[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 6th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 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
317/02:00:13
041 0
5 1
1 1
1
N/A 0
9 -0
1 226
9
000/00:02:26
082 -0
3 -0
0 219
1
Coasting Arc #1 (Orbit 3324)
---------------------------------------
Vector Time (GMT): 2014/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2858184
44 A = 6798480
44 meter
Y = 6141376
12 meter E =
0014407
Z = -474586
58 I = 51
97586
XDOT = -4466
910717 Wp = 30
43982
YDOT = -1621
114152 meter/sec RA = 118
09771 deg
ZDOT = 6015
585838 TA = 324
47018
MA = 324
56604
Ha = 226
542 n
mi
Hp = 219
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9377245
54 X = -2924340
85
Y = 20148871
78 feet Y = 6109044
12 meter
Z = -1557042
59 Z = -488632
64
XDOT = -14655
218889 XDOT = -4477
673613
YDOT = -5318
615984 feet/sec YDOT = -1671
125890 meter/sec
ZDOT = 19736
174008 ZDOT = 5993
859582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7188478
70 X = -2191048
31
Y = -21024800
26 feet Y = -6408359
12 meter
Z = -1617930
08 Z = -493145
09
XDOT = 12812
988770 XDOT = 3905
398977
YDOT = -5870
193140 feet/sec YDOT = -1789
234869 meter/sec
ZDOT = 19643
822044 ZDOT = 5987
436959
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 14309
50095346
00016717 00000-0 10270-3 0 9006
2 25544 51
6400 119
0662 0004207 358
9710 1
1432 15
50950673 33254
Satellite: ISS
Catalog Number: 25544
Epoch time: 14309
50095346 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 119
0662 deg
Eccentricity:
0004207
Arg of perigee: 358
9710 deg
Mean anomaly: 1
1432 deg
Mean motion: 15
50950673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3325
Checksum: 274
Coasting Arc #2 (Orbit 3340)
---------------------------------------
Vector Time (GMT): 2014/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2822110
98 A = 6798351
14 meter
Y = -6178644
05 meter E =
0009174
Z = -210018
64 I = 51
99011
XDOT = 4217
853902 Wp = 115
48485
YDOT = 2124
410030 meter/sec RA = 113
16399 deg
ZDOT = -6030
845097 TA = 66
76303
MA = 66
66645
Ha = 226
571 n
mi
Hp = 219
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9258894
30 X = 2892012
50
Y = -20271141
91 feet Y = -6146694
55 meter
Z = -689037
54 Z = -196138
83
XDOT = 13838
103354 XDOT = 4223
081504
YDOT = 6969
849181 feet/sec YDOT = 2171
605818 meter/sec
ZDOT = -19786
237196 ZDOT = -6010
342160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7709289
32 X = 2349791
38
Y = 20911540
28 feet Y = 6373837
48 meter
Z = -628833
77 Z = -191668
53
XDOT = -13292
936526 XDOT = -4051
687053
YDOT = 4330
803744 feet/sec YDOT = 1320
028981 meter/sec
ZDOT = -19699
182732 ZDOT = -6004
310897
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 14310
53188523
00016717 00000-0 10270-3 0 9012
2 25544 51
6400 113
9505 0004506 2
3140 357
8031 15
51023221 33417
Satellite: ISS
Catalog Number: 25544
Epoch time: 14310
53188523 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 113
9505 deg
Eccentricity:
0004506
Arg of perigee: 2
3140 deg
Mean anomaly: 357
8031 deg
Mean motion: 15
51023221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3341
Checksum: 243
Coasting Arc #3 (Orbit 3356)
---------------------------------------
Vector Time (GMT): 2014/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2736600
84 A = 6798092
93 meter
Y = 6152514
09 meter E =
0016537
Z = 863332
57 I = 52
00133
XDOT = -4034
905056 Wp = 43
55525
YDOT = -2639
208603 meter/sec RA = 108
23055 deg
ZDOT = 5962
289014 TA = 325
73166
MA = 325
83825
Ha = 226
634 n
mi
Hp = 219
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8978349
23 X = -2809390
20
Y = 20185413
69 feet Y = 6121504
67 meter
Z = 2832455
93 Z = 849861
28
XDOT = -13237
877481 XDOT = -4034
056610
YDOT = -8658
820876 feet/sec YDOT = -2684
324688 meter/sec
ZDOT = 19561
315664 ZDOT = 5942
689575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8192772
73 X = -2497157
13
Y = -20524814
39 feet Y = -6255963
43 meter
Z = 2773978
47 Z = 845508
64
XDOT = 14025
662527 XDOT = 4275
021938
YDOT = -2940
632129 feet/sec YDOT = -896
304673 meter/sec
ZDOT = 19478
199793 ZDOT = 5936
955297
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 14311
56279989
00016717 00000-0 10270-3 0 9024
2 25544 51
6407 108
8346 0004211 7
5100 352
6113 15
51016999 33571
Satellite: ISS
Catalog Number: 25544
Epoch time: 14311
56279989 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 108
8346 deg
Eccentricity:
0004211
Arg of perigee: 7
5100 deg
Mean anomaly: 352
6113 deg
Mean motion: 15
51016999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3357
Checksum: 299
Coasting Arc #4 (Orbit 3371)
---------------------------------------
Vector Time (GMT): 2014/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2674213
43 A = 6797254
94 meter
Y = -6053756
37 meter E =
0006205
Z = -1549303
21 I = 52
00826
XDOT = 3883
842258 Wp = 109
72597
YDOT = 3189
174764 meter/sec RA = 103
29766 deg
ZDOT = -5778
416106 TA = 87
08559
MA = 87
01458
Ha = 226
676 n
mi
Hp = 219
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8773666
09 X = 2749235
39
Y = -19861405
42 feet Y = -6023432
11 meter
Z = -5083015
77 Z = -1536129
71
XDOT = 12742
264626 XDOT = 3875
961909
YDOT = 10463
171798 feet/sec YDOT = 3232
562357 meter/sec
ZDOT = -18958
058092 ZDOT = -5759
567601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8439174
03 X = 2572260
24
Y = 20020272
54 feet Y = 6102179
07 meter
Z = -5025805
45 Z = -1531865
50
XDOT = -14971
851824 XDOT = -4563
420436
YDOT = 1589
333696 feet/sec YDOT = 484
428911 meter/sec
ZDOT = -18878
238833 ZDOT = -5754
087196
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 14312
52926310
00016717 00000-0 10270-3 0 9039
2 25544 51
6410 104
0386 0004468 10
9334 349
1908 15
51064159 33729
Satellite: ISS
Catalog Number: 25544
Epoch time: 14312
52926310 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 104
0386 deg
Eccentricity:
0004468
Arg of perigee: 10
9334 deg
Mean anomaly: 349
1908 deg
Mean motion: 15
51064159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3372
Checksum: 282
Coasting Arc #5 (Orbit 3387)
---------------------------------------
Vector Time (GMT): 2014/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2587567
26 A = 6796211
20 meter
Y = 5882440
99 meter E =
0016633
Z = 2182424
53 I = 52
01239
XDOT = -3805
649575 Wp = 58
40223
YDOT = -3728
755722 meter/sec RA = 98
36437 deg
ZDOT = 5515
912868 TA = 325
67727
MA = 325
78464
Ha = 226
703 n
mi
Hp = 218
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8489393
90 X = -2663755
52
Y = 19299347
08 feet Y = 5853079
11 meter
Z = 7160185
46 Z = 2169669
24
XDOT = -12485
726952 XDOT = -3790
466043
YDOT = -12233
450532 feet/sec YDOT = -3771
228149 meter/sec
ZDOT = 18096
826996 ZDOT = 5497
461971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8548691
17 X = -2605641
07
Y = -19293651
39 feet Y = -5880704
94 meter
Z = 7104770
07 Z = 2165533
92
XDOT = 16118
849777 XDOT = 4913
025412
YDOT = -479
480696 feet/sec YDOT = -146
145716 meter/sec
ZDOT = 18018
798336 ZDOT = 5492
129733
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 14313
56013861
00016717 00000-0 10270-3 0 9043
2 25544 51
6421 98
9232 0004256 14
8673 345
2603 15
51085863 33887
Satellite: ISS
Catalog Number: 25544
Epoch time: 14313
56013861 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 98
9232 deg
Eccentricity:
0004256
Arg of perigee: 14
8673 deg
Mean anomaly: 345
2603 deg
Mean motion: 15
51085863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3388
Checksum: 304
Coasting Arc #6 (Orbit 3402)
---------------------------------------
Vector Time (GMT): 2014/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2545391
07 A = 6794818
33 meter
Y = -5636496
13 meter E =
0005790
Z = -2821668
57 I = 52
01194
XDOT = 3758
246829 Wp = 71
09455
YDOT = 4262
076489 meter/sec RA = 93
43022 deg
ZDOT = -5130
322505 TA = 140
68556
MA = 140
64351
Ha = 226
746 n
mi
Hp = 218
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8351020
58 X = 2621937
52
Y = -18492441
36 feet Y = -5607603
86 meter
Z = -9257442
82 Z = -2809117
37
XDOT = 12330
206132 XDOT = 3735
229900
YDOT = 13983
190581 feet/sec YDOT = 4303
975045 meter/sec
ZDOT = -16831
766748 ZDOT = -5112
120952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8355422
82 X = 2546732
88
Y = 18517647
25 feet Y = 5644178
88 meter
Z = -9202925
06 Z = -2805051
56
XDOT = -17361
411461 XDOT = -5291
758213
YDOT = -482
055841 feet/sec YDOT = -146
930620 meter/sec
ZDOT = -16754
897389 ZDOT = -5106
892724
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 14314
52656691
00016717 00000-0 10270-3 0 9055
2 25544 51
6425 94
1274 0004449 18
2594 341
8716 15
51101746 34033
Satellite: ISS
Catalog Number: 25544
Epoch time: 14314
52656691 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 94
1274 deg
Eccentricity:
0004449
Arg of perigee: 18
2594 deg
Mean anomaly: 341
8716 deg
Mean motion: 15
51101746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3403
Checksum: 302
Coasting Arc #7 (Orbit 3418)
---------------------------------------
Vector Time (GMT): 2014/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2506221
03 A = 6793195
73 meter
Y = 5318323
49 meter E =
0014685
Z = 3386647
22 I = 52
00895
XDOT = -3777
326809 Wp = 73
24988
YDOT = -4764
635758 meter/sec RA = 88
49447 deg
ZDOT = 4674
366972 TA = 326
04746
MA = 326
14136
Ha = 226
772 n
mi
Hp = 218
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8222509
93 X = -2581956
99
Y = 17448567
89 feet Y = 5289873
79 meter
Z = 11111047
30 Z = 3374288
28
XDOT = -12392
804492 XDOT = -3746
473731
YDOT = -15632
007080 feet/sec YDOT = -4806
703837 meter/sec
ZDOT = 15335
849645 ZDOT = 4656
091830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7951952
25 X = -2423755
04
Y = -17607330
55 feet Y = -5366714
35 meter
Z = 11057392
52 Z = 3370293
24
XDOT = 18715
243452 XDOT = 5704
406204
YDOT = 1156
233855 feet/sec YDOT = 352
420079 meter/sec
ZDOT = 15258
758827 ZDOT = 4650
869690
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 14315
55740293
00016717 00000-0 10270-3 0 9062
2 25544 51
6435 89
0119 0004365 21
4132 338
7201 15
51150880 34190
Satellite: ISS
Catalog Number: 25544
Epoch time: 14315
55740293 = yrday
fracday
Element set: 906
Inclination: 51
6435 deg
RA of node: 89
0119 deg
Eccentricity:
0004365
Arg of perigee: 21
4132 deg
Mean anomaly: 338
7201 deg
Mean motion: 15
51150880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3419
Checksum: 286
Coasting Arc #8 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2014/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2530971
89 A = 6791558
42 meter
Y = -4937442
19 meter E =
0010011
Z = -3928466
02 I = 52
00190
XDOT = 3813
404445 Wp = 54
01845
YDOT = 5216
579496 meter/sec RA = 83
55695 deg
ZDOT = -4101
133439 TA = 173
14489
MA = 173
13119
Ha = 226
796 n
mi
Hp = 218
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8303713
56 X = 2605078
90
Y = -16198957
33 feet Y = -4908724
85 meter
Z = -12888668
03 Z = -3915990
77
XDOT = 12511
169438 XDOT = 3774
710275
YDOT = 17114
762127 feet/sec YDOT = 5259
007127 meter/sec
ZDOT = -13455
162200 ZDOT = -4082
702163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7228118
43 X = 2203130
50
Y = 16748243
07 feet Y = 5104864
49 meter
Z = -12834574
37 Z = -3911978
27
XDOT = -19999
981409 XDOT = -6095
994333
YDOT = -1616
001115 feet/sec YDOT = -492
557140 meter/sec
ZDOT = -13377
490633 ZDOT = -4077
459145
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 14316
52379525
00016717 00000-0 10270-3 0 9077
2 25544 51
6437 84
2163 0004502 24
5411 335
5954 15
51147034 34349
Satellite: ISS
Catalog Number: 25544
Epoch time: 14316
52379525 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 84
2163 deg
Eccentricity:
0004502
Arg of perigee: 24
5411 deg
Mean anomaly: 335
5954 deg
Mean motion: 15
51147034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 290
Coasting Arc #9 (Orbit 3442)
---------------------------------------
Vector Time (GMT): 2014/317/02:01:26
082
Vector Time (MET): N/A
Weight (LBS) : 930799
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3598358
84 A = 6787644
32 meter
Y = -2692126
52 meter E =
0015897
Z = -5101051
16 I = 51
98589
XDOT = 2598
565530 Wp = 62
19299
YDOT = 6958
176061 meter/sec RA = 80
66456 deg
ZDOT = -1836
339025 TA = 190
05509
MA = 190
08693
Ha = 226
933 n
mi
Hp = 219
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11805639
24 X = 3652974
97
Y = -8832436
07 feet Y = -2651581
96 meter
Z = -16735732
15 Z = -5083437
95
XDOT = 8525
477460 XDOT = 2529
484914
YDOT = 22828
661619 feet/sec YDOT = 6986
848651 meter/sec
ZDOT = -6024
734334 ZDOT = -1823
883200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7009115
72 X = -2136378
47
Y = -13068370
92 feet Y = -3983239
46 meter
Z = -16660124
67 Z = -5078006
00
XDOT = 22877
312420 XDOT = 6973
004826
YDOT = -4643
684905 feet/sec YDOT = -1415
395159 meter/sec
ZDOT = -5972
865889 ZDOT = -1820
529523
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 14317
10362275
00016717 00000-0 10270-3 0 9087
2 25544 51
6446 81
3426 0004500 17
1057 343
0245 15
50979114 34439
Satellite: ISS
Catalog Number: 25544
Epoch time: 14317
10362275 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 81
3426 deg
Eccentricity:
0004500
Arg of perigee: 17
1057 deg
Mean anomaly: 343
0245 deg
Mean motion: 15
50979114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3443
Checksum: 280
Coasting Arc #10 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2014/318/02:01:26
082
Vector Time (MET): N/A
Weight (LBS) : 930799
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3675405
62 A = 6786798
93 meter
Y = 2214583
57 meter E =
0005093
Z = 5253783
34 I = 51
97728
XDOT = -2696
207975 Wp = 64
95670
YDOT = -7092
250510 meter/sec RA = 75
72150 deg
ZDOT = 1104
605708 TA = 14
51323
MA = 14
49861
Ha = 227
029 n
mi
Hp = 218
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12058417
39 X = -3725417
96
Y = 7265694
14 feet Y = 2173203
24 meter
Z = 17236821
98 Z = 5235807
00
XDOT = -8845
826691 XDOT = -2622
066279
YDOT = -23268
538418 feet/sec YDOT = -7121
986691 meter/sec
ZDOT = 3624
034476 ZDOT = 1091
687919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5646286
01 X = 1720987
98
Y = 12998704
34 feet Y = 3962005
08 meter
Z = 17159746
89 Z = 5230290
85
XDOT = -23265
806149 XDOT = -7091
417714
YDOT = 5398
429805 feet/sec YDOT = 1645
441405 meter/sec
ZDOT = 3570
229072 ZDOT = 1088
205821
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 14318
13454598
00016717 00000-0 10270-3 0 9092
2 25544 51
6444 76
2276 0004455 19
1355 340
9962 15
51020282 34598
Satellite: ISS
Catalog Number: 25544
Epoch time: 14318
13454598 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 76
2276 deg
Eccentricity:
0004455
Arg of perigee: 19
1355 deg
Mean anomaly: 340
9962 deg
Mean motion: 15
51020282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 314
Coasting Arc #11 (Orbit 3473)
---------------------------------------
Vector Time (GMT): 2014/319/02:01:26
082
Vector Time (MET): N/A
Weight (LBS) : 930799
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3818779
90 A = 6786412
94 meter
Y = -1747297
01 meter E =
0017309
Z = -5345515
10 I = 51
96821
XDOT = 2770
173809 Wp = 73
36491
YDOT = 7123
502943 meter/sec RA = 70
77687 deg
ZDOT = -345
599740 TA = 193
32464
MA = 193
37041
Ha = 226
994 n
mi
Hp = 218
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12528805
43 X = 3864001
90
Y = -5732601
73 feet Y = -1704340
20 meter
Z = -17537779
21 Z = -5326853
88
XDOT = 9088
496748 XDOT = 2691
990090
YDOT = 23371
072647 feet/sec YDOT = 7154
043664 meter/sec
ZDOT = -1133
857416 ZDOT = -332
332503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4292966
36 X = -1308496
15
Y = -13198514
44 feet Y = -4022907
20 meter
Z = -17457864
83 Z = -5321157
20
XDOT = 23275
070058 XDOT = 7094
241354
YDOT = -6126
881518 feet/sec YDOT = -1867
473487 meter/sec
ZDOT = -1078
577238 ZDOT = -328
750342
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 14319
10102025
00016717 00000-0 10270-3 0 9107
2 25544 51
6451 71
4320 0004623 23
2222 336
9138 15
51036437 34745
Satellite: ISS
Catalog Number: 25544
Epoch time: 14319
10102025 = yrday
fracday
Element set: 910
Inclination: 51
6451 deg
RA of node: 71
4320 deg
Eccentricity:
0004623
Arg of perigee: 23
2222 deg
Mean anomaly: 336
9138 deg
Mean motion: 15
51036437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3474
Checksum: 256
Coasting Arc #12 (Orbit 3489)
---------------------------------------
Vector Time (GMT): 2014/320/02:01:26
082
Vector Time (MET): N/A
Weight (LBS) : 930799
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4006320
50 A = 6786281
09 meter
Y = 1255614
61 meter E =
0006786
Z = 5328116
32 I = 51
95703
XDOT = -2818
821067 Wp = 41
15874
YDOT = -7116
699303 meter/sec RA = 65
83104 deg
ZDOT = -437
130848 TA = 53
02382
MA = 52
96171
Ha = 227
072 n
mi
Hp = 218
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13144096
14 X = -4045945
99
Y = 4119470
49 feet Y = 1210591
93 meter
Z = 17480696
60 Z = 5308557
60
XDOT = -9248
100612 XDOT = -2736
907502
YDOT = -23348
750994 feet/sec YDOT = -7147
763195 meter/sec
ZDOT = -1434
156324 ZDOT = -450
625325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2855520
26 X = 870362
58
Y = 13583112
68 feet Y = 4140132
74 meter
Z = 17397043
08 Z = 5302618
73
XDOT = -23124
162932 XDOT = -7048
244862
YDOT = 6792
506190 feet/sec YDOT = 2070
355887 meter/sec
ZDOT = -1490
395797 ZDOT = -454
272639
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 14320
13190472
00016717 00000-0 10270-3 0 9116
2 25544 51
6450 66
3165 0004613 25
0151 335
1223 15
51087581 34904
Satellite: ISS
Catalog Number: 25544
Epoch time: 14320
13190472 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 66
3165 deg
Eccentricity:
0004613
Arg of perigee: 25
0151 deg
Mean anomaly: 335
1223 deg
Mean motion: 15
51087581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3490
Checksum: 264
Coasting Arc #13 (Orbit 3504)
---------------------------------------
Vector Time (GMT): 2014/321/02:01:26
082
Vector Time (MET): N/A
Weight (LBS) : 930799
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4248663
16 A = 6786709
89 meter
Y = -808033
24 meter E =
0016260
Z = -5243821
07 I = 51
94543
XDOT = 2820
009591 Wp = 83
23766
YDOT = 7009
672384 meter/sec RA = 60
88448 deg
ZDOT = 1209
774422 TA = 198
31576
MA = 198
37439
Ha = 227
043 n
mi
Hp = 218
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13939183
59 X = 4282856
26
Y = -2651027
69 feet Y = -760330
92 meter
Z = -17204137
37 Z = -5223098
22
XDOT = 9251
999970 XDOT = 2735
539411
YDOT = 22997
612807 feet/sec YDOT = 7040
735299 meter/sec
ZDOT = 3969
076189 ZDOT = 1223
268473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1563577
93 X = -476578
55
Y = -14209944
75 feet Y = -4331191
16 meter
Z = -17115601
77 Z = -5216835
42
XDOT = 22603
662146 XDOT = 6889
596222
YDOT = -7315
430869 feet/sec YDOT = -2229
743329 meter/sec
ZDOT = 4025
321244 ZDOT = 1226
917915
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 14321
09834306
00016717 00000-0 10270-3 0 9124
2 25544 51
6456 61
5206 0004727 28
7394 331
4016 15
51091472 35058
Satellite: ISS
Catalog Number: 25544
Epoch time: 14321
09834306 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 61
5206 deg
Eccentricity:
0004727
Arg of perigee: 28
7394 deg
Mean anomaly: 331
4016 deg
Mean motion: 15
51091472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3505
Checksum: 286
Coasting Arc #14 (Orbit 3520)
---------------------------------------
Vector Time (GMT): 2014/322/02:01:26
082
Vector Time (MET): N/A
Weight (LBS) : 930799
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4527245
97 A = 6787369
41 meter
Y = 352112
68 meter E =
0010430
Z = 5040557
70 I = 51
93241
XDOT = -2761
947931 Wp = 44
66775
YDOT = -6869
247742 meter/sec RA = 55
93724 deg
ZDOT = -1991
101709 TA = 64
64742
MA = 64
53944
Ha = 227
107 n
mi
Hp = 218
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14853169
20 X = -4555332
82
Y = 1155225
34 feet Y = 301329
20 meter
Z = 16537262
81 Z = 5018496
29
XDOT = -9061
508961 XDOT = -2675
256795
YDOT = -22536
902041 feet/sec YDOT = -6899
648978 meter/sec
ZDOT = -6532
485921 ZDOT = -2004
308356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 260189
31 X = 79305
70
Y = 14999627
93 feet Y = 4571886
59 meter
Z = 16443105
11 Z = 5011858
44
XDOT = -21942
768170 XDOT = -6688
155738
YDOT = 7637
256858 feet/sec YDOT = 2327
835890 meter/sec
ZDOT = -6587
517857 ZDOT = -2007
875443
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 14322
12918944
00016717 00000-0 10270-3 0 9131
2 25544 51
6458 56
4050 0004774 30
7290 329
4140 15
51151042 35213
Satellite: ISS
Catalog Number: 25544
Epoch time: 14322
12918944 = yrday
fracday
Element set: 913
Inclination: 51
6458 deg
RA of node: 56
4050 deg
Eccentricity:
0004774
Arg of perigee: 30
7290 deg
Mean anomaly: 329
4140 deg
Mean motion: 15
51151042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3521
Checksum: 278
Coasting Arc #15 (Orbit 3535)
---------------------------------------
Vector Time (GMT): 2014/323/02:01:26
082
Vector Time (MET): N/A
Weight (LBS) : 930799
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4837711
04 A = 6788531
26 meter
Y = 29692
71 meter E =
0013079
Z = -4773399
90 I = 51
91817
XDOT = 2639
423692 Wp = 87
90119
YDOT = 6648
303958 meter/sec RA = 50
98988 deg
ZDOT = 2723
243356 TA = 208
93572
MA = 209
00830
Ha = 227
085 n
mi
Hp = 218
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15871755
38 X = 4860207
64
Y = 97417
03 feet Y = 83916
81 meter
Z = -15660760
82 Z = -4749843
79
XDOT = 8659
526550 XDOT = 2551
655689
YDOT = 21812
020860 feet/sec YDOT = 6677
329025 meter/sec
ZDOT = 8934
525446 ZDOT = 2735
852272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 776592
16 X = 236705
29
Y = -15951658
40 feet Y = -4862065
48 meter
Z = -15560303
25 Z = -4742780
43
XDOT = 20996
454477 XDOT = 6399
719325
YDOT = -7722
118647 feet/sec YDOT = -2353
701764 meter/sec
ZDOT = 8987
035485 ZDOT = 2739
248416
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 14323
09559228
00016717 00000-0 10270-3 0 9145
2 25544 51
6460 51
6090 0004812 34
1723 325
9737 15
51145625 35368
Satellite: ISS
Catalog Number: 25544
Epoch time: 14323
09559228 = yrday
fracday
Element set: 914
Inclination: 51
6460 deg
RA of node: 51
6090 deg
Eccentricity:
0004812
Arg of perigee: 34
1723 deg
Mean anomaly: 325
9737 deg
Mean motion: 15
51145625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3536
Checksum: 297
Coasting Arc #16 (Orbit 3551)
---------------------------------------
Vector Time (GMT): 2014/324/02:01:26
082
Vector Time (MET): N/A
Weight (LBS) : 930799
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5165276
98 A = 6789833
55 meter
Y = -407245
17 meter E =
0013920
Z = 4382033
14 I = 51
90305
XDOT = -2427
809437 Wp = 59
52316
YDOT = -6405
618039 meter/sec RA = 46
04257 deg
ZDOT = -3442
054176 TA = 65
33553
MA = 65
19064
Ha = 227
129 n
mi
Hp = 218
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16946446
80 X = -5181626
22
Y = -1336106
19 feet Y = -465098
03 meter
Z = 14376749
14 Z = 4356900
60
XDOT = -7965
254060 XDOT = -2339
279065
YDOT = -21015
807213 feet/sec YDOT = -6432
272393 meter/sec
ZDOT = -11292
828662 ZDOT = -3453
633361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1767609
85 X = -538767
48
Y = 16997381
21 feet Y = 5180801
79 meter
Z = 14269644
08 Z = 4349387
52
XDOT = -19971
288874 XDOT = -6087
248849
YDOT = 7485
754673 feet/sec YDOT = 2281
658024 meter/sec
ZDOT = -11340
978962 ZDOT = -3456
730387
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 14324
12640143
00016717 00000-0 10270-3 0 9158
2 25544 51
6464 46
4934 0004916 36
5719 323
5767 15
51207816 35523
Satellite: ISS
Catalog Number: 25544
Epoch time: 14324
12640143 = yrday
fracday
Element set: 915
Inclination: 51
6464 deg
RA of node: 46
4934 deg
Eccentricity:
0004916
Arg of perigee: 36
5719 deg
Mean anomaly: 323
5767 deg
Mean motion: 15
51207816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3552
Checksum: 305
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