[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 8th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 ET - UTC (sec) : 68 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
132/13:18:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 213
2
135/07:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 213
1
Coasting Arc #1 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2016/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4059608
89 A = 6776705
83 meter
Y = -1528891
74 meter E =
0005201
Z = 5202483
96 I = 51
25431
XDOT = 1472
907943 Wp = 113
18531
YDOT = 7457
907896 meter/sec RA = 265
12794 deg
ZDOT = 1039
523951 TA = 326
79467
MA = 326
82730
Ha = 220
922 n
mi
Hp = 213
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13318926
81 X = 4051131
61
Y = -5016049
01 feet Y = -1483541
88 meter
Z = 17068516
92 Z = 5222184
39
XDOT = 4832
375142 XDOT = 1384
352609
YDOT = 24468
201759 feet/sec YDOT = 7473
883792 meter/sec
ZDOT = 3410
511651 ZDOT = 1046
464024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6034937
63 X = 1839448
99
Y = -12774853
03 feet Y = -3893775
20 meter
Z = 17154343
09 Z = 5228643
77
XDOT = 19507
347013 XDOT = 5945
839370
YDOT = 13846
240856 feet/sec YDOT = 4220
334213 meter/sec
ZDOT = 3439
292116 ZDOT = 1048
296237
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 16127
55003069
00016717 00000-0 10270-3 0 9002
2 25544 51
6411 265
7403 0001665 91
5236 268
6108 15
54472965 38506
Satellite: ISS
Catalog Number: 25544
Epoch time: 16127
55003069 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 265
7403 deg
Eccentricity:
0001665
Arg of perigee: 91
5236 deg
Mean anomaly: 268
6108 deg
Mean motion: 15
54472965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3850
Checksum: 302
Coasting Arc #2 (Orbit 3864)
---------------------------------------
Vector Time (GMT): 2016/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4322162
92 A = 6776662
28 meter
Y = -420496
58 meter E =
0016077
Z = -5216600
35 I = 51
25855
XDOT = -492
105020 Wp = 97
67632
YDOT = -7573
034750 meter/sec RA = 260
09884 deg
ZDOT = 1018
770989 TA = 182
14184
MA = 182
14873
Ha = 221
068 n
mi
Hp = 213
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14180324
56 X = -4291799
04
Y = -1379581
94 feet Y = -468659
98 meter
Z = -17114830
55 Z = -5237523
05
XDOT = -1614
517783 XDOT = -412
333738
YDOT = -24845
914535 feet/sec YDOT = -7578
091793 meter/sec
ZDOT = 3342
424504 ZDOT = 1016
573990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10939481
12 X = -3334353
85
Y = 8955268
22 feet Y = 2729565
75 meter
Z = -17205615
35 Z = -5244271
56
XDOT = -18046
744542 XDOT = -5500
647736
YDOT = -15643
058153 feet/sec YDOT = -4768
004125 meter/sec
ZDOT = 3334
254909 ZDOT = 1016
280896
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 16128
51435338
00016717 00000-0 10270-3 0 9018
2 25544 51
6418 260
9321 0001736 95
8490 264
2860 15
54484955 38652
Satellite: ISS
Catalog Number: 25544
Epoch time: 16128
51435338 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 260
9321 deg
Eccentricity:
0001736
Arg of perigee: 95
8490 deg
Mean anomaly: 264
2860 deg
Mean motion: 15
54484955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3865
Checksum: 324
Coasting Arc #3 (Orbit 3880)
---------------------------------------
Vector Time (GMT): 2016/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4421163
46 A = 6779304
00 meter
Y = 2304291
59 meter E =
0009934
Z = 4587187
69 I = 51
27465
XDOT = -584
800587 Wp = 71
02433
YDOT = 7050
720245 meter/sec RA = 255
07218 deg
ZDOT = -2969
708283 TA = 48
76101
MA = 48
67545
Ha = 220
998 n
mi
Hp = 213
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14505129
47 X = 4372784
72
Y = 7560011
79 feet Y = 2353461
27 meter
Z = 15049828
38 Z = 4608547
59
XDOT = -1918
637096 XDOT = -649
174209
YDOT = 23132
284268 feet/sec YDOT = 7043
820817 meter/sec
ZDOT = -9743
137411 ZDOT = -2972
705187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15457043
47 X = 4711306
85
Y = -5083707
23 feet Y = -1549513
96 meter
Z = 15142180
21 Z = 4615336
53
XDOT = 14947
944014 XDOT = 4556
133336
YDOT = 16303
976398 feet/sec YDOT = 4969
452006 meter/sec
ZDOT = -9757
423264 ZDOT = -2974
062611
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 16129
54295376
00016717 00000-0 10270-3 0 9029
2 25544 51
6427 255
8013 0001800 98
2240 261
9117 15
54463462 38812
Satellite: ISS
Catalog Number: 25544
Epoch time: 16129
54295376 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 255
8013 deg
Eccentricity:
0001800
Arg of perigee: 98
2240 deg
Mean anomaly: 261
9117 deg
Mean motion: 15
54463462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3881
Checksum: 305
Coasting Arc #4 (Orbit 3895)
---------------------------------------
Vector Time (GMT): 2016/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4348204
90 A = 6783207
15 meter
Y = -3919322
69 meter E =
0006633
Z = -3433075
73 I = 51
29702
XDOT = 1737
619470 Wp = 93
19708
YDOT = -5911
213958 meter/sec RA = 250
05782 deg
ZDOT = 4554
928576 TA = 226
39413
MA = 226
44919
Ha = 221
014 n
mi
Hp = 213
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14265764
09 X = -4287378
25
Y = -12858670
24 feet Y = -3967606
91 meter
Z = -11263371
83 Z = -3454051
01
XDOT = 5700
851279 XDOT = 1781
464807
YDOT = -19393
746581 feet/sec YDOT = -5891
537849 meter/sec
ZDOT = 14943
991391 ZDOT = 4563
475772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19087857
01 X = -5817978
82
Y = 1570498
28 feet Y = 478687
88 meter
Z = -11353775
60 Z = -3460630
80
XDOT = -10210
195999 XDOT = -3112
067740
YDOT = -15953
830168 feet/sec YDOT = -4862
727435 meter/sec
ZDOT = 14982
173645 ZDOT = 4566
566527
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 16130
50725377
00016717 00000-0 10270-3 0 9037
2 25544 51
6426 250
9929 0001660 95
9114 264
2228 15
54487696 38961
Satellite: ISS
Catalog Number: 25544
Epoch time: 16130
50725377 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 250
9929 deg
Eccentricity:
0001660
Arg of perigee: 95
9114 deg
Mean anomaly: 264
2228 deg
Mean motion: 15
54487696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3896
Checksum: 332
Coasting Arc #5 (Orbit 3911)
---------------------------------------
Vector Time (GMT): 2016/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4010282
83 A = 6786766
34 meter
Y = 5151393
35 meter E =
0015674
Z = 1828208
66 I = 51
32028
XDOT = -2956
893947 Wp = 112
83869
YDOT = 4307
266083 meter/sec RA = 245
05521 deg
ZDOT = -5618
028418 TA = 46
95273
MA = 46
82158
Ha = 220
982 n
mi
Hp = 213
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13157095
90 X = 3943499
87
Y = 16900896
83 feet Y = 5195865
49 meter
Z = 5998059
92 Z = 1847527
90
XDOT = -9701
095625 XDOT = -2977
548880
YDOT = 14131
450404 feet/sec YDOT = 4274
084966 meter/sec
ZDOT = -18431
851764 ZDOT = -5632
442329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21334370
01 X = 6502715
98
Y = 1609812
26 feet Y = 490670
78 meter
Z = 6081066
49 Z = 1853509
07
XDOT = 4167
779585 XDOT = 1270
339217
YDOT = 15029
301178 feet/sec YDOT = 4580
930999 meter/sec
ZDOT = -18495
228883 ZDOT = -5637
345763
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 16131
53583106
00016717 00000-0 10270-3 0 9044
2 25544 51
6420 245
8628 0001736 104
6354 255
4991 15
54510159 39121
Satellite: ISS
Catalog Number: 25544
Epoch time: 16131
53583106 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 245
8628 deg
Eccentricity:
0001736
Arg of perigee: 104
6354 deg
Mean anomaly: 255
4991 deg
Mean motion: 15
54510159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3912
Checksum: 299
Coasting Arc #6 (Orbit 3926)
---------------------------------------
Vector Time (GMT): 2016/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3408948
62 A = 6788139
87 meter
Y = -5863645
61 meter E =
0013055
Z = -34562
99 I = 51
34065
XDOT = 4130
393763 Wp = 51
47980
YDOT = -2427
486460 meter/sec RA = 240
06113 deg
ZDOT = 5988
506620 TA = 308
14630
MA = 308
26387
Ha = 220
956 n
mi
Hp = 213
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11184214
63 X = -3342958
62
Y = -19237682
45 feet Y = -5901397
77 meter
Z = -113395
65 Z = -50962
93
XDOT = 13551
160640 XDOT = 4128
141766
YDOT = -7964
194421 feet/sec YDOT = -2381
310538 meter/sec
ZDOT = 19647
331430 ZDOT = 6008
565584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21844976
11 X = -6658348
72
Y = -4236891
21 feet Y = -1291404
44 meter
Z = -183611
94 Z = -55964
92
XDOT = 2528
260299 XDOT = 770
613739
YDOT = -13755
128185 feet/sec YDOT = -4192
563071 meter/sec
ZDOT = 19734
901334 ZDOT = 6015
197927
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 16132
50011058
00016717 00000-0 10270-3 0 9055
2 25544 51
6432 241
0536 0001709 100
3449 259
7896 15
54536767 39278
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
50011058 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 241
0536 deg
Eccentricity:
0001709
Arg of perigee: 100
3449 deg
Mean anomaly: 259
7896 deg
Mean motion: 15
54536767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3927
Checksum: 307
Coasting Arc #7 (Orbit 3927)
---------------------------------------
Vector Time (GMT): 2016/132/13:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4935606
18 A = 6779581
44 meter
Y = -1406056
02 meter E =
0011028
Z = -4441176
39 I = 51
31303
XDOT = -976
553610 Wp = 109
30672
YDOT = -6861
672682 meter/sec RA = 239
76824 deg
ZDOT = 3260
712669 TA = 193
72871
MA = 193
75872
Ha = 220
886 n
mi
Hp = 213
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16192933
67 X = -4897943
03
Y = -4613044
69 feet Y = -1461038
45 meter
Z = -14570788
68 Z = -4465061
08
XDOT = -3203
916043 XDOT = -915
591332
YDOT = -22512
049480 feet/sec YDOT = -6872
252453 meter/sec
ZDOT = 10697
876209 ZDOT = 3256
116519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10215169
66 X = -3113583
71
Y = 13270803
44 feet Y = 4044940
89 meter
Z = -14674305
77 Z = -4472728
40
XDOT = -21167
915675 XDOT = -6451
980698
YDOT = -4496
477068 feet/sec YDOT = -1370
526210 meter/sec
ZDOT = 10679
114392 ZDOT = 3254
994067
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 16132
56439481
00016717 00000-0 10270-3 0 9066
2 25544 51
6429 240
7344 0001643 100
8672 259
2665 15
54568077 39286
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
56439481 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 240
7344 deg
Eccentricity:
0001643
Arg of perigee: 100
8672 deg
Mean anomaly: 259
2665 deg
Mean motion: 15
54568077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3928
Checksum: 326
Coasting Arc #8 (Orbit 3943)
---------------------------------------
Vector Time (GMT): 2016/133/13:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5201638
19 A = 6783736
17 meter
Y = 2980137
02 meter E =
0014503
Z = 3161148
63 I = 51
34354
XDOT = -488
420094 Wp = 94
50594
YDOT = 5964
695222 meter/sec RA = 234
75752 deg
ZDOT = -4801
520826 TA = 48
81724
MA = 48
69225
Ha = 220
839 n
mi
Hp = 213
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17065742
09 X = 5152571
38
Y = 9777352
42 feet Y = 3038030
74 meter
Z = 10371222
53 Z = 3186297
93
XDOT = -1602
428129 XDOT = -531
758675
YDOT = 19569
210045 feet/sec YDOT = 5958
991232 meter/sec
ZDOT = -15753
021082 ZDOT = -4803
998514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15135582
66 X = 4613325
59
Y = -12469271
45 feet Y = -3800633
94 meter
Z = 10479973
15 Z = 3194295
82
XDOT = 16878
090508 XDOT = 5144
441987
YDOT = 7188
427764 feet/sec YDOT = 2191
032782 meter/sec
ZDOT = -15764
823397 ZDOT = -4805
118171
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 16133
59294798
00016717 00000-0 10270-3 0 9071
2 25544 51
6426 235
6041 0001675 98
5777 261
5566 15
54563234 39448
Satellite: ISS
Catalog Number: 25544
Epoch time: 16133
59294798 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 235
6041 deg
Eccentricity:
0001675
Arg of perigee: 98
5777 deg
Mean anomaly: 261
5566 deg
Mean motion: 15
54563234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3944
Checksum: 343
Coasting Arc #9 (Orbit 3958)
---------------------------------------
Vector Time (GMT): 2016/134/13:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5126623
17 A = 6787109
38 meter
Y = -4174539
69 meter E =
0008982
Z = -1522592
89 I = 51
37304
XDOT = 2081
140775 Wp = 46
38266
YDOT = -4638
749554 meter/sec RA = 229
75977 deg
ZDOT = 5738
274121 TA = 296
92242
MA = 297
01415
Ha = 220
874 n
mi
Hp = 213
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16819629
84 X = -5072165
27
Y = -13695996
34 feet Y = -4231564
47 meter
Z = -4995383
49 Z = -1547364
67
XDOT = 6827
889683 XDOT = 2104
983566
YDOT = -15218
994601 feet/sec YDOT = -4615
343663 meter/sec
ZDOT = 18826
358665 ZDOT = 5748
441641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18538443
16 X = -5650517
48
Y = 11212793
81 feet Y = 3417659
55 meter
Z = -5102303
40 Z = -1555182
08
XDOT = -11263
756233 XDOT = -3433
192900
YDOT = -10075
399832 feet/sec YDOT = -3070
981869 meter/sec
ZDOT = 18871
337164 ZDOT = 5751
983568
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 16134
55720628
00016717 00000-0 10270-3 0 9085
2 25544 51
6418 230
7948 0001518 97
4114 262
7211 15
54537603 39597
Satellite: ISS
Catalog Number: 25544
Epoch time: 16134
55720628 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 230
7948 deg
Eccentricity:
0001518
Arg of perigee: 97
4114 deg
Mean anomaly: 262
7211 deg
Mean motion: 15
54537603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3959
Checksum: 316
Coasting Arc #10 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2016/135/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3675993
00 A = 6776218
75 meter
Y = 2236848
71 meter E =
0016368
Z = -5248919
05 I = 51
35118
XDOT = -4790
826652 Wp = 97
44082
YDOT = -5914
582400 meter/sec RA = 225
96064 deg
ZDOT = 834
816832 TA = 180
58286
MA = 180
58477
Ha = 220
924 n
mi
Hp = 213
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12060344
48 X = -3675235
67
Y = 7338742
49 feet Y = 2195745
61 meter
Z = -17220863
03 Z = -5266774
33
XDOT = -15717
935210 XDOT = -4728
387450
YDOT = -19404
797901 feet/sec YDOT = -5967
807505 meter/sec
ZDOT = 2738
900366 ZDOT = 811
695651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13466787
30 X = -4104676
77
Y = 3906802
18 feet Y = 1190793
31 meter
Z = -17298835
52 Z = -5272685
07
XDOT = -9743
068703 XDOT = -2969
687341
YDOT = -21899
740747 feet/sec YDOT = -6675
040980 meter/sec
ZDOT = 2639
438279 ZDOT = 804
500788
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 16135
32860724
00016717 00000-0 10270-3 0 9094
2 25544 51
6398 226
9447 0001842 104
3230 255
8128 15
54593832 39712
Satellite: ISS
Catalog Number: 25544
Epoch time: 16135
32860724 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 226
9447 deg
Eccentricity:
0001842
Arg of perigee: 104
3230 deg
Mean anomaly: 255
8128 deg
Mean motion: 15
54593832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 320
Coasting Arc #11 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2016/136/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4869791
39 A = 6778702
95 meter
Y = -700170
07 meter E =
0009458
Z = 4656808
39 I = 51
38214
XDOT = 3612
044454 Wp = 71
86660
YDOT = 6142
626472 meter/sec RA = 220
93879 deg
ZDOT = -2846
020582 TA = 46
51308
MA = 46
43448
Ha = 220
841 n
mi
Hp = 213
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15977005
86 X = 4854637
99
Y = -2297145
88 feet Y = -645797
57 meter
Z = 15278242
74 Z = 4680427
99
XDOT = 11850
539546 XDOT = 3556
912460
YDOT = 20152
973991 feet/sec YDOT = 6182
710513 meter/sec
ZDOT = -9337
337867 ZDOT = -2828
607915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15950751
75 X = 4861789
13
Y = 1721736
18 feet Y = 524785
19 meter
Z = 15381009
07 Z = 4688131
56
XDOT = 6654
994900 XDOT = 2028
442445
YDOT = 21316
447233 feet/sec YDOT = 6497
253117 meter/sec
ZDOT = -9262
706065 ZDOT = -2823
272809
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 16136
35713183
00016717 00000-0 10270-3 0 9106
2 25544 51
6396 221
8127 0001904 107
2342 252
9020 15
54570483 39877
Satellite: ISS
Catalog Number: 25544
Epoch time: 16136
35713183 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 221
8127 deg
Eccentricity:
0001904
Arg of perigee: 107
2342 deg
Mean anomaly: 252
9020 deg
Mean motion: 15
54570483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3987
Checksum: 297
Coasting Arc #12 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2016/137/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5763362
26 A = 6782594
19 meter
Y = -718834
40 meter E =
0007017
Z = -3510082
16 I = 51
42119
XDOT = -1999
595962 Wp = 99
56483
YDOT = -5875
278430 meter/sec RA = 215
93092 deg
ZDOT = 4492
979233 TA = 219
01073
MA = 219
06137
Ha = 220
867 n
mi
Hp = 213
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18908668
82 X = -5737845
08
Y = -2358380
59 feet Y = -783141
46 meter
Z = -11516017
57 Z = -3538017
44
XDOT = -6560
354207 XDOT = -1955
573700
YDOT = -19275
847867 feet/sec YDOT = -5897
393121 meter/sec
ZDOT = 14740
745515 ZDOT = 4483
372493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17774348
90 X = -5417621
54
Y = -6660624
66 feet Y = -2030158
40 meter
Z = -11637309
68 Z = -3547051
99
XDOT = -2492
107001 XDOT = -759
594214
YDOT = -18996
015379 feet/sec YDOT = -5789
985487 meter/sec
ZDOT = 14699
981906 ZDOT = 4480
554485
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 16137
32136420
00016717 00000-0 10270-3 0 9118
2 25544 51
6403 217
0035 0001857 109
3178 250
8176 15
54610439 40022
Satellite: ISS
Catalog Number: 25544
Epoch time: 16137
32136420 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 217
0035 deg
Eccentricity:
0001857
Arg of perigee: 109
3178 deg
Mean anomaly: 250
8176 deg
Mean motion: 15
54610439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4002
Checksum: 274
Coasting Arc #13 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2016/138/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6206572
57 A = 6786327
69 meter
Y = 1965712
24 meter E =
0015715
Z = 1888839
63 I = 51
46006
XDOT = 55
977120 Wp = 113
32201
YDOT = 5238
852012 meter/sec RA = 210
93599 deg
ZDOT = -5605
007332 TA = 45
80899
MA = 45
67998
Ha = 220
780 n
mi
Hp = 213
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20362770
89 X = 6174954
90
Y = 6449187
15 feet Y = 2034941
47 meter
Z = 6196980
41 Z = 1918913
23
XDOT = 183
651967 XDOT = 24
617883
YDOT = 17187
834685 feet/sec YDOT = 5239
302698 meter/sec
ZDOT = -18389
131668 ZDOT = -5604
811526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18460318
74 X = 5626705
15
Y = 10668554
43 feet Y = 3251775
39 meter
Z = 6327368
92 Z = 1928582
05
XDOT = -2622
329290 XDOT = -799
285968
YDOT = 15502
959136 feet/sec YDOT = 4725
301945 meter/sec
ZDOT = -18389
158818 ZDOT = -5605
015608
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 16138
34987178
00016717 00000-0 10270-3 0 9126
2 25544 51
6402 211
8724 0001762 115
1522 244
9814 15
54619600 40180
Satellite: ISS
Catalog Number: 25544
Epoch time: 16138
34987178 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 211
8724 deg
Eccentricity:
0001762
Arg of perigee: 115
1522 deg
Mean anomaly: 244
9814 deg
Mean motion: 15
54619600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4018
Checksum: 300
Coasting Arc #14 (Orbit 4032)
---------------------------------------
Vector Time (GMT): 2016/139/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6120540
72 A = 6787841
45 meter
Y = -2922341
33 meter E =
0012654
Z = -63811
72 I = 51
49494
XDOT = 2013
362222 Wp = 52
69387
YDOT = -4329
748818 meter/sec RA = 205
95169 deg
ZDOT = 6000
935015 TA = 306
61729
MA = 306
73362
Ha = 220
790 n
mi
Hp = 213
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20080514
19 X = -6087097
50
Y = -9587734
01 feet Y = -2990598
29 meter
Z = -209356
03 Z = -93463
08
XDOT = 6605
519101 XDOT = 2032
478491
YDOT = -14205
212659 feet/sec YDOT = -4307
127291 meter/sec
ZDOT = 19688
107004 ZDOT = 6010
761932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17780335
98 X = -5419446
41
Y = -13376886
51 feet Y = -4077275
01 meter
Z = -337762
04 Z = -102949
87
XDOT = 8189
537452 XDOT = 2496
171015
YDOT = -11341
133224 feet/sec YDOT = -3456
777407 meter/sec
ZDOT = 19731
548611 ZDOT = 6014
176017
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 16139
31408986
00016717 00000-0 10270-3 0 9130
2 25544 51
6419 207
0627 0001790 114
0328 246
1013 15
54638236 40338
Satellite: ISS
Catalog Number: 25544
Epoch time: 16139
31408986 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 207
0627 deg
Eccentricity:
0001790
Arg of perigee: 114
0328 deg
Mean anomaly: 246
1013 deg
Mean motion: 15
54638236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4033
Checksum: 292
Coasting Arc #15 (Orbit 4048)
---------------------------------------
Vector Time (GMT): 2016/140/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5436841
69 A = 6786436
70 meter
Y = 3628451
28 meter E =
0009077
Z = -1814561
12 I = 51
51881
XDOT = -4046
018064 Wp = 137
11579
YDOT = 3252
450198 meter/sec RA = 200
97004 deg
ZDOT = -5642
244846 TA = 62
86503
MA = 62
77250
Ha = 220
802 n
mi
Hp = 213
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17837407
12 X = 5404677
88
Y = 11904367
72 feet Y = 3689069
88 meter
Z = -5953284
51 Z = -1788227
82
XDOT = -13274
337480 XDOT = -4054
678973
YDOT = 10670
768366 feet/sec YDOT = 3207
156690 meter/sec
ZDOT = -18511
301989 ZDOT = -5661
920678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15421049
86 X = 4700336
00
Y = 14947280
48 feet Y = 4555931
09 meter
Z = -5839408
14 Z = -1779851
60
XDOT = -13781
143386 XDOT = -4200
492504
YDOT = 6982
809609 feet/sec YDOT = 2128
360369 meter/sec
ZDOT = -18597
385024 ZDOT = -5668
482955
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 16140
34258213
00016717 00000-0 10270-3 0 9142
2 25544 51
6410 201
9321 0001796 116
0877 244
0461 15
54660044 40493
Satellite: ISS
Catalog Number: 25544
Epoch time: 16140
34258213 = yrday
fracday
Element set: 914
Inclination: 51
6410 deg
RA of node: 201
9321 deg
Eccentricity:
0001796
Arg of perigee: 116
0877 deg
Mean anomaly: 244
0461 deg
Mean motion: 15
54660044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4049
Checksum: 279
Coasting Arc #16 (Orbit 4064)
---------------------------------------
Vector Time (GMT): 2016/141/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4223334
56 A = 6782783
71 meter
Y = -4042450
57 meter E =
0013925
Z = 3428297
09 I = 51
53750
XDOT = 5773
251612 Wp = 94
47839
YDOT = -2131
903788 meter/sec RA = 195
98245 deg
ZDOT = 4581
153026 TA = 305
76474
MA = 305
89414
Ha = 220
731 n
mi
Hp = 213
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13856084
52 X = -4194470
49
Y = -13262633
09 feet Y = -4089517
48 meter
Z = 11247693
86 Z = 3407850
70
XDOT = 18941
114212 XDOT = 5774
408316
YDOT = -6994
435000 feet/sec YDOT = -2067
337204 meter/sec
ZDOT = 15030
029614 ZDOT = 4609
201284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11559257
54 X = -3523261
70
Y = -15370391
12 feet Y = -4684895
21 meter
Z = 11159470
15 Z = 3401406
50
XDOT = 18616
183514 XDOT = 5674
212735
YDOT = -2957
980158 feet/sec YDOT = -901
592352 meter/sec
ZDOT = 15152
338123 ZDOT = 4618
432660
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 16141
37106692
00016717 00000-0 10270-3 0 9150
2 25544 51
6414 196
8018 0001766 124
9471 235
1848 15
54691479 40651
Satellite: ISS
Catalog Number: 25544
Epoch time: 16141
37106692 = yrday
fracday
Element set: 915
Inclination: 51
6414 deg
RA of node: 196
8018 deg
Eccentricity:
0001766
Arg of perigee: 124
9471 deg
Mean anomaly: 235
1848 deg
Mean motion: 15
54691479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4065
Checksum: 325
Coasting Arc #17 (Orbit 4079)
---------------------------------------
Vector Time (GMT): 2016/142/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2535362
01 A = 6778713
62 meter
Y = 4248333
73 meter E =
0011404
Z = -4644886
50 I = 51
55525
XDOT = -7011
682325 Wp = 77
64666
YDOT = 998
498437 meter/sec RA = 190
98450 deg
ZDOT = -2917
677074 TA = 163
27194
MA = 163
23430
Ha = 220
711 n
mi
Hp = 213
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8318116
84 X = 2510230
93
Y = 13938102
78 feet Y = 4276545
62 meter
Z = -15239128
94 Z = -4632630
87
XDOT = -23004
207104 XDOT = -7008
153571
YDOT = 3275
913507 feet/sec YDOT = 920
109063 meter/sec
ZDOT = -9572
431345 ZDOT = -2951
730086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6270486
99 X = 1911244
44
Y = 15024733
10 feet Y = 4579538
65 meter
Z = -15186547
20 Z = -4628859
59
XDOT = -22078
610638 XDOT = -6729
560523
YDOT = -598
748303 feet/sec YDOT = -182
498483 meter/sec
ZDOT = -9720
677429 ZDOT = -2962
862480
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 16142
33526737
00016717 00000-0 10270-3 0 9164
2 25544 51
6419 191
9921 0001713 125
0915 235
0398 15
54659419 40806
Satellite: ISS
Catalog Number: 25544
Epoch time: 16142
33526737 = yrday
fracday
Element set: 916
Inclination: 51
6419 deg
RA of node: 191
9921 deg
Eccentricity:
0001713
Arg of perigee: 125
0915 deg
Mean anomaly: 235
0398 deg
Mean motion: 15
54659419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4080
Checksum: 314
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