[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 22nd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
028/18:41:47
067 1
0 -1
6 1
6
N/A 0
7 0
2 220
5
000/00:03:30
135 -1
0 -0
0 216
6
Coasting Arc #1 (Orbit 520)
---------------------------------------
Vector Time (GMT): 2015/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 506037
32 A = 6790310
73 meter
Y = 6606787
76 meter E =
0008371
Z = -1458310
03 I = 52
02334
XDOT = -4719
582976 Wp = 354
42245
YDOT = 1643
986518 meter/sec RA = 95
51282 deg
ZDOT = 5815
584313 TA = 349
75395
MA = 349
77100
Ha = 220
344 n
mi
Hp = 218
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1660227
42 X = 439204
82
Y = 21675812
87 feet Y = 6612072
94 meter
Z = -4784481
74 Z = -1456014
09
XDOT = -15484
196116 XDOT = -4765
864950
YDOT = 5393
656555 feet/sec YDOT = 1590
950208 meter/sec
ZDOT = 19080
001028 ZDOT = 5792
545620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17989950
23 X = -5483336
83
Y = 12208252
14 feet Y = 3721075
25 meter
Z = -4775851
21 Z = -1455679
45
XDOT = -11528
191371 XDOT = -3513
792730
YDOT = -9569
263028 feet/sec YDOT = -2916
711371 meter/sec
ZDOT = 18981
103553 ZDOT = 5785
440363
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 15021
50283992
00016717 00000-0 10270-3 0 9004
2 25544 51
6457 96
3771 0006188 285
6128 74
4341 15
53481715 5219
Satellite: ISS
Catalog Number: 25544
Epoch time: 15021
50283992 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 96
3771 deg
Eccentricity:
0006188
Arg of perigee: 285
6128 deg
Mean anomaly: 74
4341 deg
Mean motion: 15
53481715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 521
Checksum: 307
Coasting Arc #2 (Orbit 536)
---------------------------------------
Vector Time (GMT): 2015/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 113361
71 A = 6791001
72 meter
Y = -6785431
33 meter E =
0007057
Z = -58597
65 I = 52
02781
XDOT = 4715
549881 Wp = 156
38229
YDOT = 128
746540 meter/sec RA = 90
57099 deg
ZDOT = -6043
014454 TA = 24
24528
MA = 24
21208
Ha = 220
376 n
mi
Hp = 217
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 371921
62 X = 189514
21
Y = -22261913
82 feet Y = -6783737
85 meter
Z = -192249
49 Z = -57861
94
XDOT = 15470
964176 XDOT = 4743
113801
YDOT = 422
396785 feet/sec YDOT = 181
632951 meter/sec
ZDOT = -19826
162908 ZDOT = -6020
040780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19334881
07 X = 5893271
75
Y = -11040614
66 feet Y = -3365179
35 meter
Z = -187867
81 Z = -57262
11
XDOT = 6792
789296 XDOT = 2070
442177
YDOT = 12216
874903 feet/sec YDOT = 3723
703470 meter/sec
ZDOT = -19727
860083 ZDOT = -6013
051753
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 15022
53206789
00016717 00000-0 10270-3 0 9018
2 25544 51
6451 91
2511 0006005 289
6158 70
4346 15
53552290 5379
Satellite: ISS
Catalog Number: 25544
Epoch time: 15022
53206789 = yrday
fracday
Element set: 901
Inclination: 51
6451 deg
RA of node: 91
2511 deg
Eccentricity:
0006005
Arg of perigee: 289
6158 deg
Mean anomaly: 70
4346 deg
Mean motion: 15
53552290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 537
Checksum: 291
Coasting Arc #3 (Orbit 552)
---------------------------------------
Vector Time (GMT): 2015/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -726713
99 A = 6789965
62 meter
Y = 6558772
64 meter E =
0011268
Z = 1568710
25 I = 52
02350
XDOT = -4669
997265 Wp = 37
73872
YDOT = -1902
833211 meter/sec RA = 85
62810 deg
ZDOT = 5779
155861 TA = 339
32298
MA = 339
36853
Ha = 220
681 n
mi
Hp = 217
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2384232
24 X = -807621
77
Y = 21518282
92 feet Y = 6550193
71 meter
Z = 5146687
19 Z = 1564983
40
XDOT = -15321
513335 XDOT = -4676
444692
YDOT = -6242
891113 feet/sec YDOT = -1955
092056 meter/sec
ZDOT = 18960
485107 ZDOT = 5756
454745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19582672
80 X = -5968798
67
Y = 9242089
41 feet Y = 2816988
85 meter
Z = 5129538
19 Z = 1563483
24
XDOT = -2122
221696 XDOT = -646
853173
YDOT = -14990
469330 feet/sec YDOT = -4569
095052 meter/sec
ZDOT = 18863
670722 ZDOT = 5749
646836
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 15023
56127570
00016717 00000-0 10270-3 0 9023
2 25544 51
6448 86
1243 0005991 294
9912 65
0618 15
53554460 5531
Satellite: ISS
Catalog Number: 25544
Epoch time: 15023
56127570 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 86
1243 deg
Eccentricity:
0005991
Arg of perigee: 294
9912 deg
Mean anomaly: 65
0618 deg
Mean motion: 15
53554460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 553
Checksum: 308
Coasting Arc #4 (Orbit 567)
---------------------------------------
Vector Time (GMT): 2015/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1372967
45 A = 6787128
84 meter
Y = -5947591
28 meter E =
0001491
Z = -2968090
82 I = 52
01120
XDOT = 4560
638440 Wp = 317
72721
YDOT = 3561
324323 meter/sec RA = 80
68054 deg
ZDOT = -5024
162527 TA = 255
97329
MA = 255
98986
Ha = 220
712 n
mi
Hp = 217
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4504486
37 X = 1453790
42
Y = -19513094
76 feet Y = -5931786
06 meter
Z = -9737830
77 Z = -2961224
80
XDOT = 14962
724542 XDOT = 4544
881041
YDOT = 11684
134917 feet/sec YDOT = 3612
236073 meter/sec
ZDOT = -16483
472858 ZDOT = -5002
046570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18892804
35 X = 5758526
77
Y = -6686248
01 feet Y = -2037968
39 meter
Z = -9707350
02 Z = -2958800
28
XDOT = -2192
642310 XDOT = -668
317376
YDOT = 17611
391319 feet/sec YDOT = 5367
952074 meter/sec
ZDOT = -16389
469649 ZDOT = -4995
510349
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 15024
52613873
00016717 00000-0 10270-3 0 9037
2 25544 51
6448 81
3180 0005933 298
8575 61
1981 15
53609777 5680
Satellite: ISS
Catalog Number: 25544
Epoch time: 15024
52613873 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 81
3180 deg
Eccentricity:
0005933
Arg of perigee: 298
8575 deg
Mean anomaly: 61
1981 deg
Mean motion: 15
53609777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 568
Checksum: 331
Coasting Arc #5 (Orbit 583)
---------------------------------------
Vector Time (GMT): 2015/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2051995
16 A = 6783603
37 meter
Y = 4981700
58 meter E =
0005355
Z = 4116655
69 I = 51
99355
XDOT = -4373
462661 Wp = 81
05425
YDOT = -4986
084570 meter/sec RA = 75
72466 deg
ZDOT = 3850
374462 TA = 329
34738
MA = 329
37866
Ha = 220
952 n
mi
Hp = 217
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6732267
59 X = -2127546
13
Y = 16344162
02 feet Y = 4958331
54 meter
Z = 13506088
22 Z = 4106503
96
XDOT = -14348
630778 XDOT = -4336
085497
YDOT = -16358
545178 feet/sec YDOT = -5034
782365 meter/sec
ZDOT = 12632
462146 ZDOT = 3829
220232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17384630
51 X = -5298835
38
Y = 3380288
73 feet Y = 1030312
00 meter
Z = 13461714
17 Z = 4103130
48
XDOT = 5870
111801 XDOT = 1789
210077
YDOT = -19806
359092 feet/sec YDOT = -6036
978251 meter/sec
ZDOT = 12542
845019 ZDOT = 3823
059162
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 15025
55530636
00016717 00000-0 10270-3 0 9047
2 25544 51
6446 76
1910 0005924 303
3122 56
7463 15
53642154 5840
Satellite: ISS
Catalog Number: 25544
Epoch time: 15025
55530636 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 76
1910 deg
Eccentricity:
0005924
Arg of perigee: 303
3122 deg
Mean anomaly: 56
7463 deg
Mean motion: 15
53642154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 584
Checksum: 291
Coasting Arc #6 (Orbit 598)
---------------------------------------
Vector Time (GMT): 2015/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2771910
96 A = 6780506
71 meter
Y = -3753180
54 meter E =
0009870
Z = -4928372
24 I = 51
97546
XDOT = 4052
356714 Wp = 43
98779
YDOT = 6066
244019 meter/sec RA = 70
75985 deg
ZDOT = -2336
409462 TA = 203
21046
MA = 203
25507
Ha = 221
025 n
mi
Hp = 217
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9094196
08 X = 2837613
85
Y = -12313584
46 feet Y = -3721815
97 meter
Z = -16169200
27 Z = -4914747
30
XDOT = 13295
133575 XDOT = 3995
570659
YDOT = 19902
375392 feet/sec YDOT = 6111
242548 meter/sec
ZDOT = -7665
385375 ZDOT = -2316
862155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15359370
93 X = 4681536
26
Y = 568832
93 feet Y = 173380
28 meter
Z = -16110181
74 Z = -4910383
39
XDOT = -8751
709075 XDOT = -2667
520926
YDOT = 21169
063075 feet/sec YDOT = 6452
330425 meter/sec
ZDOT = -7582
857244 ZDOT = -2311
254888
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 15026
52013414
00016717 00000-0 10270-3 0 9056
2 25544 51
6454 71
3845 0005921 307
4383 52
6230 15
53654421 5997
Satellite: ISS
Catalog Number: 25544
Epoch time: 15026
52013414 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 71
3845 deg
Eccentricity:
0005921
Arg of perigee: 307
4383 deg
Mean anomaly: 52
6230 deg
Mean motion: 15
53654421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 599
Checksum: 287
Coasting Arc #7 (Orbit 614)
---------------------------------------
Vector Time (GMT): 2015/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3509520
08 A = 6778699
60 meter
Y = 2330194
01 meter E =
0003286
Z = 5311993
60 I = 51
95810
XDOT = -3565
394723 Wp = 328
58796
YDOT = -6760
014031 meter/sec RA = 65
78830 deg
ZDOT = 612
712433 TA = 115
60517
MA = 115
57122
Ha = 221
256 n
mi
Hp = 216
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11514173
48 X = -3561119
46
Y = 7644993
47 feet Y = 2290659
81 meter
Z = 17427800
54 Z = 5294819
84
XDOT = -11697
489250 XDOT = -3492
513971
YDOT = -22178
523725 feet/sec YDOT = -6799
477089 meter/sec
ZDOT = 2010
211394 ZDOT = 595
569674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12985552
32 X = -3957996
35
Y = -4996950
21 feet Y = -1523070
42 meter
Z = 17353854
53 Z = 5289454
86
XDOT = 10846
106544 XDOT = 3305
893275
YDOT = -21488
045401 feet/sec YDOT = -6549
556238 meter/sec
ZDOT = 1938
117295 ZDOT = 590
738152
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 15027
54926304
00016717 00000-0 10270-3 0 9061
2 25544 51
6449 66
2577 0005885 312
7261 47
3395 15
53703353 6150
Satellite: ISS
Catalog Number: 25544
Epoch time: 15027
54926304 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 66
2577 deg
Eccentricity:
0005885
Arg of perigee: 312
7261 deg
Mean anomaly: 47
3395 deg
Mean motion: 15
53703353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 615
Checksum: 315
Coasting Arc #8 (Orbit 629)
---------------------------------------
Vector Time (GMT): 2015/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4221608
90 A = 6779035
70 meter
Y = -857357
80 meter E =
0010079
Z = -5242459
37 I = 51
94666
XDOT = 2867
617885 Wp = 77
81806
YDOT = 7007
480741 meter/sec RA = 60
81389 deg
ZDOT = 1167
161906 TA = 203
31490
MA = 203
36064
Ha = 221
357 n
mi
Hp = 216
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13850422
89 X = 4256347
97
Y = -2812853
66 feet Y = -809954
76 meter
Z = -17199669
86 Z = -5221867
45
XDOT = 9408
195161 XDOT = 2783
375882
YDOT = 22990
422377 feet/sec YDOT = 7039
077281 meter/sec
ZDOT = 3829
271346 ZDOT = 1180
887508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10582383
41 X = 3225510
46
Y = 9528335
77 feet Y = 2904236
74 meter
Z = -17111369
97 Z = -5215545
57
XDOT = -12167
313514 XDOT = -3708
597159
YDOT = 20469
701799 feet/sec YDOT = 6239
165108 meter/sec
ZDOT = 3886
680636 ZDOT = 1184
660258
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 15028
51405403
00016717 00000-0 10270-3 0 9072
2 25544 51
6461 61
4512 0005965 316
4385 43
6298 15
53708923 6303
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
51405403 = yrday
fracday
Element set: 907
Inclination: 51
6461 deg
RA of node: 61
4512 deg
Eccentricity:
0005965
Arg of perigee: 316
4385 deg
Mean anomaly: 43
6298 deg
Mean motion: 15
53708923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 630
Checksum: 299
Coasting Arc #9 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2015/028/18:43:32
135
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -513526
26 A = 6782583
70 meter
Y = 5397070
15 meter E =
0005594
Z = 4070043
64 I = 51
95627
XDOT = -5605
705066 Wp = 76
03890
YDOT = -3482
897878 meter/sec RA = 59
45845 deg
ZDOT = 3908
030539 TA = 333
63202
MA = 333
66048
Ha = 220
459 n
mi
Hp = 216
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1684797
43 X = -593609
94
Y = 17706923
07 feet Y = 5390879
77 meter
Z = 13353161
54 Z = 4067354
57
XDOT = -18391
420820 XDOT = -5585
325406
YDOT = -11426
830309 feet/sec YDOT = -3545
470593 meter/sec
ZDOT = 12821
622503 ZDOT = 3880
848874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11920851
18 X = 3633475
44
Y = 13213696
98 feet Y = 4027534
84 meter
Z = 13340618
78 Z = 4066220
60
XDOT = -19912
877021 XDOT = -6069
444916
YDOT = 5126
063502 feet/sec YDOT = 1562
424155 meter/sec
ZDOT = 12705
947628 ZDOT = 3872
772837
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 15028
83563468
00016717 00000-0 10270-3 0 9084
2 25544 51
6448 59
8487 0006158 306
3718 53
6866 15
54035436 6353
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
83563468 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 59
8487 deg
Eccentricity:
0006158
Arg of perigee: 306
3718 deg
Mean anomaly: 53
6866 deg
Mean motion: 15
54035436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 341
Coasting Arc #10 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2015/029/18:43:32
135
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1671590
09 A = 6779162
45 meter
Y = -4330978
51 meter E =
0010352
Z = -4948941
19 I = 51
92889
XDOT = 5569
344190 Wp = 43
32976
YDOT = 4746
199846 meter/sec RA = 54
48748 deg
ZDOT = -2267
888074 TA = 204
55670
MA = 204
60603
Ha = 220
546 n
mi
Hp = 216
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5484219
47 X = 1743935
66
Y = -14209247
09 feet Y = -4311881
13 meter
Z = -16236683
70 Z = -4940645
38
XDOT = 18272
126609 XDOT = 5526
873550
YDOT = 15571
521803 feet/sec YDOT = 4808
242438 meter/sec
ZDOT = -7440
577670 ZDOT = -2240
936728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6999728
19 X = -2133517
15
Y = -13570631
90 feet Y = -4136328
60 meter
Z = -16200340
09 Z = -4937863
66
XDOT = 22795
869420 XDOT = 6948
180999
YDOT = -2994
558260 feet/sec YDOT = -912
741358 meter/sec
ZDOT = -7326
136315 ZDOT = -2233
006349
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 15029
80021706
00016717 00000-0 10270-3 0 9097
2 25544 51
6453 55
0408 0006164 311
1200 48
9420 15
54075697 6500
Satellite: ISS
Catalog Number: 25544
Epoch time: 15029
80021706 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 55
0408 deg
Eccentricity:
0006164
Arg of perigee: 311
1200 deg
Mean anomaly: 48
9420 deg
Mean motion: 15
54075697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 650
Checksum: 281
Coasting Arc #11 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2015/030/18:43:32
135
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2891693
96 A = 6777397
66 meter
Y = 3040837
43 meter E =
0004141
Z = 5323662
22 I = 51
90414
XDOT = -5200
605004 Wp = 330
01808
YDOT = -5620
834116 meter/sec RA = 49
50835 deg
ZDOT = 389
352886 TA = 116
30367
MA = 116
26112
Ha = 220
677 n
mi
Hp = 216
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9487184
91 X = -2951342
33
Y = 9976500
77 feet Y = 3008167
04 meter
Z = 17466083
39 Z = 5309470
33
XDOT = -17062
352375 XDOT = -5139
256296
YDOT = -18441
056811 feet/sec YDOT = -5678
647650 meter/sec
ZDOT = 1277
404482 ZDOT = 364
238697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1410145
35 X = 429812
30
Y = 13772710
67 feet Y = 4197922
21 meter
Z = 17404747
77 Z = 5304967
12
XDOT = -24100
150125 XDOT = -7345
725758
YDOT = 1002
813746 feet/sec YDOT = 305
657630 meter/sec
ZDOT = 1171
001100 ZDOT = 356
921135
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 15030
82908335
00016717 00000-0 10270-3 0 9105
2 25544 51
6451 49
9124 0006259 313
7058 46
3576 15
54125332 6662
Satellite: ISS
Catalog Number: 25544
Epoch time: 15030
82908335 = yrday
fracday
Element set: 910
Inclination: 51
6451 deg
RA of node: 49
9124 deg
Eccentricity:
0006259
Arg of perigee: 313
7058 deg
Mean anomaly: 46
3576 deg
Mean motion: 15
54125332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 666
Checksum: 301
Coasting Arc #12 (Orbit 680)
---------------------------------------
Vector Time (GMT): 2015/031/18:43:32
135
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4066470
47 A = 6778162
01 meter
Y = -1681585
71 meter E =
0009409
Z = -5163042
04 I = 51
88591
XDOT = 4441
363068 Wp = 78
25044
YDOT = 6052
963956 meter/sec RA = 44
52576 deg
ZDOT = 1530
858502 TA = 206
43638
MA = 206
48441
Ha = 220
828 n
mi
Hp = 216
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13341438
54 X = 4110051
75
Y = -5517013
49 feet Y = -1635868
06 meter
Z = -16939114
30 Z = -5143182
47
XDOT = 14571
401142 XDOT = 4365
911123
YDOT = 19858
805631 feet/sec YDOT = 6102
208276 meter/sec
ZDOT = 5022
501646 ZDOT = 1552
250154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4243127
29 X = 1293305
20
Y = -13903630
33 feet Y = -4237826
53 meter
Z = -16853781
41 Z = -5137032
57
XDOT = 23563
365652 XDOT = 7182
113851
YDOT = 1010
205776 feet/sec YDOT = 307
910721 meter/sec
ZDOT = 5112
882696 ZDOT = 1558
406646
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 15031
79362881
00016717 00000-0 10270-3 0 9113
2 25544 51
6456 45
1039 0006206 318
5405 41
5276 15
54125008 6812
Satellite: ISS
Catalog Number: 25544
Epoch time: 15031
79362881 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 45
1039 deg
Eccentricity:
0006206
Arg of perigee: 318
5405 deg
Mean anomaly: 41
5276 deg
Mean motion: 15
54125008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 681
Checksum: 289
Coasting Arc #13 (Orbit 696)
---------------------------------------
Vector Time (GMT): 2015/032/18:43:32
135
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5104931
69 A = 6780953
08 meter
Y = 316832
52 meter E =
0009536
Z = 4452427
63 I = 51
87199
XDOT = -3280
049624 Wp = 31
07760
YDOT = -6084
321669 meter/sec RA = 39
54683 deg
ZDOT = -3316
658698 TA = 92
34041
MA = 92
23123
Ha = 220
932 n
mi
Hp = 215
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16748463
57 X = -5129722
92
Y = 1039476
76 feet Y = 259607
23 meter
Z = 14607702
20 Z = 4427569
21
XDOT = -10761
317663 XDOT = -3195
658808
YDOT = -19961
685266 feet/sec YDOT = -6120
529463 meter/sec
ZDOT = -10881
426175 ZDOT = -3332
387208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9619792
40 X = -2932112
72
Y = 13861823
99 feet Y = 4225083
95 meter
Z = 14501239
16 Z = 4419977
69
XDOT = -21282
466631 XDOT = -6486
895829
YDOT = -3278
541613 feet/sec YDOT = -999
299484 meter/sec
ZDOT = -10947
557414 ZDOT = -3336
815500
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 15032
82245550
00016717 00000-0 10270-3 0 9122
2 25544 51
6452 39
9751 0006214 322
7513 37
3208 15
54160946 6971
Satellite: ISS
Catalog Number: 25544
Epoch time: 15032
82245550 = yrday
fracday
Element set: 912
Inclination: 51
6452 deg
RA of node: 39
9751 deg
Eccentricity:
0006214
Arg of perigee: 322
7513 deg
Mean anomaly: 37
3208 deg
Mean motion: 15
54160946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 697
Checksum: 297
Coasting Arc #14 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2015/033/18:43:32
135
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5862649
98 A = 6784652
70 meter
Y = 905984
26 meter E =
0005876
Z = -3286970
60 I = 51
86051
XDOT = 1771
169717 Wp = 10
45045
YDOT = 5751
816443 meter/sec RA = 34
57483 deg
ZDOT = 4751
389695 TA = 311
50917
MA = 311
55958
Ha = 221
048 n
mi
Hp = 215
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19234415
96 X = 5868049
82
Y = 2972389
32 feet Y = 971574
37 meter
Z = -10784024
28 Z = -3258478
58
XDOT = 5810
924270 XDOT = 1683
640009
YDOT = 18870
788854 feet/sec YDOT = 5771
133481 meter/sec
ZDOT = 15588
548869 ZDOT = 4759
780799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14063205
05 X = 4286464
90
Y = -13551226
07 feet Y = -4130413
71 meter
Z = -10662249
80 Z = -3249853
74
XDOT = 17484
329942 XDOT = 5329
223766
YDOT = 5870
466785 feet/sec YDOT = 1789
318276 meter/sec
ZDOT = 15623
336679 ZDOT = 4761
993020
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 15033
78696071
00016717 00000-0 10270-3 0 9137
2 25544 51
6459 35
1660 0006213 326
0798 33
9957 15
54195011 7128
Satellite: ISS
Catalog Number: 25544
Epoch time: 15033
78696071 = yrday
fracday
Element set: 913
Inclination: 51
6459 deg
RA of node: 35
1660 deg
Eccentricity:
0006213
Arg of perigee: 326
0798 deg
Mean anomaly: 33
9957 deg
Mean motion: 15
54195011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 309
Coasting Arc #15 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2015/034/18:43:32
135
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6252139
16 A = 6787911
16 meter
Y = -1978533
89 meter E =
0009528
Z = 1742728
03 I = 51
84479
XDOT = 28
764704 Wp = 94
23772
YDOT = -5130
763902 meter/sec RA = 29
61178 deg
ZDOT = -5695
695058 TA = 66
69833
MA = 66
59808
Ha = 221
051 n
mi
Hp = 215
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20512267
60 X = -6238015
37
Y = -6491252
92 feet Y = -2048370
35 meter
Z = 5717611
65 Z = 1712391
49
XDOT = 94
372389 XDOT = 113
802834
YDOT = -16833
214903 feet/sec YDOT = -5129
966950 meter/sec
ZDOT = -18686
663577 ZDOT = -5695
348614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17401368
08 X = -5303936
99
Y = 12710053
77 feet Y = 3874024
39 meter
Z = 5588156
36 Z = 1703270
06
XDOT = -12510
513646 XDOT = -3813
204559
YDOT = -8874
878954 feet/sec YDOT = -2705
063105 meter/sec
ZDOT = -18684
174022 ZDOT = -5694
936242
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 15034
81574636
00016717 00000-0 10270-3 0 9145
2 25544 51
6458 30
0368 0006092 329
8377 30
2424 15
54193240 7283
Satellite: ISS
Catalog Number: 25544
Epoch time: 15034
81574636 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 30
0368 deg
Eccentricity:
0006092
Arg of perigee: 329
8377 deg
Mean anomaly: 30
2424 deg
Mean motion: 15
54193240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 302
Coasting Arc #16 (Orbit 743)
---------------------------------------
Vector Time (GMT): 2015/035/18:43:32
135
Vector Time (MET): N/A
Weight (LBS) : 949918
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6169883
78 A = 6788958
08 meter
Y = 2809274
37 meter E =
0015239
Z = -25858
70 I = 51
82164
XDOT = -1948
537249 Wp = 22
14623
YDOT = 4324
257259 meter/sec RA = 24
65259 deg
ZDOT = 6031
813570 TA = 337
57575
MA = 337
64230
Ha = 221
124 n
mi
Hp = 215
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20242400
86 X = 6138136
87
Y = 9216779
43 feet Y = 2878092
52 meter
Z = -84838
24 Z = 4035
41
XDOT = -6392
838745 XDOT = -2026
046867
YDOT = 14187
195732 feet/sec YDOT = 4302
034372 meter/sec
ZDOT = 19789
414601 ZDOT = 6022
159709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19227167
37 X = 5860440
61
Y = -11181468
48 feet Y = -3408111
59 meter
Z = 42555
13 Z = 12970
80
XDOT = 6988
966526 XDOT = 2130
236997
YDOT = 12122
148882 feet/sec YDOT = 3694
830979 meter/sec
ZDOT = 19747
248435 ZDOT = 6018
961323
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 15035
84450784
00016717 00000-0 10270-3 0 9157
2 25544 51
6463 24
9069 0006272 333
3522 26
7307 15
54258190 7445
Satellite: ISS
Catalog Number: 25544
Epoch time: 15035
84450784 = yrday
fracday
Element set: 915
Inclination: 51
6463 deg
RA of node: 24
9069 deg
Eccentricity:
0006272
Arg of perigee: 333
3522 deg
Mean anomaly: 26
7307 deg
Mean motion: 15
54258190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 744
Checksum: 306
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