[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 10th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
229/22:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 212
8
233/21:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 212
9
237/07:37:09
920 1
3 4
6 4
6
N/A 4
4 -0
5 219
7
000/00:14:15
840 0
4 -0
0 215
9
Coasting Arc #1 (Orbit 1342)
---------------------------------------
Vector Time (GMT): 2016/223/11:03:48
188
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5397424
35 A = 6779874
79 meter
Y = -247303
20 meter E =
0012371
Z = 4087361
11 I = 51
83946
XDOT = 3202
101831 Wp = 104
16335
YDOT = -5804
255788 meter/sec RA = 146
14976 deg
ZDOT = 3864
514481 TA = 305
94765
MA = 306
06235
Ha = 220
360 n
mi
Hp = 212
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17708085
13 X = -5414112
27
Y = -811362
22 feet Y = -307754
07 meter
Z = 13409977
41 Z = 4061101
46
XDOT = 10505
583434 XDOT = 3247
996505
YDOT = -19042
833951 feet/sec YDOT = -5768
191085 meter/sec
ZDOT = 12678
853284 ZDOT = 3880
180907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9399662
90 X = 2865017
25
Y = 15130855
38 feet Y = 4611884
72 meter
Z = 13295323
79 Z = 4052414
69
XDOT = -20494
938882 XDOT = -6246
857371
YDOT = 1493
229204 feet/sec YDOT = 455
136261 meter/sec
ZDOT = 12748
218143 ZDOT = 3885
656890
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 16223
51637333
00016717 00000-0 10270-3 0 9002
2 25544 51
6414 146
9466 0001697 113
5366 246
5966 15
54981114 13435
Satellite: ISS
Catalog Number: 25544
Epoch time: 16223
51637333 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 146
9466 deg
Eccentricity:
0001697
Arg of perigee: 113
5366 deg
Mean anomaly: 246
5966 deg
Mean motion: 15
54981114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1343
Checksum: 311
Coasting Arc #2 (Orbit 1357)
---------------------------------------
Vector Time (GMT): 2016/224/11:03:48
188
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4146650
72 A = 6776086
18 meter
Y = 1773928
75 meter E =
0014472
Z = -5070053
49 I = 51
85294
XDOT = -4741
052056 Wp = 80
01023
YDOT = 5713
293870 meter/sec RA = 141
16320 deg
ZDOT = -1880
699086 TA = 171
80670
MA = 171
78304
Ha = 220
279 n
mi
Hp = 212
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13604497
12 X = 4151133
96
Y = 5819976
21 feet Y = 1820324
43 meter
Z = -16634033
75 Z = -5049899
37
XDOT = -15554
632729 XDOT = -4795
451635
YDOT = 18744
402461 feet/sec YDOT = 5659
972087 meter/sec
ZDOT = -6170
272593 ZDOT = -1903
861887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3210804
20 X = -978653
12
Y = -14544987
58 feet Y = -4433312
21 meter
Z = -16546287
09 Z = -5043308
30
XDOT = 23206
500928 XDOT = 7073
341483
YDOT = 2004
647041 feet/sec YDOT = 611
016418 meter/sec
ZDOT = -6272
382392 ZDOT = -1911
822153
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 16224
48038414
00016717 00000-0 10270-3 0 9015
2 25544 51
6412 142
1347 0001757 109
8357 250
2986 15
54980674 13584
Satellite: ISS
Catalog Number: 25544
Epoch time: 16224
48038414 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 142
1347 deg
Eccentricity:
0001757
Arg of perigee: 109
8357 deg
Mean anomaly: 250
2986 deg
Mean motion: 15
54980674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1358
Checksum: 313
Coasting Arc #3 (Orbit 1373)
---------------------------------------
Vector Time (GMT): 2016/225/11:03:48
188
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2601433
51 A = 6774798
74 meter
Y = -3288417
98 meter E =
0003823
Z = 5318052
16 I = 51
87378
XDOT = 5720
016819 Wp = 91
45736
YDOT = -5102
431012 meter/sec RA = 136
17180 deg
ZDOT = -356
899950 TA = 1
93302
MA = 1
93154
Ha = 220
216 n
mi
Hp = 212
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8534886
83 X = -2590300
82
Y = -10788772
90 feet Y = -3317446
75 meter
Z = 17447677
68 Z = 5305442
17
XDOT = 18766
459379 XDOT = 5778
382021
YDOT = -16740
259226 feet/sec YDOT = -5038
139618 meter/sec
ZDOT = -1170
931593 ZDOT = -328
972073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3544527
54 X = -1080371
99
Y = 13363334
93 feet Y = 4073144
49 meter
Z = 17393130
09 Z = 5301426
05
XDOT = -23642
858311 XDOT = -7206
343213
YDOT = -4906
413277 feet/sec YDOT = -1495
474767 meter/sec
ZDOT = -1048
086655 ZDOT = -319
456812
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 16225
50865310
00016717 00000-0 10270-3 0 9023
2 25544 51
6414 137
0037 0001530 118
0297 242
1011 15
55014515 13749
Satellite: ISS
Catalog Number: 25544
Epoch time: 16225
50865310 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 137
0037 deg
Eccentricity:
0001530
Arg of perigee: 118
0297 deg
Mean anomaly: 242
1011 deg
Mean motion: 15
55014515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1374
Checksum: 256
Coasting Arc #4 (Orbit 1388)
---------------------------------------
Vector Time (GMT): 2016/226/11:03:48
188
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 965847
56 A = 6776899
33 meter
Y = 4657877
87 meter E =
0013203
Z = -4839264
35 I = 51
90433
XDOT = -6074
190757 Wp = 109
55426
YDOT = 3907
181374 meter/sec RA = 131
18130 deg
ZDOT = 2549
762239 TA = 185
46340
MA = 185
47782
Ha = 220
161 n
mi
Hp = 212
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3168791
20 X = 937197
01
Y = 15281751
55 feet Y = 4668518
51 meter
Z = -15876851
53 Z = -4834642
06
XDOT = -19928
447367 XDOT = -6129
815913
YDOT = 12818
836528 feet/sec YDOT = 3838
944649 meter/sec
ZDOT = 8365
361675 ZDOT = 2520
120627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10149222
85 X = 3093483
13
Y = -11882038
13 feet Y = -3621645
22 meter
Z = -15857428
16 Z = -4833344
10
XDOT = 21456
125116 XDOT = 6539
826935
YDOT = 7342
529312 feet/sec YDOT = 2238
002934 meter/sec
ZDOT = 8235
206851 ZDOT = 2510
091048
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 16226
47264915
00016717 00000-0 10270-3 0 9035
2 25544 51
6424 132
1914 0001621 118
9928 241
1388 15
55002164 13890
Satellite: ISS
Catalog Number: 25544
Epoch time: 16226
47264915 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 132
1914 deg
Eccentricity:
0001621
Arg of perigee: 118
9928 deg
Mean anomaly: 241
1388 deg
Mean motion: 15
55002164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1389
Checksum: 299
Coasting Arc #5 (Orbit 1404)
---------------------------------------
Vector Time (GMT): 2016/227/11:03:48
188
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 613620
65 A = 6781117
35 meter
Y = -5675312
00 meter E =
0013236
Z = 3648904
05 I = 51
93910
XDOT = 5885
819763 Wp = 90
02714
YDOT = -2203
536237 meter/sec RA = 126
20445 deg
ZDOT = -4403
319193 TA = 46
81238
MA = 46
70187
Ha = 220
169 n
mi
Hp = 212
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2013191
09 X = 659313
26
Y = -18619790
01 feet Y = -5668194
67 meter
Z = 11971469
97 Z = 3651995
69
XDOT = 19310
432292 XDOT = 5931
411947
YDOT = -7229
449598 feet/sec YDOT = -2137
462063 meter/sec
ZDOT = -14446
585280 ZDOT = -4374
617057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15793955
76 X = -4813997
72
Y = 10047593
54 feet Y = 3062506
51 meter
Z = 11985926
64 Z = 3653310
44
XDOT = -16986
177504 XDOT = -5177
386903
YDOT = -9563
614082 feet/sec YDOT = -2914
989572 meter/sec
ZDOT = -14320
800740 ZDOT = -4364
980065
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 16227
50090222
00016717 00000-0 10270-3 0 9049
2 25544 51
6425 127
0598 0001652 121
5158 238
6157 15
55003241 14052
Satellite: ISS
Catalog Number: 25544
Epoch time: 16227
50090222 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 127
0598 deg
Eccentricity:
0001652
Arg of perigee: 121
5158 deg
Mean anomaly: 238
6157 deg
Mean motion: 15
55003241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1405
Checksum: 275
Coasting Arc #6 (Orbit 1419)
---------------------------------------
Vector Time (GMT): 2016/228/11:03:48
188
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1955670
52 A = 6785048
00 meter
Y = 6190648
17 meter E =
0007057
Z = -1967446
86 I = 51
97116
XDOT = -5216
656117 Wp = 53
03109
YDOT = 131
089697 meter/sec RA = 121
24197 deg
ZDOT = 5615
893304 TA = 285
36497
MA = 285
44294
Ha = 220
065 n
mi
Hp = 212
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6416241
87 X = -2015193
72
Y = 20310525
50 feet Y = 6168445
76 meter
Z = -6454878
14 Z = -1977091
36
XDOT = -17115
013507 XDOT = -5245
013408
YDOT = 430
084308 feet/sec YDOT = 72
594944 meter/sec
ZDOT = 18424
846798 ZDOT = 5590
483653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19742346
35 X = 6017467
17
Y = -7960274
24 feet Y = -2426291
59 meter
Z = -6498065
26 Z = -1980610
29
XDOT = 10688
404192 XDOT = 3257
825598
YDOT = 11606
491579 feet/sec YDOT = 3537
658633 meter/sec
ZDOT = 18313
783103 ZDOT = 5582
041090
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 16228
46488223
00016717 00000-0 10270-3 0 9058
2 25544 51
6429 122
2484 0001576 127
1610 232
9687 15
55027198 14206
Satellite: ISS
Catalog Number: 25544
Epoch time: 16228
46488223 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 122
2484 deg
Eccentricity:
0001576
Arg of perigee: 127
1610 deg
Mean anomaly: 232
9687 deg
Mean motion: 15
55027198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1420
Checksum: 308
Coasting Arc #7 (Orbit 1435)
---------------------------------------
Vector Time (GMT): 2016/229/11:03:48
188
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3028091
98 A = 6786761
94 meter
Y = -6066402
05 meter E =
0013667
Z = -35681
99 I = 51
99341
XDOT = 4215
398597 Wp = 134
88097
YDOT = 2131
350567 meter/sec RA = 116
29080 deg
ZDOT = -6044
218748 TA = 45
50171
MA = 45
39008
Ha = 220
075 n
mi
Hp = 212
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9934684
97 X = 3095876
29
Y = -19902893
87 feet Y = -6032160
90 meter
Z = -117066
90 Z = -20807
90
XDOT = 13830
047892 XDOT = 4220
611632
YDOT = 6992
619970 feet/sec YDOT = 2178
519092 meter/sec
ZDOT = -19830
114001 ZDOT = -6023
729149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21598828
13 X = -6583322
81
Y = 5322111
72 feet Y = 1622179
65 meter
Z = -51035
25 Z = -15555
55
XDOT = -3326
622491 XDOT = -1013
954535
YDOT = -13587
348156 feet/sec YDOT = -4141
423718 meter/sec
ZDOT = -19740
924744 ZDOT = -6017
033862
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 16229
49312004
00016717 00000-0 10270-3 0 9066
2 25544 51
6437 117
1164 0001580 135
4553 224
6727 15
55012447 14367
Satellite: ISS
Catalog Number: 25544
Epoch time: 16229
49312004 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 117
1164 deg
Eccentricity:
0001580
Arg of perigee: 135
4553 deg
Mean anomaly: 224
6727 deg
Mean motion: 15
55012447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1436
Checksum: 287
Coasting Arc #8 (Orbit 1442)
---------------------------------------
Vector Time (GMT): 2016/229/22:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1450640
32 A = 6778783
09 meter
Y = 5038129
96 meter E =
0009970
Z = -4307560
51 I = 51
97410
XDOT = -5057
241486 Wp = 116
35728
YDOT = 4509
853940 meter/sec RA = 113
91658 deg
ZDOT = 3573
705332 TA = 189
94661
MA = 189
96636
Ha = 219
973 n
mi
Hp = 212
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4759318
64 X = 1415118
71
Y = 16529297
75 feet Y = 5054153
31 meter
Z = -14132416
37 Z = -4300600
15
XDOT = -16591
999626 XDOT = -5124
655116
YDOT = 14796
108728 feet/sec YDOT = 4452
923602 meter/sec
ZDOT = 11724
755027 ZDOT = 3548
975226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11694490
21 X = -3564480
62
Y = 12646839
90 feet Y = 3854756
80 meter
Z = -14102848
29 Z = -4298548
16
XDOT = -20332
350017 XDOT = -6197
300285
YDOT = -5855
658244 feet/sec YDOT = -1784
804633 meter/sec
ZDOT = 11615
904726 ZDOT = 3540
527761
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 16229
94296928
00016717 00000-0 10270-3 0 9073
2 25544 51
6438 114
8683 0001793 144
6386 215
4887 15
55063554 14438
Satellite: ISS
Catalog Number: 25544
Epoch time: 16229
94296928 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 114
8683 deg
Eccentricity:
0001793
Arg of perigee: 144
6386 deg
Mean anomaly: 215
4887 deg
Mean motion: 15
55063554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1443
Checksum: 345
Coasting Arc #9 (Orbit 1458)
---------------------------------------
Vector Time (GMT): 2016/230/22:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -202453
40 A = 6783307
86 meter
Y = -6163875
05 meter E =
0014696
Z = 2807235
37 I = 52
00075
XDOT = 5110
926868 Wp = 104
91076
YDOT = -2517
657429 meter/sec RA = 108
95037 deg
ZDOT = -5140
779835 TA = 43
37163
MA = 43
25607
Ha = 220
003 n
mi
Hp = 212
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -664217
18 X = -147148
39
Y = -20222687
16 feet Y = -6165829
69 meter
Z = 9210089
79 Z = 2806386
46
XDOT = 16768
132770 XDOT = 5163
671264
YDOT = -8260
030936 feet/sec YDOT = -2460
208895 meter/sec
ZDOT = -16866
075574 ZDOT = -5115
824564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16791155
81 X = 5117944
29
Y = -11291783
28 feet Y = -3441735
55 meter
Z = 9207428
04 Z = 2806424
07
XDOT = 15103
624959 XDOT = 4603
584887
YDOT = 8746
018884 feet/sec YDOT = 2665
786556 meter/sec
ZDOT = -16756
568748 ZDOT = -5107
402154
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 16230
97119548
00016717 00000-0 10270-3 0 9081
2 25544 51
6433 109
7363 0001744 144
7723 215
3546 15
55050441 14592
Satellite: ISS
Catalog Number: 25544
Epoch time: 16230
97119548 = yrday
fracday
Element set: 908
Inclination: 51
6433 deg
RA of node: 109
7363 deg
Eccentricity:
0001744
Arg of perigee: 144
7723 deg
Mean anomaly: 215
3546 deg
Mean motion: 15
55050441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1459
Checksum: 307
Coasting Arc #10 (Orbit 1473)
---------------------------------------
Vector Time (GMT): 2016/231/22:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -909476
16 A = 6786358
15 meter
Y = 6656751
22 meter E =
0009503
Z = -931965
62 I = 52
01967
XDOT = -4830
946741 Wp = 47
82292
YDOT = 167
020988 meter/sec RA = 103
99711 deg
ZDOT = 5952
236948 TA = 302
13829
MA = 302
23047
Ha = 219
943 n
mi
Hp = 212
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2983845
68 X = -979319
05
Y = 21839734
96 feet Y = 6646190
28 meter
Z = -3057630
00 Z = -936553
54
XDOT = -15849
562799 XDOT = -4861
368194
YDOT = 547
969120 feet/sec YDOT = 112
828337 meter/sec
ZDOT = 19528
336445 ZDOT = 5928
695992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19954004
68 X = -6081980
63
Y = 9358686
09 feet Y = 2852527
52 meter
Z = -3078823
00 Z = -938425
25
XDOT = -8446
521727 XDOT = -2574
499822
YDOT = -11666
683018 feet/sec YDOT = -3556
004984 meter/sec
ZDOT = 19425
406163 ZDOT = 5920
863799
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 16231
93515132
00016717 00000-0 10270-3 0 9098
2 25544 51
6427 104
9248 0001546 148
8514 211
2731 15
55020905 14747
Satellite: ISS
Catalog Number: 25544
Epoch time: 16231
93515132 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 104
9248 deg
Eccentricity:
0001546
Arg of perigee: 148
8514 deg
Mean anomaly: 211
2731 deg
Mean motion: 15
55020905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1474
Checksum: 289
Coasting Arc #11 (Orbit 1489)
---------------------------------------
Vector Time (GMT): 2016/232/22:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1904909
62 A = 6786081
59 meter
Y = -6411262
49 meter E =
0011081
Z = -1118192
72 I = 52
02558
XDOT = 4306
837013 Wp = 143
51083
YDOT = 2304
235042 meter/sec RA = 99
04917 deg
ZDOT = -5913
198622 TA = 48
56384
MA = 48
46869
Ha = 219
892 n
mi
Hp = 212
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6249703
47 X = 1981892
01
Y = -21034325
77 feet Y = -6389530
16 meter
Z = -3668611
28 Z = -1108751
88
XDOT = 14130
042693 XDOT = 4309
473666
YDOT = 7559
826252 feet/sec YDOT = 2352
411305 meter/sec
ZDOT = -19400
257945 ZDOT = -5892
271200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20964550
01 X = 6389994
84
Y = -6503721
62 feet Y = -1982334
35 meter
Z = -3626239
22 Z = -1105277
71
XDOT = 1186
846774 XDOT = 361
750897
YDOT = 14520
403073 feet/sec YDOT = 4425
818857 meter/sec
ZDOT = -19309
174207 ZDOT = -5885
436298
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 16232
96336466
00016717 00000-0 10270-3 0 9105
2 25544 51
6423 99
7921 0001654 153
0025 207
1214 15
55067147 14904
Satellite: ISS
Catalog Number: 25544
Epoch time: 16232
96336466 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 99
7921 deg
Eccentricity:
0001654
Arg of perigee: 153
0025 deg
Mean anomaly: 207
1214 deg
Mean motion: 15
55067147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1490
Checksum: 293
Coasting Arc #12 (Orbit 1504)
---------------------------------------
Vector Time (GMT): 2016/233/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3855079
65 A = 6775381
20 meter
Y = -2169589
38 meter E =
0004957
Z = 5128258
95 I = 51
99533
XDOT = 1856
609048 Wp = 72
66377
YDOT = -7255
346321 meter/sec RA = 94
31243 deg
ZDOT = -1671
049405 TA = 33
39599
MA = 33
36473
Ha = 219
866 n
mi
Hp = 212
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12647899
11 X = -3855442
78
Y = -7118075
41 feet Y = -2212701
09 meter
Z = 16824996
54 Z = 5109531
47
XDOT = 6091
237034 XDOT = 1945
719314
YDOT = -23803
629661 feet/sec YDOT = -7234
086361 meter/sec
ZDOT = -5482
445553 ZDOT = -1661
813580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3256034
43 X = 992439
30
Y = -14239734
41 feet Y = -4340271
05 meter
Z = 16743508
05 Z = 5103421
25
XDOT = 23528
785144 XDOT = 7171
573712
YDOT = -1028
132744 feet/sec YDOT = -313
374860 meter/sec
ZDOT = -5440
814410 ZDOT = -1658
360232
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 16233
92730642
00016717 00000-0 10270-3 0 9117
2 25544 51
6433 94
9789 0001545 158
1861 201
9358 15
55116044 15056
Satellite: ISS
Catalog Number: 25544
Epoch time: 16233
92730642 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 94
9789 deg
Eccentricity:
0001545
Arg of perigee: 158
1861 deg
Mean anomaly: 201
9358 deg
Mean motion: 15
55116044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1505
Checksum: 307
Coasting Arc #13 (Orbit 1519)
---------------------------------------
Vector Time (GMT): 2016/234/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3340513
86 A = 6779017
30 meter
Y = 4136531
26 meter E =
0009076
Z = -4215125
45 I = 52
00766
XDOT = -2832
163241 Wp = 117
75496
YDOT = 6071
654617 meter/sec RA = 89
33541 deg
ZDOT = 3715
924369 TA = 190
22031
MA = 190
23878
Ha = 219
758 n
mi
Hp = 212
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10959691
15 X = 3314484
93
Y = 13571296
77 feet Y = 4173741
25 meter
Z = -13829151
73 Z = -4198961
76
XDOT = -9291
874149 XDOT = -2917
897731
YDOT = 19920
126696 feet/sec YDOT = 6039
504395 meter/sec
ZDOT = 12191
352917 ZDOT = 3701
957836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9680118
10 X = -2950500
00
Y = 14578051
79 feet Y = 4443390
18 meter
Z = -13759218
12 Z = -4193809
68
XDOT = -20741
500710 XDOT = -6322
009416
YDOT = -2331
007906 feet/sec YDOT = -710
491210 meter/sec
ZDOT = 12129
236561 ZDOT = 3696
991304
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 16234
89124596
00016717 00000-0 10270-3 0 9120
2 25544 51
6421 90
1678 0001678 158
5610 201
5614 15
55112046 15207
Satellite: ISS
Catalog Number: 25544
Epoch time: 16234
89124596 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 90
1678 deg
Eccentricity:
0001678
Arg of perigee: 158
5610 deg
Mean anomaly: 201
5614 deg
Mean motion: 15
55112046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1520
Checksum: 291
Coasting Arc #14 (Orbit 1535)
---------------------------------------
Vector Time (GMT): 2016/235/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2644046
65 A = 6783509
49 meter
Y = -5642993
46 meter E =
0014392
Z = 2661573
67 I = 52
02187
XDOT = 3696
384823 Wp = 107
60002
YDOT = -4213
056124 meter/sec RA = 84
37118 deg
ZDOT = -5241
378996 TA = 42
51293
MA = 42
40157
Ha = 219
741 n
mi
Hp = 212
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8674693
73 X = -2593677
47
Y = -18513758
06 feet Y = -5672279
14 meter
Z = 8732197
07 Z = 2648852
36
XDOT = 12127
246794 XDOT = 3768
681788
YDOT = -13822
362611 feet/sec YDOT = -4171
316809 meter/sec
ZDOT = -17196
125316 ZDOT = -5223
247084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14848066
22 X = 4525690
58
Y = -14088833
89 feet Y = -4294276
57 meter
Z = 8677586
29 Z = 2644928
30
XDOT = 15933
448618 XDOT = 4856
515139
YDOT = 6211
340735 feet/sec YDOT = 1893
216656 meter/sec
ZDOT = -17116
116951 ZDOT = -5216
992447
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 16235
91944103
00016717 00000-0 10270-3 0 9139
2 25544 51
6426 85
0348 0001504 162
5616 197
5589 15
55109845 15363
Satellite: ISS
Catalog Number: 25544
Epoch time: 16235
91944103 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 85
0348 deg
Eccentricity:
0001504
Arg of perigee: 162
5616 deg
Mean anomaly: 197
5589 deg
Mean motion: 15
55109845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1536
Checksum: 316
Coasting Arc #15 (Orbit 1550)
---------------------------------------
Vector Time (GMT): 2016/236/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1806465
19 A = 6786384
55 meter
Y = 6494640
59 meter E =
0009820
Z = -747149
83 I = 52
02700
XDOT = -4397
356877 Wp = 46
04303
YDOT = 1905
417319 meter/sec RA = 79
41903 deg
ZDOT = 5986
298810 TA = 305
92403
MA = 306
01511
Ha = 219
723 n
mi
Hp = 213
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5926723
06 X = 1737335
53
Y = 21307875
96 feet Y = 6514455
13 meter
Z = -2451278
97 Z = -738542
77
XDOT = -14427
023876 XDOT = -4447
415675
YDOT = 6251
369156 feet/sec YDOT = 1855
963570 meter/sec
ZDOT = 19640
087960 ZDOT = 5964
815936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18160804
19 X = -5535413
12
Y = 12629894
60 feet Y = 3849591
88 meter
Z = -2414818
03 Z = -736036
53
XDOT = -9777
368333 XDOT = -2980
141868
YDOT = -10357
184503 feet/sec YDOT = -3156
869837 meter/sec
ZDOT = 19545
834751 ZDOT = 5957
570432
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 16236
88336805
00016717 00000-0 10270-3 0 9141
2 25544 51
6427 80
2227 0001258 163
3508 196
7687 15
55061536 15513
Satellite: ISS
Catalog Number: 25544
Epoch time: 16236
88336805 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 80
2227 deg
Eccentricity:
0001258
Arg of perigee: 163
3508 deg
Mean anomaly: 196
7687 deg
Mean motion: 15
55061536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1551
Checksum: 318
Coasting Arc #16 (Orbit 1557)
---------------------------------------
Vector Time (GMT): 2016/237/07:44:17
840
Vector Time (MET): N/A
Weight (LBS) : 929483
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4283560
29 A = 6780120
16 meter
Y = 2470266
12 meter E =
0007725
Z = -4646470
87 I = 51
99558
XDOT = -802
350404 Wp = 124
76693
YDOT = 7009
823520 meter/sec RA = 77
21656 deg
ZDOT = 2986
272828 TA = 174
88439
MA = 174
87649
Ha = 219
746 n
mi
Hp = 215
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14053675
50 X = 4278189
26
Y = 8104547
63 feet Y = 2518137
50 meter
Z = -15244327
02 Z = -4625675
65
XDOT = -2632
383214 XDOT = -895
182372
YDOT = 22998
108663 feet/sec YDOT = 7000
332191 meter/sec
ZDOT = 9797
483033 ZDOT = 2982
149410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8533542
74 X = 2601023
83
Y = -13896689
41 feet Y = -4235710
93 meter
Z = -15153866
35 Z = -4618898
46
XDOT = 21892
096660 XDOT = 6672
711062
YDOT = 2777
721113 feet/sec YDOT = 846
649395 meter/sec
ZDOT = 9778
193845 ZDOT = 2980
393484
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 16237
33320185
00016717 00000-0 10270-3 0 9157
2 25544 51
6434 77
9776 0003445 254
6141 105
4632 15
54188549 15587
Satellite: ISS
Catalog Number: 25544
Epoch time: 16237
33320185 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 77
9776 deg
Eccentricity:
0003445
Arg of perigee: 254
6141 deg
Mean anomaly: 105
4632 deg
Mean motion: 15
54188549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1558
Checksum: 318
Coasting Arc #17 (Orbit 1573)
---------------------------------------
Vector Time (GMT): 2016/238/07:44:17
840
Vector Time (MET): N/A
Weight (LBS) : 929483
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4183168
28 A = 6783935
49 meter
Y = -3989098
34 meter E =
0008807
Z = 3543144
70 I = 51
99982
XDOT = 1812
638160 Wp = 92
23274
YDOT = -5924
744677 meter/sec RA = 72
25371 deg
ZDOT = -4521
060368 TA = 46
22329
MA = 46
15045
Ha = 219
820 n
mi
Hp = 215
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13724305
37 X = -4155461
26
Y = -13087592
99 feet Y = -4035722
29 meter
Z = 11624490
49 Z = 3522891
44
XDOT = 5946
975589 XDOT = 1900
716698
YDOT = -19438
138705 feet/sec YDOT = -5903
982215 meter/sec
ZDOT = -14832
875224 ZDOT = -4512
040944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13271399
03 X = -4045122
42
Y = 13621505
66 feet Y = 4151834
92 meter
Z = 11536679
71 Z = 3516379
98
XDOT = -18362
940348 XDOT = -5597
024218
YDOT = -5336
517671 feet/sec YDOT = -1626
570586 meter/sec
ZDOT = -14792
365355 ZDOT = -4508
712960
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 16238
36199708
00016717 00000-0 10270-3 0 9167
2 25544 51
6430 72
8500 0003468 257
3657 102
7108 15
54179570 15749
Satellite: ISS
Catalog Number: 25544
Epoch time: 16238
36199708 = yrday
fracday
Element set: 916
Inclination: 51
6430 deg
RA of node: 72
8500 deg
Eccentricity:
0003468
Arg of perigee: 257
3657 deg
Mean anomaly: 102
7108 deg
Mean motion: 15
54179570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1574
Checksum: 320
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