[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 7th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
016/01:58:23
453 -1
1 2
9 2
9
N/A 2
6 -0
2 228
7
000/00:06:46
906 -0
9 -0
1 221
0
Coasting Arc #1 (Orbit 2625)
---------------------------------------
Vector Time (GMT): 2014/006/14:50:14
676
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4498778
14 A = 6794100
69 meter
Y = 3195871
59 meter E =
0006930
Z = -3966135
43 I = 51
64341
XDOT = -5735
682665 Wp = 63
03536
YDOT = -3103
717722 meter/sec RA = 179
27423 deg
ZDOT = 4013
510271 TA = 248
86968
MA = 248
94377
Ha = 227
880 n
mi
Hp = 220
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14759770
80 X = -4514914
63
Y = 10485143
01 feet Y = 3145473
24 meter
Z = -13012255
35 Z = -3988028
85
XDOT = -18817
856512 XDOT = -5720
046137
YDOT = -10182
800926 feet/sec YDOT = -3167
770442 meter/sec
ZDOT = 13167
684616 ZDOT = 3985
685216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18006506
52 X = -5488383
19
Y = 1064545
83 feet Y = 324473
57 meter
Z = -13104972
81 Z = -3994395
71
XDOT = -10504
824935 XDOT = -3201
870640
YDOT = -17365
152958 feet/sec YDOT = -5292
898622 meter/sec
ZDOT = 13050
873870 ZDOT = 3977
906356
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 14006
62692216
00016717 00000-0 10270-3 0 9002
2 25544 51
6471 180
3596 0005254 355
6539 4
4565 15
50179868 26260
Satellite: ISS
Catalog Number: 25544
Epoch time: 14006
62692216 = yrday
fracday
Element set: 900
Inclination: 51
6471 deg
RA of node: 180
3596 deg
Eccentricity:
0005254
Arg of perigee: 355
6539 deg
Mean anomaly: 4
4565 deg
Mean motion: 15
50179868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2626
Checksum: 316
Coasting Arc #2 (Orbit 2641)
---------------------------------------
Vector Time (GMT): 2014/007/14:50:14
676
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4619928
80 A = 6795042
20 meter
Y = -3370702
86 meter E =
0013281
Z = 3665139
87 I = 51
67767
XDOT = 5591
747722 Wp = 62
55509
YDOT = 2905
484126 meter/sec RA = 174
31959 deg
ZDOT = -4358
234563 TA = 73
99072
MA = 73
84448
Ha = 227
965 n
mi
Hp = 220
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15157246
73 X = 4639473
38
Y = -11058736
43 feet Y = -3318930
68 meter
Z = 12024737
10 Z = 3687630
15
XDOT = 18345
629008 XDOT = 5580
013194
YDOT = 9532
428235 feet/sec YDOT = 2967
949113 meter/sec
ZDOT = -14298
669827 ZDOT = -4331
099158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18627799
13 X = 5677753
17
Y = -1656100
48 feet Y = -504779
43 meter
Z = 12120004
67 Z = 3694177
42
XDOT = 10720
039466 XDOT = 3267
468029
YDOT = 16337
734072 feet/sec YDOT = 4979
741345 meter/sec
ZDOT = -14184
725911 ZDOT = -4323
504458
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 14007
65836389
00016717 00000-0 10270-3 0 9018
2 25544 51
6472 175
2481 0005185
4830 359
6324 15
50191503 26425
Satellite: ISS
Catalog Number: 25544
Epoch time: 14007
65836389 = yrday
fracday
Element set: 901
Inclination: 51
6472 deg
RA of node: 175
2481 deg
Eccentricity:
0005185
Arg of perigee:
4830 deg
Mean anomaly: 359
6324 deg
Mean motion: 15
50191503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2642
Checksum: 297
Coasting Arc #3 (Orbit 2656)
---------------------------------------
Vector Time (GMT): 2014/008/14:50:14
676
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4684307
55 A = 6795863
49 meter
Y = 3587084
03 meter E =
0007473
Z = -3371167
66 I = 51
71173
XDOT = -5432
672733 Wp = 43
28048
YDOT = -2724
306220 meter/sec RA = 169
36823 deg
ZDOT = 4661
456510 TA = 277
51682
MA = 277
60171
Ha = 228
052 n
mi
Hp = 220
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15368463
09 X = -4707694
94
Y = 11768648
38 feet Y = 3534570
46 meter
Z = -11060261
35 Z = -3393980
02
XDOT = -17823
729438 XDOT = -5424
448994
YDOT = -8938
012534 feet/sec YDOT = -2785
012010 meter/sec
ZDOT = 15293
492488 ZDOT = 4635
085265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19141281
07 X = -5834262
47
Y = 2480808
86 feet Y = 756150
54 meter
Z = -11156929
23 Z = -3400632
03
XDOT = -10815
805942 XDOT = -3296
657651
YDOT = -15338
033294 feet/sec YDOT = -4675
032548 meter/sec
ZDOT = 15182
732799 ZDOT = 4627
696957
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 14008
62532787
00016717 00000-0 10270-3 0 9022
2 25544 51
6477 170
4568 0005423 2
6076 357
5102 15
50209171 26572
Satellite: ISS
Catalog Number: 25544
Epoch time: 14008
62532787 = yrday
fracday
Element set: 902
Inclination: 51
6477 deg
RA of node: 170
4568 deg
Eccentricity:
0005423
Arg of perigee: 2
6076 deg
Mean anomaly: 357
5102 deg
Mean motion: 15
50209171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2657
Checksum: 298
Coasting Arc #4 (Orbit 2672)
---------------------------------------
Vector Time (GMT): 2014/009/14:50:14
676
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4759693
95 A = 6796771
51 meter
Y = -3795474
37 meter E =
0014235
Z = 3015377
77 I = 51
74505
XDOT = 5229
779837 Wp = 74
72503
YDOT = 2600
547801 meter/sec RA = 164
41913 deg
ZDOT = -4958
541188 TA = 70
85652
MA = 70
70247
Ha = 228
132 n
mi
Hp = 220
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15615793
81 X = 4787134
31
Y = -12452343
74 feet Y = -3742095
15 meter
Z = 9892971
70 Z = 3038566
16
XDOT = 17158
070333 XDOT = 5224
398229
YDOT = 8531
980973 feet/sec YDOT = 2659
000674 meter/sec
ZDOT = -16268
179750 ZDOT = -4933
148617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19651591
68 X = 5989805
14
Y = -3282418
40 feet Y = -1000481
13 meter
Z = 9991268
38 Z = 3045338
60
XDOT = 10665
907572 XDOT = 3250
968628
YDOT = 14432
931233 feet/sec YDOT = 4399
157440 meter/sec
ZDOT = -16161
517081 ZDOT = -4926
030406
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 14009
65674550
00016717 00000-0 10270-3 0 9032
2 25544 51
6476 165
3455 0005331 7
9464 352
1770 15
50231509 26736
Satellite: ISS
Catalog Number: 25544
Epoch time: 14009
65674550 = yrday
fracday
Element set: 903
Inclination: 51
6476 deg
RA of node: 165
3455 deg
Eccentricity:
0005331
Arg of perigee: 7
9464 deg
Mean anomaly: 352
1770 deg
Mean motion: 15
50231509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2673
Checksum: 302
Coasting Arc #5 (Orbit 2687)
---------------------------------------
Vector Time (GMT): 2014/010/14:50:14
676
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4768786
44 A = 6797567
17 meter
Y = 4034119
17 meter E =
0009631
Z = -2673802
12 I = 51
77775
XDOT = -5027
889249 Wp = 31
63423
YDOT = -2500
169114 meter/sec RA = 159
47246 deg
ZDOT = 5211
705211 TA = 298
30524
MA = 298
40237
Ha = 228
222 n
mi
Hp = 220
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15645624
80 X = -4800553
98
Y = 13235299
13 feet Y = 3980614
10 meter
Z = -8772316
67 Z = -2697045
11
XDOT = -16495
699637 XDOT = -5024
874871
YDOT = -8202
654572 feet/sec YDOT = -2556
377630 meter/sec
ZDOT = 17098
770376 ZDOT = 5187
287639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19994827
58 X = -6094423
45
Y = 4292595
37 feet Y = 1308383
07 meter
Z = -8870893
60 Z = -2703848
37
XDOT = -10440
149647 XDOT = -3182
157612
YDOT = -13617
044477 feet/sec YDOT = -4150
475157 meter/sec
ZDOT = 16996
192798 ZDOT = 5180
439565
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 14010
62368673
00016717 00000-0 10270-3 0 9048
2 25544 51
6480 160
5537 0005595 9
6473 350
4784 15
50239742 26889
Satellite: ISS
Catalog Number: 25544
Epoch time: 14010
62368673 = yrday
fracday
Element set: 904
Inclination: 51
6480 deg
RA of node: 160
5537 deg
Eccentricity:
0005595
Arg of perigee: 9
6473 deg
Mean anomaly: 350
4784 deg
Mean motion: 15
50239742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2688
Checksum: 321
Coasting Arc #6 (Orbit 2703)
---------------------------------------
Vector Time (GMT): 2014/011/14:50:14
676
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4786065
09 A = 6798337
98 meter
Y = -4256410
72 meter E =
0014645
Z = 2268272
50 I = 51
80887
XDOT = 4789
351485 Wp = 85
96379
YDOT = 2465
495579 meter/sec RA = 154
52856 deg
ZDOT = -5447
713716 TA = 68
90183
MA = 68
74532
Ha = 228
295 n
mi
Hp = 219
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15702313
28 X = 4822287
01
Y = -13964602
10 feet Y = -4202687
52 meter
Z = 7441838
92 Z = 2291610
14
XDOT = 15713
095424 XDOT = 4787
888958
YDOT = 8088
896256 feet/sec YDOT = 2519
045360 meter/sec
ZDOT = -17873
076496 ZDOT = -5424
451182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20309515
92 X = 6190340
45
Y = -5254774
50 feet Y = -1601655
27 meter
Z = 7540863
93 Z = 2298455
33
XDOT = 9988
192029 XDOT = 3044
400930
YDOT = 12949
871445 feet/sec YDOT = 3947
120816 meter/sec
ZDOT = -17775
352934 ZDOT = -5417
927574
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 14011
65507985
00016717 00000-0 10270-3 0 9054
2 25544 51
6477 155
4424 0005502 15
3034 344
8282 15
50271632 27041
Satellite: ISS
Catalog Number: 25544
Epoch time: 14011
65507985 = yrday
fracday
Element set: 905
Inclination: 51
6477 deg
RA of node: 155
4424 deg
Eccentricity:
0005502
Arg of perigee: 15
3034 deg
Mean anomaly: 344
8282 deg
Mean motion: 15
50271632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2704
Checksum: 289
Coasting Arc #7 (Orbit 2718)
---------------------------------------
Vector Time (GMT): 2014/012/14:50:14
676
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4731983
93 A = 6799013
00 meter
Y = 4495306
17 meter E =
0012517
Z = -1884954
35 I = 51
83932
XDOT = -4569
527508 Wp = 29
57413
YDOT = -2456
454457 meter/sec RA = 149
58648 deg
ZDOT = 5639
641706 TA = 309
76238
MA = 309
87258
Ha = 228
388 n
mi
Hp = 219
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15524881
68 X = -4772743
32
Y = 14748379
82 feet Y = 4442162
35 meter
Z = -6184233
43 Z = -1908040
18
XDOT = -14991
888150 XDOT = -4569
114658
YDOT = -8059
233783 feet/sec YDOT = -2507
551942 meter/sec
ZDOT = 18502
761504 ZDOT = 5617
444545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20410587
43 X = -6221147
05
Y = 6381431
92 feet Y = 1945060
45 meter
Z = -6282248
71 Z = -1914829
41
XDOT = -9522
522871 XDOT = -2902
464971
YDOT = -12418
194154 feet/sec YDOT = -3785
065578 meter/sec
ZDOT = 18409
518298 ZDOT = 5611
221177
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 14012
62199803
00016717 00000-0 10270-3 0 9069
2 25544 51
6483 150
6504 0005765 16
7328 343
4012 15
50271509 27191
Satellite: ISS
Catalog Number: 25544
Epoch time: 14012
62199803 = yrday
fracday
Element set: 906
Inclination: 51
6483 deg
RA of node: 150
6504 deg
Eccentricity:
0005765
Arg of perigee: 16
7328 deg
Mean anomaly: 343
4012 deg
Mean motion: 15
50271509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2719
Checksum: 294
Coasting Arc #8 (Orbit 2734)
---------------------------------------
Vector Time (GMT): 2014/013/14:50:14
676
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4685707
53 A = 6799533
56 meter
Y = -4707748
23 meter E =
0014363
Z = 1437495
56 I = 51
86713
XDOT = 4323
366783 Wp = 95
75511
YDOT = 2516
878134 meter/sec RA = 144
64725 deg
ZDOT = -5801
478160 TA = 68
64529
MA = 68
49206
Ha = 228
443 n
mi
Hp = 219
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15373056
22 X = 4731019
55
Y = -15445368
20 feet Y = -4655096
41 meter
Z = 4716192
78 Z = 1460367
55
XDOT = 14184
274222 XDOT = 4323
082608
YDOT = 8257
474192 feet/sec YDOT = 2565
223627 meter/sec
ZDOT = -19033
720999 ZDOT = -5780
476558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20466179
14 X = 6238091
40
Y = -7422928
17 feet Y = -2262508
51 meter
Z = 4813354
24 Z = 1467110
37
XDOT = 8872
344216 XDOT = 2704
290517
YDOT = 12076
403576 feet/sec YDOT = 3680
887810 meter/sec
ZDOT = -18945
518432 ZDOT = -5774
594018
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 14013
65336648
00016717 00000-0 10270-3 0 9074
2 25544 51
6478 145
5390 0005701 22
3032 337
8365 15
50313845 27352
Satellite: ISS
Catalog Number: 25544
Epoch time: 14013
65336648 = yrday
fracday
Element set: 907
Inclination: 51
6478 deg
RA of node: 145
5390 deg
Eccentricity:
0005701
Arg of perigee: 22
3032 deg
Mean anomaly: 337
8365 deg
Mean motion: 15
50313845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2735
Checksum: 300
Coasting Arc #9 (Orbit 2749)
---------------------------------------
Vector Time (GMT): 2014/014/14:50:14
676
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4568162
87 A = 6800003
42 meter
Y = 4922205
54 meter E =
0015410
Z = -1020651
62 I = 51
89403
XDOT = -4113
341682 Wp = 33
25960
YDOT = -2601
009899 meter/sec RA = 139
70941 deg
ZDOT = 5921
361435 TA = 315
73152
MA = 315
85468
Ha = 228
550 n
mi
Hp = 219
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14987411
00 X = -4617906
62
Y = 16148968
29 feet Y = 4870843
36 meter
Z = -3348594
57 Z = -1042963
31
XDOT = -13495
215491 XDOT = -4112
714592
YDOT = -8533
497045 feet/sec YDOT = -2647
004818 meter/sec
ZDOT = 19427
038828 ZDOT = 5901
381000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20280920
85 X = -6181624
67
Y = 8570397
91 feet Y = 2612257
28 meter
Z = -3443440
21 Z = -1049560
57
XDOT = -8281
333705 XDOT = -2524
150513
YDOT = -11895
388694 feet/sec YDOT = -3625
714474 meter/sec
ZDOT = 19343
146326 ZDOT = 5895
791000
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 14014
62026156
00016717 00000-0 10270-3 0 9083
2 25544 51
6486 140
7469 0005941 23
8224 336
3201 15
50303990 27500
Satellite: ISS
Catalog Number: 25544
Epoch time: 14014
62026156 = yrday
fracday
Element set: 908
Inclination: 51
6486 deg
RA of node: 140
7469 deg
Eccentricity:
0005941
Arg of perigee: 23
8224 deg
Mean anomaly: 336
3201 deg
Mean motion: 15
50303990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2750
Checksum: 287
Coasting Arc #10 (Orbit 2765)
---------------------------------------
Vector Time (GMT): 2014/015/14:50:14
676
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4461334
20 A = 6800170
02 meter
Y = -5099495
23 meter E =
0013339
Z = 541831
36 I = 51
91764
XDOT = 3889
162547 Wp = 103
22443
YDOT = 2752
383919 meter/sec RA = 134
77402 deg
ZDOT = -5997
189980 TA = 70
96313
MA = 70
81869
Ha = 228
577 n
mi
Hp = 219
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14636923
22 X = 4515394
31
Y = -16730627
39 feet Y = -5049303
51 meter
Z = 1777661
95 Z = 563634
56
XDOT = 12759
719644 XDOT = 3887
227687
YDOT = 9030
130967 feet/sec YDOT = 2795
864554 meter/sec
ZDOT = -19675
820144 ZDOT = -5978
301809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20047527
09 X = 6110486
26
Y = -9587061
36 feet Y = -2922136
30 meter
Z = 1870403
21 Z = 570098
90
XDOT = 7565
484876 XDOT = 2305
959790
YDOT = 11923
308590 feet/sec YDOT = 3634
224458 meter/sec
ZDOT = -19596
549317 ZDOT = -5973
028232
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 14015
65160523
00016717 00000-0 10270-3 0 9095
2 25544 51
6481 135
6354 0005925 28
9841 331
1638 15
50358837 27668
Satellite: ISS
Catalog Number: 25544
Epoch time: 14015
65160523 = yrday
fracday
Element set: 909
Inclination: 51
6481 deg
RA of node: 135
6354 deg
Eccentricity:
0005925
Arg of perigee: 28
9841 deg
Mean anomaly: 331
1638 deg
Mean motion: 15
50358837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2766
Checksum: 317
Coasting Arc #11 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2014/016/02:01:46
906
Vector Time (MET): N/A
Weight (LBS) : 900891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3946766
36 A = 6790380
13 meter
Y = 1781400
00 meter E =
0016364
Z = -5244631
88 I = 51
89079
XDOT = -4372
962371 Wp = 65
71346
YDOT = 6161
531369 meter/sec RA = 132
48644 deg
ZDOT = -1194
361763 TA = 192
82012
MA = 192
86178
Ha = 228
696 n
mi
Hp = 220
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12948708
55 X = 3952029
33
Y = 5844488
20 feet Y = 1825564
97 meter
Z = -17206797
50 Z = -5225446
49
XDOT = -14346
989407 XDOT = -4435
735254
YDOT = 20214
997929 feet/sec YDOT = 6112
279193 meter/sec
ZDOT = -3918
509721 ZDOT = -1215
756785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7356440
96 X = -2242243
21
Y = -12267013
83 feet Y = -3738985
82 meter
Z = -17126124
01 Z = -5220042
60
XDOT = 22423
283209 XDOT = 6834
616722
YDOT = -7832
499456 feet/sec YDOT = -2387
345834 meter/sec
ZDOT = -4009
693950 ZDOT = -1222
154716
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 14016
10281732
00016717 00000-0 10270-3 0 9104
2 25544 51
6490 133
3996 0004631 12
5827 347
5439 15
49836407 27731
Satellite: ISS
Catalog Number: 25544
Epoch time: 14016
10281732 = yrday
fracday
Element set: 910
Inclination: 51
6490 deg
RA of node: 133
3996 deg
Eccentricity:
0004631
Arg of perigee: 12
5827 deg
Mean anomaly: 347
5439 deg
Mean motion: 15
49836407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 309
Coasting Arc #12 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2014/017/02:01:46
906
Vector Time (MET): N/A
Weight (LBS) : 900891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3885945
63 A = 6790072
44 meter
Y = -1741665
54 meter E =
0004933
Z = 5284861
56 I = 51
91028
XDOT = 4075
539308 Wp = 57
02144
YDOT = -6432
225405 meter/sec RA = 127
54983 deg
ZDOT = 878
967707 TA = 24
61277
MA = 24
58923
Ha = 228
817 n
mi
Hp = 220
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12749165
44 X = -3891852
81
Y = -5714125
79 feet Y = -1785153
89 meter
Z = 17338784
65 Z = 5265970
12
XDOT = 13371
191954 XDOT = 4142
893319
YDOT = -21103
101722 feet/sec YDOT = -6386
273557 meter/sec
ZDOT = 2883
752318 ZDOT = 898
929102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7474346
42 X = 2278180
79
Y = 11919534
57 feet Y = 3633074
14 meter
Z = 17259337
98 Z = 5260646
22
XDOT = -21993
235547 XDOT = -6703
538195
YDOT = 9501
890315 feet/sec YDOT = 2896
176168 meter/sec
ZDOT = 2968
940714 ZDOT = 904
933130
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 14017
13450777
00016717 00000-0 10270-3 0 9116
2 25544 51
6491 128
2901 0004609 15
1131 345
0157 15
49858692 27890
Satellite: ISS
Catalog Number: 25544
Epoch time: 14017
13450777 = yrday
fracday
Element set: 911
Inclination: 51
6491 deg
RA of node: 128
2901 deg
Eccentricity:
0004609
Arg of perigee: 15
1131 deg
Mean anomaly: 345
0157 deg
Mean motion: 15
49858692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 310
Coasting Arc #13 (Orbit 2803)
---------------------------------------
Vector Time (GMT): 2014/018/02:01:46
906
Vector Time (MET): N/A
Weight (LBS) : 900891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3858208
57 A = 6789884
24 meter
Y = 1717844
37 meter E =
0017090
Z = -5330942
57 I = 51
92843
XDOT = -3737
173142 Wp = 70
92199
YDOT = 6650
797188 meter/sec RA = 122
61439 deg
ZDOT = -557
613191 TA = 193
74154
MA = 193
78812
Ha = 228
786 n
mi
Hp = 220
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12658164
61 X = 3864608
04
Y = 5635972
34 feet Y = 1761025
20 meter
Z = -17489969
07 Z = -5312184
71
XDOT = -12261
066740 XDOT = -3808
557430
YDOT = 21820
200747 feet/sec YDOT = 6608
606610 meter/sec
ZDOT = -1829
439603 ZDOT = -575
940778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7645255
10 X = -2330273
75
Y = -11674623
21 feet Y = -3558425
15 meter
Z = -17411076
39 Z = -5306896
08
XDOT = 21299
325648 XDOT = 6492
034457
YDOT = -11083
407257 feet/sec YDOT = -3378
222532 meter/sec
ZDOT = -1907
777690 ZDOT = -581
490640
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 14018
10170725
00016717 00000-0 10270-3 0 9127
2 25544 51
6497 123
5001 0004746 18
5707 341
5616 15
49874733 28046
Satellite: ISS
Catalog Number: 25544
Epoch time: 14018
10170725 = yrday
fracday
Element set: 912
Inclination: 51
6497 deg
RA of node: 123
5001 deg
Eccentricity:
0004746
Arg of perigee: 18
5707 deg
Mean anomaly: 341
5616 deg
Mean motion: 15
49874733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2804
Checksum: 297
Coasting Arc #14 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2014/019/02:01:46
906
Vector Time (MET): N/A
Weight (LBS) : 900891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3817015
30 A = 6789713
76 meter
Y = -1723526
86 meter E =
0005727
Z = 5340428
93 I = 51
94397
XDOT = 3404
603931 Wp = 46
95304
YDOT = -6864
171757 meter/sec RA = 117
67963 deg
ZDOT = 221
773510 TA = 40
96275
MA = 40
91974
Ha = 228
915 n
mi
Hp = 220
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12523016
08 X = -3823400
39
Y = -5654615
69 feet Y = -1766246
88 meter
Z = 17521092
29 Z = 5321871
22
XDOT = 11169
960402 XDOT = 3480
030308
YDOT = -22520
248547 feet/sec YDOT = -6825
677569 meter/sec
ZDOT = 727
603379 ZDOT = 238
495498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7720603
34 X = 2353239
90
Y = 11485726
25 feet Y = 3500849
36 meter
Z = 17443040
49 Z = 5316638
74
XDOT = -20560
772289 XDOT = -6266
923394
YDOT = 12625
332290 feet/sec YDOT = 3848
201282 meter/sec
ZDOT = 799
208127 ZDOT = 243
598637
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 14019
13337351
00016717 00000-0 10270-3 0 9132
2 25544 51
6496 118
3904 0004737 21
5352 338
5997 15
49895506 28206
Satellite: ISS
Catalog Number: 25544
Epoch time: 14019
13337351 = yrday
fracday
Element set: 913
Inclination: 51
6496 deg
RA of node: 118
3904 deg
Eccentricity:
0004737
Arg of perigee: 21
5352 deg
Mean anomaly: 338
5997 deg
Mean motion: 15
49895506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 322
Coasting Arc #15 (Orbit 2834)
---------------------------------------
Vector Time (GMT): 2014/020/02:01:46
906
Vector Time (MET): N/A
Weight (LBS) : 900891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3816404
25 A = 6789668
01 meter
Y = 1735027
94 meter E =
0017350
Z = -5355275
80 I = 51
95726
XDOT = -3038
510337 Wp = 76
07972
YDOT = 7018
915517 meter/sec RA = 112
74550 deg
ZDOT = 113
007183 TA = 194
96944
MA = 195
02086
Ha = 228
863 n
mi
Hp = 220
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12521011
33 X = 3822732
95
Y = 5692348
88 feet Y = 1777740
73 meter
Z = -17569802
50 Z = -5336721
18
XDOT = -9968
865934 XDOT = -3117
320532
YDOT = 23027
938048 feet/sec YDOT = 6984
496302 meter/sec
ZDOT = 370
758474 ZDOT = 98
055254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7896144
42 X = -2406744
82
Y = -11382691
73 feet Y = -3469444
44 meter
Z = -17491762
42 Z = -5331489
19
XDOT = 19576
079714 XDOT = 5966
789097
YDOT = -14028
929405 feet/sec YDOT = -4276
017683 meter/sec
ZDOT = 306
590326 ZDOT = 93
448731
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 14020
10055005
00016717 00000-0 10270-3 0 9145
2 25544 51
6494 113
5999 0004839 24
3286 335
8092 15
49910883 28353
Satellite: ISS
Catalog Number: 25544
Epoch time: 14020
10055005 = yrday
fracday
Element set: 914
Inclination: 51
6494 deg
RA of node: 113
5999 deg
Eccentricity:
0004839
Arg of perigee: 24
3286 deg
Mean anomaly: 335
8092 deg
Mean motion: 15
49910883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2835
Checksum: 312
Coasting Arc #16 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2014/021/02:01:46
906
Vector Time (MET): N/A
Weight (LBS) : 900891
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3807542
61 A = 6789659
31 meter
Y = -1777004
91 meter E =
0007050
Z = 5329541
60 I = 51
96856
XDOT = 2684
568818 Wp = 42
78243
YDOT = -7164
823719 meter/sec RA = 107
81205 deg
ZDOT = -465
622770 TA = 51
67215
MA = 51
60879
Ha = 228
995 n
mi
Hp = 220
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12491937
69 X = -3813277
63
Y = -5830068
60 feet Y = -1819615
25 meter
Z = 17485372
70 Z = 5311031
43
XDOT = 8807
640480 XDOT = 2766
749771
YDOT = -23506
639499 feet/sec YDOT = -7134
343665 meter/sec
ZDOT = -1527
633761 ZDOT = -452
381933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7996257
56 X = 2437259
30
Y = 11349643
43 feet Y = 3459371
32 meter
Z = 17407524
94 Z = 5305813
60
XDOT = -18564
456743 XDOT = -5658
446415
YDOT = 15362
262904 feet/sec YDOT = 4682
417733 meter/sec
ZDOT = -1470
654198 ZDOT = -448
255399
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 14021
13219219
00016717 00000-0 10270-3 0 9159
2 25544 51
6494 108
4900 0004838 27
6888 332
4520 15
49930752 28515
Satellite: ISS
Catalog Number: 25544
Epoch time: 14021
13219219 = yrday
fracday
Element set: 915
Inclination: 51
6494 deg
RA of node: 108
4900 deg
Eccentricity:
0004838
Arg of perigee: 27
6888 deg
Mean anomaly: 332
4520 deg
Mean motion: 15
49930752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2851
Checksum: 308
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