[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 4th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
224/13:30:14
000 0
0 0
0 0
0
N/A 0
0 0
0 227
9
000/00:00:00
000 0
0 0
0 219
7
226/17:17:51
104 -2
5 3
7 3
7
N/A 1
8 0
2 228
1
000/00:07:42
209 -2
0 -0
3 221
6
Coasting Arc #1 (Orbit 1835)
---------------------------------------
Vector Time (GMT): 2014/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3552994
04 A = 6799743
38 meter
Y = 5760072
24 meter E =
0003983
Z = -639453
64 I = 51
36978
XDOT = -4380
828952 Wp = 140
53427
YDOT = 2045
476161 meter/sec RA = 234
00196 deg
ZDOT = -5939
406320 TA = 46
38175
MA = 46
34872
Ha = 226
596 n
mi
Hp = 221
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11656804
59 X = 3491425
75
Y = 18897874
80 feet Y = 5799459
86 meter
Z = -2097945
00 Z = -622343
44
XDOT = -14372
798400 XDOT = -4374
524912
YDOT = 6710
879794 feet/sec YDOT = 1996
522130 meter/sec
ZDOT = -19486
241207 ZDOT = -5960
672248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7272343
02 X = 2216610
15
Y = -20986174
50 feet Y = -6396585
99 meter
Z = -2026239
14 Z = -617597
69
XDOT = 12674
221995 XDOT = 3863
102864
YDOT = 6274
469344 feet/sec YDOT = 1912
458256 meter/sec
ZDOT = -19576
832740 ZDOT = -5967
018619
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 14213
53105397
00016717 00000-0 10270-3 0 9001
2 25544 51
6452 234
8344 0006742 318
6996 41
3644 15
50495980 18360
Satellite: ISS
Catalog Number: 25544
Epoch time: 14213
53105397 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 234
8344 deg
Eccentricity:
0006742
Arg of perigee: 318
6996 deg
Mean anomaly: 41
3644 deg
Mean motion: 15
50495980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1836
Checksum: 315
Coasting Arc #2 (Orbit 1851)
---------------------------------------
Vector Time (GMT): 2014/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3662975
48 A = 6799349
64 meter
Y = -5602797
99 meter E =
0014765
Z = 1136799
61 I = 51
38759
XDOT = 4607
881529 Wp = 29
90505
YDOT = -1821
143725 meter/sec RA = 229
02925 deg
ZDOT = 5851
456476 TA = 342
46771
MA = 342
51862
Ha = 226
739 n
mi
Hp = 221
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12017636
10 X = -3605573
64
Y = -18381883
18 feet Y = -5643438
80 meter
Z = 3729657
51 Z = 1119144
95
XDOT = 15117
721553 XDOT = 4599
479224
YDOT = -5974
880986 feet/sec YDOT = -1769
662403 meter/sec
ZDOT = 19197
691849 ZDOT = 5873
820340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6276514
93 X = -1913081
75
Y = 21058714
86 feet Y = 6418696
29 meter
Z = 3655603
97 Z = 1114228
09
XDOT = -12703
296724 XDOT = -3871
964842
YDOT = -7147
092022 feet/sec YDOT = -2178
433648 meter/sec
ZDOT = 19292
911834 ZDOT = 5880
479527
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 14214
56229490
00016717 00000-0 10270-3 0 9017
2 25544 51
6452 229
7218 0006850 322
9762 37
0915 15
50509901 18522
Satellite: ISS
Catalog Number: 25544
Epoch time: 14214
56229490 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 229
7218 deg
Eccentricity:
0006850
Arg of perigee: 322
9762 deg
Mean anomaly: 37
0915 deg
Mean motion: 15
50509901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1852
Checksum: 303
Coasting Arc #3 (Orbit 1866)
---------------------------------------
Vector Time (GMT): 2014/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3734088
76 A = 6798753
78 meter
Y = 5438422
77 meter E =
0001229
Z = -1643541
59 I = 51
40616
XDOT = -4860
055134 Wp = 117
96056
YDOT = 1618
126761 meter/sec RA = 224
05695 deg
ZDOT = -5691
441434 TA = 80
05662
MA = 80
04275
Ha = 226
887 n
mi
Hp = 221
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12250947
36 X = 3680981
29
Y = 17842594
40 feet Y = 5479882
84 meter
Z = -5392196
80 Z = -1625530
95
XDOT = -15945
062776 XDOT = -4850
141150
YDOT = 5308
814833 feet/sec YDOT = 1563
833982 meter/sec
ZDOT = -18672
708118 ZDOT = -5715
026669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5346792
39 X = 1629702
32
Y = -20992029
45 feet Y = -6398370
58 meter
Z = -5316595
09 Z = -1620498
18
XDOT = 12882
161124 XDOT = 3926
482710
YDOT = 8032
540184 feet/sec YDOT = 2448
318248 meter/sec
ZDOT = -18773
086795 ZDOT = -5722
036855
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 14215
52907645
00016717 00000-0 10270-3 0 9020
2 25544 51
6446 224
9281 0006809 326
5114 33
5606 15
50510646 18679
Satellite: ISS
Catalog Number: 25544
Epoch time: 14215
52907645 = yrday
fracday
Element set: 902
Inclination: 51
6446 deg
RA of node: 224
9281 deg
Eccentricity:
0006809
Arg of perigee: 326
5114 deg
Mean anomaly: 33
5606 deg
Mean motion: 15
50510646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1867
Checksum: 303
Coasting Arc #4 (Orbit 1882)
---------------------------------------
Vector Time (GMT): 2014/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3762631
13 A = 6797905
84 meter
Y = -5236803
18 meter E =
0014415
Z = 2122155
52 I = 51
42638
XDOT = 5144
703639 Wp = 41
79201
YDOT = -1465
741457 meter/sec RA = 219
08625 deg
ZDOT = 5493
654468 TA = 341
77680
MA = 341
82841
Ha = 226
988 n
mi
Hp = 221
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12344590
33 X = -3714101
05
Y = -17181112
81 feet Y = -5278608
06 meter
Z = 6962452
49 Z = 2103995
03
XDOT = 16878
948947 XDOT = 5134
025262
YDOT = -4808
863049 feet/sec YDOT = -1408
269903 meter/sec
ZDOT = 18023
800748 ZDOT = 5518
620612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4424909
53 X = -1348712
42
Y = 20713669
58 feet Y = 6313526
49 meter
Z = 6886171
70 Z = 2098905
14
XDOT = -13303
975521 XDOT = -4055
051739
YDOT = -8881
458611 feet/sec YDOT = -2707
068585 meter/sec
ZDOT = 18130
026568 ZDOT = 5526
032098
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 14216
56030157
00016717 00000-0 10270-3 0 9031
2 25544 51
6443 219
8155 0006913 330
0106 30
0648 15
50546130 18839
Satellite: ISS
Catalog Number: 25544
Epoch time: 14216
56030157 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 219
8155 deg
Eccentricity:
0006913
Arg of perigee: 330
0106 deg
Mean anomaly: 30
0648 deg
Mean motion: 15
50546130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1883
Checksum: 274
Coasting Arc #5 (Orbit 1897)
---------------------------------------
Vector Time (GMT): 2014/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3748371
17 A = 6796997
89 meter
Y = 5041790
21 meter E =
0003213
Z = -2599701
89 I = 51
44717
XDOT = -5433
408411 Wp = 18
88656
YDOT = 1346
140606 meter/sec RA = 214
11556 deg
ZDOT = -5222
313319 TA = 190
38349
MA = 190
39013
Ha = 227
166 n
mi
Hp = 221
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12297805
66 X = 3704342
56
Y = 16541306
47 feet Y = 5083460
84 meter
Z = -8529205
68 Z = -2581599
70
XDOT = -17826
143082 XDOT = -5422
689287
YDOT = 4416
471803 feet/sec YDOT = 1285
440866 meter/sec
ZDOT = -17133
573880 ZDOT = -5248
681793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3626191
20 X = 1105263
08
Y = -20322242
15 feet Y = -6194219
41 meter
Z = -8453129
89 Z = -2576513
99
XDOT = 13853
760488 XDOT = 4222
626197
YDOT = 9647
034563 feet/sec YDOT = 2940
416135 meter/sec
ZDOT = -17245
746351 ZDOT = -5256
503488
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 14217
52706949
00016717 00000-0 10270-3 0 9048
2 25544 51
6435 215
0216 0006931 334
3664 25
7143 15
50533368 18988
Satellite: ISS
Catalog Number: 25544
Epoch time: 14217
52706949 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 215
0216 deg
Eccentricity:
0006931
Arg of perigee: 334
3664 deg
Mean anomaly: 25
7143 deg
Mean motion: 15
50533368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1898
Checksum: 310
Coasting Arc #6 (Orbit 1913)
---------------------------------------
Vector Time (GMT): 2014/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3681232
80 A = 6795824
71 meter
Y = -4824550
68 meter E =
0012976
Z = 3039947
92 I = 51
46954
XDOT = 5743
358129 Wp = 52
53245
YDOT = -1280
032805 meter/sec RA = 209
14656 deg
ZDOT = 4916
746588 TA = 342
39464
MA = 342
43957
Ha = 227
235 n
mi
Hp = 220
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12077535
45 X = -3641776
93
Y = -15828578
34 feet Y = -4865496
14 meter
Z = 9973582
40 Z = 3022160
77
XDOT = 18843
038480 XDOT = 5733
361140
YDOT = -4199
582695 feet/sec YDOT = -1215
863014 meter/sec
ZDOT = 16131
058361 ZDOT = 4944
622409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2911341
13 X = -887376
78
Y = 19733752
93 feet Y = 6014847
89 meter
Z = 9898797
34 Z = 3017153
43
XDOT = -14621
537916 XDOT = -4456
644757
YDOT = -10319
361572 feet/sec YDOT = -3145
341407 meter/sec
ZDOT = 16249
635149 ZDOT = 4952
888794
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 14218
55827856
00016717 00000-0 10270-3 0 9054
2 25544 51
6430 209
9088 0007008 337
0056 23
0780 15
50577818 19148
Satellite: ISS
Catalog Number: 25544
Epoch time: 14218
55827856 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 209
9088 deg
Eccentricity:
0007008
Arg of perigee: 337
0056 deg
Mean anomaly: 23
0780 deg
Mean motion: 15
50577818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1914
Checksum: 316
Coasting Arc #7 (Orbit 1928)
---------------------------------------
Vector Time (GMT): 2014/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3573882
20 A = 6794717
09 meter
Y = 4629328
70 meter E =
0007349
Z = -3468323
36 I = 51
49282
XDOT = -6032
520601 Wp = 22
26954
YDOT = 1252
288775 meter/sec RA = 204
17721 deg
ZDOT = -4541
149053 TA = 198
41132
MA = 198
43793
Ha = 227
425 n
mi
Hp = 220
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11725335
30 X = 3538698
14
Y = 15188086
27 feet Y = 4669097
61 meter
Z = -11379013
63 Z = -3451047
39
XDOT = -19791
734256 XDOT = -6024
016488
YDOT = 4108
558973 feet/sec YDOT = 1184
877029 meter/sec
ZDOT = -14898
782983 ZDOT = -4570
433074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2362535
00 X = 720100
67
Y = -19084762
88 feet Y = -5817035
73 meter
Z = -11306354
76 Z = -3446176
93
XDOT = 15461
001966 XDOT = 4712
513399
YDOT = 10821
021176 feet/sec YDOT = 3298
247254 meter/sec
ZDOT = -15023
352010 ZDOT = -4579
117693
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 14219
52503196
00016717 00000-0 10270-3 0 9061
2 25544 51
6425 205
1144 0007066 342
0697 18
0204 15
50560016 19297
Satellite: ISS
Catalog Number: 25544
Epoch time: 14219
52503196 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 205
1144 deg
Eccentricity:
0007066
Arg of perigee: 342
0697 deg
Mean anomaly: 18
0204 deg
Mean motion: 15
50560016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1929
Checksum: 282
Coasting Arc #8 (Orbit 1944)
---------------------------------------
Vector Time (GMT): 2014/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3408009
02 A = 6793388
09 meter
Y = -4428765
67 meter E =
0010723
Z = 3850421
76 I = 51
51754
XDOT = 6330
964031 Wp = 60
70557
YDOT = -1274
335356 meter/sec RA = 199
20982 deg
ZDOT = 4134
229317 TA = 345
74737
MA = 345
77760
Ha = 227
475 n
mi
Hp = 220
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11181131
95 X = -3376936
03
Y = -14530071
10 feet Y = -4466702
66 meter
Z = 12632617
31 Z = 3833941
70
XDOT = 20770
879367 XDOT = 6324
661019
YDOT = -4180
890277 feet/sec YDOT = -1203
573859 meter/sec
ZDOT = 13563
744478 ZDOT = 4164
968328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1963846
39 X = -598580
38
Y = 18276506
12 feet Y = 5570679
07 meter
Z = 12563292
93 Z = 3829291
68
XDOT = -16468
232964 XDOT = -5019
517407
YDOT = -11191
252222 feet/sec YDOT = -3411
093677 meter/sec
ZDOT = 13694
514206 ZDOT = 4174
087930
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 14220
55622465
00016717 00000-0 10270-3 0 9078
2 25544 51
6424 200
0014 0007113 344
1574 15
9353 15
50605834 19453
Satellite: ISS
Catalog Number: 25544
Epoch time: 14220
55622465 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 200
0014 deg
Eccentricity:
0007113
Arg of perigee: 344
1574 deg
Mean anomaly: 15
9353 deg
Mean motion: 15
50605834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1945
Checksum: 275
Coasting Arc #9 (Orbit 1959)
---------------------------------------
Vector Time (GMT): 2014/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3211698
22 A = 6792249
46 meter
Y = 4265101
77 meter E =
0011395
Z = -4210389
02 I = 51
54354
XDOT = -6583
261105 Wp = 32
23323
YDOT = 1333
195077 meter/sec RA = 194
24208 deg
ZDOT = -3666
386625 TA = 200
02209
MA = 200
06684
Ha = 227
652 n
mi
Hp = 220
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10537067
65 X = 3184218
44
Y = 13993116
04 feet Y = 4300863
50 meter
Z = -13813612
28 Z = -4194854
03
XDOT = -21598
625672 XDOT = -6579
870182
YDOT = 4373
999598 feet/sec YDOT = 1259
595855 meter/sec
ZDOT = -12028
827510 ZDOT = -3698
358210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1749591
02 X = 533275
34
Y = -17480766
12 feet Y = -5328137
51 meter
Z = -13748262
53 Z = -4190470
42
XDOT = 17463
376786 XDOT = 5322
837244
YDOT = 11327
774984 feet/sec YDOT = 3452
705815 meter/sec
ZDOT = -12164
859459 ZDOT = -3707
849163
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 14221
52296270
00016717 00000-0 10270-3 0 9088
2 25544 51
6426 195
2068 0007191 349
2910 10
8087 15
50587028 19604
Satellite: ISS
Catalog Number: 25544
Epoch time: 14221
52296270 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 195
2068 deg
Eccentricity:
0007191
Arg of perigee: 349
2910 deg
Mean anomaly: 10
8087 deg
Mean motion: 15
50587028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1960
Checksum: 306
Coasting Arc #10 (Orbit 1975)
---------------------------------------
Vector Time (GMT): 2014/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2956316
46 A = 6790954
60 meter
Y = -4112822
43 meter E =
0008152
Z = 4515199
54 I = 51
57069
XDOT = 6833
504272 Wp = 62
65719
YDOT = -1431
757172 meter/sec RA = 189
27672 deg
ZDOT = 3169
319090 TA = 355
49287
MA = 355
50021
Ha = 227
692 n
mi
Hp = 220
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9699200
98 X = -2932039
08
Y = -13493511
90 feet Y = -4145746
11 meter
Z = 14813646
80 Z = 4500897
49
XDOT = 22419
633437 XDOT = 6833
611461
YDOT = -4697
366050 feet/sec YDOT = -1355
339913 meter/sec
ZDOT = 10398
028510 ZDOT = 3202
514768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1733243
34 X = -528292
57
Y = 16580821
35 feet Y = 5053834
35 meter
Z = 14753498
75 Z = 4496866
42
XDOT = -18557
824122 XDOT = -5656
424792
YDOT = -11319
855417 feet/sec YDOT = -3450
291931 meter/sec
ZDOT = 10539
291987 ZDOT = 3212
376198
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 14222
55413882
00016717 00000-0 10270-3 0 9093
2 25544 51
6432 190
0938 0007214 351
3003 8
8022 15
50632946 19766
Satellite: ISS
Catalog Number: 25544
Epoch time: 14222
55413882 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 190
0938 deg
Eccentricity:
0007214
Arg of perigee: 351
3003 deg
Mean anomaly: 8
8022 deg
Mean motion: 15
50632946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1976
Checksum: 293
Coasting Arc #11 (Orbit 1990)
---------------------------------------
Vector Time (GMT): 2014/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2687157
82 A = 6789980
55 meter
Y = 4009329
39 meter E =
0014777
Z = -4789128
74 I = 51
59884
XDOT = -7015
531498 Wp = 43
22474
YDOT = 1558
438119 meter/sec RA = 184
31133 deg
ZDOT = -2625
998995 TA = 200
77230
MA = 200
83241
Ha = 227
850 n
mi
Hp = 219
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8816134
59 X = 2665388
39
Y = 13153967
81 feet Y = 4039257
07 meter
Z = -15712364
63 Z = -4776128
19
XDOT = -23016
835624 XDOT = -7019
680932
YDOT = 5112
985956 feet/sec YDOT = 1479
962645 meter/sec
ZDOT = -8615
482267 ZDOT = -2660
088811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1887823
76 X = 575408
68
Y = -15776609
84 feet Y = -4808710
68 meter
Z = -15657720
26 Z = -4772473
14
XDOT = 19542
446486 XDOT = 5956
537689
YDOT = 11051
629403 feet/sec YDOT = 3368
536642 meter/sec
ZDOT = -8760
578097 ZDOT = -2670
224204
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 14223
52086105
00016717 00000-0 10270-3 0 9107
2 25544 51
6438 185
2994 0007297 356
0368 4
0724 15
50613532 19911
Satellite: ISS
Catalog Number: 25544
Epoch time: 14223
52086105 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 185
2994 deg
Eccentricity:
0007297
Arg of perigee: 356
0368 deg
Mean anomaly: 4
0724 deg
Mean motion: 15
50613532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1991
Checksum: 302
Coasting Arc #12 (Orbit 2006)
---------------------------------------
Vector Time (GMT): 2014/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2363113
66 A = 6788919
37 meter
Y = -3931722
99 meter E =
0006310
Z = 4999149
40 I = 51
62775
XDOT = 7186
135385 Wp = 51
62971
YDOT = -1708
925419 meter/sec RA = 179
34855 deg
ZDOT = 2054
946173 TA = 18
39094
MA = 18
36814
Ha = 227
881 n
mi
Hp = 219
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7752997
56 X = -2343256
40
Y = -12899353
63 feet Y = -3958037
59 meter
Z = 16401408
80 Z = 4987718
36
XDOT = 23576
559662 XDOT = 7194
728816
YDOT = -5606
710691 feet/sec YDOT = -1628
517271 meter/sec
ZDOT = 6741
949388 ZDOT = 2089
875690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2264037
24 X = -690078
55
Y = 14931459
14 feet Y = 4551108
74 meter
Z = 16353414
61 Z = 4984520
77
XDOT = -20548
738452 XDOT = -6263
255480
YDOT = -10655
177023 feet/sec YDOT = -3247
697957 meter/sec
ZDOT = 6890
648610 ZDOT = 2100
269696
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 14224
55202037
00016717 00000-0 10270-3 0 9116
2 25544 51
6446 180
1867 0007308 358
3849 1
7277 15
50659430 20078
Satellite: ISS
Catalog Number: 25544
Epoch time: 14224
55202037 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 180
1867 deg
Eccentricity:
0007308
Arg of perigee: 358
3849 deg
Mean anomaly: 1
7277 deg
Mean motion: 15
50659430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2007
Checksum: 298
Coasting Arc #13 (Orbit 2007)
---------------------------------------
Vector Time (GMT): 2014/224/13:30:14
000
Vector Time (MET): N/A
Weight (LBS) : 941131
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3450295
51 A = 6790543
54 meter
Y = -3590622
96 meter E =
0008560
Z = 4608215
06 I = 51
63609
XDOT = 6602
004211 Wp = 63
95219
YDOT = -2488
159254 meter/sec RA = 179
04380 deg
ZDOT = 3003
717368 TA = 356
07197
MA = 356
07868
Ha = 227
925 n
mi
Hp = 219
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11319867
15 X = -3432272
71
Y = -11780259
05 feet Y = -3629105
40 meter
Z = 15118815
80 Z = 4591498
27
XDOT = 21660
118801 XDOT = 6614
745885
YDOT = -8163
252145 feet/sec YDOT = -2414
259998 meter/sec
ZDOT = 9854
715774 ZDOT = 3035
819434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7383545
68 X = 2250504
72
Y = 14646644
84 feet Y = 4464297
35 meter
Z = 15048306
71 Z = 4586723
89
XDOT = -21980
981002 XDOT = -6699
803009
YDOT = 813
112984 feet/sec YDOT = 247
836838 meter/sec
ZDOT = 9991
515552 ZDOT = 3045
413940
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 14224
61646785
00016717 00000-0 10270-3 0 9126
2 25544 51
6457 179
8675 0007277 359
0382 1
0753 15
50654735 20083
Satellite: ISS
Catalog Number: 25544
Epoch time: 14224
61646785 = yrday
fracday
Element set: 912
Inclination: 51
6457 deg
RA of node: 179
8675 deg
Eccentricity:
0007277
Arg of perigee: 359
0382 deg
Mean anomaly: 1
0753 deg
Mean motion: 15
50654735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2008
Checksum: 323
Coasting Arc #14 (Orbit 2022)
---------------------------------------
Vector Time (GMT): 2014/225/13:30:14
000
Vector Time (MET): N/A
Weight (LBS) : 941131
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3152549
40 A = 6789534
61 meter
Y = 3545650
09 meter E =
0015888
Z = -4870941
09 I = 51
66440
XDOT = -6752
239660 Wp = 46
85346
YDOT = 2641
204266 meter/sec RA = 174
08291 deg
ZDOT = -2442
010819 TA = 199
10469
MA = 199
16434
Ha = 228
026 n
mi
Hp = 219
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10343009
85 X = 3136327
95
Y = 11632710
27 feet Y = 3580812
97 meter
Z = -15980777
85 Z = -4855666
26
XDOT = -22153
017258 XDOT = -6769
410039
YDOT = 8665
368326 feet/sec YDOT = 2565
600228 meter/sec
ZDOT = -8011
846519 ZDOT = -2474
853621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6743906
13 X = -2055542
59
Y = -14102181
53 feet Y = -4298344
93 meter
Z = -15916383
64 Z = -4851313
73
XDOT = 22619
569665 XDOT = 6894
444834
YDOT = -1595
853166 feet/sec YDOT = -486
416045 meter/sec
ZDOT = -8151
828280 ZDOT = -2484
677260
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 14225
58317326
00016717 00000-0 10270-3 0 9130
2 25544 51
6462 175
0736 0007422 3
3791 356
7409 15
50657575 20230
Satellite: ISS
Catalog Number: 25544
Epoch time: 14225
58317326 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 175
0736 deg
Eccentricity:
0007422
Arg of perigee: 3
3791 deg
Mean anomaly: 356
7409 deg
Mean motion: 15
50657575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2023
Checksum: 304
Coasting Arc #15 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2014/226/13:30:14
000
Vector Time (MET): N/A
Weight (LBS) : 941131
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2805678
25 A = 6788576
82 meter
Y = -3535349
07 meter E =
0006807
Z = 5065065
98 I = 51
69237
XDOT = 6887
542861 Wp = 53
20627
YDOT = -2814
142140 meter/sec RA = 169
12372 deg
ZDOT = 1853
223249 TA = 18
86685
MA = 18
84164
Ha = 228
080 n
mi
Hp = 219
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9204981
12 X = -2790540
84
Y = -11598914
27 feet Y = -3566639
09 meter
Z = 16617670
53 Z = 5051473
47
XDOT = 22596
925396 XDOT = 6909
497078
YDOT = -9232
749802 feet/sec YDOT = -2736
998345 meter/sec
ZDOT = 6080
128769 ZDOT = 1886
735073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5901052
57 X = 1798640
82
Y = 13650769
35 feet Y = 4160754
50 meter
Z = 16560420
83 Z = 5047616
27
XDOT = -23203
294966 XDOT = -7072
364306
YDOT = 2490
091622 feet/sec YDOT = 758
979926 meter/sec
ZDOT = 6222
992542 ZDOT = 1896
768127
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 14226
61431511
00016717 00000-0 10270-3 0 9149
2 25544 51
6461 169
9605 0007328 6
1215 354
0024 15
50684184 20390
Satellite: ISS
Catalog Number: 25544
Epoch time: 14226
61431511 = yrday
fracday
Element set: 914
Inclination: 51
6461 deg
RA of node: 169
9605 deg
Eccentricity:
0007328
Arg of perigee: 6
1215 deg
Mean anomaly: 354
0024 deg
Mean motion: 15
50684184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 283
Coasting Arc #16 (Orbit 2040)
---------------------------------------
Vector Time (GMT): 2014/226/17:21:42
209
Vector Time (MET): N/A
Weight (LBS) : 940793
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3087609
55 A = 6790956
94 meter
Y = 3403909
47 meter E =
0013773
Z = -5011629
64 I = 51
69871
XDOT = -6709
695926 Wp = 49
70356
YDOT = 3046
809256 meter/sec RA = 168
32907 deg
ZDOT = -2059
424036 TA = 200
21077
MA = 200
26535
Ha = 228
106 n
mi
Hp = 221
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10129952
59 X = 3073661
42
Y = 11167681
99 feet Y = 3438358
89 meter
Z = -16442354
46 Z = -4996664
66
XDOT = -22013
438079 XDOT = -6733
263447
YDOT = 9996
093358 feet/sec YDOT = 2971
645232 meter/sec
ZDOT = -6756
640539 ZDOT = -2092
075856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15091939
99 X = -4600023
31
Y = -1279677
29 feet Y = -390045
64 meter
Z = -16379250
71 Z = -4992395
62
XDOT = 9293
988451 XDOT = 2832
807680
YDOT = -21136
627789 feet/sec YDOT = -6442
444150 meter/sec
ZDOT = -6895
885640 ZDOT = -2101
865943
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 14226
74321207
00016717 00000-0 10270-3 0 9154
2 25544 51
6466 169
3217 0005875 343
7600 16
3361 15
49970900 20418
Satellite: ISS
Catalog Number: 25544
Epoch time: 14226
74321207 = yrday
fracday
Element set: 915
Inclination: 51
6466 deg
RA of node: 169
3217 deg
Eccentricity:
0005875
Arg of perigee: 343
7600 deg
Mean anomaly: 16
3361 deg
Mean motion: 15
49970900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2041
Checksum: 296
Coasting Arc #17 (Orbit 2056)
---------------------------------------
Vector Time (GMT): 2014/227/17:21:42
209
Vector Time (MET): N/A
Weight (LBS) : 940793
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2994924
82 A = 6790536
52 meter
Y = -3314244
44 meter E =
0004160
Z = 5111014
91 I = 51
72749
XDOT = 6658
711956 Wp = 49
84996
YDOT = -3391
229169 meter/sec RA = 163
37836 deg
ZDOT = 1704
490464 TA = 23
70411
MA = 23
68495
Ha = 228
319 n
mi
Hp = 221
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9825868
83 X = -2982469
06
Y = -10873505
38 feet Y = -3347665
79 meter
Z = 16768421
63 Z = 5096496
48
XDOT = 21846
167836 XDOT = 6687
858766
YDOT = -11126
079951 feet/sec YDOT = -3316
604122 meter/sec
ZDOT = 5592
160315 ZDOT = 1736
908218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14690108
84 X = 4477545
18
Y = 1015374
23 feet Y = 309486
06 meter
Z = 16707199
01 Z = 5092354
26
XDOT = -8033
770430 XDOT = -2448
693227
YDOT = 22031
636635 feet/sec YDOT = 6715
242846 meter/sec
ZDOT = 5730
476943 ZDOT = 1746
649372
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 14227
77481035
00016717 00000-0 10270-3 0 9165
2 25544 51
6466 164
2113 0005834 348
5633 11
5384 15
49952948 20572
Satellite: ISS
Catalog Number: 25544
Epoch time: 14227
77481035 = yrday
fracday
Element set: 916
Inclination: 51
6466 deg
RA of node: 164
2113 deg
Eccentricity:
0005834
Arg of perigee: 348
5633 deg
Mean anomaly: 11
5384 deg
Mean motion: 15
49952948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2057
Checksum: 321
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