[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 23rd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
176/10:51:32
574 1
4 3
3 3
3
N/A 3
0 -0
0 227
2
000/00:01:05
148 0
6 -0
0 220
8
Coasting Arc #1 (Orbit 1182)
---------------------------------------
Vector Time (GMT): 2014/171/09:48:56
023
Vector Time (MET): N/A
Weight (LBS) : 888612
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -362637
43 A = 6798864
98 meter
Y = -6754843
10 meter E =
0014340
Z = -621388
56 I = 52
02288
XDOT = 4757
772337 Wp = 133
20987
YDOT = 287
721671 meter/sec RA = 82
81483 deg
ZDOT = -6000
725767 TA = 53
45410
MA = 53
32217
Ha = 227
582 n
mi
Hp = 218
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1189755
34 X = -284057
77
Y = -22161558
71 feet Y = -6758458
93 meter
Z = -2038676
37 Z = -622959
88
XDOT = 15609
489293 XDOT = 4783
351002
YDOT = 943
968736 feet/sec YDOT = 341
069642 meter/sec
ZDOT = -19687
420496 ZDOT = -5977
550986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18816371
39 X = -5735230
00
Y = -11767414
07 feet Y = -3586707
81 meter
Z = -2044147
15 Z = -623056
05
XDOT = 8950
831495 XDOT = 2728
213440
YDOT = -10964
523052 feet/sec YDOT = -3341
986626 meter/sec
ZDOT = -19589
134748 ZDOT = -5970
768271
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 14171
44005216
00016717 00000-0 10270-3 0 9003
2 25544 51
6459 83
4493 0003849 116
5170 243
6376 15
50797236 11837
Satellite: ISS
Catalog Number: 25544
Epoch time: 14171
44005216 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 83
4493 deg
Eccentricity:
0003849
Arg of perigee: 116
5170 deg
Mean anomaly: 243
6376 deg
Mean motion: 15
50797236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1183
Checksum: 304
Coasting Arc #2 (Orbit 1198)
---------------------------------------
Vector Time (GMT): 2014/172/09:48:56
023
Vector Time (MET): N/A
Weight (LBS) : 888612
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 472665
04 A = 6798352
55 meter
Y = 6668837
36 meter E =
0015837
Z = 1200728
33 I = 52
01655
XDOT = -4855
427462 Wp = 70
33913
YDOT = -725
820477 meter/sec RA = 77
88438 deg
ZDOT = 5884
756626 TA = 302
62117
MA = 302
77392
Ha = 227
500 n
mi
Hp = 218
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1550738
32 X = 392224
67
Y = 21879387
66 feet Y = 6673673
13 meter
Z = 3939397
41 Z = 1202829
70
XDOT = -15929
880124 XDOT = -4875
536685
YDOT = -2381
300779 feet/sec YDOT = -780
229963 meter/sec
ZDOT = 19306
944310 ZDOT = 5861
120625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18977983
54 X = 5784489
38
Y = 10994891
34 feet Y = 3351242
88 meter
Z = 3947119
28 Z = 1203081
96
XDOT = -10162
246380 XDOT = -3097
452697
YDOT = 10577
707445 feet/sec YDOT = 3224
085229 meter/sec
ZDOT = 19206
779194 ZDOT = 5854
226298
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 14172
47108688
00016717 00000-0 10270-3 0 9015
2 25544 51
6458 78
3354 0003799 120
3834 239
7693 15
50821134 11999
Satellite: ISS
Catalog Number: 25544
Epoch time: 14172
47108688 = yrday
fracday
Element set: 901
Inclination: 51
6458 deg
RA of node: 78
3354 deg
Eccentricity:
0003799
Arg of perigee: 120
3834 deg
Mean anomaly: 239
7693 deg
Mean motion: 15
50821134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1199
Checksum: 328
Coasting Arc #3 (Orbit 1213)
---------------------------------------
Vector Time (GMT): 2014/173/09:48:56
023
Vector Time (MET): N/A
Weight (LBS) : 888612
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -513768
83 A = 6797496
95 meter
Y = -6525724
43 meter E =
0010920
Z = -1820422
44 I = 52
00764
XDOT = 5003
128086 Wp = 135
03798
YDOT = 1182
755174 meter/sec RA = 72
95282 deg
ZDOT = -5680
116247 TA = 64
83741
MA = 64
72419
Ha = 227
431 n
mi
Hp = 218
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1685593
28 X = -431915
43
Y = -21409857
06 feet Y = -6531011
86 meter
Z = -5972514
56 Z = -1822720
15
XDOT = 16414
462226 XDOT = 5017
122737
YDOT = 3880
430362 feet/sec YDOT = 1238
782224 meter/sec
ZDOT = -18635
551993 ZDOT = -5655
777495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18837728
42 X = -5741739
62
Y = -10308287
38 feet Y = -3141965
99 meter
Z = -5981081
31 Z = -1823033
58
XDOT = 11523
233873 XDOT = 3512
281684
YDOT = -10358
730822 feet/sec YDOT = -3157
341155 meter/sec
ZDOT = -18532
487591 ZDOT = -5648
702218
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 14173
43767031
00016717 00000-0 10270-3 0 9026
2 25544 51
6469 73
5408 0003757 123
4073 236
7438 15
50840265 12149
Satellite: ISS
Catalog Number: 25544
Epoch time: 14173
43767031 = yrday
fracday
Element set: 902
Inclination: 51
6469 deg
RA of node: 73
5408 deg
Eccentricity:
0003757
Arg of perigee: 123
4073 deg
Mean anomaly: 236
7438 deg
Mean motion: 15
50840265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1214
Checksum: 299
Coasting Arc #4 (Orbit 1229)
---------------------------------------
Vector Time (GMT): 2014/174/09:48:56
023
Vector Time (MET): N/A
Weight (LBS) : 888612
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 558870
39 A = 6796492
39 meter
Y = 6338027
10 meter E =
0016266
Z = 2372484
59 I = 51
99436
XDOT = -5195
694079 Wp = 83
90254
YDOT = -1578
114094 meter/sec RA = 68
02002 deg
ZDOT = 5409
705158 TA = 302
41873
MA = 302
57598
Ha = 227
370 n
mi
Hp = 218
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1833564
29 X = 476430
77
Y = 20794052
17 feet Y = 6343815
51 meter
Z = 7783742
11 Z = 2375000
06
XDOT = -17046
240417 XDOT = -5203
939834
YDOT = -5177
539678 feet/sec YDOT = -1636
262454 meter/sec
ZDOT = 17748
376504 ZDOT = 5384
444850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18563352
23 X = 5658109
76
Y = 9539830
15 feet Y = 2907740
23 meter
Z = 7793253
45 Z = 2375383
65
XDOT = -12807
266707 XDOT = -3903
654892
YDOT = 10429
189867 feet/sec YDOT = 3178
817072 meter/sec
ZDOT = 17641
474359 ZDOT = 5377
121385
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 14174
46868053
00016717 00000-0 10270-3 0 9037
2 25544 51
6469 68
4271 0003717 126
9872 233
1620 15
50851837 12300
Satellite: ISS
Catalog Number: 25544
Epoch time: 14174
46868053 = yrday
fracday
Element set: 903
Inclination: 51
6469 deg
RA of node: 68
4271 deg
Eccentricity:
0003717
Arg of perigee: 126
9872 deg
Mean anomaly: 233
1620 deg
Mean motion: 15
50851837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1230
Checksum: 311
Coasting Arc #5 (Orbit 1244)
---------------------------------------
Vector Time (GMT): 2014/175/09:48:56
023
Vector Time (MET): N/A
Weight (LBS) : 888612
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -517237
93 A = 6795110
76 meter
Y = -6102947
00 meter E =
0008151
Z = -2943384
38 I = 51
97862
XDOT = 5419
217314 Wp = 120
66014
YDOT = 1965
578109 meter/sec RA = 63
08507 deg
ZDOT = -5042
230203 TA = 92
69523
MA = 92
60192
Ha = 227
274 n
mi
Hp = 218
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1696974
82 X = -434656
88
Y = -20022791
99 feet Y = -6108268
95 meter
Z = -9656772
90 Z = -2945697
31
XDOT = 17779
584365 XDOT = 5421
328615
YDOT = 6448
747076 feet/sec YDOT = 2026
191772 meter/sec
ZDOT = -16542
750009 ZDOT = -5015
898920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17987903
44 X = -5482712
97
Y = -8947596
40 feet Y = -2727227
38 meter
Z = -9665455
72 Z = -2946030
90
XDOT = 14109
228561 XDOT = 4300
492865
YDOT = -10665
977484 feet/sec YDOT = -3250
989937 meter/sec
ZDOT = -16431
375352 ZDOT = -5008
283207
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 14175
43524039
00016717 00000-0 10270-3 0 9049
2 25544 51
6479 63
6325 0003677 130
3052 229
8421 15
50883523 12456
Satellite: ISS
Catalog Number: 25544
Epoch time: 14175
43524039 = yrday
fracday
Element set: 904
Inclination: 51
6479 deg
RA of node: 63
6325 deg
Eccentricity:
0003677
Arg of perigee: 130
3052 deg
Mean anomaly: 229
8421 deg
Mean motion: 15
50883523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1245
Checksum: 299
Coasting Arc #6 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2014/176/09:48:56
023
Vector Time (MET): N/A
Weight (LBS) : 888612
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 463663
52 A = 6793780
78 meter
Y = 5837611
91 meter E =
0015216
Z = 3433907
40 I = 51
95902
XDOT = -5674
330616 Wp = 99
64224
YDOT = -2280
001741 meter/sec RA = 58
14802 deg
ZDOT = 4622
269423 TA = 300
31957
MA = 300
47000
Ha = 227
226 n
mi
Hp = 218
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1521205
77 X = 381670
73
Y = 19152270
05 feet Y = 5842337
95 meter
Z = 11266100
40 Z = 3435961
51
XDOT = -18616
570264 XDOT = -5670
866895
YDOT = -7480
320673 feet/sec YDOT = -2343
437057 meter/sec
ZDOT = 15164
925927 ZDOT = 4594
712387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17293085
35 X = 5270932
41
Y = 8360674
86 feet Y = 2548333
70 meter
Z = 11273723
80 Z = 3436231
01
XDOT = -15251
912313 XDOT = -4648
782873
YDOT = 11167
261150 feet/sec YDOT = 3403
781199 meter/sec
ZDOT = 15048
408766 ZDOT = 4586
754992
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 14176
46622619
00016717 00000-0 10270-3 0 9057
2 25544 51
6476 58
5186 0003653 133
9831 226
1622 15
50887596 12614
Satellite: ISS
Catalog Number: 25544
Epoch time: 14176
46622619 = yrday
fracday
Element set: 905
Inclination: 51
6476 deg
RA of node: 58
5186 deg
Eccentricity:
0003653
Arg of perigee: 133
9831 deg
Mean anomaly: 226
1622 deg
Mean motion: 15
50887596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1261
Checksum: 325
Coasting Arc #7 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2014/176/10:52:05
148
Vector Time (MET): N/A
Weight (LBS) : 888288
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4369616
61 A = 6789397
59 meter
Y = -649762
08 meter E =
0014056
Z = -5168119
92 I = 51
93874
XDOT = 2885
256612 Wp = 109
54503
YDOT = 6910
631346 meter/sec RA = 57
89362 deg
ZDOT = 1569
532826 TA = 175
56269
MA = 175
55021
Ha = 227
171 n
mi
Hp = 220
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14336012
51 X = 4401662
71
Y = -2131765
36 feet Y = -600718
29 meter
Z = -16955774
01 Z = -5146815
18
XDOT = 9466
065001 XDOT = 2800
141631
YDOT = 22672
675021 feet/sec YDOT = 6942
420007 meter/sec
ZDOT = 5149
385913 ZDOT = 1583
343270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1500474
76 X = 457344
71
Y = -14521576
22 feet Y = -4426176
43 meter
Z = -16865240
88 Z = -5140525
42
XDOT = 23241
881938 XDOT = 7084
125615
YDOT = -3649
696391 feet/sec YDOT = -1112
427460 meter/sec
ZDOT = 5206
698376 ZDOT = 1587
001665
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 14176
46622568
00016717 00000-0 10270-3 0 9061
2 25544 51
6487 58
5187 0001940 180
4652 179
6497 15
50287440 12616
Satellite: ISS
Catalog Number: 25544
Epoch time: 14176
46622568 = yrday
fracday
Element set: 906
Inclination: 51
6487 deg
RA of node: 58
5187 deg
Eccentricity:
0001940
Arg of perigee: 180
4652 deg
Mean anomaly: 179
6497 deg
Mean motion: 15
50287440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1261
Checksum: 331
Coasting Arc #8 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2014/177/10:52:05
148
Vector Time (MET): N/A
Weight (LBS) : 888288
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4529589
17 A = 6789816
01 meter
Y = 535031
70 meter E =
0005011
Z = 5026070
61 I = 51
92316
XDOT = -3066
049373 Wp = 72
57816
YDOT = -6720
976834 meter/sec RA = 52
95473 deg
ZDOT = -2044
586761 TA = 37
24643
MA = 37
21169
Ha = 227
136 n
mi
Hp = 220
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14860856
84 X = -4559650
32
Y = 1755353
35 feet Y = 484210
10 meter
Z = 16489732
98 Z = 5003993
63
XDOT = -10059
217104 XDOT = -2980
734087
YDOT = -22050
448929 feet/sec YDOT = -6754
786040 meter/sec
ZDOT = -6707
961814 ZDOT = -2059
274929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1737003
29 X = -529438
60
Y = 14966414
77 feet Y = 4561763
22 meter
Z = 16395940
77 Z = 4997482
75
XDOT = -22673
949234 XDOT = -6911
019727
YDOT = 4795
376000 feet/sec YDOT = 1461
630605 meter/sec
ZDOT = -6769
026268 ZDOT = -2063
199207
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 14177
49760747
00016717 00000-0 10270-3 0 9078
2 25544 51
6485 53
4073 0001861 188
6276 171
4843 15
50337070 12773
Satellite: ISS
Catalog Number: 25544
Epoch time: 14177
49760747 = yrday
fracday
Element set: 907
Inclination: 51
6485 deg
RA of node: 53
4073 deg
Eccentricity:
0001861
Arg of perigee: 188
6276 deg
Mean anomaly: 171
4843 deg
Mean motion: 15
50337070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1277
Checksum: 325
Coasting Arc #9 (Orbit 1291)
---------------------------------------
Vector Time (GMT): 2014/178/10:52:05
148
Vector Time (MET): N/A
Weight (LBS) : 888288
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4725898
22 A = 6790563
39 meter
Y = -451708
29 meter E =
0011863
Z = -4866517
36 I = 51
90620
XDOT = 3197
712209 Wp = 116
65664
YDOT = 6486
201537 meter/sec RA = 48
01435 deg
ZDOT = 2502
801859 TA = 177
90139
MA = 177
89641
Ha = 226
962 n
mi
Hp = 220
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15504915
42 X = 4754237
92
Y = -1481982
57 feet Y = -398701
09 meter
Z = -15966264
30 Z = -4843490
97
XDOT = 10491
181788 XDOT = 3112
786632
YDOT = 21280
188769 feet/sec YDOT = 6521
485201 meter/sec
ZDOT = 8211
292188 ZDOT = 2518
130468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1883250
73 X = 574014
82
Y = -15561675
34 feet Y = -4743198
64 meter
Z = -15868456
06 Z = -4836705
41
XDOT = 21884
585022 XDOT = 6670
421515
YDOT = -5791
372446 feet/sec YDOT = -1765
210322 meter/sec
ZDOT = 8275
112714 ZDOT = 2522
254355
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 14178
46451867
00016717 00000-0 10270-3 0 9087
2 25544 51
6486 48
6148 0001867 192
6718 167
4386 15
50323621 12926
Satellite: ISS
Catalog Number: 25544
Epoch time: 14178
46451867 = yrday
fracday
Element set: 908
Inclination: 51
6486 deg
RA of node: 48
6148 deg
Eccentricity:
0001867
Arg of perigee: 192
6718 deg
Mean anomaly: 167
4386 deg
Mean motion: 15
50323621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1292
Checksum: 337
Coasting Arc #10 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2014/179/10:52:05
148
Vector Time (MET): N/A
Weight (LBS) : 888288
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4928597
00 A = 6791243
00 meter
Y = 386938
76 meter E =
0007242
Z = 4651061
89 I = 51
88739
XDOT = -3291
211985 Wp = 75
13035
YDOT = -6257
181327 meter/sec RA = 43
07324 deg
ZDOT = -2961
389526 TA = 44
30722
MA = 44
24928
Ha = 226
934 n
mi
Hp = 220
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16169937
66 X = -4955150
69
Y = 1269484
11 feet Y = 331674
91 meter
Z = 15259389
39 Z = 4627055
22
XDOT = -10797
939582 XDOT = -3206
612795
YDOT = -20528
810127 feet/sec YDOT = -6293
512349 meter/sec
ZDOT = -9715
844903 ZDOT = -2977
173005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1953645
10 X = -595471
03
Y = 16197622
59 feet Y = 4937035
37 meter
Z = 15157431
56 Z = 4619985
14
XDOT = -21059
464906 XDOT = -6418
924903
YDOT = 6630
904633 feet/sec YDOT = 2021
099732 meter/sec
ZDOT = -9781
634813 ZDOT = -2981
442291
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 14179
49587715
00016717 00000-0 10270-3 0 9094
2 25544 51
6485 43
5030 0001777 200
2529 159
8552 15
50374546 13085
Satellite: ISS
Catalog Number: 25544
Epoch time: 14179
49587715 = yrday
fracday
Element set: 909
Inclination: 51
6485 deg
RA of node: 43
5030 deg
Eccentricity:
0001777
Arg of perigee: 200
2529 deg
Mean anomaly: 159
8552 deg
Mean motion: 15
50374546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 323
Coasting Arc #11 (Orbit 1322)
---------------------------------------
Vector Time (GMT): 2014/180/10:52:05
148
Vector Time (MET): N/A
Weight (LBS) : 888288
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5153224
63 A = 6792205
95 meter
Y = -365063
60 meter E =
0008887
Z = -4418940
37 I = 51
86672
XDOT = 3331
802961 Wp = 122
00213
YDOT = 5998
835591 meter/sec RA = 38
13042 deg
ZDOT = 3390
270897 TA = 182
26901
MA = 182
27304
Ha = 226
757 n
mi
Hp = 220
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16906904
97 X = 5178389
42
Y = -1197715
21 feet Y = -307295
67 meter
Z = -14497835
85 Z = -4393845
91
XDOT = 10931
112076 XDOT = 3248
006317
YDOT = 19681
219129 feet/sec YDOT = 6035
624999 meter/sec
ZDOT = 11122
936014 ZDOT = 3406
253368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1877063
04 X = 572128
81
Y = -16936154
16 feet Y = -5162139
79 meter
Z = -14391265
34 Z = -4386457
68
XDOT = 20079
413984 XDOT = 6120
205382
YDOT = -7281
622839 feet/sec YDOT = -2219
438641 meter/sec
ZDOT = 11189
616190 ZDOT = 3410
595015
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 14180
46276638
00016717 00000-0 10270-3 0 9104
2 25544 51
6482 38
7100 0001832 205
5188 154
5873 15
50358135 13238
Satellite: ISS
Catalog Number: 25544
Epoch time: 14180
46276638 = yrday
fracday
Element set: 910
Inclination: 51
6482 deg
RA of node: 38
7100 deg
Eccentricity:
0001832
Arg of perigee: 205
5188 deg
Mean anomaly: 154
5873 deg
Mean motion: 15
50358135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1323
Checksum: 296
Coasting Arc #12 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2014/181/10:52:05
148
Vector Time (MET): N/A
Weight (LBS) : 888288
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5375394
25 A = 6793070
23 meter
Y = 361554
23 meter E =
0009390
Z = 4130280
71 I = 51
84522
XDOT = -3325
302270 Wp = 84
03228
YDOT = -5756
747589 meter/sec RA = 33
18710 deg
ZDOT = -3815
416454 TA = 45
27796
MA = 45
20155
Ha = 226
723 n
mi
Hp = 220
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17635807
91 X = -5399101
07
Y = 1186201
54 feet Y = 301310
11 meter
Z = 13550789
72 Z = 4104110
55
XDOT = -10909
784349 XDOT = -3242
148007
YDOT = -18886
967156 feet/sec YDOT = -5793
467897 meter/sec
ZDOT = -12517
770520 ZDOT = -3831
368781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1714654
10 X = -522626
57
Y = 17677338
82 feet Y = 5388052
87 meter
Z = 13439655
89 Z = 4096407
12
XDOT = -19110
886416 XDOT = -5824
998180
YDOT = 7735
011740 feet/sec YDOT = 2357
631578 meter/sec
ZDOT = -12584
365917 ZDOT = -3835
714732
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 14181
49410176
00016717 00000-0 10270-3 0 9116
2 25544 51
6483 33
5979 0001734 212
9990 147
1053 15
50410114 13391
Satellite: ISS
Catalog Number: 25544
Epoch time: 14181
49410176 = yrday
fracday
Element set: 911
Inclination: 51
6483 deg
RA of node: 33
5979 deg
Eccentricity:
0001734
Arg of perigee: 212
9990 deg
Mean anomaly: 147
1053 deg
Mean motion: 15
50410114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 291
Coasting Arc #13 (Orbit 1353)
---------------------------------------
Vector Time (GMT): 2014/182/10:52:05
148
Vector Time (MET): N/A
Weight (LBS) : 888288
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5602764
24 A = 6794152
32 meter
Y = -407273
79 meter E =
0005504
Z = -3827929
28 I = 51
82130
XDOT = 3268
005555 Wp = 120
53166
YDOT = 5503
665115 meter/sec RA = 28
24175 deg
ZDOT = 4199
440257 TA = 193
71430
MA = 193
72926
Ha = 226
571 n
mi
Hp = 221
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18381772
45 X = 5625496
70
Y = -1336200
10 feet Y = -344492
61 meter
Z = -12558823
10 Z = -3800656
96
XDOT = 10721
803001 XDOT = 3185
820126
YDOT = 18056
644078 feet/sec YDOT = 5539
750130 meter/sec
ZDOT = 13777
691133 ZDOT = 4215
116499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1369930
35 X = 417554
77
Y = -18457895
91 feet Y = -5625966
67 meter
Z = -12443005
91 Z = -3792628
20
XDOT = 18070
138549 XDOT = 5507
778230
YDOT = -7986
964501 feet/sec YDOT = -2434
426780 meter/sec
ZDOT = 13843
160102 ZDOT = 4219
395199
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 14182
46096939
00016717 00000-0 10270-3 0 9122
2 25544 51
6475 28
8044 0001840 217
6196 142
4826 15
50390580 13547
Satellite: ISS
Catalog Number: 25544
Epoch time: 14182
46096939 = yrday
fracday
Element set: 912
Inclination: 51
6475 deg
RA of node: 28
8044 deg
Eccentricity:
0001840
Arg of perigee: 217
6196 deg
Mean anomaly: 142
4826 deg
Mean motion: 15
50390580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1354
Checksum: 313
Coasting Arc #14 (Orbit 1369)
---------------------------------------
Vector Time (GMT): 2014/183/10:52:05
148
Vector Time (MET): N/A
Weight (LBS) : 888288
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5817539
68 A = 6795084
93 meter
Y = 467736
19 meter E =
0011163
Z = 3469345
59 I = 51
79747
XDOT = -3158
598733 Wp = 95
51511
YDOT = -5278
610540 meter/sec RA = 23
29624 deg
ZDOT = -4573
198211 TA = 43
92517
MA = 43
83648
Ha = 226
510 n
mi
Hp = 220
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19086416
27 X = -5839190
44
Y = 1534567
56 feet Y = 402559
38 meter
Z = 11382367
43 Z = 3441032
53
XDOT = -10362
856734 XDOT = -3077
122440
YDOT = -17318
276050 feet/sec YDOT = -5313
476085 meter/sec
ZDOT = -15003
931139 ZDOT = -4588
344630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -945449
57 X = -288173
03
Y = 19195705
43 feet Y = 5850851
02 meter
Z = 11262126
36 Z = 3432696
11
XDOT = -17098
449742 XDOT = -5211
607481
YDOT = 8020
354611 feet/sec YDOT = 2444
604085 meter/sec
ZDOT = -15067
191174 ZDOT = -4592
479870
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 14183
49228183
00016717 00000-0 10270-3 0 9135
2 25544 51
6479 23
6923 0001750 225
8622 134
2385 15
50444045 13708
Satellite: ISS
Catalog Number: 25544
Epoch time: 14183
49228183 = yrday
fracday
Element set: 913
Inclination: 51
6479 deg
RA of node: 23
6923 deg
Eccentricity:
0001750
Arg of perigee: 225
8622 deg
Mean anomaly: 134
2385 deg
Mean motion: 15
50444045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1370
Checksum: 297
Coasting Arc #15 (Orbit 1384)
---------------------------------------
Vector Time (GMT): 2014/184/10:52:05
148
Vector Time (MET): N/A
Weight (LBS) : 888288
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6020450
58 A = 6796163
89 meter
Y = -577829
05 meter E =
0002914
Z = -3102062
96 I = 51
77077
XDOT = 3006
666049 Wp = 87
50288
YDOT = 5061
118103 meter/sec RA = 18
34830 deg
ZDOT = 4896
657657 TA = 236
97879
MA = 237
00678
Ha = 226
412 n
mi
Hp = 221
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19752134
46 X = 6041533
26
Y = -1895764
59 feet Y = -510386
39 meter
Z = -10177371
92 Z = -3072765
51
XDOT = 9864
389926 XDOT = 2926
061799
YDOT = 16604
718185 feet/sec YDOT = 5094
289534 meter/sec
ZDOT = 16065
149792 ZDOT = 4911
068100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 329845
07 X = 100536
78
Y = -19903499
12 feet Y = -6066586
53 meter
Z = -10052938
05 Z = -3064135
52
XDOT = 16141
875849 XDOT = 4920
043759
YDOT = -7870
258478 feet/sec YDOT = -2398
854784 meter/sec
ZDOT = 16125
324244 ZDOT = 4914
998830
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 14184
45912815
00016717 00000-0 10270-3 0 9145
2 25544 51
6467 18
8985 0001874 228
0418 132
0574 15
50421415 13852
Satellite: ISS
Catalog Number: 25544
Epoch time: 14184
45912815 = yrday
fracday
Element set: 914
Inclination: 51
6467 deg
RA of node: 18
8985 deg
Eccentricity:
0001874
Arg of perigee: 228
0418 deg
Mean anomaly: 132
0574 deg
Mean motion: 15
50421415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1385
Checksum: 311
Coasting Arc #16 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2014/185/10:52:05
148
Vector Time (MET): N/A
Weight (LBS) : 888288
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6200612
20 A = 6797017
18 meter
Y = 695191
11 meter E =
0012343
Z = 2680193
12 I = 51
74482
XDOT = -2802
512791 Wp = 108
08664
YDOT = -4883
353580 meter/sec RA = 13
40042 deg
ZDOT = -5201
004555 TA = 41
74030
MA = 41
64620
Ha = 226
301 n
mi
Hp = 221
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20343215
89 X = -6220944
60
Y = 2280810
72 feet Y = 625738
00 meter
Z = 8793284
51 Z = 2650022
22
XDOT = -9194
595770 XDOT = -2722
433037
YDOT = -16021
501247 feet/sec YDOT = -4914
244972 meter/sec
ZDOT = -17063
663237 ZDOT = -5214
424534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 340643
05 X = 103828
00
Y = 20522424
30 feet Y = 6255234
93 meter
Z = 8665128
18 Z = 2641131
07
XDOT = -15314
674197 XDOT = -4667
912695
YDOT = 7505
005764 feet/sec YDOT = 2287
525757 meter/sec
ZDOT = -17119
664361 ZDOT = -5218
073697
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 14185
49041760
00016717 00000-0 10270-3 0 9153
2 25544 51
6472 13
7863 0001808 237
5821 122
5155 15
50478393 14012
Satellite: ISS
Catalog Number: 25544
Epoch time: 14185
49041760 = yrday
fracday
Element set: 915
Inclination: 51
6472 deg
RA of node: 13
7863 deg
Eccentricity:
0001808
Arg of perigee: 237
5821 deg
Mean anomaly: 122
5155 deg
Mean motion: 15
50478393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1401
Checksum: 299
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