[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 23rd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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 749)
---------------------------------------
Vector Time (GMT): 2014/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5535156
56 A = 6799539
59 meter
Y = 3833561
94 meter E =
0013334
Z = 915427
36 I = 51
42619
XDOT = -2078
282430 Wp = 109
98304
YDOT = 4425
107555 meter/sec RA = 220
93090 deg
ZDOT = -5899
070139 TA = 60
09424
MA = 59
96185
Ha = 227
542 n
mi
Hp = 219
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18159962
48 X = 5487430
51
Y = 12577302
95 feet Y = 3895192
74 meter
Z = 3003370
62 Z = 942200
87
XDOT = -6818
511909 XDOT = -2098
954397
YDOT = 14518
069405 feet/sec YDOT = 4401
751441 meter/sec
ZDOT = -19353
904655 ZDOT = -5909
216354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19930192
26 X = 6074722
60
Y = -9490553
82 feet Y = -2892720
80 meter
Z = 3116062
66 Z = 949775
90
XDOT = 8576
067392 XDOT = 2613
985341
YDOT = 11572
716300 feet/sec YDOT = 3527
363928 meter/sec
ZDOT = -19397
522926 ZDOT = -5912
364988
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 14143
53411024
00016717 00000-0 10270-3 0 9000
2 25544 51
6472 221
8082 0003520 25
1055 335
0267 15
50492250 7509
Satellite: ISS
Catalog Number: 25544
Epoch time: 14143
53411024 = yrday
fracday
Element set: 900
Inclination: 51
6472 deg
RA of node: 221
8082 deg
Eccentricity:
0003520
Arg of perigee: 25
1055 deg
Mean anomaly: 335
0267 deg
Mean motion: 15
50492250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 750
Checksum: 253
Coasting Arc #2 (Orbit 764)
---------------------------------------
Vector Time (GMT): 2014/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5679920
45 A = 6799853
10 meter
Y = -3700568
00 meter E =
0014731
Z = -427047
28 I = 51
45149
XDOT = 2303
563874 Wp = 38
22656
YDOT = -4211
178219 meter/sec RA = 215
96216 deg
ZDOT = 5975
405963 TA = 317
16254
MA = 317
27722
Ha = 227
593 n
mi
Hp = 219
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18634909
60 X = -5636043
22
Y = -12140971
14 feet Y = -3763839
17 meter
Z = -1401073
75 Z = -454533
52
XDOT = 7557
624260 XDOT = 2321
455971
YDOT = -13816
201506 feet/sec YDOT = -4185
318469 meter/sec
ZDOT = 19604
350272 ZDOT = 5986
639828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19615334
25 X = -5978753
88
Y = 10467281
61 feet Y = 3190427
43 meter
Z = -1516813
07 Z = -462324
62
XDOT = -7757
071054 XDOT = -2364
355257
YDOT = -11742
207745 feet/sec YDOT = -3579
024921 meter/sec
ZDOT = 19652
539091 ZDOT = 5990
093915
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 14144
50089395
00016717 00000-0 10270-3 0 9011
2 25544 51
6475 217
0152 0003741 25
8919 334
2418 15
50484203 7652
Satellite: ISS
Catalog Number: 25544
Epoch time: 14144
50089395 = yrday
fracday
Element set: 901
Inclination: 51
6475 deg
RA of node: 217
0152 deg
Eccentricity:
0003741
Arg of perigee: 25
8919 deg
Mean anomaly: 334
2418 deg
Mean motion: 15
50484203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 765
Checksum: 297
Coasting Arc #3 (Orbit 780)
---------------------------------------
Vector Time (GMT): 2014/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5775633
32 A = 6799721
72 meter
Y = 3580095
71 meter E =
0011613
Z = -118805
92 I = 51
47696
XDOT = -2596
275295 Wp = 117
22809
YDOT = 4004
813900 meter/sec RA = 210
99569 deg
ZDOT = -5991
718418 TA = 64
05224
MA = 63
93263
Ha = 227
607 n
mi
Hp = 219
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18948928
23 X = 5735747
75
Y = 11745720
83 feet Y = 3644459
54 meter
Z = -389783
21 Z = -90844
90
XDOT = -8517
963566 XDOT = -2611
758715
YDOT = 13139
153214 feet/sec YDOT = 3975
694427 meter/sec
ZDOT = -19657
868824 ZDOT = -6004
368378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19234552
82 X = 5862691
70
Y = -11275360
79 feet Y = -3436729
97 meter
Z = -272005
18 Z = -82907
18
XDOT = 6876
550039 XDOT = 2095
972452
YDOT = 12154
314800 feet/sec YDOT = 3704
635151 meter/sec
ZDOT = -19712
022252 ZDOT = -6008
224382
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 14145
53211179
00016717 00000-0 10270-3 0 9023
2 25544 51
6470 211
9026 0003748 31
4378 328
6997 15
50558162 7812
Satellite: ISS
Catalog Number: 25544
Epoch time: 14145
53211179 = yrday
fracday
Element set: 902
Inclination: 51
6470 deg
RA of node: 211
9026 deg
Eccentricity:
0003748
Arg of perigee: 31
4378 deg
Mean anomaly: 328
6997 deg
Mean motion: 15
50558162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 781
Checksum: 309
Coasting Arc #4 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2014/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5839676
73 A = 6799632
78 meter
Y = -3408762
34 meter E =
0016862
Z = 628962
71 I = 51
50323
XDOT = 2901
920877 Wp = 47
67793
YDOT = -3855
414745 meter/sec RA = 206
03049 deg
ZDOT = 5956
957627 TA = 319
11835
MA = 319
24470
Ha = 227
702 n
mi
Hp = 219
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19159044
38 X = -5804180
51
Y = -11183603
48 feet Y = -3473866
93 meter
Z = 2063525
96 Z = 600679
84
XDOT = 9520
737784 XDOT = 2915
879805
YDOT = -12648
998507 feet/sec YDOT = -3822
885977 meter/sec
ZDOT = 19543
824234 ZDOT = 5971
088641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18635708
03 X = -5680163
81
Y = 12055289
60 feet Y = 3674452
27 meter
Z = 1944347
41 Z = 592637
09
XDOT = -6161
263459 XDOT = -1877
953102
YDOT = -12737
529260 feet/sec YDOT = -3882
398918 meter/sec
ZDOT = 19604
228954 ZDOT = 5975
368985
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 14146
56331080
00016717 00000-0 10270-3 0 9032
2 25544 51
6467 206
7898 0003954 33
7664 326
3738 15
50541627 7972
Satellite: ISS
Catalog Number: 25544
Epoch time: 14146
56331080 = yrday
fracday
Element set: 903
Inclination: 51
6467 deg
RA of node: 206
7898 deg
Eccentricity:
0003954
Arg of perigee: 33
7664 deg
Mean anomaly: 326
3738 deg
Mean motion: 15
50541627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 328
Coasting Arc #5 (Orbit 811)
---------------------------------------
Vector Time (GMT): 2014/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5844545
54 A = 6798983
41 meter
Y = 3261604
91 meter E =
0009213
Z = -1186453
62 I = 51
53007
XDOT = -3256
917799 Wp = 117
60962
YDOT = 3723
633668 meter/sec RA = 201
06694 deg
ZDOT = -5846
460970 TA = 75
27201
MA = 75
16992
Ha = 227
669 n
mi
Hp = 219
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19175018
17 X = 5813402
66
Y = 10700803
50 feet Y = 3326788
35 meter
Z = -3892564
38 Z = -1158136
50
XDOT = -10685
425850 XDOT = -3269
913529
YDOT = 12216
645892 feet/sec YDOT = 3687
140578 meter/sec
ZDOT = -19181
302395 ZDOT = -5862
314133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18002952
89 X = 5487300
04
Y = -12609408
73 feet Y = -3843347
78 meter
Z = -3773204
71 Z = -1150072
79
XDOT = 5464
281529 XDOT = 1665
513010
YDOT = 13521
999204 feet/sec YDOT = 4121
505357 meter/sec
ZDOT = -19248
984427 ZDOT = -5867
090453
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 14147
53003945
00016717 00000-0 10270-3 0 9047
2 25544 51
6466 201
9963 0003954 38
2686 321
8745 15
50620011 8126
Satellite: ISS
Catalog Number: 25544
Epoch time: 14147
53003945 = yrday
fracday
Element set: 904
Inclination: 51
6466 deg
RA of node: 201
9963 deg
Eccentricity:
0003954
Arg of perigee: 38
2686 deg
Mean anomaly: 321
8745 deg
Mean motion: 15
50620011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 812
Checksum: 297
Coasting Arc #6 (Orbit 827)
---------------------------------------
Vector Time (GMT): 2014/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5808252
79 A = 6798436
91 meter
Y = -3078831
25 meter E =
0017817
Z = 1696641
02 I = 51
55640
XDOT = 3611
310354 Wp = 59
17390
YDOT = -3658
077803 meter/sec RA = 196
10462 deg
ZDOT = 5689
218568 TA = 319
43277
MA = 319
56542
Ha = 227
805 n
mi
Hp = 219
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19055947
46 X = -5781634
78
Y = -10101152
39 feet Y = -3143634
21 meter
Z = 5566407
54 Z = 1668489
24
XDOT = 11848
131082 XDOT = 3624
310587
YDOT = -12001
567594 feet/sec YDOT = -3617
621715 meter/sec
ZDOT = 18665
415248 ZDOT = 5706
793275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17193563
88 X = -5240598
27
Y = 13071005
41 feet Y = 3984042
45 meter
Z = 5447704
55 Z = 1660460
35
XDOT = -4999
357840 XDOT = -1523
804270
YDOT = -14436
322631 feet/sec YDOT = -4400
191138 meter/sec
ZDOT = 18740
385041 ZDOT = 5712
069361
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 14148
56120072
00016717 00000-0 10270-3 0 9053
2 25544 51
6456 196
8831 0004156 41
6751 318
4716 15
50603574 8289
Satellite: ISS
Catalog Number: 25544
Epoch time: 14148
56120072 = yrday
fracday
Element set: 905
Inclination: 51
6456 deg
RA of node: 196
8831 deg
Eccentricity:
0004156
Arg of perigee: 41
6751 deg
Mean anomaly: 318
4716 deg
Mean motion: 15
50603574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 828
Checksum: 306
Coasting Arc #7 (Orbit 842)
---------------------------------------
Vector Time (GMT): 2014/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5707984
43 A = 6797323
76 meter
Y = 2935323
51 meter E =
0007259
Z = -2240524
15 I = 51
58409
XDOT = -3989
458325 Wp = 103
18175
YDOT = 3614
759878 meter/sec RA = 191
14337 deg
ZDOT = -5444
388088 TA = 101
69245
MA = 101
61098
Ha = 227
713 n
mi
Hp = 219
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18726983
05 X = 5685620
63
Y = 9630326
46 feet Y = 2999029
07 meter
Z = -7350801
01 Z = -2212849
19
XDOT = -13088
774031 XDOT = -4003
135465
YDOT = 11859
448419 feet/sec YDOT = 3570
071346 meter/sec
ZDOT = -17862
165644 ZDOT = -5463
801368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16406862
57 X = 5000811
71
Y = -13265003
87 feet Y = -4043173
18 meter
Z = -7234078
41 Z = -2204947
10
XDOT = 4619
907530 XDOT = 1408
147815
YDOT = 15470
394557 feet/sec YDOT = 4715
376261 meter/sec
ZDOT = -17944
924593 ZDOT = -5469
613016
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 14149
52789421
00016717 00000-0 10270-3 0 9060
2 25544 51
6462 192
0891 0004108 45
3250 314
8235 15
50677142 8437
Satellite: ISS
Catalog Number: 25544
Epoch time: 14149
52789421 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 192
0891 deg
Eccentricity:
0004108
Arg of perigee: 45
3250 deg
Mean anomaly: 314
8235 deg
Mean motion: 15
50677142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 843
Checksum: 301
Coasting Arc #8 (Orbit 858)
---------------------------------------
Vector Time (GMT): 2014/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5562673
32 A = 6796347
98 meter
Y = -2774562
69 meter E =
0017390
Z = 2725318
38 I = 51
61008
XDOT = 4353
135579 Wp = 71
72440
YDOT = -3639
334621 meter/sec RA = 186
18318 deg
ZDOT = 5158
411658 TA = 319
09135
MA = 319
22172
Ha = 227
872 n
mi
Hp = 218
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18250240
55 X = -5544472
94
Y = -9102895
96 feet Y = -2836666
63 meter
Z = 8941333
26 Z = 2698339
31
XDOT = 14281
940877 XDOT = 4368
449773
YDOT = -11940
074217 feet/sec YDOT = -3590
570054 meter/sec
ZDOT = 16923
922762 ZDOT = 5179
595540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15508632
14 X = -4727031
08
Y = 13320612
98 feet Y = 4060122
84 meter
Z = 8827515
74 Z = 2690626
80
XDOT = -4509
442902 XDOT = -1374
478197
YDOT = -16573
226961 feet/sec YDOT = -5051
519578 meter/sec
ZDOT = 17014
195816 ZDOT = 5185
926885
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 14150
55901796
00016717 00000-0 10270-3 0 9077
2 25544 51
6449 186
9755 0004304 49
2563 310
8961 15
50669627 8599
Satellite: ISS
Catalog Number: 25544
Epoch time: 14150
55901796 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 186
9755 deg
Eccentricity:
0004304
Arg of perigee: 49
2563 deg
Mean anomaly: 310
8961 deg
Mean motion: 15
50669627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 859
Checksum: 340
Coasting Arc #9 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2014/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5356038
19 A = 6794919
93 meter
Y = 2669315
72 meter E =
0007978
Z = -3227124
51 I = 51
63795
XDOT = -4710
068110 Wp = 78
02079
YDOT = 3683
061863 meter/sec RA = 181
22385 deg
ZDOT = -4779
232575 TA = 139
23209
MA = 139
17237
Ha = 227
727 n
mi
Hp = 218
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17572303
76 X = 5341467
65
Y = 8757597
50 feet Y = 2729129
28 meter
Z = -10587678
84 Z = -3201140
54
XDOT = -15452
979362 XDOT = -4727
686762
YDOT = 12083
536297 feet/sec YDOT = 3630
292906 meter/sec
ZDOT = -15679
896898 ZDOT = -4802
155931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14707539
47 X = 4482858
03
Y = -13095007
31 feet Y = -3991358
23 meter
Z = -10478042
88 Z = -3193707
47
XDOT = 4522
805480 XDOT = 1378
551110
YDOT = 17681
948590 feet/sec YDOT = 5389
457930 meter/sec
ZDOT = -15777
556954 ZDOT = -4808
999360
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 14151
52567684
00016717 00000-0 10270-3 0 9080
2 25544 51
6459 182
1812 0004205 52
2464 307
9067 15
50730866 8741
Satellite: ISS
Catalog Number: 25544
Epoch time: 14151
52567684 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 182
1812 deg
Eccentricity:
0004205
Arg of perigee: 52
2464 deg
Mean anomaly: 307
9067 deg
Mean motion: 15
50730866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 315
Coasting Arc #10 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2014/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5106597
53 A = 6793652
10 meter
Y = -2565847
41 meter E =
0015589
Z = 3658428
11 I = 51
66354
XDOT = 5040
782270 Wp = 84
38021
YDOT = -3788
066033 meter/sec RA = 176
26519 deg
ZDOT = 4364
861160 TA = 319
04022
MA = 319
15722
Ha = 227
886 n
mi
Hp = 218
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16753928
90 X = -5095297
64
Y = -8418134
55 feet Y = -2622889
88 meter
Z = 12002716
89 Z = 3633648
05
XDOT = 16537
999572 XDOT = 5061
563471
YDOT = -12428
038165 feet/sec YDOT = -3731
581049 meter/sec
ZDOT = 14320
410631 ZDOT = 4389
398730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13873747
40 X = -4228718
21
Y = 12711314
74 feet Y = 3874408
73 meter
Z = 11898148
86 Z = 3626555
77
XDOT = -4803
795322 XDOT = -1464
196814
YDOT = -18790
223057 feet/sec YDOT = -5727
259988 meter/sec
ZDOT = 14424
937999 ZDOT = 4396
721102
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 14152
55676327
00016717 00000-0 10270-3 0 9090
2 25544 51
6446 177
0671 0004366 56
0925 304
0640 15
50735125 8901
Satellite: ISS
Catalog Number: 25544
Epoch time: 14152
55676327 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 177
0671 deg
Eccentricity:
0004366
Arg of perigee: 56
0925 deg
Mean anomaly: 304
0640 deg
Mean motion: 15
50735125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 305
Coasting Arc #11 (Orbit 904)
---------------------------------------
Vector Time (GMT): 2014/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4807143
48 A = 6792137
33 meter
Y = 2532204
63 meter E =
0011340
Z = -4088072
80 I = 51
69081
XDOT = -5333
501597 Wp = 67
39090
YDOT = 3900
337499 meter/sec RA = 171
30749 deg
ZDOT = -3860
032642 TA = 162
62446
MA = 162
58562
Ha = 227
716 n
mi
Hp = 218
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15771468
10 X = 4798329
10
Y = 8307757
98 feet Y = 2585912
31 meter
Z = -13412312
34 Z = -4064741
48
XDOT = -17498
364818 XDOT = -5357
968818
YDOT = 12796
382871 feet/sec YDOT = 3840
558431 meter/sec
ZDOT = -12664
149087 ZDOT = -3886
001154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13217047
43 X = 4028556
06
Y = -12070579
56 feet Y = -3679112
65 meter
Z = -13313862
59 Z = -4058065
32
XDOT = 5205
531056 XDOT = 1586
645866
YDOT = 19774
808868 feet/sec YDOT = 6027
361743 meter/sec
ZDOT = -12774
769461 ZDOT = -3893
749732
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 14153
52338780
00016717 00000-0 10270-3 0 9108
2 25544 51
6455 172
2728 0004257 58
9361 301
2207 15
50781601 9050
Satellite: ISS
Catalog Number: 25544
Epoch time: 14153
52338780 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 172
2728 deg
Eccentricity:
0004257
Arg of perigee: 58
9361 deg
Mean anomaly: 301
2207 deg
Mean motion: 15
50781601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 905
Checksum: 292
Coasting Arc #12 (Orbit 920)
---------------------------------------
Vector Time (GMT): 2014/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4472678
52 A = 6790808
96 meter
Y = -2517313
83 meter E =
0012692
Z = 4436499
22 I = 51
71604
XDOT = 5592
533919 Wp = 95
53635
YDOT = -4059
243700 meter/sec RA = 166
35004 deg
ZDOT = 3325
504011 TA = 320
88375
MA = 320
97544
Ha = 227
850 n
mi
Hp = 218
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14674142
12 X = -4465748
05
Y = -8258903
63 feet Y = -2567291
82 meter
Z = 14555443
64 Z = 4414788
15
XDOT = 18348
208396 XDOT = 5621
355393
YDOT = -13317
728674 feet/sec YDOT = -3996
543528 meter/sec
ZDOT = 10910
446231 ZDOT = 3352
741469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12606968
41 X = -3842603
97
Y = 11281064
83 feet Y = 3438468
56 meter
Z = 14463844
57 Z = 4408579
82
XDOT = -5832
450118 XDOT = -1777
730796
YDOT = -20695
104835 feet/sec YDOT = -6307
867954 meter/sec
ZDOT = 11026
481199 ZDOT = 3360
871469
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 14154
55443685
00016717 00000-0 10270-3 0 9114
2 25544 51
6445 167
1584 0004348 62
2271 297
9321 15
50796358 9212
Satellite: ISS
Catalog Number: 25544
Epoch time: 14154
55443685 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 167
1584 deg
Eccentricity:
0004348
Arg of perigee: 62
2271 deg
Mean anomaly: 297
9321 deg
Mean motion: 15
50796358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 921
Checksum: 320
Coasting Arc #13 (Orbit 935)
---------------------------------------
Vector Time (GMT): 2014/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4107906
22 A = 6789482
76 meter
Y = 2581167
66 meter E =
0015188
Z = -4764340
88 I = 51
74229
XDOT = -5786
696574 Wp = 69
80511
YDOT = 4205
440424 meter/sec RA = 161
39367 deg
ZDOT = -2712
948477 TA = 173
35904
MA = 173
33889
Ha = 227
686 n
mi
Hp = 218
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13477382
62 X = 4101881
41
Y = 8468397
82 feet Y = 2627071
57 meter
Z = -15631039
62 Z = -4744399
63
XDOT = -18985
224979 XDOT = -5820
114016
YDOT = 13797
376719 feet/sec YDOT = 4140
543221 meter/sec
ZDOT = -8900
749597 ZDOT = -2741
140368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12243010
63 X = 3731669
64
Y = -10299725
37 feet Y = -3139356
29 meter
Z = -15546940
27 Z = -4738707
39
XDOT = 6530
763567 XDOT = 1990
576735
YDOT = 21369
944152 feet/sec YDOT = 6513
558977 meter/sec
ZDOT = -9020
865143 ZDOT = -2749
559695
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 14155
52102680
00016717 00000-0 10270-3 0 9120
2 25544 51
6448 162
3641 0004278 65
3976 294
7621 15
50829884 9369
Satellite: ISS
Catalog Number: 25544
Epoch time: 14155
52102680 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 162
3641 deg
Eccentricity:
0004278
Arg of perigee: 65
3976 deg
Mean anomaly: 294
7621 deg
Mean motion: 15
50829884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 936
Checksum: 323
Coasting Arc #14 (Orbit 951)
---------------------------------------
Vector Time (GMT): 2014/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3720010
37 A = 6788375
57 meter
Y = -2676012
68 meter E =
0009323
Z = 5000915
93 I = 51
76719
XDOT = 5945
402531 Wp = 101
18714
YDOT = -4376
777278 meter/sec RA = 156
43746 deg
ZDOT = 2075
504173 TA = 328
63114
MA = 328
68672
Ha = 227
778 n
mi
Hp = 218
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12204758
44 X = -3714103
06
Y = -8779569
16 feet Y = -2717579
53 meter
Z = 16407204
49 Z = 4982858
73
XDOT = 19505
913815 XDOT = 5983
820596
YDOT = -14359
505504 feet/sec YDOT = -4310
077296 meter/sec
ZDOT = 6809
396892 ZDOT = 2104
479256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11991143
47 X = -3654900
53
Y = 9205491
66 feet Y = 2805833
86 meter
Z = 16331096
84 Z = 4977718
32
XDOT = -7374
232799 XDOT = -2247
666157
YDOT = -21934
560590 feet/sec YDOT = -6685
654068 meter/sec
ZDOT = 6932
871979 ZDOT = 2113
139379
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 14156
55203799
00016717 00000-0 10270-3 0 9138
2 25544 51
6440 157
2494 0004290 68
0564 292
1043 15
50853568 9521
Satellite: ISS
Catalog Number: 25544
Epoch time: 14156
55203799 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 157
2494 deg
Eccentricity:
0004290
Arg of perigee: 68
0564 deg
Mean anomaly: 292
1043 deg
Mean motion: 15
50853568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 952
Checksum: 313
Coasting Arc #15 (Orbit 966)
---------------------------------------
Vector Time (GMT): 2014/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3327866
21 A = 6787507
31 meter
Y = 2850017
63 meter E =
0018048
Z = -5199939
93 I = 51
79254
XDOT = -6021
786316 Wp = 77
77800
YDOT = 4510
174789 meter/sec RA = 151
48236 deg
ZDOT = -1382
204140 TA = 178
92951
MA = 178
92564
Ha = 227
640 n
mi
Hp = 218
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10918196
21 X = 3321009
14
Y = 9350451
54 feet Y = 2887193
95 meter
Z = -17060170
37 Z = -5183789
99
XDOT = -19756
516785 XDOT = -6065
058212
YDOT = 14797
161381 feet/sec YDOT = 4442
593442 meter/sec
ZDOT = -4534
790485 ZDOT = -1411
562162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12026165
35 X = 3665575
20
Y = -8020282
48 feet Y = -2444582
10 meter
Z = -16992168
25 Z = -5179212
88
XDOT = 8199
678695 XDOT = 2499
262066
YDOT = 22165
552374 feet/sec YDOT = 6756
060364 meter/sec
ZDOT = -4659
923944 ZDOT = -1420
344818
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 14157
51859255
00016717 00000-0 10270-3 0 9140
2 25544 51
6439 152
4548 0004279 71
6041 288
5575 15
50878687 9677
Satellite: ISS
Catalog Number: 25544
Epoch time: 14157
51859255 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 152
4548 deg
Eccentricity:
0004279
Arg of perigee: 71
6041 deg
Mean anomaly: 288
5575 deg
Mean motion: 15
50878687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 967
Checksum: 351
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