[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: October 3rd 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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


284/02:47:17 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 212 5

286/10:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 212 2

287/18:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 212 2

Coasting Arc #1 (Orbit 2135)
---------------------------------------

Vector Time (GMT): 2016/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2241736
96                 A    =         6789635
45  meter
 Y    =       -6396577
11  meter          E    =           
0018157
 Z    =        -159612
94                 I    =           51
30433
 XDOT =       4484
565124                 Wp   =           36
18598
 YDOT =      -1711
965351  meter/sec      RA   =          251
76738  deg
 ZDOT =       5986
121585                 TA   =          322
08550
                                          MA   =          322
21322
                                          Ha   =            222
892  n
mi
                                          Hp   =            213
574

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7354780
06                 X    =        -2169266
86
 Y    =      -20986145
38  feet           Y    =        -6421240
54  meter
 Z    =        -523664
51                 Z    =         -170325
85
 XDOT =      14713
140171                 XDOT =        4474
297222
 YDOT =      -5616
684221  feet/sec       YDOT =       -1661
872458  meter/sec
 ZDOT =      19639
506512                 ZDOT =        6007
881960

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10478809
98                 X    =         3193941
28
 Y    =       19612639
40  feet           Y    =         5977932
49  meter
 Z    =        -569411
44                 Z    =         -173556
61
 XDOT =     -12123
442635                 XDOT =       -3695
225315
 YDOT =       7018
566345  feet/sec       YDOT =        2139
259022  meter/sec
 ZDOT =      19734
815747                 ZDOT =        6015
171840


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   16274
50033672  
00016717  00000-0  10270-3 0  9003
2 25544  51
6383 252
7108 0006713  21
8902 338
2536 15
54019889 21364


Satellite: ISS
Catalog Number: 25544
Epoch time:      16274
50033672   =   yrday
fracday
Element set:     900
Inclination:       51
6383  deg
RA of node:       252
7108  deg
Eccentricity:     
0006713     
Arg of perigee:    21
8902  deg
Mean anomaly:     338
2536  deg
Mean motion:   15
54019889  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2136
Checksum:              301


Coasting Arc #2 (Orbit 2151)
---------------------------------------

Vector Time (GMT): 2016/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1448911
89                 A    =         6788713
03  meter
 Y    =        6457766
44  meter          E    =           
0007901
 Z    =       -1517567
86                 I    =           51
31346
 XDOT =      -5080
079430                 Wp   =           91
89621
 YDOT =       -200
813319  meter/sec      RA   =          246
77378  deg
 ZDOT =      -5730
979747                 TA   =          104
74180
                                          MA   =          104
65422
                                          Ha   =            223
078  n
mi
                                          Hp   =            213
459

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4753647
95                 X    =         1383963
60
 Y    =       21186897
78  feet           Y    =         6473605
78  meter
 Z    =       -4978897
17                 Z    =        -1510688
02
 XDOT =     -16666
927263                 XDOT =       -5049
617367
 YDOT =       -658
836348  feet/sec       YDOT =        -257
452685  meter/sec
 ZDOT =     -18802
426993                 ZDOT =       -5755
583761

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8320636
88                 X    =        -2536130
12
 Y    =      -20063320
44  feet           Y    =        -6115300
07  meter
 Z    =       -4949888
69                 Z    =        -1508726
07
 XDOT =      14952
997403                 XDOT =        4557
673609
 YDOT =      -1557
307904  feet/sec       YDOT =        -474
667449  meter/sec
 ZDOT =     -18909
847805                 ZDOT =       -5763
721611


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   16275
52925800  
00016717  00000-0  10270-3 0  9010
2 25544  51
6397 247
5816 0006920  24
4526 335
6954 15
54006206 21520


Satellite: ISS
Catalog Number: 25544
Epoch time:      16275
52925800   =   yrday
fracday
Element set:     901
Inclination:       51
6397  deg
RA of node:       247
5816  deg
Eccentricity:     
0006920     
Arg of perigee:    24
4526  deg
Mean anomaly:     335
6954  deg
Mean motion:   15
54006206  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2152
Checksum:              304


Coasting Arc #3 (Orbit 2167)
---------------------------------------

Vector Time (GMT): 2016/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -515307
35                 A    =         6785736
61  meter
 Y    =       -6049892
43  meter          E    =           
0017845
 Z    =        3006313
53                 I    =           51
31798
 XDOT =       5541
754545                 Wp   =           65
14476
 YDOT =       1984
034186  meter/sec      RA   =          241
77715  deg
 ZDOT =       4926
918293                 TA   =          329
49475
                                          MA   =          329
59843
                                          Ha   =            222
991  n
mi
                                          Hp   =            213
340

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1690640
91                 X    =         -462221
20
 Y    =      -19848728
43  feet           Y    =        -6055357
70  meter
 Z    =        9863233
35                 Z    =         3003940
03
 XDOT =      18181
609399                 XDOT =        5495
223492
 YDOT =       6509
298512  feet/sec       YDOT =        2045
746309  meter/sec
 ZDOT =      16164
430096                 ZDOT =        4953
725847

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5436297
28                 X    =         1656983
41
 Y    =       19169307
19  feet           Y    =         5842804
83  meter
 Z    =        9853831
39                 Z    =         3003447
81
 XDOT =     -17577
590694                 XDOT =       -5357
649643
 YDOT =      -3410
737148  feet/sec       YDOT =       -1039
592683  meter/sec
 ZDOT =      16281
195118                 ZDOT =        4962
508272


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   16276
55816902  
00016717  00000-0  10270-3 0  9027
2 25544  51
6402 242
4542 0006765  27
7073 332
4439 15
54047924 21689


Satellite: ISS
Catalog Number: 25544
Epoch time:      16276
55816902   =   yrday
fracday
Element set:     902
Inclination:       51
6402  deg
RA of node:       242
4542  deg
Eccentricity:     
0006765     
Arg of perigee:    27
7073  deg
Mean anomaly:     332
4439  deg
Mean motion:   15
54047924  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2168
Checksum:              310


Coasting Arc #4 (Orbit 2182)
---------------------------------------

Vector Time (GMT): 2016/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -592418
05                 A    =         6782036
49  meter
 Y    =        5278565
43  meter          E    =           
0014196
 Z    =       -4232313
55                 I    =           51
32132
 XDOT =      -5759
251122                 Wp   =           52
25488
 YDOT =      -3532
703826  meter/sec      RA   =          236
77094  deg
 ZDOT =      -3599
641208                 TA   =          180
70829
                                          MA   =          180
71030
                                          Ha   =            223
187  n
mi
                                          Hp   =            213
162

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1943628
78                 X    =         -630841
18
 Y    =       17318128
05  feet           Y    =         5271725
25  meter
 Z    =      -13885543
15                 Z    =        -4235285
41
 XDOT =     -18895
180846                 XDOT =       -5701
833681
 YDOT =     -11590
235649  feet/sec       YDOT =       -3596
787047  meter/sec
 ZDOT =     -11809
846483                 ZDOT =       -3627
478772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1716749
43                 X    =         -523265
23
 Y    =      -17331017
22  feet           Y    =        -5282494
05  meter
 Z    =      -13899358
77                 Z    =        -4236524
55
 XDOT =      19522
934618                 XDOT =        5950
590472
 YDOT =       7635
174536  feet/sec       YDOT =        2327
201199  meter/sec
 ZDOT =     -11930
873653                 ZDOT =       -3636
530290


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   16277
52276915  
00016717  00000-0  10270-3 0  9030
2 25544  51
6400 237
6461 0006973  31
1371 329
0193 15
54027554 21837


Satellite: ISS
Catalog Number: 25544
Epoch time:      16277
52276915   =   yrday
fracday
Element set:     903
Inclination:       51
6400  deg
RA of node:       237
6461  deg
Eccentricity:     
0006973     
Arg of perigee:    31
1371  deg
Mean anomaly:     329
0193  deg
Mean motion:   15
54027554  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2183
Checksum:              301


Coasting Arc #5 (Orbit 2198)
---------------------------------------

Vector Time (GMT): 2016/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1796452
45                 A    =         6778783
24  meter
 Y    =       -4193009
06  meter          E    =           
0008895
 Z    =        5006171
46                 I    =           51
33031
 XDOT =       5710
520034                 Wp   =           74
47389
 YDOT =       4751
041007  meter/sec      RA   =          231
75780  deg
 ZDOT =       1929
588749                 TA   =          356
73876
                                          MA   =          356
74455
                                          Ha   =            223
012  n
mi
                                          Hp   =            213
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5893872
88                 X    =         1818887
96
 Y    =      -13756591
41  feet           Y    =        -4172793
92  meter
 Z    =       16424447
06                 Z    =         5014953
30
 XDOT =      18735
301950                 XDOT =        5647
594980
 YDOT =      15587
404878  feet/sec       YDOT =        4814
548254  meter/sec
 ZDOT =       6330
671750                 ZDOT =        1957
176154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2608314
67                 X    =         -795014
31
 Y    =       14693365
68  feet           Y    =         4478537
86  meter
 Z    =       16463465
78                 Z    =         5018064
37
 XDOT =     -20602
281576                 XDOT =       -6279
575424
 YDOT =     -10886
674850  feet/sec       YDOT =       -3318
258494  meter/sec
 ZDOT =       6450
426283                 ZDOT =        1966
089931


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   16278
55166525  
00016717  00000-0  10270-3 0  9040
2 25544  51
6409 232
5188 0006787  33
5816 326
5765 15
54072319 21992


Satellite: ISS
Catalog Number: 25544
Epoch time:      16278
55166525   =   yrday
fracday
Element set:     904
Inclination:       51
6409  deg
RA of node:       232
5188  deg
Eccentricity:     
0006787     
Arg of perigee:    33
5816  deg
Mean anomaly:     326
5765  deg
Mean motion:   15
54072319  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2199
Checksum:              336


Coasting Arc #6 (Orbit 2213)
---------------------------------------

Vector Time (GMT): 2016/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3044812
95                 A    =         6777601
57  meter
 Y    =        2953142
60  meter          E    =           
0019905
 Z    =       -5302838
87                 I    =           51
34718
 XDOT =      -5276
321729                 Wp   =           73
71664
 YDOT =      -5544
745281  meter/sec      RA   =          226
73810  deg
 ZDOT =        -52
968381                 TA   =          195
74463
                                          MA   =          195
80661
                                          Ha   =            223
239  n
mi
                                          Hp   =            212
867

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9989543
79                 X    =        -3051850
06
 Y    =        9688788
04  feet           Y    =         2919053
58  meter
 Z    =      -17397765
33                 Z    =        -5317647
47
 XDOT =     -17310
766829                 XDOT =       -5213
669523
 YDOT =     -18191
421527  feet/sec       YDOT =       -5603
398346  meter/sec
 ZDOT =       -173
780776                 ZDOT =         -78
447175

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7293549
97                 X    =         2223074
03
 Y    =      -11755700
92  feet           Y    =        -3583137
64  meter
 Z    =      -17462916
77                 Z    =        -5322697
03
 XDOT =      20277
083101                 XDOT =        6180
454929
 YDOT =      13028
393220  feet/sec       YDOT =        3971
054253  meter/sec
 ZDOT =       -284
214170                 ZDOT =         -86
628479


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   16279
51624793  
00016717  00000-0  10270-3 0  9054
2 25544  51
6412 227
7105 0006930  37
4285 322
7349 15
54046756 22144


Satellite: ISS
Catalog Number: 25544
Epoch time:      16279
51624793   =   yrday
fracday
Element set:     905
Inclination:       51
6412  deg
RA of node:       227
7105  deg
Eccentricity:     
0006930     
Arg of perigee:    37
4285  deg
Mean anomaly:     322
7349  deg
Mean motion:   15
54046756  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2214
Checksum:              312


Coasting Arc #7 (Orbit 2229)
---------------------------------------

Vector Time (GMT): 2016/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4239031
61                 A    =         6778635
64  meter
 Y    =       -1608888
92  meter          E    =           
0012376
 Z    =        5033421
62                 I    =           51
37338
 XDOT =       4467
014281                 Wp   =           47
82402
 YDOT =       5959
254196  meter/sec      RA   =          221
72101  deg
 ZDOT =      -1846
112213                 TA   =           60
17460
                                          MA   =           60
05162
                                          Ha   =            223
183  n
mi
                                          Hp   =            212
839

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13907584
02                 X    =         4232256
94
 Y    =       -5278506
95  feet           Y    =        -1561522
67  meter
 Z    =       16513850
45                 Z    =         5053997
81
 XDOT =      14655
558665                 XDOT =        4409
012158
 YDOT =      19551
358910  feet/sec       YDOT =        6008
882878  meter/sec
 ZDOT =      -6056
798599                 ZDOT =       -1824
553592

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12005993
99                 X    =        -3659426
97
 Y    =        8611287
63  feet           Y    =         2624720
47  meter
 Z    =       16603994
07                 Z    =         5060897
39
 XDOT =     -18553
052580                 XDOT =       -5654
970426
 YDOT =     -14298
544794  feet/sec       YDOT =       -4358
196453  meter/sec
 ZDOT =      -5963
540584                 ZDOT =       -1817
687170


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   16280
54512568  
00016717  00000-0  10270-3 0  9066
2 25544  51
6409 222
5831 0007008  41
4121 318
7561 15
54063132 22306


Satellite: ISS
Catalog Number: 25544
Epoch time:      16280
54512568   =   yrday
fracday
Element set:     906
Inclination:       51
6409  deg
RA of node:       222
5831  deg
Eccentricity:     
0007008     
Arg of perigee:    41
4121  deg
Mean anomaly:     318
7561  deg
Mean motion:   15
54063132  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2230
Checksum:              276


Coasting Arc #8 (Orbit 2244)
---------------------------------------

Vector Time (GMT): 2016/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5255036
96                 A    =         6781601
14  meter
 Y    =         344839
21  meter          E    =           
0012974
 Z    =       -4282629
06                 I    =           51
40800
 XDOT =      -3265
333728                 Wp   =           81
70503
 YDOT =      -5957
127195  meter/sec      RA   =          216
71105  deg
 ZDOT =       3538
129986                 TA   =          224
47050
                                          MA   =          224
57473
                                          Ha   =            223
251  n
mi
                                          Hp   =            212
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17240934
90                 X    =        -5237698
97
 Y    =        1131362
24  feet           Y    =          286170
48  meter
 Z    =      -14050620
28                 Z    =        -4308115
03
 XDOT =     -10713
037165                 XDOT =       -3215
663908
 YDOT =     -19544
380560  feet/sec       YDOT =       -5993
364357  meter/sec
 ZDOT =      11608
038012                 ZDOT =        3522
388661

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16203036
08                 X    =         4938685
40
 Y    =       -5731344
11  feet           Y    =        -1746913
69  meter
 Z    =      -14162028
92                 Z    =        -4316586
42
 XDOT =      15258
631388                 XDOT =        4650
830847
 YDOT =      14710
842877  feet/sec       YDOT =        4483
864909  meter/sec
 ZDOT =      11540
181514                 ZDOT =        3517
447325


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   16281
50968947  
00016717  00000-0  10270-3 0  9070
2 25544  51
6407 217
7757 0006905  44
5150 315
6556 15
54073099 22457


Satellite: ISS
Catalog Number: 25544
Epoch time:      16281
50968947   =   yrday
fracday
Element set:     907
Inclination:       51
6407  deg
RA of node:       217
7757  deg
Eccentricity:     
0006905     
Arg of perigee:    44
5150  deg
Mean anomaly:     315
6556  deg
Mean motion:   15
54073099  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2245
Checksum:              331


Coasting Arc #9 (Orbit 2260)
---------------------------------------

Vector Time (GMT): 2016/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5997348
51                 A    =         6785352
89  meter
 Y    =         852961
30  meter          E    =           
0018417
 Z    =        3045331
26                 I    =           51
44809
 XDOT =       1702
007338                 Wp   =           79
70105
 YDOT =       5646
358557  meter/sec      RA   =          211
71183  deg
 ZDOT =      -4904
801960                 TA   =           65
24570
                                          MA   =           65
05416
                                          Ha   =            223
240  n
mi
                                          Hp   =            212
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19676340
24                 X    =         5972571
63
 Y    =        2798429
45  feet           Y    =          919889
35  meter
 Z    =        9991244
31                 Z    =         3074405
02
 XDOT =       5584
013575                 XDOT =        1662
567553
 YDOT =      18524
798414  feet/sec       YDOT =        5665
170674  meter/sec
 ZDOT =     -16091
869947                 ZDOT =       -4896
630123

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19588761
77                 X    =        -5970654
59
 Y    =        2952591
47  feet           Y    =          899949
88  meter
 Z    =       10118159
49                 Z    =         3084015
01
 XDOT =     -10554
381222                 XDOT =       -3216
975397
 YDOT =     -14680
049975  feet/sec       YDOT =       -4474
479232  meter/sec
 ZDOT =     -16057
029028                 ZDOT =       -4894
182448


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   16282
53854548  
00016717  00000-0  10270-3 0  9086
2 25544  51
6415 212
6470 0006950  47
8428 312
3314 15
54110159 22619


Satellite: ISS
Catalog Number: 25544
Epoch time:      16282
53854548   =   yrday
fracday
Element set:     908
Inclination:       51
6415  deg
RA of node:       212
6470  deg
Eccentricity:     
0006950     
Arg of perigee:    47
8428  deg
Mean anomaly:     312
3314  deg
Mean motion:   15
54110159  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2261
Checksum:              299


Coasting Arc #10 (Orbit 2275)
---------------------------------------

Vector Time (GMT): 2016/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6349341
91                 A    =         6788318
70  meter
 Y    =       -1826361
60  meter          E    =           
0014932
 Z    =       -1538012
07                 I    =           51
48522
 XDOT =         79
988428                 Wp   =           44
53816
 YDOT =      -5078
649386  meter/sec      RA   =          206
72451  deg
 ZDOT =       5744
892243                 TA   =          298
61764
                                          MA   =          298
76777
                                          Ha   =            223
301  n
mi
                                          Hp   =            212
514

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20831174
26                 X    =        -6320976
09
 Y    =       -5992000
01  feet           Y    =        -1897205
71  meter
 Z    =       -5045971
37                 Z    =        -1568786
88
 XDOT =        262
429225                 XDOT =         108
866722
 YDOT =     -16662
235520  feet/sec       YDOT =       -5077
593013  meter/sec
 ZDOT =      18848
071664                 ZDOT =        5745
351325

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21635632
50                 X    =         6594540
79
 Y    =        -607261
67  feet           Y    =         -185093
36  meter
 Z    =       -5180188
37                 Z    =        -1578921
42
 XDOT =       4881
982793                 XDOT =        1488
028355
 YDOT =      14338
522575  feet/sec       YDOT =        4370
381681  meter/sec
 ZDOT =      18850
853846                 ZDOT =        5745
740252


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   16283
50308634  
00016717  00000-0  10270-3 0  9095
2 25544  51
6408 207
8395 0006993  51
4632 308
7147 15
54110916 22768


Satellite: ISS
Catalog Number: 25544
Epoch time:      16283
50308634   =   yrday
fracday
Element set:     909
Inclination:       51
6408  deg
RA of node:       207
8395  deg
Eccentricity:     
0006993     
Arg of perigee:    51
4632  deg
Mean anomaly:     308
7147  deg
Mean motion:   15
54110916  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2276
Checksum:              317


Coasting Arc #11 (Orbit 2285)
---------------------------------------

Vector Time (GMT): 2016/284/02:47:17
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5668325
55                 A    =         6788708
79  meter
 Y    =        3533879
08  meter          E    =           
0011859
 Z    =       -1208192
01                 I    =           51
50490
 XDOT =      -3453
419236                 Wp   =          107
60207
 YDOT =       3559
280205  meter/sec      RA   =          203
67053  deg
 ZDOT =      -5842
229357                 TA   =           85
54275
                                          MA   =           85
40727
                                          Ha   =            223
310  n
mi
                                          Hp   =            212
485

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18596868
61                 X    =         5634256
46
 Y    =       11594091
48  feet           Y    =         3597075
52  meter
 Z    =       -3963884
56                 Z    =        -1180739
48
 XDOT =     -11330
115603                 XDOT =       -3464
584045
 YDOT =      11677
428494  feet/sec       YDOT =        3520
598872  meter/sec
 ZDOT =     -19167
419150                 ZDOT =       -5859
032756

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19331878
53                 X    =         5892356
58
 Y    =      -10367142
33  feet           Y    =        -3159904
98  meter
 Z    =       -3844436
52                 Z    =        -1171784
25
 XDOT =       3782
132035                 XDOT =        1152
793844
 YDOT =      14124
058740  feet/sec       YDOT =        4305
013104  meter/sec
 ZDOT =     -19241
402418                 ZDOT =       -5864
779457


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   16284
14610683  
00016717  00000-0  10270-3 0  9108
2 25544  51
6412 204
6330 0006783  56
1085 304
0712 15
54139426 22863


Satellite: ISS
Catalog Number: 25544
Epoch time:      16284
14610683   =   yrday
fracday
Element set:     910
Inclination:       51
6412  deg
RA of node:       204
6330  deg
Eccentricity:     
0006783     
Arg of perigee:    56
1085  deg
Mean anomaly:     304
0712  deg
Mean motion:   15
54139426  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2286
Checksum:              285


Coasting Arc #12 (Orbit 2301)
---------------------------------------

Vector Time (GMT): 2016/285/02:47:17
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4766172
35                 A    =         6786101
14  meter
 Y    =       -3938175
77  meter          E    =           
0019984
 Z    =        2772668
99                 I    =           51
52603
 XDOT =       5111
863191                 Wp   =           73
03943
 YDOT =      -2565
252292  meter/sec      RA   =          198
68770  deg
 ZDOT =       5118
823428                 TA   =          318
47208
                                          MA   =          318
62373
                                          Ha   =            223
363  n
mi
                                          Hp   =            212
433

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15637048
38                 X    =        -4735248
97
 Y    =      -12920524
19  feet           Y    =        -3991301
15  meter
 Z    =        9096683
03                 Z    =         2749591
40
 XDOT =      16771
204694                 XDOT =        5115
303327
 YDOT =      -8416
182060  feet/sec       YDOT =       -2508
068305  meter/sec
 ZDOT =      16794
040118                 ZDOT =        5143
664369

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18896890
83                 X    =        -5759772
33
 Y    =        7495274
77  feet           Y    =         2284559
75  meter
 Z    =        8996401
64                 Z    =         2742103
22
 XDOT =       1234
096948                 XDOT =         376
152750
 YDOT =     -17275
721849  feet/sec       YDOT =       -5265
640020  meter/sec
 ZDOT =      16903
011664                 ZDOT =        5152
037955


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   16285
17493067  
00016717  00000-0  10270-3 0  9118
2 25544  51
6412 199
5043 0006767  59
8963 300
2860 15
54142829 23025


Satellite: ISS
Catalog Number: 25544
Epoch time:      16285
17493067   =   yrday
fracday
Element set:     911
Inclination:       51
6412  deg
RA of node:       199
5043  deg
Eccentricity:     
0006767     
Arg of perigee:    59
8963  deg
Mean anomaly:     300
2860  deg
Mean motion:   15
54142829  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2302
Checksum:              317


Coasting Arc #13 (Orbit 2316)
---------------------------------------

Vector Time (GMT): 2016/286/02:47:17
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3433086
30                 A    =         6782190
47  meter
 Y    =        4187286
13  meter          E    =           
0014073
 Z    =       -4099051
38                 I    =           51
54509
 XDOT =      -6449
735532                 Wp   =           67
89261
 YDOT =       1551
994586  meter/sec      RA   =          193
69734  deg
 ZDOT =      -3821
823488                 TA   =          162
52889
                                          MA   =          162
48042
                                          Ha   =            223
340  n
mi
                                          Hp   =            212
359

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11263406
49                 X    =         3405919
43
 Y    =       13737815
38  feet           Y    =         4225524
86  meter
 Z    =      -13448331
29                 Z    =        -4082440
61
 XDOT =     -21160
549646                 XDOT =       -6448
046044
 YDOT =       5091
845753  feet/sec       YDOT =        1479
878348  meter/sec
 ZDOT =     -12538
790972                 ZDOT =       -3853
151008

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17452325
29                 X    =         5319468
75
 Y    =       -3597124
86  feet           Y    =        -1096403
66  meter
 Z    =      -13376342
80                 Z    =        -4077109
28
 XDOT =      -5634
036354                 XDOT =       -1717
254281
 YDOT =      19736
429493  feet/sec       YDOT =        6015
663709  meter/sec
 ZDOT =     -12675
977170                 ZDOT =       -3863
637841


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   16286
13944078  
00016717  00000-0  10270-3 0  9129
2 25544  51
6422 194
6959 0006836  63
2945 296
8907 15
54165829 23177


Satellite: ISS
Catalog Number: 25544
Epoch time:      16286
13944078   =   yrday
fracday
Element set:     912
Inclination:       51
6422  deg
RA of node:       194
6959  deg
Eccentricity:     
0006836     
Arg of perigee:    63
2945  deg
Mean anomaly:     296
8907  deg
Mean motion:   15
54165829  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2317
Checksum:              350


Coasting Arc #14 (Orbit 2321)
---------------------------------------

Vector Time (GMT): 2016/286/10:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907704
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6016318
46                 A    =         6785438
52  meter
 Y    =        1108817
46  meter          E    =           
0011444
 Z    =       -2938019
64                 I    =           51
56636
 XDOT =      -3312
875194                 Wp   =           64
88819
 YDOT =      -4762
759434  meter/sec      RA   =          191
95953  deg
 ZDOT =       5006
489628                 TA   =          261
56191
                                          MA   =          261
69164
                                          Ha   =            223
289  n
mi
                                          Hp   =            212
207

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19738577
62                 X    =        -6013998
63
 Y    =        3637852
56  feet           Y    =         1041551
59  meter
 Z    =       -9639172
06                 Z    =        -2967240
15
 XDOT =     -10869
013103                 XDOT =       -3283
690167
 YDOT =     -15625
851162  feet/sec       YDOT =       -4799
642475  meter/sec
 ZDOT =      16425
490907                 ZDOT =        4990
467802

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19343829
10                 X    =         5895999
11
 Y    =       -5116579
30  feet           Y    =        -1559533
37  meter
 Z    =       -9767084
92                 Z    =        -2977007
48
 XDOT =      11753
733346                 XDOT =        3582
537924
 YDOT =      13337
822903  feet/sec       YDOT =        4065
368421  meter/sec
 ZDOT =      16356
159355                 ZDOT =        4985
357372


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   16286
46094216  
00016717  00000-0  10270-3 0  9136
2 25544  51
6416 193
0946 0006919  61
9143 298
2709 15
54172795 23228


Satellite: ISS
Catalog Number: 25544
Epoch time:      16286
46094216   =   yrday
fracday
Element set:     913
Inclination:       51
6416  deg
RA of node:       193
0946  deg
Eccentricity:     
0006919     
Arg of perigee:    61
9143  deg
Mean anomaly:     298
2709  deg
Mean motion:   15
54172795  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2322
Checksum:              328


Coasting Arc #15 (Orbit 2337)
---------------------------------------

Vector Time (GMT): 2016/287/10:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907704
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6647413
42                 A    =         6788373
65  meter
 Y    =        -243472
00  meter          E    =           
0018736
 Z    =        1324698
86                 I    =           51
60857
 XDOT =       1348
810703                 Wp   =          103
01480
 YDOT =       4810
319230  meter/sec      RA   =          186
98123  deg
 ZDOT =      -5819
063091                 TA   =           62
55563
                                          MA   =           62
36521
                                          Ha   =            223
331  n
mi
                                          Hp   =            212
169

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21809099
16                 X    =         6643207
05
 Y    =        -798792
65  feet           Y    =         -169159
51  meter
 Z    =        4346124
87                 Z    =         1356980
50
 XDOT =       4425
231965                 XDOT =        1323
187061
 YDOT =      15781
887238  feet/sec       YDOT =        4825
258523  meter/sec
 ZDOT =     -19091
414342                 ZDOT =       -5812
573687

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21612225
98                 X    =        -6587406
48
 Y    =        2817705
26  feet           Y    =          858836
56  meter
 Z    =        4487304
58                 Z    =         1367730
44
 XDOT =      -5789
125669                 XDOT =       -1764
525504
 YDOT =     -13713
573530  feet/sec       YDOT =       -4179
897212  meter/sec
 ZDOT =     -19063
757741                 ZDOT =       -5810
633359


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   16287
48973748  
00016717  00000-0  10270-3 0  9146
2 25544  51
6423 187
9660 0006892  66
1018 294
0857 15
54185620 23385


Satellite: ISS
Catalog Number: 25544
Epoch time:      16287
48973748   =   yrday
fracday
Element set:     914
Inclination:       51
6423  deg
RA of node:       187
9660  deg
Eccentricity:     
0006892     
Arg of perigee:    66
1018  deg
Mean anomaly:     294
0857  deg
Mean motion:   15
54185620  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2338
Checksum:              345


Coasting Arc #16 (Orbit 2342)
---------------------------------------

Vector Time (GMT): 2016/287/18:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907704
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5981551
04                 A    =         6787041
80  meter
 Y    =        2324330
63  meter          E    =           
0010815
 Z    =       -2214379
67                 I    =           51
61227
 XDOT =      -3572
224976                 Wp   =          102
36155
 YDOT =       4011
631895  meter/sec      RA   =          185
37009  deg
 ZDOT =      -5463
414878                 TA   =          102
23038
                                          MA   =          102
10924
                                          Ha   =            223
312  n
mi
                                          Hp   =            212
175

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19624511
29                 X    =         5965871
86
 Y    =        7625756
67  feet           Y    =         2391132
39  meter
 Z    =       -7265025
17                 Z    =        -2185360
83
 XDOT =     -11719
898216                 XDOT =       -3590
279323
 YDOT =      13161
521966  feet/sec       YDOT =        3971
583215  meter/sec
 ZDOT =     -17924
589495                 ZDOT =       -5480
812442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4643427
97                 X    =         1415316
84
 Y    =       20579959
69  feet           Y    =         6272771
71  meter
 Z    =       -7138489
68                 Z    =        -2175811
66
 XDOT =     -15894
142832                 XDOT =       -4844
534735
 YDOT =      -2629
090953  feet/sec       YDOT =        -801
346922  meter/sec
 ZDOT =     -18001
255417                 ZDOT =       -5486
782651


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   16287
81123242  
00016717  00000-0  10270-3 0  9150
2 25544  51
6397 186
3590 0006823  69
8177 290
3709 15
54222955 23434


Satellite: ISS
Catalog Number: 25544
Epoch time:      16287
81123242   =   yrday
fracday
Element set:     915
Inclination:       51
6397  deg
RA of node:       186
3590  deg
Eccentricity:     
0006823     
Arg of perigee:    69
8177  deg
Mean anomaly:     290
3709  deg
Mean motion:   15
54222955  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2343
Checksum:              328


Coasting Arc #17 (Orbit 2358)
---------------------------------------

Vector Time (GMT): 2016/288/18:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907704
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4919199
66                 A    =         6783501
65  meter
 Y    =       -2911617
00  meter          E    =           
0018394
 Z    =        3635672
33                 I    =           51
63364
 XDOT =       5284
408324                 Wp   =           87
24319
 YDOT =      -3433
277004  meter/sec      RA   =          180
38932  deg
 ZDOT =       4382
204224                 TA   =          315
95117
                                          MA   =          316
09758
                                          Ha   =            223
315  n
mi
                                          Hp   =            212
145

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16139106
48                 X    =        -4903936
43
 Y    =       -9552549
22  feet           Y    =        -2966540
97  meter
 Z    =       11928058
81                 Z    =         3611813
15
 XDOT =      17337
297651                 XDOT =        5301
120131
 YDOT =     -11264
032164  feet/sec       YDOT =       -3374
089177  meter/sec
 ZDOT =      14377
310445                 ZDOT =        4407
916034

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1440335
33                 X    =         -439014
21
 Y    =      -18764732
58  feet           Y    =        -5719490
49  meter
 Z    =       11824161
16                 Z    =         3604004
32
 XDOT =      17733
220517                 XDOT =        5405
085614
 YDOT =       7807
634211  feet/sec       YDOT =        2379
766908  meter/sec
 ZDOT =      14490
252883                 ZDOT =        4416
629079


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   16288
84001224  
00016717  00000-0  10270-3 0  9160
2 25544  51
6406 181
2299 0006652  74
7338 285
4550 15
54236047 23592


Satellite: ISS
Catalog Number: 25544
Epoch time:      16288
84001224   =   yrday
fracday
Element set:     916
Inclination:       51
6406  deg
RA of node:       181
2299  deg
Eccentricity:     
0006652     
Arg of perigee:    74
7338  deg
Mean anomaly:     285
4550  deg
Mean motion:   15
54236047  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2359
Checksum:              316
Forward to a Friend
 
  • 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