[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 6th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14800 38 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 272)
---------------------------------------
Vector Time (GMT): 2015/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 551886
44 A = 6780978
83 meter
Y = -4234221
51 meter E =
0004041
Z = 5268161
22 I = 51
64651
XDOT = 7622
198995 Wp = 195
69079
YDOT = -25
430929 meter/sec RA = 174
90843 deg
ZDOT = -822
883435 TA = 262
15314
MA = 262
19902
Ha = 222
948 n
mi
Hp = 217
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1810651
05 X = 573602
95
Y = -13891802
85 feet Y = -4227928
98 meter
Z = 17283993
51 Z = 5270894
55
XDOT = 25007
214552 XDOT = 7625
914097
YDOT = -83
434805 feet/sec YDOT = 59
826291 meter/sec
ZDOT = -2699
748804 ZDOT = -785
847574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13891202
35 X = 4234038
48
Y = -1693134
01 feet Y = -516067
25 meter
Z = 17296383
14 Z = 5271937
58
XDOT = 5982
762493 XDOT = 1823
546008
YDOT = 23254
528963 feet/sec YDOT = 7087
980428 meter/sec
ZDOT = -2541
500833 ZDOT = -774
649454
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 15005
54694699
00016717 00000-0 10270-3 0 9000
2 25544 51
6398 175
8004 0006647 215
6632 144
4077 15
52949905 2735
Satellite: ISS
Catalog Number: 25544
Epoch time: 15005
54694699 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 175
8004 deg
Eccentricity:
0006647
Arg of perigee: 215
6632 deg
Mean anomaly: 144
4077 deg
Mean motion: 15
52949905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 273
Checksum: 329
Coasting Arc #2 (Orbit 287)
---------------------------------------
Vector Time (GMT): 2015/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1874043
29 A = 6782265
93 meter
Y = 4283755
30 meter E =
0011454
Z = -4922459
10 I = 51
68394
XDOT = -7286
471572 Wp = 139
28466
YDOT = -545
868227 meter/sec RA = 169
92294 deg
ZDOT = 2293
549171 TA = 153
18391
MA = 153
12465
Ha = 222
677 n
mi
Hp = 217
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6148436
00 X = -1897894
78
Y = 14054315
29 feet Y = 4262665
52 meter
Z = -16149800
19 Z = -4931620
37
XDOT = -23905
746628 XDOT = -7290
967077
YDOT = -1790
906258 feet/sec YDOT = -627
375582 meter/sec
ZDOT = 7524
767620 ZDOT = 2258
142346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15135663
89 X = -4613350
35
Y = -2224736
25 feet Y = -678099
61 meter
Z = -16189666
99 Z = -4934610
50
XDOT = -4598
559458 XDOT = -1401
640923
YDOT = -22502
727201 feet/sec YDOT = -6858
831251 meter/sec
ZDOT = 7373
554061 ZDOT = 2247
459278
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 15006
51217231
00016717 00000-0 10270-3 0 9012
2 25544 51
6409 170
9962 0006658 219
1114 140
9558 15
53018947 2888
Satellite: ISS
Catalog Number: 25544
Epoch time: 15006
51217231 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 170
9962 deg
Eccentricity:
0006658
Arg of perigee: 219
1114 deg
Mean anomaly: 140
9558 deg
Mean motion: 15
53018947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 288
Checksum: 304
Coasting Arc #3 (Orbit 303)
---------------------------------------
Vector Time (GMT): 2015/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3073295
77 A = 6784824
11 meter
Y = -4299168
66 meter E =
0005345
Z = 4249501
54 I = 51
72313
XDOT = 6655
185691 Wp = 112
26838
YDOT = 1172
310905 meter/sec RA = 164
94414 deg
ZDOT = -3625
439210 TA = 14
76818
MA = 14
75258
Ha = 222
483 n
mi
Hp = 217
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10082991
39 X = 3100499
45
Y = -14104884
05 feet Y = -4264649
19 meter
Z = 13941934
18 Z = 4264496
67
XDOT = 21834
598725 XDOT = 6659
192813
YDOT = 3846
164386 feet/sec YDOT = 1246
756112 meter/sec
ZDOT = -11894
485598 ZDOT = -3593
100219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16302452
83 X = 4968987
62
Y = 5747455
51 feet Y = 1751824
44 meter
Z = 14006740
70 Z = 4269254
57
XDOT = 2724
700037 XDOT = 830
488571
YDOT = 20935
654054 feet/sec YDOT = 6381
187356 meter/sec
ZDOT = -11756
468166 ZDOT = -3583
371497
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 15007
54173133
00016717 00000-0 10270-3 0 9029
2 25544 51
6407 165
8717 0006642 223
2807 136
7823 15
53020768 3046
Satellite: ISS
Catalog Number: 25544
Epoch time: 15007
54173133 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 165
8717 deg
Eccentricity:
0006642
Arg of perigee: 223
2807 deg
Mean anomaly: 136
7823 deg
Mean motion: 15
53020768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 304
Checksum: 289
Coasting Arc #4 (Orbit 318)
---------------------------------------
Vector Time (GMT): 2015/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4119100
30 A = 6787717
56 meter
Y = 4270203
45 meter E =
0004182
Z = -3301679
87 I = 51
76513
XDOT = -5732
027954 Wp = 181
54413
YDOT = -1872
889793 meter/sec RA = 159
97375 deg
ZDOT = 4724
641172 TA = 140
20797
MA = 140
17729
Ha = 222
291 n
mi
Hp = 217
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13514108
59 X = -4150506
45
Y = 14009853
82 feet Y = 4223965
51 meter
Z = -10832283
02 Z = -3321765
53
XDOT = -18805
865992 XDOT = -5733
609097
YDOT = -6144
651551 feet/sec YDOT = -1936
998065 meter/sec
ZDOT = 15500
791248 ZDOT = 4696
792531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17310739
91 X = -5276313
52
Y = -8795594
07 feet Y = -2680897
07 meter
Z = -10918850
64 Z = -3328065
67
XDOT = -254
914012 XDOT = -77
697791
YDOT = -18610
640056 feet/sec YDOT = -5672
523089 meter/sec
ZDOT = 15382
067576 ZDOT = 4688
454197
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 15008
50692685
00016717 00000-0 10270-3 0 9035
2 25544 51
6423 161
0677 0006573 226
6723 133
3882 15
53071287 3190
Satellite: ISS
Catalog Number: 25544
Epoch time: 15008
50692685 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 161
0677 deg
Eccentricity:
0006573
Arg of perigee: 226
6723 deg
Mean anomaly: 133
3882 deg
Mean motion: 15
53071287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 319
Checksum: 309
Coasting Arc #5 (Orbit 334)
---------------------------------------
Vector Time (GMT): 2015/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4935655
29 A = 6790410
32 meter
Y = -4141096
24 meter E =
0011867
Z = 2120476
74 I = 51
80295
XDOT = 4605
967370 Wp = 138
30551
YDOT = 2653
584892 meter/sec RA = 155
01164 deg
ZDOT = -5529
606160 TA = 18
25369
MA = 18
21113
Ha = 222
050 n
mi
Hp = 218
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16193094
77 X = 4971294
80
Y = -13586273
74 feet Y = -4085703
31 meter
Z = 6956944
70 Z = 2144539
40
XDOT = 15111
441504 XDOT = 4602
812491
YDOT = 8705
987178 feet/sec YDOT = 2705
074295 meter/sec
ZDOT = -18141
752494 ZDOT = -5507
239119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17886458
05 X = 5451792
41
Y = 11199382
65 feet Y = 3413571
83 meter
Z = 7060501
31 Z = 2152040
80
XDOT = -2794
163770 XDOT = -851
661117
YDOT = 15858
329640 feet/sec YDOT = 4833
618874 meter/sec
ZDOT = -18046
579512 ZDOT = -5500
597435
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 15009
53645262
00016717 00000-0 10270-3 0 9049
2 25544 51
6419 155
9432 0006587 231
2153 128
8411 15
53082892 3359
Satellite: ISS
Catalog Number: 25544
Epoch time: 15009
53645262 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 155
9432 deg
Eccentricity:
0006587
Arg of perigee: 231
2153 deg
Mean anomaly: 128
8411 deg
Mean motion: 15
53082892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 335
Checksum: 302
Coasting Arc #6 (Orbit 349)
---------------------------------------
Vector Time (GMT): 2015/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5502887
06 A = 6791963
24 meter
Y = 3895265
63 meter E =
0004306
Z = -799884
37 I = 51
83820
XDOT = -3330
863098 Wp = 16
09379
YDOT = -3484
510935 meter/sec RA = 150
05657 deg
ZDOT = 5957
900307 TA = 335
28850
MA = 335
30912
Ha = 221
846 n
mi
Hp = 218
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18054091
41 X = -5542150
35
Y = 12779742
90 feet Y = 3833509
25 meter
Z = -2624292
56 Z = -826711
40
XDOT = -10928
028536 XDOT = -3320
591905
YDOT = -11432
122490 feet/sec YDOT = -3521
701456 meter/sec
ZDOT = 19546
917017 ZDOT = 5941
744673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17924035
89 X = -5463246
14
Y = -12937630
31 feet Y = -3943389
72 meter
Z = -2739637
91 Z = -835041
63
XDOT = 6300
727967 XDOT = 1920
461884
YDOT = -12846
056557 feet/sec YDOT = -3915
478039 meter/sec
ZDOT = 19478
430056 ZDOT = 5937
025481
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 15010
50161726
00016717 00000-0 10270-3 0 9057
2 25544 51
6435 151
1394 0006480 234
9851 125
0694 15
53119786 3501
Satellite: ISS
Catalog Number: 25544
Epoch time: 15010
50161726 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 151
1394 deg
Eccentricity:
0006480
Arg of perigee: 234
9851 deg
Mean anomaly: 125
0694 deg
Mean motion: 15
53119786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 350
Checksum: 292
Coasting Arc #7 (Orbit 365)
---------------------------------------
Vector Time (GMT): 2015/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5797448
05 A = 6792024
01 meter
Y = -3473123
26 meter E =
0011554
Z = -595977
04 I = 51
86498
XDOT = 1991
637102 Wp = 172
47425
YDOT = 4349
029048 meter/sec RA = 145
10513 deg
ZDOT = -5994
804695 TA = 13
93810
MA = 13
90623
Ha = 221
614 n
mi
Hp = 218
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19020498
84 X = 5838749
46
Y = -11394761
37 feet Y = -3408061
50 meter
Z = -1955305
26 Z = -567714
06
XDOT = 6534
242460 XDOT = 1971
977536
YDOT = 14268
468004 feet/sec YDOT = 4371
190948 meter/sec
ZDOT = -19667
994407 ZDOT = -5985
177493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17179509
86 X = 5236314
61
Y = 14033692
06 feet Y = 4277469
34 meter
Z = -1833878
29 Z = -558966
10
XDOT = -10135
513546 XDOT = -3089
304529
YDOT = 9853
735616 feet/sec YDOT = 3003
418616 meter/sec
ZDOT = -19627
562016 ZDOT = -5982
480903
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 15011
53110925
00016717 00000-0 10270-3 0 9067
2 25544 51
6429 146
0148 0006445 239
8754 120
1760 15
53157096 3664
Satellite: ISS
Catalog Number: 25544
Epoch time: 15011
53110925 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 146
0148 deg
Eccentricity:
0006445
Arg of perigee: 239
8754 deg
Mean anomaly: 120
1760 deg
Mean motion: 15
53157096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 366
Checksum: 295
Coasting Arc #8 (Orbit 381)
---------------------------------------
Vector Time (GMT): 2015/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5830895
76 A = 6790504
93 meter
Y = 2876830
50 meter E =
0007544
Z = 1946869
42 I = 51
88671
XDOT = -673
375581 Wp = 70
93212
YDOT = -5174
878988 meter/sec RA = 140
15396 deg
ZDOT = 5614
661756 TA = 310
44935
MA = 310
51511
Ha = 221
350 n
mi
Hp = 218
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19130235
44 X = -5872088
91
Y = 9438420
27 feet Y = 2811395
30 meter
Z = 6387366
87 Z = 1918444
15
XDOT = -2209
237469 XDOT = -642
732632
YDOT = -16977
949436 feet/sec YDOT = -5182
237814 meter/sec
ZDOT = 18420
806285 ZDOT = 5611
465036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15639284
06 X = -4766853
78
Y = -14560444
34 feet Y = -4438023
44 meter
Z = 6265332
83 Z = 1909673
45
XDOT = 13977
702482 XDOT = 4260
403716
YDOT = -7070
361326 feet/sec YDOT = -2155
046132 meter/sec
ZDOT = 18408
010989 ZDOT = 5610
761749
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 15012
56058338
00016717 00000-0 10270-3 0 9071
2 25544 51
6441 140
8904 0006430 243
1928 116
8567 15
53193651 3827
Satellite: ISS
Catalog Number: 25544
Epoch time: 15012
56058338 = yrday
fracday
Element set: 907
Inclination: 51
6441 deg
RA of node: 140
8904 deg
Eccentricity:
0006430
Arg of perigee: 243
1928 deg
Mean anomaly: 116
8567 deg
Mean motion: 15
53193651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 382
Checksum: 302
Coasting Arc #9 (Orbit 396)
---------------------------------------
Vector Time (GMT): 2015/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5624155
82 A = 6787853
23 meter
Y = -2066485
41 meter E =
0003764
Z = -3184275
57 I = 51
90125
XDOT = -567
772696 Wp = 204
01843
YDOT = 5915
199901 meter/sec RA = 135
19975 deg
ZDOT = -4842
917166 TA = 12
58955
MA = 12
58015
Ha = 221
250 n
mi
Hp = 218
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18451954
79 X = 5662313
73
Y = -6779807
77 feet Y = -2003379
05 meter
Z = -10447098
34 Z = -3156861
92
XDOT = -1862
771311 XDOT = -610
350624
YDOT = 19406
823821 feet/sec YDOT = 5908
612685 meter/sec
ZDOT = -15888
835848 ZDOT = -4845
778640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13177057
15 X = 4016367
02
Y = 14671352
86 feet Y = 4471828
35 meter
Z = -10329514
16 Z = -3148435
92
XDOT = -17600
529771 XDOT = -5364
641474
YDOT = 4615
004393 feet/sec YDOT = 1406
653339 meter/sec
ZDOT = -15902
079214 ZDOT = -4846
953744
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 15013
52570106
00016717 00000-0 10270-3 0 9081
2 25544 51
6440 136
0863 0006407 247
7895 112
2578 15
53191853 3974
Satellite: ISS
Catalog Number: 25544
Epoch time: 15013
52570106 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 136
0863 deg
Eccentricity:
0006407
Arg of perigee: 247
7895 deg
Mean anomaly: 112
2578 deg
Mean motion: 15
53191853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 397
Checksum: 309
Coasting Arc #10 (Orbit 412)
---------------------------------------
Vector Time (GMT): 2015/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5221575
85 A = 6784541
64 meter
Y = 1081389
56 meter E =
0006017
Z = 4194444
17 I = 51
91321
XDOT = 1659
391795 Wp = 139
33308
YDOT = -6487
081839 meter/sec RA = 130
23992 deg
ZDOT = 3730
755018 TA = 272
43414
MA = 272
50302
Ha = 220
827 n
mi
Hp = 218
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17131154
35 X = -5253655
14
Y = 3547866
00 feet Y = 1022819
05 meter
Z = 13761299
77 Z = 4169000
90
XDOT = 5444
198802 XDOT = 1713
685946
YDOT = -21283
076899 feet/sec YDOT = -6468
221946 meter/sec
ZDOT = 12240
009900 ZDOT = 3738
947746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9944656
97 X = -3031131
44
Y = -14496748
95 feet Y = -4418609
08 meter
Z = 13652298
04 Z = 4161220
44
XDOT = 20641
435257 XDOT = 6291
509466
YDOT = -2575
591146 feet/sec YDOT = -785
040181 meter/sec
ZDOT = 12276
162208 ZDOT = 3741
774241
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 15014
55514063
00016717 00000-0 10270-3 0 9096
2 25544 51
6447 130
9613 0006380 252
2073 107
8384 15
53253630 4132
Satellite: ISS
Catalog Number: 25544
Epoch time: 15014
55514063 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 130
9613 deg
Eccentricity:
0006380
Arg of perigee: 252
2073 deg
Mean anomaly: 107
8384 deg
Mean motion: 15
53253630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 413
Checksum: 282
Coasting Arc #11 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2015/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4669654
28 A = 6781787
58 meter
Y = 76791
92 meter E =
0005640
Z = -4922696
90 I = 51
92365
XDOT = -2580
346304 Wp = 68
86056
YDOT = 6824
107084 meter/sec RA = 125
27495 deg
ZDOT = -2341
432034 TA = 178
29816
MA = 178
29624
Ha = 220
647 n
mi
Hp = 218
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15320388
04 X = 4692361
10
Y = 251941
99 feet Y = 129138
17 meter
Z = -16150580
38 Z = -4899957
50
XDOT = -8465
703098 XDOT = -2645
089509
YDOT = 22388
802769 feet/sec YDOT = 6794
890060 meter/sec
ZDOT = -7681
863628 ZDOT = -2354
123845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5991494
35 X = 1826207
48
Y = 14213076
06 feet Y = 4332145
58 meter
Z = -16053332
23 Z = -4893055
66
XDOT = -22844
652530 XDOT = -6963
050091
YDOT = 891
645224 feet/sec YDOT = 271
773464 meter/sec
ZDOT = -7737
332182 ZDOT = -2358
338849
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 15015
52022671
00016717 00000-0 10270-3 0 9105
2 25544 51
6449 126
1573 0006376 256
9073 103
1368 15
53237284 4286
Satellite: ISS
Catalog Number: 25544
Epoch time: 15015
52022671 = yrday
fracday
Element set: 910
Inclination: 51
6449 deg
RA of node: 126
1573 deg
Eccentricity:
0006376
Arg of perigee: 256
9073 deg
Mean anomaly: 103
1368 deg
Mean motion: 15
53237284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 428
Checksum: 295
Coasting Arc #12 (Orbit 443)
---------------------------------------
Vector Time (GMT): 2015/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4024050
09 A = 6779955
40 meter
Y = -1331900
92 meter E =
0004240
Z = 5294804
59 I = 51
93627
XDOT = 3306
100135 Wp = 233
54464
YDOT = -6870
598258 meter/sec RA = 120
30519 deg
ZDOT = 782
326777 TA = 208
99478
MA = 209
01834
Ha = 220
336 n
mi
Hp = 218
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13202264
09 X = -4034577
48
Y = -4369753
67 feet Y = -1376959
60 meter
Z = 17371406
13 Z = 5275230
96
XDOT = 10846
785220 XDOT = 3378
882822
YDOT = -22541
332868 feet/sec YDOT = -6833
220387 meter/sec
ZDOT = 2566
688901 ZDOT = 798
563544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1612034
92 X = -491348
24
Y = -13917247
86 feet Y = -4241977
15 meter
Z = 17287909
95 Z = 5269354
95
XDOT = 23990
060832 XDOT = 7312
170542
YDOT = 505
592788 feet/sec YDOT = 154
104682 meter/sec
ZDOT = 2637
347171 ZDOT = 803
863418
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 15016
54963280
00016717 00000-0 10270-3 0 9119
2 25544 51
6454 121
0321 0006303 261
4171 98
6267 15
53307354 4447
Satellite: ISS
Catalog Number: 25544
Epoch time: 15016
54963280 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 121
0321 deg
Eccentricity:
0006303
Arg of perigee: 261
4171 deg
Mean anomaly: 98
6267 deg
Mean motion: 15
53307354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 444
Checksum: 280
Coasting Arc #13 (Orbit 458)
---------------------------------------
Vector Time (GMT): 2015/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3335021
90 A = 6779949
02 meter
Y = 2632638
22 meter E =
0008498
Z = -5290774
25 I = 51
95162
XDOT = -3844
444208 Wp = 104
01233
YDOT = 6572
372133 meter/sec RA = 115
33553 deg
ZDOT = 846
150858 TA = 174
05523
MA = 174
04514
Ha = 220
054 n
mi
Hp = 218
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10941672
91 X = 3331035
69
Y = 8637264
51 feet Y = 2669910
65 meter
Z = -17358183
22 Z = -5274582
98
XDOT = -12613
005933 XDOT = -3921
762545
YDOT = 21562
900700 feet/sec YDOT = 6528
948694 meter/sec
ZDOT = 2776
085493 ZDOT = 827
288035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2974693
68 X = -906686
63
Y = 13706115
37 feet Y = 4177623
96 meter
Z = -17289380
21 Z = -5269803
09
XDOT = -23909
937844 XDOT = -7287
749055
YDOT = -1787
081573 feet/sec YDOT = -544
702463 meter/sec
ZDOT = 2694
226349 ZDOT = 821
200191
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 15017
51468732
00016717 00000-0 10270-3 0 9120
2 25544 51
6456 116
2284 0006197 266
1267 93
9177 15
53313414 4590
Satellite: ISS
Catalog Number: 25544
Epoch time: 15017
51468732 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 116
2284 deg
Eccentricity:
0006197
Arg of perigee: 266
1267 deg
Mean anomaly: 93
9177 deg
Mean motion: 15
53313414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 459
Checksum: 314
Coasting Arc #14 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2015/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2639581
15 A = 6781528
16 meter
Y = -3885424
61 meter E =
0003610
Z = 4892913
03 I = 51
97036
XDOT = 4220
207959 Wp = 356
05781
YDOT = -5922
561803 meter/sec RA = 110
36755 deg
ZDOT = -2422
984295 TA = 117
61956
MA = 117
58289
Ha = 220
047 n
mi
Hp = 218
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8660043
14 X = -2619704
91
Y = -12747456
07 feet Y = -3914831
31 meter
Z = 16052864
27 Z = 4880138
62
XDOT = 13845
826637 XDOT = 4297
891598
YDOT = -19430
977044 feet/sec YDOT = -5874
934181 meter/sec
ZDOT = -7949
423540 ZDOT = -2402
295279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7439546
32 X = 2267573
72
Y = -13560117
40 feet Y = -4133123
78 meter
Z = 15998900
00 Z = 4876464
72
XDOT = 22617
467604 XDOT = 6893
804126
YDOT = 3122
076264 feet/sec YDOT = 951
608845 meter/sec
ZDOT = -7859
848126 ZDOT = -2395
681709
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 15018
54406105
00016717 00000-0 10270-3 0 9131
2 25544 51
6461 111
1031 0006185 270
8634 89
1810 15
53346750 4755
Satellite: ISS
Catalog Number: 25544
Epoch time: 15018
54406105 = yrday
fracday
Element set: 913
Inclination: 51
6461 deg
RA of node: 111
1031 deg
Eccentricity:
0006185
Arg of perigee: 270
8634 deg
Mean anomaly: 89
1810 deg
Mean motion: 15
53346750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 280
Coasting Arc #15 (Orbit 489)
---------------------------------------
Vector Time (GMT): 2015/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1973493
78 A = 6784328
27 meter
Y = 5004865
54 meter E =
0002245
Z = -4135523
25 I = 51
98988
XDOT = -4458
092919 Wp = 153
87475
YDOT = 4920
657464 meter/sec RA = 105
40657 deg
ZDOT = 3826
446863 TA = 155
45562
MA = 155
44493
Ha = 220
026 n
mi
Hp = 218
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6474717
12 X = 1937470
02
Y = 16420162
53 feet Y = 5026733
25 meter
Z = -13567989
66 Z = -4126023
76
XDOT = -14626
289104 XDOT = -4531
372674
YDOT = 16143
889316 feet/sec YDOT = 4870
394220 meter/sec
ZDOT = 12553
959523 ZDOT = 3804
612959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11480433
93 X = -3499236
26
Y = 13446949
22 feet Y = 4098630
12 meter
Z = -13528238
47 Z = -4123407
08
XDOT = -20152
804430 XDOT = -6142
574790
YDOT = -4666
756301 feet/sec YDOT = -1422
427321 meter/sec
ZDOT = 12459
648479 ZDOT = 3797
700857
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 15019
50908409
00016717 00000-0 10270-3 0 9143
2 25544 51
6459 106
2992 0006127 274
2365 85
8087 15
53372233 4909
Satellite: ISS
Catalog Number: 25544
Epoch time: 15019
50908409 = yrday
fracday
Element set: 914
Inclination: 51
6459 deg
RA of node: 106
2992 deg
Eccentricity:
0006127
Arg of perigee: 274
2365 deg
Mean anomaly: 85
8087 deg
Mean motion: 15
53372233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 490
Checksum: 316
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