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

 
Date: December 22nd 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19116 7 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 ET - UTC (sec) : 67 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


There are no maneuvers



Coasting Arc #1 (Orbit 1671)
---------------------------------------

Vector Time (GMT): 2015/352/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1251627
56                 A    =         6785252
17  meter
 Y    =        6311099
26  meter          E    =           
0003651
 Z    =       -2149115
78                 I    =           51
32612
 XDOT =      -5310
252086                 Wp   =          247
40402
 YDOT =       -811
564870  meter/sec      RA   =          243
27570  deg
 ZDOT =      -5469
815597                 TA   =          316
53749
                                          MA   =          316
56627
                                          Ha   =            218
921  n
mi
                                          Hp   =            216
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4106389
62                 X    =         1191401
85
 Y    =       20705706
22  feet           Y    =         6324759
11  meter
 Z    =       -7050904
79                 Z    =        -2143181
71
 XDOT =     -17422
086896                 XDOT =       -5274
212049
 YDOT =      -2662
614402  feet/sec       YDOT =        -870
745927  meter/sec
 ZDOT =     -17945
589229                 ZDOT =       -5495
524198

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20870133
88                 X    =        -6361216
81
 Y    =        3220395
65  feet           Y    =          981576
60  meter
 Z    =       -7026416
42                 Z    =        -2141651
72
 XDOT =       3671
265025                 XDOT =        1119
001580
 YDOT =     -15648
284991  feet/sec       YDOT =       -4769
597265  meter/sec
 ZDOT =     -18056
560636                 ZDOT =       -5503
639682


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   15352
53204125  
00016717  00000-0  10270-3 0  9005
2 25544  51
6431 244
0899 0008255 293
5867  66
4419 15
54861409 16727


Satellite: ISS
Catalog Number: 25544
Epoch time:      15352
53204125   =   yrday
fracday
Element set:     900
Inclination:       51
6431  deg
RA of node:       244
0899  deg
Eccentricity:     
0008255     
Arg of perigee:   293
5867  deg
Mean anomaly:      66
4419  deg
Mean motion:   15
54861409  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1672
Checksum:              316


Coasting Arc #2 (Orbit 1687)
---------------------------------------

Vector Time (GMT): 2015/353/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          58139
63                 A    =         6781056
97  meter
 Y    =       -5635485
59  meter          E    =           
0005027
 Z    =        3765062
02                 I    =           51
32771
 XDOT =       5735
022096                 Wp   =           58
75454
 YDOT =       2871
337915  meter/sec      RA   =          238
26824  deg
 ZDOT =       4207
606462                 TA   =          346
60387
                                          MA   =          346
61721
                                          Ha   =            219
060  n
mi
                                          Hp   =            216
029

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         190746
81                 X    =          102863
41
 Y    =      -18489125
95  feet           Y    =        -5634585
50  meter
 Z    =       12352565
67                 Z    =         3765452
89
 XDOT =      18815
689292                 XDOT =        5682
048860
 YDOT =       9420
399985  feet/sec       YDOT =        2935
174391  meter/sec
 ZDOT =      13804
483143                 ZDOT =        4235
337538

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18477847
97                 X    =         5632048
06
 Y    =         621413
73  feet           Y    =          189406
90  meter
 Z    =       12355283
12                 Z    =         3765890
29
 XDOT =      -9889
244393                 XDOT =       -3014
241691
 YDOT =      17112
513495  feet/sec       YDOT =        5215
894113  meter/sec
 ZDOT =      13923
829768                 ZDOT =        4243
983313


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   15353
56036302  
00016717  00000-0  10270-3 0  9010
2 25544  51
6432 238
9567 0008217 298
9091  61
1238 15
54902569 16889


Satellite: ISS
Catalog Number: 25544
Epoch time:      15353
56036302   =   yrday
fracday
Element set:     901
Inclination:       51
6432  deg
RA of node:       238
9567  deg
Eccentricity:     
0008217     
Arg of perigee:   298
9091  deg
Mean anomaly:      61
1238  deg
Mean motion:   15
54902569  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1688
Checksum:              323


Coasting Arc #3 (Orbit 1702)
---------------------------------------

Vector Time (GMT): 2015/354/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1521999
31                 A    =         6776824
02  meter
 Y    =        4470854
58  meter          E    =           
0009054
 Z    =       -4866765
88                 I    =           51
33176
 XDOT =      -5725
269440                 Wp   =           28
31674
 YDOT =      -4518
208185  meter/sec      RA   =          233
24877  deg
 ZDOT =      -2354
149269                 TA   =          218
48335
                                          MA   =          218
54795
                                          Ha   =            219
197  n
mi
                                          Hp   =            215
671

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4993436
05                 X    =        -1548239
38
 Y    =       14668158
07  feet           Y    =         4453688
07  meter
 Z    =      -15967079
67                 Z    =        -4874223
02
 XDOT =     -18783
692388                 XDOT =       -5662
884598
 YDOT =     -14823
517668  feet/sec       YDOT =       -4581
883013  meter/sec
 ZDOT =      -7723
586842                 ZDOT =       -2381
810284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14615094
85                 X    =        -4454680
91
 Y    =       -5042999
38  feet           Y    =        -1537106
21  meter
 Z    =      -16000126
80                 Z    =        -4876838
65
 XDOT =      14650
136259                 XDOT =        4465
361532
 YDOT =     -17513
232017  feet/sec       YDOT =       -5338
033119  meter/sec
 ZDOT =      -7842
344457                 ZDOT =       -2390
346590


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   15354
52439534  
00016717  00000-0  10270-3 0  9022
2 25544  51
6432 234
1451 0008400 302
1598  57
8739 15
54962074 17036


Satellite: ISS
Catalog Number: 25544
Epoch time:      15354
52439534   =   yrday
fracday
Element set:     902
Inclination:       51
6432  deg
RA of node:       234
1451  deg
Eccentricity:     
0008400     
Arg of perigee:   302
1598  deg
Mean anomaly:      57
8739  deg
Mean motion:   15
54962074  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1703
Checksum:              302


Coasting Arc #4 (Orbit 1718)
---------------------------------------

Vector Time (GMT): 2015/355/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3037792
38                 A    =         6774875
64  meter
 Y    =       -2951908
99  meter          E    =           
0006257
 Z    =        5291113
22                 I    =           51
34553
 XDOT =       5201
648883                 Wp   =          315
87428
 YDOT =       5630
520320  meter/sec      RA   =          228
22006  deg
 ZDOT =        159
359493                 TA   =          132
62698
                                          MA   =          132
57421
                                          Ha   =            219
248  n
mi
                                          Hp   =            215
516

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9966510
45                 X    =         3044873
22
 Y    =       -9684740
78  feet           Y    =        -2917899
12  meter
 Z    =       17359295
36                 Z    =         5305887
32
 XDOT =      17065
777176                 XDOT =        5137
526312
 YDOT =      18472
835697  feet/sec       YDOT =        5688
330054  meter/sec
 ZDOT =        522
832981                 ZDOT =         184
472804

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9750115
48                 X    =         2971835
20
 Y    =        9788797
14  feet           Y    =         2983625
37  meter
 Z    =       17423701
34                 Z    =         5310744
17
 XDOT =     -17642
220609                 XDOT =       -5377
348842
 YDOT =      16476
753052  feet/sec       YDOT =        5022
114330  meter/sec
 ZDOT =        630
390083                 ZDOT =         192
142897


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   15355
55267911  
00016717  00000-0  10270-3 0  9035
2 25544  51
6433 229
0122 0008361 305
6520  54
3854 15
54982506 17193


Satellite: ISS
Catalog Number: 25544
Epoch time:      15355
55267911   =   yrday
fracday
Element set:     903
Inclination:       51
6433  deg
RA of node:       229
0122  deg
Eccentricity:     
0008361     
Arg of perigee:   305
6520  deg
Mean anomaly:      54
3854  deg
Mean motion:   15
54982506  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1719
Checksum:              302


Coasting Arc #5 (Orbit 1733)
---------------------------------------

Vector Time (GMT): 2015/356/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4418001
28                 A    =         6776131
87  meter
 Y    =        1304168
16  meter          E    =           
0006077
 Z    =       -4973875
75                 I    =           51
37127
 XDOT =      -4122
190497                 Wp   =           70
60244
 YDOT =      -6126
726494  meter/sec      RA   =          223
19138  deg
 ZDOT =       2059
089116                 TA   =          219
48534
                                          MA   =          219
52964
                                          Ha   =            219
374  n
mi
                                          Hp   =            215
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14494754
85                 X    =        -4408095
14
 Y    =        4278766
94  feet           Y    =         1254818
94  meter
 Z    =      -16318490
01                 Z    =        -4995313
46
 XDOT =     -13524
247038                 XDOT =       -4063
375885
 YDOT =     -20100
808706  feet/sec       YDOT =       -6172
494863  meter/sec
 ZDOT =       6755
541720                 ZDOT =        2039
206609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4621677
44                 X    =        -1408687
29
 Y    =      -14283009
54  feet           Y    =        -4353461
31  meter
 Z    =      -16411417
27                 Z    =        -5002199
98
 XDOT =      18726
899291                 XDOT =        5707
958904
 YDOT =     -13709
201075  feet/sec       YDOT =       -4178
564488  meter/sec
 ZDOT =       6670
675077                 ZDOT =        2033
221764


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   15356
51667752  
00016717  00000-0  10270-3 0  9040
2 25544  51
6425 224
1997 0008491 309
1595  50
8803 15
55015687 17345


Satellite: ISS
Catalog Number: 25544
Epoch time:      15356
51667752   =   yrday
fracday
Element set:     904
Inclination:       51
6425  deg
RA of node:       224
1997  deg
Eccentricity:     
0008491     
Arg of perigee:   309
1595  deg
Mean anomaly:      50
8803  deg
Mean motion:   15
55015687  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1734
Checksum:              329


Coasting Arc #6 (Orbit 1749)
---------------------------------------

Vector Time (GMT): 2015/357/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5510734
09                 A    =         6779893
01  meter
 Y    =         335272
78  meter          E    =           
0009096
 Z    =        3937506
83                 I    =           51
40828
 XDOT =       2504
254850                 Wp   =           29
81553
 YDOT =       6036
632940  meter/sec      RA   =          218
17388  deg
 ZDOT =      -4007
098424                 TA   =          102
20624
                                          MA   =          102
10435
                                          Ha   =            219
573  n
mi
                                          Hp   =            214
866

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18079836
26                 X    =         5487448
48
 Y    =        1099976
33  feet           Y    =          396766
88  meter
 Z    =       12918329
49                 Z    =         3964220
40
 XDOT =       8216
059220                 XDOT =        2456
030611
 YDOT =      19805
226182  feet/sec       YDOT =        6064
367918  meter/sec
 ZDOT =     -13146
648373                 ZDOT =       -3995
049784

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -358513
00                 X    =         -109274
76
 Y    =       18026798
65  feet           Y    =         5494568
23  meter
 Z    =       13033789
27                 Z    =         3972698
97
 XDOT =     -18130
510692                 XDOT =       -5526
179659
 YDOT =       9135
464062  feet/sec       YDOT =        2784
489446  meter/sec
 ZDOT =     -13095
627174                 ZDOT =       -3991
547163


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   15357
54492329  
00016717  00000-0  10270-3 0  9051
2 25544  51
6424 219
0670 0008648 313
2497  46
7933 15
55072585 17502


Satellite: ISS
Catalog Number: 25544
Epoch time:      15357
54492329   =   yrday
fracday
Element set:     905
Inclination:       51
6424  deg
RA of node:       219
0670  deg
Eccentricity:     
0008648     
Arg of perigee:   313
2497  deg
Mean anomaly:      46
7933  deg
Mean motion:   15
55072585  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1750
Checksum:              327


Coasting Arc #7 (Orbit 1764)
---------------------------------------

Vector Time (GMT): 2015/358/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6110484
64                 A    =         6784253
25  meter
 Y    =       -1765090
92  meter          E    =           
0010333
 Z    =       -2341169
27                 I    =           51
44676
 XDOT =       -487
598921                 Wp   =          349
67077
 YDOT =      -5444
813407  meter/sec      RA   =          213
17072  deg
 ZDOT =       5383
954385                 TA   =          344
11604
                                          MA   =          344
14842
                                          Ha   =            219
680  n
mi
                                          Hp   =            214
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20047521
78                 X    =        -6078920
33
 Y    =       -5790980
70  feet           Y    =        -1833245
66  meter
 Z    =       -7681001
55                 Z    =        -2370776
24
 XDOT =      -1599
733993                 XDOT =        -452
830578
 YDOT =     -17863
561047  feet/sec       YDOT =       -5450
072232  meter/sec
 ZDOT =      17663
892339                 ZDOT =        5381
669601

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4614013
20                 X    =         1406351
22
 Y    =      -20301991
90  feet           Y    =        -6188047
13  meter
 Z    =       -7808737
35                 Z    =        -2380103
15
 XDOT =      16250
923542                 XDOT =        4953
281496
 YDOT =      -3089
499804  feet/sec       YDOT =        -941
679540  meter/sec
 ZDOT =      17654
982434                 ZDOT =        5381
238646


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   15358
50888836  
00016717  00000-0  10270-3 0  9061
2 25544  51
6408 214
2538 0008665 316
3183  43
7284 15
55046843 17659


Satellite: ISS
Catalog Number: 25544
Epoch time:      15358
50888836   =   yrday
fracday
Element set:     906
Inclination:       51
6408  deg
RA of node:       214
2538  deg
Eccentricity:     
0008665     
Arg of perigee:   316
3183  deg
Mean anomaly:      43
7284  deg
Mean motion:   15
55046843  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1765
Checksum:              334


Coasting Arc #8 (Orbit 1780)
---------------------------------------

Vector Time (GMT): 2015/359/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6108902
44                 A    =         6786500
05  meter
 Y    =        2927882
90  meter          E    =           
0004636
 Z    =         382268
69                 I    =           51
48126
 XDOT =      -1759
289293                 Wp   =          112
67029
 YDOT =       4459
013242  meter/sec      RA   =          208
18189  deg
 ZDOT =      -5981
724252                 TA   =           63
20037
                                          MA   =           63
15296
                                          Ha   =            219
888  n
mi
                                          Hp   =            214
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20042330
84                 X    =         6073851
21
 Y    =        9605915
04  feet           Y    =         2996000
66  meter
 Z    =        1254162
37                 Z    =          411859
49
 XDOT =      -5771
946498                 XDOT =       -1779
963591
 YDOT =      14629
308538  feet/sec       YDOT =        4439
224766  meter/sec
 ZDOT =     -19625
079567                 ZDOT =       -5990
320194

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8064807
65                 X    =        -2458153
37
 Y    =       20702451
36  feet           Y    =         6310107
17  meter
 Z    =        1381643
16                 Z    =          421124
84
 XDOT =     -13502
593489                 XDOT =       -4115
590495
 YDOT =      -3936
581960  feet/sec       YDOT =       -1199
870181  meter/sec
 ZDOT =     -19663
054908                 ZDOT =       -5993
299136


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   15359
53709923  
00016717  00000-0  10270-3 0  9075
2 25544  51
6404 209
1208 0008561 320
2670  39
7855 15
55074852 17810


Satellite: ISS
Catalog Number: 25544
Epoch time:      15359
53709923   =   yrday
fracday
Element set:     907
Inclination:       51
6404  deg
RA of node:       209
1208  deg
Eccentricity:     
0008561     
Arg of perigee:   320
2670  deg
Mean anomaly:      39
7855  deg
Mean motion:   15
55074852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1781
Checksum:              319


Coasting Arc #9 (Orbit 1796)
---------------------------------------

Vector Time (GMT): 2015/360/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5416073
29                 A    =         6785347
24  meter
 Y    =       -3730476
55  meter          E    =           
0015070
 Z    =        1629295
61                 I    =           51
50518
 XDOT =       3960
330592                 Wp   =           29
10892
 YDOT =      -3249
028124  meter/sec      RA   =          203
19498  deg
 ZDOT =       5716
455870                 TA   =          348
78478
                                          MA   =          348
81834
                                          Ha   =            219
966  n
mi
                                          Hp   =            214
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17769269
32                 X    =        -5381870
06
 Y    =      -12239096
31  feet           Y    =        -3790851
59  meter
 Z    =        5345458
05                 Z    =         1603068
40
 XDOT =      12993
210603                 XDOT =        3968
599639
 YDOT =     -10659
541088  feet/sec       YDOT =       -3204
695451  meter/sec
 ZDOT =      18754
776476                 ZDOT =        5735
713890

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10535512
23                 X    =         3211224
13
 Y    =      -18861036
79  feet           Y    =        -5748844
01  meter
 Z    =        5232648
05                 Z    =         1594911
12
 XDOT =      10429
813843                 XDOT =        3179
007259
 YDOT =      11061
077257  feet/sec       YDOT =        3371
416348  meter/sec
 ZDOT =      18838
667369                 ZDOT =        5742
025814


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   15360
56528962  
00016717  00000-0  10270-3 0  9083
2 25544  51
6392 203
9857 0008623 323
3611  36
6952 15
55129030 17976


Satellite: ISS
Catalog Number: 25544
Epoch time:      15360
56528962   =   yrday
fracday
Element set:     908
Inclination:       51
6392  deg
RA of node:       203
9857  deg
Eccentricity:     
0008623     
Arg of perigee:   323
3611  deg
Mean anomaly:      36
6952  deg
Mean motion:   15
55129030  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1797
Checksum:              323


Coasting Arc #10 (Orbit 1811)
---------------------------------------

Vector Time (GMT): 2015/361/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4084005
21                 A    =         6781508
17  meter
 Y    =        4203774
05  meter          E    =           
0007251
 Z    =       -3419119
78                 I    =           51
52120
 XDOT =      -5827
092894                 Wp   =            1
77218
 YDOT =       1923
260156  meter/sec      RA   =          198
20292  deg
 ZDOT =      -4588
768770                 TA   =          218
29447
                                          MA   =          218
34598
                                          Ha   =            220
128  n
mi
                                          Hp   =            214
080

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13398967
23                 X    =         4053302
58
 Y    =       13791909
60  feet           Y    =         4249272
73  meter
 Z    =      -11217584
57                 Z    =        -3399354
98
 XDOT =     -19117
758838                 XDOT =       -5825
876019
 YDOT =       6309
908647  feet/sec       YDOT =        1858
104971  meter/sec
 ZDOT =     -15055
015648                 ZDOT =       -4617
072077

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12228167
07                 X    =        -3727145
32
 Y    =       14903556
89  feet           Y    =         4542604
14  meter
 Z    =      -11132799
26                 Z    =        -3393277
21
 XDOT =      -7272
312754                 XDOT =       -2216
600927
 YDOT =     -17321
390119  feet/sec       YDOT =       -5279
559708  meter/sec
 ZDOT =     -15177
821906                 ZDOT =       -4626
200117


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   15361
52920329  
00016717  00000-0  10270-3 0  9094
2 25544  51
6382 199
1727 0008679 327
6258  32
4362 15
55140364 18122


Satellite: ISS
Catalog Number: 25544
Epoch time:      15361
52920329   =   yrday
fracday
Element set:     909
Inclination:       51
6382  deg
RA of node:       199
1727  deg
Eccentricity:     
0008679     
Arg of perigee:   327
6258  deg
Mean anomaly:      32
4362  deg
Mean motion:   15
55140364  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1812
Checksum:              320


Coasting Arc #11 (Orbit 1827)
---------------------------------------

Vector Time (GMT): 2015/362/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2201070
69                 A    =         6777059
85  meter
 Y    =       -4352031
40  meter          E    =           
0005076
 Z    =        4701249
85                 I    =           51
53700
 XDOT =       7124
972187                 Wp   =           36
41349
 YDOT =       -599
916824  meter/sec      RA   =          193
19708  deg
 ZDOT =       2782
934832                 TA   =           26
00403
                                          MA   =           25
97854
                                          Ha   =            220
327  n
mi
                                          Hp   =            213
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7221360
53                 X    =        -2175078
12
 Y    =      -14278318
25  feet           Y    =        -4376500
23  meter
 Z    =       15424048
08                 Z    =         4690620
49
 XDOT =      23375
893001                 XDOT =        7117
632847
 YDOT =      -1968
231049  feet/sec       YDOT =        -520
281911  meter/sec
 ZDOT =       9130
363623                 ZDOT =        2817
528088

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13232553
91                 X    =         4033282
43
 Y    =       -9072568
85  feet           Y    =        -2765318
99  meter
 Z    =       15378806
54                 Z    =         4687460
23
 XDOT =       4248
694596                 XDOT =        1295
002113
 YDOT =      21913
820898  feet/sec       YDOT =        6679
332610  meter/sec
 ZDOT =       9280
174893                 ZDOT =        2828
597307


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   15362
55736019  
00016717  00000-0  10270-3 0  9101
2 25544  51
6382 194
0375 0008733 331
6435  28
4242 15
55135432 18287


Satellite: ISS
Catalog Number: 25544
Epoch time:      15362
55736019   =   yrday
fracday
Element set:     910
Inclination:       51
6382  deg
RA of node:       194
0375  deg
Eccentricity:     
0008733     
Arg of perigee:   331
6435  deg
Mean anomaly:      28
4242  deg
Mean motion:   15
55135432  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1828
Checksum:              302


Coasting Arc #12 (Orbit 1842)
---------------------------------------

Vector Time (GMT): 2015/363/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          27260
59                 A    =         6774379
35  meter
 Y    =        4245454
83  meter          E    =           
0014246
 Z    =       -5289309
40                 I    =           51
55939
 XDOT =      -7613
782706                 Wp   =           51
28914
 YDOT =       -650
633501  meter/sec      RA   =          188
18184  deg
 ZDOT =       -553
762677                 TA   =          213
37116
                                          MA   =          213
46104
                                          Ha   =            220
321  n
mi
                                          Hp   =            213
482

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          89437
62                 X    =            5477
87
 Y    =       13928657
57  feet           Y    =         4245638
15  meter
 Z    =      -17353377
30                 Z    =        -5289229
66
 XDOT =     -24979
602054                 XDOT =       -7603
251368
 YDOT =      -2134
624348  feet/sec       YDOT =        -735
716939  meter/sec
 ZDOT =      -1816
806684                 ZDOT =        -590
722759

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13753100
50                 X    =        -4191945
03
 Y    =        2203219
25  feet           Y    =          671541
23  meter
 Z    =      -17353767
77                 Z    =        -5289428
42
 XDOT =      -1320
570118                 XDOT =        -402
509772
 YDOT =     -24011
837302  feet/sec       YDOT =       -7318
808010  meter/sec
 ZDOT =      -1976
664277                 ZDOT =        -602
487272


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   15363
52123851  
00016717  00000-0  10270-3 0  9114
2 25544  51
6376 189
2238 0008588 335
2833  24
7907 15
55193595 18432


Satellite: ISS
Catalog Number: 25544
Epoch time:      15363
52123851   =   yrday
fracday
Element set:     911
Inclination:       51
6376  deg
RA of node:       189
2238  deg
Eccentricity:     
0008588     
Arg of perigee:   335
2833  deg
Mean anomaly:      24
7907  deg
Mean motion:   15
55193595  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1843
Checksum:              330


Coasting Arc #13 (Orbit 1858)
---------------------------------------

Vector Time (GMT): 2015/364/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2237304
96                 A    =         6775252
69  meter
 Y    =       -3901116
19  meter          E    =           
0011088
 Z    =        5069375
93                 I    =           51
59460
 XDOT =       7233
777817                 Wp   =            6
64574
 YDOT =       1816
248399  meter/sec      RA   =          183
16571  deg
 ZDOT =      -1783
678039                 TA   =          100
68309
                                          MA   =          100
55820
                                          Ha   =            220
386  n
mi
                                          Hp   =            213
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7340239
36                 X    =         2256137
19
 Y    =      -12798937
63  feet           Y    =        -3875992
06  meter
 Z    =       16631810
78                 Z    =         5080289
74
 XDOT =      23732
866855                 XDOT =        7221
594751
 YDOT =       5958
820208  feet/sec       YDOT =        1897
073231  meter/sec
 ZDOT =      -5851
962071                 ZDOT =       -1748
567849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13794697
31                 X    =         4204623
74
 Y    =        5079576
41  feet           Y    =         1548254
89  meter
 Z    =       16679726
55                 Z    =         5083980
65
 XDOT =      -1684
655101                 XDOT =        -513
482875
 YDOT =      23413
029238  feet/sec       YDOT =        7136
291312  meter/sec
 ZDOT =      -5700
293360                 ZDOT =       -1737
449416


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   15364
54935840  
00016717  00000-0  10270-3 0  9127
2 25544  51
6379 184
0893 0008607 338
7685  21
3109 15
55195794 18597


Satellite: ISS
Catalog Number: 25544
Epoch time:      15364
54935840   =   yrday
fracday
Element set:     912
Inclination:       51
6379  deg
RA of node:       184
0893  deg
Eccentricity:     
0008607     
Arg of perigee:   338
7685  deg
Mean anomaly:      21
3109  deg
Mean motion:   15
55195794  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1859
Checksum:              348


Coasting Arc #14 (Orbit 1873)
---------------------------------------

Vector Time (GMT): 2015/365/12:05:57
727
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4221479
46                 A    =         6778869
40  meter
 Y    =        3375417
70  meter          E    =           
0007317
 Z    =       -4091244
95                 I    =           51
63938
 XDOT =      -5993
179795                 Wp   =           39
33078
 YDOT =      -2849
854790  meter/sec      RA   =          178
15964  deg
 ZDOT =       3842
025723                 TA   =          270
34286
                                          MA   =          270
42671
                                          Ha   =            220
426  n
mi
                                          Hp   =            212
947

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13849998
22                 X    =        -4239037
01
 Y    =       11074205
05  feet           Y    =         3328112
27  meter
 Z    =      -13422719
65                 Z    =        -4111794
33
 XDOT =     -19662
663371                 XDOT =       -5979
529449
 YDOT =      -9349
917289  feet/sec       YDOT =       -2916
798276  meter/sec
 ZDOT =      12605
071271                 ZDOT =        3812
945506

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13344788
20                 X    =        -4067491
44
 Y    =      -11574335
70  feet           Y    =        -3527857
52  meter
 Z    =      -13512263
03                 Z    =        -4118537
77
 XDOT =       4843
435129                 XDOT =        1476
279027
 YDOT =     -20118
111522  feet/sec       YDOT =       -6132
000392  meter/sec
 ZDOT =      12479
667281                 ZDOT =        3803
802587


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   15365
51320319  
00016717  00000-0  10270-3 0  9135
2 25544  51
6380 179
2751 0008540 342
9097  17
1768 15
55248207 18747


Satellite: ISS
Catalog Number: 25544
Epoch time:      15365
51320319   =   yrday
fracday
Element set:     913
Inclination:       51
6380  deg
RA of node:       179
2751  deg
Eccentricity:     
0008540     
Arg of perigee:   342
9097  deg
Mean anomaly:      17
1768  deg
Mean motion:   15
55248207  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1874
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