Time (GMT): 2017/219/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3757340
14 A = 6786422
96 meter
Y = -5118494
38 meter E =
0019745
Z = 2368741
76 I = 51
87227
XDOT = 5276
758447 Wp = 108
31356
YDOT = 1358
118124 meter/sec RA = 143
30736 deg
ZDOT = -5404
622179 TA = 45
30586
MA = 45
14518
Ha = 222
838 n
mi
Hp = 212
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12327231
43 X = 3802791
29
Y = -16792960
58 feet Y = -5076223
19 meter
Z = 7771462
46 Z = 2387103
62
XDOT = 17312
199628 XDOT = 5287
431902
YDOT = 4455
768125 feet/sec YDOT = 1417
186267 meter/sec
ZDOT = -17731
700061 ZDOT = -5378
963879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13008398
46 X = 3964959
85
Y = -16231580
08 feet Y = -4947385
61 meter
Z = 7853481
14 Z = 2393741
05
XDOT = 16029
751500 XDOT = 4885
868257
YDOT = 4273
865841 feet/sec YDOT = 1302
674308 meter/sec
ZDOT = -17618
312823 ZDOT = -5370
061748
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 17219
15504137
00016717 00000-0 10270-3 0 9137
2 25544 51
6408 144
2489 0005987 112
1038 248
0751 15
54293566 29670
Satellite: ISS
Catalog Number: 25544
Epoch time: 17219
15504137 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 144
2489 deg
Eccentricity:
0005987
Arg of perigee: 112
1038 deg
Mean anomaly: 248
0751 deg
Mean motion: 15
54293566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2967
Checksum: 321
Coasting Arc #15 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2017/219/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -127311
82 A = 6778784
11 meter
Y = -4707870
29 meter E =
0011796
Z = 4865971
05 I = 51
84901
XDOT = 6747
040016 Wp = 84
10020
YDOT = -2720
388191 meter/sec RA = 142
70563 deg
ZDOT = -2449
202769 TA = 29
87116
MA = 29
80389
Ha = 222
972 n
mi
Hp = 212
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -417689
70 X = -98293
72
Y = -15445768
68 feet Y = -4709131
87 meter
Z = 15964471
96 Z = 4865422
97
XDOT = 22135
958059 XDOT = 6788
855448
YDOT = -8925
158107 feet/sec YDOT = -2644
704330 meter/sec
ZDOT = -8035
442156 ZDOT = -2416
326927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10591372
92 X = -3228250
46
Y = -11252773
31 feet Y = -3429845
30 meter
Z = 15962722
58 Z = 4865437
84
XDOT = 9946
682792 XDOT = 3031
748915
YDOT = -20582
976125 feet/sec YDOT = -6273
691123 meter/sec
ZDOT = -7889
516470 ZDOT = -2404
724620
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 17219
28363382
00016717 00000-0 10270-3 0 9147
2 25544 51
6398 143
6085 0006198 111
3243 248
8571 15
54291746 29695
Satellite: ISS
Catalog Number: 25544
Epoch time: 17219
28363382 = yrday
fracday
Element set: 914
Inclination: 51
6398 deg
RA of node: 143
6085 deg
Eccentricity:
0006198
Arg of perigee: 111
3243 deg
Mean anomaly: 248
8571 deg
Mean motion: 15
54291746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 336
Coasting Arc #16 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2017/220/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1356296
27 A = 6782410
59 meter
Y = 5381134
72 meter E =
0012629
Z = -3913117
56 I = 51
88736
XDOT = -6313
685749 Wp = 110
61737
YDOT = 1388
379885 meter/sec RA = 137
72999 deg
ZDOT = 4103
946356 TA = 202
29187
MA = 202
34681
Ha = 222
920 n
mi
Hp = 212
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4449790
91 X = -1397361
13
Y = 17654641
48 feet Y = 5365738
13 meter
Z = -12838312
19 Z = -3919805
57
XDOT = -20714
192090 XDOT = -6348
676280
YDOT = 4555
052116 feet/sec YDOT = 1317
580275 meter/sec
ZDOT = 13464
390931 ZDOT = 4073
192095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8656202
42 X = 2638410
50
Y = 15993000
16 feet Y = 4874666
45 meter
Z = -12868697
30 Z = -3922378
94
XDOT = -11148
717592 XDOT = -3398
129122
YDOT = 16741
796940 feet/sec YDOT = 5102
899707 meter/sec
ZDOT = 13328
033089 ZDOT = 4062
384486
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 17220
24807598
00016717 00000-0 10270-3 0 9158
2 25544 51
6409 138
8006 0006101 114
6514 245
5275 15
54268668 29847
Satellite: ISS
Catalog Number: 25544
Epoch time: 17220
24807598 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 138
8006 deg
Eccentricity:
0006101
Arg of perigee: 114
6514 deg
Mean anomaly: 245
5275 deg
Mean motion: 15
54268668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 319
Coasting Arc #17 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2017/221/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2640017
53 A = 6786167
40 meter
Y = -5724077
44 meter E =
0019716
Z = 2487091
74 I = 51
92278
XDOT = 5507
921234 Wp = 108
65936
YDOT = 207
391175 meter/sec RA = 132
76576 deg
ZDOT = -5340
911880 TA = 43
54977
MA = 43
39427
Ha = 222
849 n
mi
Hp = 212
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8661474
85 X = 2691748
64
Y = -18779781
61 feet Y = -5694265
70 meter
Z = 8159749
81 Z = 2500041
57
XDOT = 18070
607723 XDOT = 5531
135791
YDOT = 680
417240 feet/sec YDOT = 269
114252 meter/sec
ZDOT = -17522
676773 ZDOT = -5314
100255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6614571
64 X = -2016121
44
Y = -19570288
06 feet Y = -5965023
80 meter
Z = 8217915
08 Z = 2504820
52
XDOT = 12273
026188 XDOT = 3740
818382
YDOT = -11495
217410 feet/sec YDOT = -3503
742267 meter/sec
ZDOT = -17403
992977 ZDOT = -5304
737059
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 17221
27680925
00016717 00000-0 10270-3 0 9166
2 25544 51
6400 133
6709 0006114 116
9716 243
2061 15
54301823 30003
Satellite: ISS
Catalog Number: 25544
Epoch time: 17221
27680925 = yrday
fracday
Element set: 916
Inclination: 51
6400 deg
RA of node: 133
6709 deg
Eccentricity:
0006114
Arg of perigee: 116
9716 deg
Mean anomaly: 243
2061 deg
Mean motion: 15
54301823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 273
Coasting Arc #18 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2017/221/12:27:05
697
Vector Time (MET): N/A
Weight (LBS) : 902191
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2695481
88 A = 6777417
67 meter
Y = 3249077
08 meter E =
0019648
Z = -5318921
16 I = 51
90033
XDOT = -5378
728871 Wp = 101
60615
YDOT = 5414
515891 meter/sec RA = 131
39598 deg
ZDOT = 579
645805 TA = 173
92819
MA = 173
90434
Ha = 222
803 n
mi
Hp = 212
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8843444
49 X = 2684785
72
Y = 10659701
71 feet Y = 3279159
92 meter
Z = -17450528
76 Z = -5305853
62
XDOT = -17646
748263 XDOT = -5441
691245
YDOT = 17764
159746 feet/sec YDOT = 5354
015250 meter/sec
ZDOT = 1901
725083 ZDOT = 553
365118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1006121
31 X = -306665
78
Y = -13886077
79 feet Y = -4232476
51 meter
Z = -17393138
55 Z = -5301428
63
XDOT = 23708
353469 XDOT = 7226
306137
YDOT = -3961
475320 feet/sec YDOT = -1207
457678 meter/sec
ZDOT = 1784
575997 ZDOT = 543
938764
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 17221
53399369
00016717 00000-0 10270-3 0 9175
2 25544 51
6422 132
3895 0005354 121
0961 239
0718 15
54142834 30044
Satellite: ISS
Catalog Number: 25544
Epoch time: 17221
53399369 = yrday
fracday
Element set: 917
Inclination: 51
6422 deg
RA of node: 132
3895 deg
Eccentricity:
0005354
Arg of perigee: 121
0961 deg
Mean anomaly: 239
0718 deg
Mean motion: 15
54142834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 303
Coasting Arc #19 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2017/222/12:27:05
697
Vector Time (MET): N/A
Weight (LBS) : 902191
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1425469
85 A = 6779171
45 meter
Y = -4489512
88 meter E =
0010305
Z = 4866728
63 I = 51
92655
XDOT = 5713
919213 Wp = 87
17572
YDOT = -4492
124538 meter/sec RA = 126
41758 deg
ZDOT = -2465
350078 TA = 26
93274
MA = 26
87928
Ha = 222
747 n
mi
Hp = 212
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4676738
35 X = -1398800
78
Y = -14729372
98 feet Y = -4505304
21 meter
Z = 15966957
45 Z = 4859869
15
XDOT = 18746
454111 XDOT = 5775
701935
YDOT = -14737
941396 feet/sec YDOT = -4427
882224 meter/sec
ZDOT = -8088
418891 ZDOT = -2437
443910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4509165
51 X = -1374393
65
Y = 14813574
00 feet Y = 4515177
35 meter
Z = 15937236
03 Z = 4857669
54
XDOT = -22770
832891 XDOT = -6940
549865
YDOT = 1654
611566 feet/sec YDOT = 504
325605 meter/sec
ZDOT = -7964
193431 ZDOT = -2427
486158
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 17222
56282277
00016717 00000-0 10270-3 0 9189
2 25544 51
6414 127
2617 0005217 124
9599 235
2044 15
54170895 30203
Satellite: ISS
Catalog Number: 25544
Epoch time: 17222
56282277 = yrday
fracday
Element set: 918
Inclination: 51
6414 deg
RA of node: 127
2617 deg
Eccentricity:
0005217
Arg of perigee: 124
9599 deg
Mean anomaly: 235
2044 deg
Mean motion: 15
54170895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 306
Coasting Arc #20 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2017/223/12:27:05
697
Vector Time (MET): N/A
Weight (LBS) : 902191
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 230807
88 A = 6782724
92 meter
Y = 5527560
64 meter E =
0011544
Z = -3937052
98 I = 51
95732
XDOT = -5665
687254 Wp = 116
73819
YDOT = 3141
483315 meter/sec RA = 121
44699 deg
ZDOT = 4082
614188 TA = 195
85166
MA = 195
88782
Ha = 222
648 n
mi
Hp = 213
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 757243
70 X = 188104
11
Y = 18135041
47 feet Y = 5529902
78 meter
Z = -12916840
47 Z = -3936035
71
XDOT = -18588
212774 XDOT = -5720
226152
YDOT = 10306
703788 feet/sec YDOT = 3077
820944 meter/sec
ZDOT = 13394
403504 ZDOT = 4054
959813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9423390
47 X = 2872249
41
Y = -15516065
46 feet Y = -4729296
75 meter
Z = -12913146
00 Z = -3935926
90
XDOT = 20117
669457 XDOT = 6131
865650
YDOT = 1184
372039 feet/sec YDOT = 360
996597 meter/sec
ZDOT = 13271
478550 ZDOT = 4045
146662
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 17223
52734800
00016717 00000-0 10270-3 0 9191
2 25544 51
6419 122
4533 0005155 129
4401 230
7208 15
54145333 30352
Satellite: ISS
Catalog Number: 25544
Epoch time: 17223
52734800 = yrday
fracday
Element set: 919
Inclination: 51
6419 deg
RA of node: 122
4533 deg
Eccentricity:
0005155
Arg of perigee: 129
4401 deg
Mean anomaly: 230
7208 deg
Mean motion: 15
54145333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 277
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list