[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 22nd 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 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
217/02:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 212
7
Coasting Arc #1 (Orbit 1047)
---------------------------------------
Vector Time (GMT): 2016/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 65021
58 A = 6781780
48 meter
Y = -5758015
45 meter E =
0013903
Z = 3570225
54 I = 51
31654
XDOT = 5611
910116 Wp = 89
58174
YDOT = 2810
282986 meter/sec RA = 240
88330 deg
ZDOT = 4415
361501 TA = 312
87543
MA = 312
99209
Ha = 220
521 n
mi
Hp = 212
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 213325
41 X = 112062
07
Y = -18891126
82 feet Y = -5757025
49 meter
Z = 11713338
39 Z = 3570655
37
XDOT = 18411
778597 XDOT = 5558
620254
YDOT = 9220
088536 feet/sec YDOT = 2872
740937 meter/sec
ZDOT = 14486
094162 ZDOT = 4442
492901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16457724
26 X = -5016314
36
Y = 9273400
38 feet Y = 2826532
44 meter
Z = 11716220
97 Z = 3571104
15
XDOT = -431
436121 XDOT = -131
501730
YDOT = -19277
945340 feet/sec YDOT = -5875
917740 meter/sec
ZDOT = 14603
856530 ZDOT = 4451
255470
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 16204
55673918
00016717 00000-0 10270-3 0 9004
2 25544 51
6408 241
5667 0002010 67
6285 292
5081 15
54862507 10487
Satellite: ISS
Catalog Number: 25544
Epoch time: 16204
55673918 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 241
5667 deg
Eccentricity:
0002010
Arg of perigee: 67
6285 deg
Mean anomaly: 292
5081 deg
Mean motion: 15
54862507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1048
Checksum: 305
Coasting Arc #2 (Orbit 1062)
---------------------------------------
Vector Time (GMT): 2016/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1475678
75 A = 6777559
79 meter
Y = 4609794
67 meter E =
0013065
Z = -4756732
95 I = 51
31975
XDOT = -5603
355053 Wp = 71
57772
YDOT = -4508
771455 meter/sec RA = 235
86570 deg
ZDOT = -2633
081474 TA = 172
30337
MA = 172
28330
Ha = 220
495 n
mi
Hp = 212
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4841465
71 X = -1504011
22
Y = 15123998
26 feet Y = 4593134
38 meter
Z = -15606079
25 Z = -4763969
97
XDOT = -18383
710803 XDOT = -5539
730241
YDOT = -14792
557266 feet/sec YDOT = -4571
076083 meter/sec
ZDOT = -8638
718748 ZDOT = -2660
146280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15416845
52 X = 4699054
51
Y = -3672255
76 feet Y = -1119303
56 meter
Z = -15638421
75 Z = -4766590
95
XDOT = -3588
979079 XDOT = -1093
920823
YDOT = 22193
412421 feet/sec YDOT = 6764
552106 meter/sec
ZDOT = -8755
912163 ZDOT = -2668
802027
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 16205
52080819
00016717 00000-0 10270-3 0 9015
2 25544 51
6415 236
7557 0001884 71
4460 288
6898 15
54868746 10635
Satellite: ISS
Catalog Number: 25544
Epoch time: 16205
52080819 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 236
7557 deg
Eccentricity:
0001884
Arg of perigee: 71
4460 deg
Mean anomaly: 288
6898 deg
Mean motion: 15
54868746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1063
Checksum: 334
Coasting Arc #3 (Orbit 1078)
---------------------------------------
Vector Time (GMT): 2016/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2908094
17 A = 6775225
51 meter
Y = -3106117
52 meter E =
0004558
Z = 5268557
25 I = 51
32998
XDOT = 5142
317159 Wp = 96
60319
YDOT = 5673
254541 meter/sec RA = 230
83840 deg
ZDOT = 505
404686 TA = 348
55257
MA = 348
56293
Ha = 220
412 n
mi
Hp = 212
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9540991
36 X = 2917019
42
Y = -10190674
28 feet Y = -3073547
47 meter
Z = 17285292
81 Z = 5282705
45
XDOT = 16871
119287 XDOT = 5076
040207
YDOT = 18613
039834 feet/sec YDOT = 5730
388779 meter/sec
ZDOT = 1658
151858 ZDOT = 530
223543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13627837
71 X = -4153764
93
Y = -2647270
68 feet Y = -806888
10 meter
Z = 17347498
47 Z = 5287517
53
XDOT = 6746
462497 XDOT = 2056
321769
YDOT = -23142
441762 feet/sec YDOT = -7053
816249 meter/sec
ZDOT = 1765
373027 ZDOT = 538
085699
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 16206
54914351
00016717 00000-0 10270-3 0 9026
2 25544 51
6404 231
6237 0002020 73
7837 286
3538 15
54889183 10799
Satellite: ISS
Catalog Number: 25544
Epoch time: 16206
54914351 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 231
6237 deg
Eccentricity:
0002020
Arg of perigee: 73
7837 deg
Mean anomaly: 286
3538 deg
Mean motion: 15
54889183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1079
Checksum: 309
Coasting Arc #4 (Orbit 1093)
---------------------------------------
Vector Time (GMT): 2016/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4255666
59 A = 6776111
61 meter
Y = 1452375
18 meter E =
0015076
Z = -5082624
54 I = 51
35582
XDOT = -4145
214448 Wp = 99
36042
YDOT = -6211
571960 meter/sec RA = 225
81039 deg
ZDOT = 1697
713587 TA = 187
11795
MA = 187
13938
Ha = 220
481 n
mi
Hp = 212
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13962160
73 X = -4246902
20
Y = 4765010
44 feet Y = 1404834
57 meter
Z = -16675277
37 Z = -5103275
97
XDOT = -13599
784935 XDOT = -4083
693674
YDOT = -20379
173096 feet/sec YDOT = -6257
582563 meter/sec
ZDOT = 5569
926466 ZDOT = 1677
726706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11504847
58 X = 3506677
54
Y = 9070106
36 feet Y = 2764568
42 meter
Z = -16765553
53 Z = -5110140
72
XDOT = -9091
883468 XDOT = -2771
206081
YDOT = 21657
492728 feet/sec YDOT = 6601
203783 meter/sec
ZDOT = 5483
844424 ZDOT = 1671
475780
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 16207
51320209
00016717 00000-0 10270-3 0 9038
2 25544 51
6423 226
8128 0001869 72
5108 287
6249 15
54873917 10941
Satellite: ISS
Catalog Number: 25544
Epoch time: 16207
51320209 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 226
8128 deg
Eccentricity:
0001869
Arg of perigee: 72
5108 deg
Mean anomaly: 287
6249 deg
Mean motion: 15
54873917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1094
Checksum: 313
Coasting Arc #5 (Orbit 1109)
---------------------------------------
Vector Time (GMT): 2016/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5333086
24 A = 6779489
18 meter
Y = 200420
74 meter E =
0012195
Z = 4172773
44 I = 51
38907
XDOT = 2660
374353 Wp = 74
93222
YDOT = 6182
631879 meter/sec RA = 220
79111 deg
ZDOT = -3684
962036 TA = 53
04407
MA = 52
93246
Ha = 220
353 n
mi
Hp = 212
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17497002
09 X = 5310179
34
Y = 657548
35 feet Y = 259930
68 meter
Z = 13690201
56 Z = 4198624
40
XDOT = 8728
262312 XDOT = 2608
940698
YDOT = 20284
225324 feet/sec YDOT = 6212
094476 meter/sec
ZDOT = -12089
770460 ZDOT = -3672
163464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9126247
73 X = -2781680
31
Y = -14838844
66 feet Y = -4522879
85 meter
Z = 13802875
14 Z = 4207116
34
XDOT = 10887
079581 XDOT = 3318
381856
YDOT = -17927
325571 feet/sec YDOT = -5464
248834 meter/sec
ZDOT = -12035
008939 ZDOT = -3668
270725
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 16208
54152585
00016717 00000-0 10270-3 0 9043
2 25544 51
6405 221
6809 0002042 75
1654 284
9726 15
54926265 11103
Satellite: ISS
Catalog Number: 25544
Epoch time: 16208
54152585 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 221
6809 deg
Eccentricity:
0002042
Arg of perigee: 75
1654 deg
Mean anomaly: 284
9726 deg
Mean motion: 15
54926265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1110
Checksum: 300
Coasting Arc #6 (Orbit 1124)
---------------------------------------
Vector Time (GMT): 2016/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5993584
87 A = 6783803
49 meter
Y = -1649700
62 meter E =
0006710
Z = -2716937
59 I = 51
42851
XDOT = -780
181405 Wp = 65
11031
YDOT = -5624
136988 meter/sec RA = 215
78731 deg
ZDOT = 5148
787156 TA = 264
07730
MA = 264
15379
Ha = 220
447 n
mi
Hp = 212
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19663992
36 X = -5961494
42
Y = -5412403
62 feet Y = -1716545
35 meter
Z = -8913837
23 Z = -2745974
87
XDOT = -2559
650279 XDOT = -742
243332
YDOT = -18451
893006 feet/sec YDOT = -5632
649592 meter/sec
ZDOT = 16892
346312 ZDOT = 5145
089161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6726073
40 X = 2050107
17
Y = 19195270
40 feet Y = 5850718
42 meter
Z = -9040173
32 Z = -2755444
83
XDOT = -12239
764867 XDOT = -3730
680331
YDOT = 12217
823980 feet/sec YDOT = 3723
992749 meter/sec
ZDOT = 16877
161791 ZDOT = 5144
158914
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 16209
50557597
00016717 00000-0 10270-3 0 9053
2 25544 51
6406 216
8705 0002026 80
3441 279
7941 15
54920077 11251
Satellite: ISS
Catalog Number: 25544
Epoch time: 16209
50557597 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 216
8705 deg
Eccentricity:
0002026
Arg of perigee: 80
3441 deg
Mean anomaly: 279
7941 deg
Mean motion: 15
54920077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1125
Checksum: 308
Coasting Arc #7 (Orbit 1140)
---------------------------------------
Vector Time (GMT): 2016/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6094315
88 A = 6786690
11 meter
Y = 2849057
00 meter E =
0014970
Z = 844802
88 I = 51
46395
XDOT = -1357
997286 Wp = 120
25860
YDOT = 4682
128854 meter/sec RA = 210
79597 deg
ZDOT = -5922
681179 TA = 50
57580
MA = 50
44338
Ha = 220
488 n
mi
Hp = 212
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19994474
68 X = 6057900
41
Y = 9347299
87 feet Y = 2917004
05 meter
Z = 2771662
98 Z = 874319
05
XDOT = -4455
371673 XDOT = -1381
483477
YDOT = 15361
315139 feet/sec YDOT = 4666
811857 meter/sec
ZDOT = -19431
368697 ZDOT = -5929
334708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4077665
35 X = -1242872
40
Y = -21674786
05 feet Y = -6606474
79 meter
Z = 2899903
99 Z = 883890
74
XDOT = 13416
293477 XDOT = 4089
286252
YDOT = -5157
580608 feet/sec YDOT = -1572
030569 meter/sec
ZDOT = -19461
162794 ZDOT = -5931
762420
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 16210
53388975
00016717 00000-0 10270-3 0 9061
2 25544 51
6398 211
7377 0002067 80
3383 279
8003 15
54923549 11415
Satellite: ISS
Catalog Number: 25544
Epoch time: 16210
53388975 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 211
7377 deg
Eccentricity:
0002067
Arg of perigee: 80
3383 deg
Mean anomaly: 279
8003 deg
Mean motion: 15
54923549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1141
Checksum: 320
Coasting Arc #8 (Orbit 1156)
---------------------------------------
Vector Time (GMT): 2016/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5585353
95 A = 6786401
47 meter
Y = -3679833
04 meter E =
0015297
Z = 1106817
30 I = 51
49058
XDOT = 3482
243357 Wp = 60
86290
YDOT = -3503
754922 meter/sec RA = 205
81213 deg
ZDOT = 5869
537871 TA = 311
17947
MA = 311
31131
Ha = 220
383 n
mi
Hp = 212
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18324652
08 X = -5549166
41
Y = -12072943
06 feet Y = -3742089
94 meter
Z = 3631290
36 Z = 1079772
95
XDOT = 11424
682930 XDOT = 3492
653022
YDOT = -11495
258930 feet/sec YDOT = -3464
756370 meter/sec
ZDOT = 19257
014013 ZDOT = 5886
478603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1291924
95 X = 393778
73
Y = 21925286
66 feet Y = 6682827
37 meter
Z = 3513948
29 Z = 1071051
44
XDOT = -14370
195392 XDOT = -4380
035556
YDOT = -2280
861070 feet/sec YDOT = -695
206454 meter/sec
ZDOT = 19331
480447 ZDOT = 5892
235240
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 16211
56219533
00016717 00000-0 10270-3 0 9079
2 25544 51
6389 206
6064 0001928 88
5728 271
5646 15
54970062 11570
Satellite: ISS
Catalog Number: 25544
Epoch time: 16211
56219533 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 206
6064 deg
Eccentricity:
0001928
Arg of perigee: 88
5728 deg
Mean anomaly: 271
5646 deg
Mean motion: 15
54970062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1157
Checksum: 323
Coasting Arc #9 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2016/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4440170
65 A = 6783392
22 meter
Y = 4197649
92 meter E =
0006415
Z = -2949030
76 I = 51
50856
XDOT = -5385
256222 Wp = 106
20064
YDOT = 2197
762310 meter/sec RA = 200
82326 deg
ZDOT = -4990
736142 TA = 107
53294
MA = 107
46283
Ha = 220
502 n
mi
Hp = 212
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14567489
01 X = 4407226
39
Y = 13771817
33 feet Y = 4247118
90 meter
Z = -9675297
77 Z = -2927541
52
XDOT = -17668
163459 XDOT = -5385
189407
YDOT = 7210
506266 feet/sec YDOT = 2137
541529 meter/sec
ZDOT = -16373
806241 ZDOT = -5016
895679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1948623
65 X = 593940
49
Y = -19996734
16 feet Y = -6095004
57 meter
Z = -9582252
59 Z = -2920670
59
XDOT = 14985
759127 XDOT = 4567
659382
YDOT = 9344
226132 feet/sec YDOT = 2848
120125 meter/sec
ZDOT = -16488
278613 ZDOT = -5025
627321
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 16212
52623142
00016717 00000-0 10270-3 0 9082
2 25544 51
6380 201
7943 0002011 85
7549 274
3834 15
54925293 11720
Satellite: ISS
Catalog Number: 25544
Epoch time: 16212
52623142 = yrday
fracday
Element set: 908
Inclination: 51
6380 deg
RA of node: 201
7943 deg
Eccentricity:
0002011
Arg of perigee: 85
7549 deg
Mean anomaly: 274
3834 deg
Mean motion: 15
54925293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1172
Checksum: 296
Coasting Arc #10 (Orbit 1187)
---------------------------------------
Vector Time (GMT): 2016/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2789267
68 A = 6778937
40 meter
Y = -4382132
95 meter E =
0011392
Z = 4347922
00 I = 51
52481
XDOT = 6801
122710 Wp = 105
70188
YDOT = -910
007968 meter/sec RA = 195
82488 deg
ZDOT = 3435
348609 TA = 309
36906
MA = 309
46993
Ha = 220
406 n
mi
Hp = 212
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9151140
70 X = -2761178
21
Y = -14377076
62 feet Y = -4413167
65 meter
Z = 14264835
97 Z = 4334440
60
XDOT = 22313
394717 XDOT = 6794
106037
YDOT = -2985
590447 feet/sec YDOT = -833
992746 meter/sec
ZDOT = 11270
828770 ZDOT = 3468
369061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5443507
28 X = -1659181
02
Y = 16200804
09 feet Y = 4938005
09 meter
Z = 14206738
85 Z = 4330214
00
XDOT = -15050
041733 XDOT = -4587
252720
YDOT = -15097
269281 feet/sec YDOT = -4601
647677 meter/sec
ZDOT = 11415
037864 ZDOT = 3479
303541
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 16213
55452702
00016717 00000-0 10270-3 0 9099
2 25544 51
6383 196
6623 0001802 89
4110 270
7250 15
54962004 11882
Satellite: ISS
Catalog Number: 25544
Epoch time: 16213
55452702 = yrday
fracday
Element set: 909
Inclination: 51
6383 deg
RA of node: 196
6623 deg
Eccentricity:
0001802
Arg of perigee: 89
4110 deg
Mean anomaly: 270
7250 deg
Mean motion: 15
54962004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1188
Checksum: 295
Coasting Arc #11 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2016/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 760988
04 A = 6775665
47 meter
Y = 4327099
12 meter E =
0015770
Z = -5172164
98 I = 51
54519
XDOT = -7525
861898 Wp = 80
83144
YDOT = -322
957123 meter/sec RA = 190
81430 deg
ZDOT = -1378
619843 TA = 175
88453
MA = 175
87154
Ha = 220
441 n
mi
Hp = 212
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2496679
92 X = 737668
38
Y = 14196519
41 feet Y = 4335478
90 meter
Z = -16969045
21 Z = -5168524
76
XDOT = -24691
147958 XDOT = -7514
994578
YDOT = -1059
570613 feet/sec YDOT = -407
055494 meter/sec
ZDOT = -4523
030981 ZDOT = -1415
151440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9261902
77 X = 2823027
96
Y = -11068271
52 feet Y = -3373609
16 meter
Z = -16953866
58 Z = -5167538
53
XDOT = 14121
160405 XDOT = 4304
129692
YDOT = 18983
077969 feet/sec YDOT = 5786
042165 meter/sec
ZDOT = -4682
380587 ZDOT = -1427
189603
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 16214
51854995
00016717 00000-0 10270-3 0 9108
2 25544 51
6385 191
8500 0001974 89
1313 271
0066 15
54942016 12035
Satellite: ISS
Catalog Number: 25544
Epoch time: 16214
51854995 = yrday
fracday
Element set: 910
Inclination: 51
6385 deg
RA of node: 191
8500 deg
Eccentricity:
0001974
Arg of perigee: 89
1313 deg
Mean anomaly: 271
0066 deg
Mean motion: 15
54942016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1203
Checksum: 297
Coasting Arc #12 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2016/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1390652
45 A = 6775171
82 meter
Y = -4045131
89 meter E =
0004937
Z = 5250249
32 I = 51
57537
XDOT = 7485
834366 Wp = 72
54504
YDOT = 1449
399040 meter/sec RA = 185
80083 deg
ZDOT = -863
968398 TA = 25
73003
MA = 25
70547
Ha = 220
342 n
mi
Hp = 212
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4562508
03 X = 1410279
93
Y = -13271430
08 feet Y = -4029471
15 meter
Z = 17225227
44 Z = 5257052
12
XDOT = 24559
824037 XDOT = 7473
267149
YDOT = 4755
246195 feet/sec YDOT = 1533
040407 meter/sec
ZDOT = -2834
541988 ZDOT = -827
635402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12966643
71 X = -3952233
00
Y = 5269465
24 feet Y = 1606133
00 meter
Z = 17255569
63 Z = 5259497
62
XDOT = -12022
349974 XDOT = -3664
412272
YDOT = -20797
179152 feet/sec YDOT = -6338
980206 meter/sec
ZDOT = -2676
218209 ZDOT = -815
711310
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 16215
54683522
00016717 00000-0 10270-3 0 9119
2 25544 51
6383 186
7180 0001861 92
4598 267
6768 15
54950847 12195
Satellite: ISS
Catalog Number: 25544
Epoch time: 16215
54683522 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 186
7180 deg
Eccentricity:
0001861
Arg of perigee: 92
4598 deg
Mean anomaly: 267
6768 deg
Mean motion: 15
54950847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1219
Checksum: 338
Coasting Arc #13 (Orbit 1233)
---------------------------------------
Vector Time (GMT): 2016/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3423043
88 A = 6777828
44 meter
Y = 3609104
73 meter E =
0012175
Z = -4615803
88 I = 51
61752
XDOT = -6612
197230 Wp = 107
99894
YDOT = -2456
595704 meter/sec RA = 180
79317 deg
ZDOT = 2985
545182 TA = 191
80434
MA = 191
83290
Ha = 220
368 n
mi
Hp = 212
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11230458
93 X = -3440726
34
Y = 11840894
79 feet Y = 3570727
19 meter
Z = -15143713
50 Z = -4632474
65
XDOT = -21693
560466 XDOT = -6598
737675
YDOT = -8059
697192 feet/sec YDOT = -2530
462514 meter/sec
ZDOT = 9795
095740 ZDOT = 2953
458186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16244981
72 X = 4951470
43
Y = 451513
85 feet Y = 137621
42 meter
Z = -15217054
91 Z = -4638158
34
XDOT = 8468
096957 XDOT = 2581
075952
YDOT = 20428
667795 feet/sec YDOT = 6226
657944 meter/sec
ZDOT = 9655
443698 ZDOT = 2942
979239
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 16216
51084659
00016717 00000-0 10270-3 0 9124
2 25544 51
6393 181
9066 0001840 94
6087 265
5277 15
54951129 12343
Satellite: ISS
Catalog Number: 25544
Epoch time: 16216
51084659 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 181
9066 deg
Eccentricity:
0001840
Arg of perigee: 94
6087 deg
Mean anomaly: 265
5277 deg
Mean motion: 15
54951129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1234
Checksum: 321
Coasting Arc #14 (Orbit 1243)
---------------------------------------
Vector Time (GMT): 2016/217/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3041926
22 A = 6777065
68 meter
Y = -3686410
68 meter E =
0009292
Z = 4799425
44 I = 51
63829
XDOT = 6854
841810 Wp = 117
82220
YDOT = -2296
835915 meter/sec RA = 177
83376 deg
ZDOT = 2572
433605 TA = 306
82359
MA = 306
90880
Ha = 220
342 n
mi
Hp = 212
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9980072
91 X = -3023790
77
Y = -12094523
22 feet Y = -3720326
16 meter
Z = 15746146
46 Z = 4784692
89
XDOT = 22489
638483 XDOT = 6867
520662
YDOT = -7535
550902 feet/sec YDOT = -2220
109621 meter/sec
ZDOT = 8439
742797 ZDOT = 2605
762716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7465065
18 X = -2275351
87
Y = -13861985
63 feet Y = -4225133
22 meter
Z = 15682430
67 Z = 4780004
87
XDOT = 22476
275203 XDOT = 6850
768682
YDOT = -2360
992157 feet/sec YDOT = -719
630409 meter/sec
ZDOT = 8585
589354 ZDOT = 2616
887635
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 16217
15351617
00016717 00000-0 10270-3 0 9137
2 25544 51
6430 178
6957 0001842 112
1919 247
9430 15
55005516 12446
Satellite: ISS
Catalog Number: 25544
Epoch time: 16217
15351617 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 178
6957 deg
Eccentricity:
0001842
Arg of perigee: 112
1919 deg
Mean anomaly: 247
9430 deg
Mean motion: 15
55005516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1244
Checksum: 297
Coasting Arc #15 (Orbit 1258)
---------------------------------------
Vector Time (GMT): 2016/218/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 949973
99 A = 6774927
18 meter
Y = 4114445
05 meter E =
0016428
Z = -5312173
05 I = 51
66318
XDOT = -7545
130693 Wp = 89
87366
YDOT = 1252
371973 meter/sec RA = 172
82907 deg
ZDOT = -380
273596 TA = 176
50232
MA = 176
49082
Ha = 220
273 n
mi
Hp = 212
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3116712
55 X = 929698
32
Y = 13498835
46 feet Y = 4124954
86 meter
Z = -17428389
26 Z = -5307607
70
XDOT = -24754
365790 XDOT = -7556
727100
YDOT = 4108
831933 feet/sec YDOT = 1167
932436 meter/sec
ZDOT = -1247
616786 ZDOT = -416
953353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 708854
98 X = 216059
00
Y = 13860065
46 feet Y = 4224547
95 meter
Z = -17409115
95 Z = -5306298
54
XDOT = -24069
246717 XDOT = -7336
306399
YDOT = -533
417279 feet/sec YDOT = -162
585587 meter/sec
ZDOT = -1407
938148 ZDOT = -429
139548
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 16218
11751845
00016717 00000-0 10270-3 0 9142
2 25544 51
6430 173
8854 0001800 112
5529 247
5814 15
54984580 12598
Satellite: ISS
Catalog Number: 25544
Epoch time: 16218
11751845 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 173
8854 deg
Eccentricity:
0001800
Arg of perigee: 112
5529 deg
Mean anomaly: 247
5814 deg
Mean motion: 15
54984580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1259
Checksum: 314
Coasting Arc #16 (Orbit 1274)
---------------------------------------
Vector Time (GMT): 2016/219/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1211397
60 A = 6775837
66 meter
Y = -4343751
06 meter E =
0006526
Z = 5052658
40 I = 51
69885
XDOT = 7442
962965 Wp = 69
66439
YDOT = -98
903956 meter/sec RA = 167
82349 deg
ZDOT = -1865
343864 TA = 38
40294
MA = 38
35651
Ha = 220
173 n
mi
Hp = 212
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3974401
58 X = 1235337
30
Y = -14251151
79 feet Y = -4330070
43 meter
Z = 16576963
24 Z = 5058601
20
XDOT = 24419
169834 XDOT = 7452
576631
YDOT = -324
488046 feet/sec YDOT = -15
618061 meter/sec
ZDOT = -6119
894568 ZDOT = -1829
165127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6175845
49 X = 1882397
70
Y = -13411424
60 feet Y = -4087802
22 meter
Z = 16603599
86 Z = 5060777
24
XDOT = 23195
721327 XDOT = 7070
055861
YDOT = 3283
549034 feet/sec YDOT = 1000
825745 meter/sec
ZDOT = -5961
928322 ZDOT = -1817
195753
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 16219
14578055
00016717 00000-0 10270-3 0 9157
2 25544 51
6432 168
7530 0001789 116
0015 244
1323 15
55022182 12757
Satellite: ISS
Catalog Number: 25544
Epoch time: 16219
14578055 = yrday
fracday
Element set: 915
Inclination: 51
6432 deg
RA of node: 168
7530 deg
Eccentricity:
0001789
Arg of perigee: 116
0015 deg
Mean anomaly: 244
1323 deg
Mean motion: 15
55022182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1275
Checksum: 288
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