[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 23rd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 32291 73 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 3 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
087/22:41:29
107 -1
3 3
2 3
2
N/A 2
7 -0
2 226
2
000/00:06:58
215 -1
0 -0
1 221
0
087/22:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
2
000/00:00:00
000 0
0 0
0 221
0
Coasting Arc #1 (Orbit 3772)
---------------------------------------
Vector Time (GMT): 2014/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5179627
44 A = 6793139
83 meter
Y = -2331791
29 meter E =
0009998
Z = 3715629
59 I = 51
68734
XDOT = 4905
261934 Wp = 79
81417
YDOT = -4019
943513 meter/sec RA = 173
11657 deg
ZDOT = 4307
081071 TA = 324
42557
MA = 324
49219
Ha = 225
933 n
mi
Hp = 220
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16993528
36 X = -5171217
30
Y = -7650233
88 feet Y = -2389665
80 meter
Z = 12190385
79 Z = 3690488
22
XDOT = 16093
379049 XDOT = 4928
926748
YDOT = -13188
791052 feet/sec YDOT = -3964
956970 meter/sec
ZDOT = 14130
843409 ZDOT = 4330
968157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16807102
79 X = -5122804
93
Y = -8209658
39 feet Y = -2502303
88 meter
Z = 12084469
18 Z = 3683346
21
XDOT = 15833
453025 XDOT = 4826
036482
YDOT = -11425
449593 feet/sec YDOT = -3482
477036 meter/sec
ZDOT = 14232
309856 ZDOT = 4338
008044
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 14080
55660956
00016717 00000-0 10270-3 0 9002
2 25544 51
6490 173
9150 0003428 326
4032 33
6901 15
50850905 37730
Satellite: ISS
Catalog Number: 25544
Epoch time: 14080
55660956 = yrday
fracday
Element set: 900
Inclination: 51
6490 deg
RA of node: 173
9150 deg
Eccentricity:
0003428
Arg of perigee: 326
4032 deg
Mean anomaly: 33
6901 deg
Mean motion: 15
50850905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3773
Checksum: 296
Coasting Arc #2 (Orbit 3787)
---------------------------------------
Vector Time (GMT): 2014/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4852556
80 A = 6791662
39 meter
Y = 2329841
68 meter E =
0007645
Z = -4149855
17 I = 51
71255
XDOT = -5216
900980 Wp = 44
51958
YDOT = 4138
814750 meter/sec RA = 168
16047 deg
ZDOT = -3775
550381 TA = 186
54624
MA = 186
55623
Ha = 225
905 n
mi
Hp = 220
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15920461
95 X = 4846302
06
Y = 7643837
53 feet Y = 2384070
74 meter
Z = -13615010
39 Z = -4126297
46
XDOT = -17115
816863 XDOT = -5244
453940
YDOT = 13578
788550 feet/sec YDOT = 4080
321628 meter/sec
ZDOT = -12386
976315 ZDOT = -3800
960711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15881940
59 X = 4840815
49
Y = 7895927
44 feet Y = 2406678
68 meter
Z = -13515774
55 Z = -4119608
08
XDOT = -16675
672442 XDOT = -5082
744960
YDOT = 12147
375169 feet/sec YDOT = 3702
519952 meter/sec
ZDOT = -12494
910978 ZDOT = -3808
448866
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 14081
52317771
00016717 00000-0 10270-3 0 9015
2 25544 51
6483 169
1215 0003521 330
5782 29
5170 15
50870298 37888
Satellite: ISS
Catalog Number: 25544
Epoch time: 14081
52317771 = yrday
fracday
Element set: 901
Inclination: 51
6483 deg
RA of node: 169
1215 deg
Eccentricity:
0003521
Arg of perigee: 330
5782 deg
Mean anomaly: 29
5170 deg
Mean motion: 15
50870298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3788
Checksum: 307
Coasting Arc #3 (Orbit 3803)
---------------------------------------
Vector Time (GMT): 2014/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4474170
30 A = 6790057
82 meter
Y = -2371263
89 meter E =
0006873
Z = 4517797
89 I = 51
73837
XDOT = 5497
169140 Wp = 90
73785
YDOT = -4287
037580 meter/sec RA = 163
20323 deg
ZDOT = 3189
659625 TA = 327
24285
MA = 327
28545
Ha = 226
012 n
mi
Hp = 220
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14679036
42 X = -4469267
76
Y = -7779737
17 feet Y = -2421269
15 meter
Z = 14822171
55 Z = 4496075
12
XDOT = 18035
331823 XDOT = 5529
204864
YDOT = -14065
083925 feet/sec YDOT = -4225
385331 meter/sec
ZDOT = 10464
762550 ZDOT = 3216
442237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14781746
92 X = -4505476
46
Y = -7758999
22 feet Y = -2364942
96 meter
Z = 14730684
96 Z = 4489912
77
XDOT = 17385
106884 XDOT = 5298
980578
YDOT = -13010
063754 feet/sec YDOT = -3965
467432 meter/sec
ZDOT = 10578
533532 ZDOT = 3224
337021
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 14082
55414858
00016717 00000-0 10270-3 0 9024
2 25544 51
6485 164
0066 0003605 335
6487 24
4493 15
50950288 38048
Satellite: ISS
Catalog Number: 25544
Epoch time: 14082
55414858 = yrday
fracday
Element set: 902
Inclination: 51
6485 deg
RA of node: 164
0066 deg
Eccentricity:
0003605
Arg of perigee: 335
6487 deg
Mean anomaly: 24
4493 deg
Mean motion: 15
50950288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3804
Checksum: 316
Coasting Arc #4 (Orbit 3818)
---------------------------------------
Vector Time (GMT): 2014/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4070440
43 A = 6788766
41 meter
Y = 2484514
71 meter E =
0011922
Z = -4842934
69 I = 51
76281
XDOT = -5711
067789 Wp = 54
21728
YDOT = 4423
707519 meter/sec RA = 158
24733 deg
ZDOT = -2528
230308 TA = 190
89971
MA = 190
92557
Ha = 226
004 n
mi
Hp = 220
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13354463
35 X = 4065880
82
Y = 8151294
99 feet Y = 2530007
09 meter
Z = -15888893
35 Z = -4823172
44
XDOT = -18737
099044 XDOT = -5747
828946
YDOT = 14513
476111 feet/sec YDOT = 4359
636943 meter/sec
ZDOT = -8294
718858 ZDOT = -2556
063402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13602263
43 X = 4145969
89
Y = 7899403
02 feet Y = 2407738
04 meter
Z = -15805698
18 Z = -4817576
81
XDOT = -17836
775504 XDOT = -5436
649174
YDOT = 13864
510147 feet/sec YDOT = 4225
902693 meter/sec
ZDOT = -8412
965390 ZDOT = -2564
271851
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 14083
52065485
00016717 00000-0 10270-3 0 9031
2 25544 51
6477 159
2125 0003694 340
3811 19
7198 15
50963626 38198
Satellite: ISS
Catalog Number: 25544
Epoch time: 14083
52065485 = yrday
fracday
Element set: 903
Inclination: 51
6477 deg
RA of node: 159
2125 deg
Eccentricity:
0003694
Arg of perigee: 340
3811 deg
Mean anomaly: 19
7198 deg
Mean motion: 15
50963626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3819
Checksum: 323
Coasting Arc #5 (Orbit 3834)
---------------------------------------
Vector Time (GMT): 2014/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3627954
66 A = 6787471
31 meter
Y = -2653764
75 meter E =
0003616
Z = 5082560
04 I = 51
78848
XDOT = 5885
526543 Wp = 82
22267
YDOT = -4563
317081 meter/sec RA = 153
29082 deg
ZDOT = 1817
835053 TA = 350
20845
MA = 350
21550
Ha = 226
086 n
mi
Hp = 219
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11902738
37 X = -3622699
29
Y = -8706577
27 feet Y = -2694305
00 meter
Z = 16675065
74 Z = 5064949
09
XDOT = 19309
470284 XDOT = 5927
286763
YDOT = -14971
512734 feet/sec YDOT = -4497
267681 meter/sec
ZDOT = 5964
025765 ZDOT = 1846
527763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12310113
22 X = -3752122
51
Y = -8270798
64 feet Y = -2520939
43 meter
Z = 16600978
53 Z = 5059978
26
XDOT = 18121
616519 XDOT = 5523
468715
YDOT = -14752
161364 feet/sec YDOT = -4496
458784 meter/sec
ZDOT = 6085
941017 ZDOT = 1854
994822
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 14084
55156008
00016717 00000-0 10270-3 0 9048
2 25544 51
6484 154
0975 0003777 344
9480 15
1558 15
51046276 38358
Satellite: ISS
Catalog Number: 25544
Epoch time: 14084
55156008 = yrday
fracday
Element set: 904
Inclination: 51
6484 deg
RA of node: 154
0975 deg
Eccentricity:
0003777
Arg of perigee: 344
9480 deg
Mean anomaly: 15
1558 deg
Mean motion: 15
51046276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3835
Checksum: 320
Coasting Arc #6 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2014/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3189207
16 A = 6786709
67 meter
Y = 2892642
91 meter E =
0014649
Z = -5258560
86 I = 51
81268
XDOT = -5976
074716 Wp = 66
65551
YDOT = 4662
149467 meter/sec RA = 148
33528 deg
ZDOT = -1056
481269 TA = 193
20940
MA = 193
24780
Ha = 226
112 n
mi
Hp = 219
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10463278
10 X = 3182168
13
Y = 9490298
26 feet Y = 2928266
72 meter
Z = -17252496
27 Z = -5243085
70
XDOT = -19606
544345 XDOT = -6022
631765
YDOT = 15295
765967 feet/sec YDOT = 4595
060731 meter/sec
ZDOT = -3466
145897 ZDOT = -1085
625553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11058215
70 X = 3370544
15
Y = 8916362
78 feet Y = 2717707
38 meter
Z = -17187463
96 Z = -5238739
01
XDOT = -18097
665578 XDOT = -5516
168468
YDOT = 15503
771675 feet/sec YDOT = 4725
549607 meter/sec
ZDOT = -3589
997998 ZDOT = -1094
231390
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 14085
51800527
00016717 00000-0 10270-3 0 9058
2 25544 51
6477 149
3026 0003871 350
1707 9
9368 15
51057879 38508
Satellite: ISS
Catalog Number: 25544
Epoch time: 14085
51800527 = yrday
fracday
Element set: 905
Inclination: 51
6477 deg
RA of node: 149
3026 deg
Eccentricity:
0003871
Arg of perigee: 350
1707 deg
Mean anomaly: 9
9368 deg
Mean motion: 15
51057879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3850
Checksum: 320
Coasting Arc #7 (Orbit 3865)
---------------------------------------
Vector Time (GMT): 2014/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2728192
36 A = 6786073
69 meter
Y = -3190827
53 meter E =
0003927
Z = 5329699
27 I = 51
83781
XDOT = 6026
937011 Wp = 32
45908
YDOT = -4730
196443 meter/sec RA = 143
38027 deg
ZDOT = 256
328289 TA = 55
12199
MA = 55
08508
Ha = 226
150 n
mi
Hp = 219
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8950762
33 X = -2718198
81
Y = -10468594
26 feet Y = -3221279
35 meter
Z = 17485890
00 Z = 5316470
89
XDOT = 19773
415392 XDOT = 6078
138048
YDOT = -15519
017203 feet/sec YDOT = -4662
513052 meter/sec
ZDOT = 840
972076 ZDOT = 285
731054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9771195
44 X = -2978260
37
Y = -9806583
86 feet Y = -2989046
76 meter
Z = 17430393
39 Z = 5312783
91
XDOT = 17916
602943 XDOT = 5460
980577
YDOT = -16153
457215 feet/sec YDOT = -4923
573759 meter/sec
ZDOT = 965
938851 ZDOT = 294
418162
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 14086
54884550
00016717 00000-0 10270-3 0 9061
2 25544 51
6481 144
1876 0003933 354
6758 5
4351 15
51144579 38667
Satellite: ISS
Catalog Number: 25544
Epoch time: 14086
54884550 = yrday
fracday
Element set: 906
Inclination: 51
6481 deg
RA of node: 144
1876 deg
Eccentricity:
0003933
Arg of perigee: 354
6758 deg
Mean anomaly: 5
4351 deg
Mean motion: 15
51144579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3866
Checksum: 332
Coasting Arc #8 (Orbit 3880)
---------------------------------------
Vector Time (GMT): 2014/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2302895
37 A = 6786116
75 meter
Y = 3543208
93 meter E =
0014972
Z = -5322215
16 I = 51
86206
XDOT = -5991
844349 Wp = 78
73625
YDOT = 4728
049659 meter/sec RA = 138
42601 deg
ZDOT = 559
187448 TA = 196
56963
MA = 196
61861
Ha = 226
212 n
mi
Hp = 219
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7555431
00 X = 2288956
75
Y = 11624701
22 feet Y = 3568882
68 meter
Z = -17461335
84 Z = -5311062
45
XDOT = -19658
281985 XDOT = -6046
985480
YDOT = 15511
973948 feet/sec YDOT = 4660
736780 meter/sec
ZDOT = 1834
604488 ZDOT = 529
945433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8649136
23 X = 2636256
72
Y = 10910473
85 feet Y = 3325512
43 meter
Z = -17414662
45 Z = -5307989
11
XDOT = -17445
812411 XDOT = -5317
483623
YDOT = 16537
892174 feet/sec YDOT = 5040
749535 meter/sec
ZDOT = 1710
306339 ZDOT = 521
301372
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 14087
51522989
00016717 00000-0 10270-3 0 9075
2 25544 51
6478 139
3918 0004047 359
8777
2373 15
51154760 38818
Satellite: ISS
Catalog Number: 25544
Epoch time: 14087
51522989 = yrday
fracday
Element set: 907
Inclination: 51
6478 deg
RA of node: 139
3918 deg
Eccentricity:
0004047
Arg of perigee: 359
8777 deg
Mean anomaly:
2373 deg
Mean motion: 15
51154760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3881
Checksum: 337
Coasting Arc #9 (Orbit 3887)
---------------------------------------
Vector Time (GMT): 2014/087/22:44:58
215
Vector Time (MET): N/A
Weight (LBS) : 900608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3849187
44 A = 6788108
52 meter
Y = 1999358
69 meter E =
0012934
Z = -5232664
49 I = 51
87501
XDOT = -4738
162380 Wp = 64
79848
YDOT = 5881
955655 meter/sec RA = 136
22574 deg
ZDOT = -1235
008519 TA = 193
34722
MA = 193
38147
Ha = 226
225 n
mi
Hp = 221
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12628567
73 X = 3851962
62
Y = 6559575
77 feet Y = 2042417
52 meter
Z = -17167534
40 Z = -5213959
29
XDOT = -15545
152166 XDOT = -4797
584324
YDOT = 19297
754774 feet/sec YDOT = 5828
638052 meter/sec
ZDOT = -4051
865219 ZDOT = -1258
170984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10883463
82 X = -3317279
77
Y = -9314457
55 feet Y = -2839046
66 meter
Z = -17088712
37 Z = -5208639
53
XDOT = 18866
620899 XDOT = 5750
546050
YDOT = -14411
796383 feet/sec YDOT = -4392
715538 meter/sec
ZDOT = -4150
618959 ZDOT = -1265
108659
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 14087
96620161
00016717 00000-0 10270-3 0 9086
2 25544 51
6490 137
1542 0003867 326
3564 33
7341 15
50624304 38881
Satellite: ISS
Catalog Number: 25544
Epoch time: 14087
96620161 = yrday
fracday
Element set: 908
Inclination: 51
6490 deg
RA of node: 137
1542 deg
Eccentricity:
0003867
Arg of perigee: 326
3564 deg
Mean anomaly: 33
7341 deg
Mean motion: 15
50624304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3888
Checksum: 311
Coasting Arc #10 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2014/088/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3293463
67 A = 6787465
37 meter
Y = -2593480
85 meter E =
0002903
Z = 5337702
08 I = 51
89483
XDOT = 4934
587217 Wp = 10
13194
YDOT = -5860
282189 meter/sec RA = 131
27245 deg
ZDOT = 200
109232 TA = 77
98272
MA = 77
95018
Ha = 226
327 n
mi
Hp = 220
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10805327
00 X = -3290146
90
Y = -8508795
43 feet Y = -2630291
11 meter
Z = 17512145
92 Z = 5321711
32
XDOT = 16189
590608 XDOT = 4998
779395
YDOT = -19226
647603 feet/sec YDOT = -5804
741519 meter/sec
ZDOT = 656
526351 ZDOT = 224
237614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8894741
50 X = 2711117
21
Y = 10601394
21 feet Y = 3231304
95 meter
Z = 17444883
50 Z = 5317200
49
XDOT = -19074
272299 XDOT = -5813
838197
YDOT = 14769
049372 feet/sec YDOT = 4501
606249 meter/sec
ZDOT = 759
373532 ZDOT = 231
457053
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 14088
99736058
00016717 00000-0 10270-3 0 9094
2 25544 51
6487 132
0409 0003852 329
8094 30
2834 15
50664976 39040
Satellite: ISS
Catalog Number: 25544
Epoch time: 14088
99736058 = yrday
fracday
Element set: 909
Inclination: 51
6487 deg
RA of node: 132
0409 deg
Eccentricity:
0003852
Arg of perigee: 329
8094 deg
Mean anomaly: 30
2834 deg
Mean motion: 15
50664976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 338
Coasting Arc #11 (Orbit 3918)
---------------------------------------
Vector Time (GMT): 2014/089/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3079251
58 A = 6787361
44 meter
Y = 2870484
71 meter E =
0013265
Z = -5335215
13 I = 51
91395
XDOT = -4796
779205 Wp = 78
40780
YDOT = 5947
993844 meter/sec RA = 126
32631 deg
ZDOT = 435
192778 TA = 195
71442
MA = 195
75563
Ha = 226
282 n
mi
Hp = 220
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10102531
42 X = 3072841
24
Y = 9417600
75 feet Y = 2904882
25 meter
Z = -17503986
66 Z = -5320272
46
XDOT = -15737
464583 XDOT = -4865
048545
YDOT = 19514
415498 feet/sec YDOT = 5893
971528 meter/sec
ZDOT = 1427
797827 ZDOT = 411
723858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8211361
37 X = -2502822
95
Y = -11203575
41 feet Y = -3414849
78 meter
Z = -17441196
53 Z = -5316076
70
XDOT = 18386
682450 XDOT = 5604
260811
YDOT = -15524
971608 feet/sec YDOT = -4732
011346 meter/sec
ZDOT = 1327
713187 ZDOT = 404
686979
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 14089
96404256
00016717 00000-0 10270-3 0 9106
2 25544 51
6480 127
2465 0003949 333
5368 26
5580 15
50716218 39193
Satellite: ISS
Catalog Number: 25544
Epoch time: 14089
96404256 = yrday
fracday
Element set: 910
Inclination: 51
6480 deg
RA of node: 127
2465 deg
Eccentricity:
0003949
Arg of perigee: 333
5368 deg
Mean anomaly: 26
5580 deg
Mean motion: 15
50716218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3919
Checksum: 323
Coasting Arc #12 (Orbit 3934)
---------------------------------------
Vector Time (GMT): 2014/090/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2870171
70 A = 6787528
80 meter
Y = -3196890
60 meter E =
0005875
Z = 5254273
39 I = 51
93261
XDOT = 4656
103946 Wp = 15
92074
YDOT = -5987
962810 meter/sec RA = 121
38151 deg
ZDOT = -1094
085504 TA = 84
56029
MA = 84
49327
Ha = 226
335 n
mi
Hp = 220
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9416573
83 X = -2859733
85
Y = -10488486
21 feet Y = -3228927
63 meter
Z = 17238429
77 Z = 5240356
16
XDOT = 15275
931581 XDOT = 4728
031410
YDOT = -19645
547276 feet/sec YDOT = -5935
493245 meter/sec
ZDOT = -3589
519370 ZDOT = -1071
291080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7538158
53 X = 2297630
72
Y = 11994438
69 feet Y = 3655904
91 meter
Z = 17180025
41 Z = 5236471
74
XDOT = -17630
782321 XDOT = -5373
862451
YDOT = 16109
822137 feet/sec YDOT = 4910
273787 meter/sec
ZDOT = -3492
265222 ZDOT = -1064
442440
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 14090
99513776
00016717 00000-0 10270-3 0 9110
2 25544 51
6479 122
1328 0003947 336
9175 23
1798 15
50766866 39350
Satellite: ISS
Catalog Number: 25544
Epoch time: 14090
99513776 = yrday
fracday
Element set: 911
Inclination: 51
6479 deg
RA of node: 122
1328 deg
Eccentricity:
0003947
Arg of perigee: 336
9175 deg
Mean anomaly: 23
1798 deg
Mean motion: 15
50766866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3935
Checksum: 344
Coasting Arc #13 (Orbit 3949)
---------------------------------------
Vector Time (GMT): 2014/091/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2716592
80 A = 6788013
29 meter
Y = 3543017
05 meter E =
0011691
Z = -5123016
90 I = 51
94894
XDOT = -4484
258950 Wp = 86
39513
YDOT = 5953
480407 meter/sec RA = 116
43681 deg
ZDOT = 1743
619776 TA = 200
39564
MA = 200
44237
Ha = 226
326 n
mi
Hp = 220
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8912706
04 X = 2701658
33
Y = 11624071
69 feet Y = 3573311
64 meter
Z = -16807798
23 Z = -5109856
62
XDOT = -14712
135662 XDOT = -4558
968868
YDOT = 19532
416035 feet/sec YDOT = 5902
917022 meter/sec
ZDOT = 5720
537322 ZDOT = 1721
653480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7063371
16 X = -2152915
53
Y = -12904068
69 feet Y = -3933160
14 meter
Z = -16752649
10 Z = -5106207
45
XDOT = 16713
755392 XDOT = 5094
352643
YDOT = -16435
934523 feet/sec YDOT = -5009
672843 meter/sec
ZDOT = 5626
772393 ZDOT = 1715
040225
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 14091
96176031
00016717 00000-0 10270-3 0 9128
2 25544 51
6469 117
3375 0003979 340
5784 19
5215 15
50806741 39506
Satellite: ISS
Catalog Number: 25544
Epoch time: 14091
96176031 = yrday
fracday
Element set: 912
Inclination: 51
6469 deg
RA of node: 117
3375 deg
Eccentricity:
0003979
Arg of perigee: 340
5784 deg
Mean anomaly: 19
5215 deg
Mean motion: 15
50806741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3950
Checksum: 318
Coasting Arc #14 (Orbit 3965)
---------------------------------------
Vector Time (GMT): 2014/092/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2574711
63 A = 6788736
19 meter
Y = -3926588
99 meter E =
0008739
Z = 4901667
35 I = 51
96528
XDOT = 4326
177361 Wp = 33
02728
YDOT = -5850
714151 meter/sec RA = 111
49431 deg
ZDOT = -2405
275619 TA = 80
50496
MA = 80
40621
Ha = 226
327 n
mi
Hp = 220
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8447216
64 X = -2554423
25
Y = -12882509
81 feet Y = -3955267
16 meter
Z = 16081585
79 Z = 4889209
29
XDOT = 14193
495280 XDOT = 4402
964017
YDOT = -19195
256400 feet/sec YDOT = -5801
906952 meter/sec
ZDOT = -7891
324210 ZDOT = -2384
072361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6641102
93 X = 2024208
17
Y = 13960080
54 feet Y = 4255032
55 meter
Z = 16029467
63 Z = 4885781
73
XDOT = -15794
950936 XDOT = -4814
301045
YDOT = 16505
694973 feet/sec YDOT = 5030
935828 meter/sec
ZDOT = -7800
782731 ZDOT = -2377
678576
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 14092
99279114
00016717 00000-0 10270-3 0 9139
2 25544 51
6472 112
2234 0003997 343
5754 16
5267 15
50868009 39664
Satellite: ISS
Catalog Number: 25544
Epoch time: 14092
99279114 = yrday
fracday
Element set: 913
Inclination: 51
6472 deg
RA of node: 112
2234 deg
Eccentricity:
0003997
Arg of perigee: 343
5754 deg
Mean anomaly: 16
5267 deg
Mean motion: 15
50868009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3966
Checksum: 327
Coasting Arc #15 (Orbit 3980)
---------------------------------------
Vector Time (GMT): 2014/093/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2496751
40 A = 6789756
60 meter
Y = 4302538
30 meter E =
0008749
Z = -4628532
90 I = 51
97837
XDOT = -4158
026570 Wp = 87
76783
YDOT = 5668
968626 meter/sec RA = 106
55202 deg
ZDOT = 3032
017119 TA = 212
38391
MA = 212
43764
Ha = 226
350 n
mi
Hp = 219
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8191441
61 X = 2470938
02
Y = 14115939
31 feet Y = 4330313
88 meter
Z = -15185475
38 Z = -4616466
96
XDOT = -13641
819456 XDOT = -4235
837921
YDOT = 18598
978433 feet/sec YDOT = 5622
036078 meter/sec
ZDOT = 9947
562725 ZDOT = 3011
628380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6467581
02 X = -1971318
69
Y = -15035224
03 feet Y = -4582736
28 meter
Z = -15135076
97 Z = -4613171
46
XDOT = 14813
098873 XDOT = 4515
032536
YDOT = -16280
527685 feet/sec YDOT = -4962
304839 meter/sec
ZDOT = 9860
475093 ZDOT = 3005
472808
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 14093
95935350
00016717 00000-0 10270-3 0 9148
2 25544 51
6461 107
4276 0003929 347
8475 12
2580 15
50898994 39810
Satellite: ISS
Catalog Number: 25544
Epoch time: 14093
95935350 = yrday
fracday
Element set: 914
Inclination: 51
6461 deg
RA of node: 107
4276 deg
Eccentricity:
0003929
Arg of perigee: 347
8475 deg
Mean anomaly: 12
2580 deg
Mean motion: 15
50898994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3981
Checksum: 342
Coasting Arc #16 (Orbit 3996)
---------------------------------------
Vector Time (GMT): 2014/094/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2430558
59 A = 6790929
98 meter
Y = -4697346
55 meter E =
0011181
Z = 4256215
03 I = 51
99148
XDOT = 4024
379415 Wp = 53
36888
YDOT = -5403
511315 meter/sec RA = 101
61242 deg
ZDOT = -3652
258540 TA = 73
90998
MA = 73
78690
Ha = 226
302 n
mi
Hp = 219
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7974273
57 X = -2398526
62
Y = -15411241
96 feet Y = -4724347
22 meter
Z = 13963960
08 Z = 4244485
77
XDOT = 13203
344536 XDOT = 4102
245213
YDOT = -17728
055494 feet/sec YDOT = -5358
073004 meter/sec
ZDOT = -11982
475524 ZDOT = -3632
519035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6362856
67 X = 1939398
71
Y = 16185580
46 feet Y = 4933364
92 meter
Z = 13915050
81 Z = 4241307
49
XDOT = -13922
067982 XDOT = -4243
446321
YDOT = 15739
259271 feet/sec YDOT = 4797
326226 meter/sec
ZDOT = -11898
157258 ZDOT = -3626
558332
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 14094
99031877
00016717 00000-0 10270-3 0 9155
2 25544 51
6467 102
3132 0003974 350
1727 9
9346 15
50969062 39973
Satellite: ISS
Catalog Number: 25544
Epoch time: 14094
99031877 = yrday
fracday
Element set: 915
Inclination: 51
6467 deg
RA of node: 102
3132 deg
Eccentricity:
0003974
Arg of perigee: 350
1727 deg
Mean anomaly: 9
9346 deg
Mean motion: 15
50969062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3997
Checksum: 332
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