[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 7th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 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
011/02:13:29
648 -0
2 4
9 4
9
N/A 4
4 -0
6 221
9
000/00:16:59
296 -2
2 -0
4 214
0
Coasting Arc #1 (Orbit 1967)
---------------------------------------
Vector Time (GMT): 2016/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4644240
68 A = 6776648
43 meter
Y = -1476860
21 meter E =
0009517
Z = 4699532
74 I = 51
81590
XDOT = 4599
277176 Wp = 59
25434
YDOT = -5455
488437 meter/sec RA = 148
31605 deg
ZDOT = 2831
247545 TA = 2
76541
MA = 2
76015
Ha = 221
269 n
mi
Hp = 211
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15237010
10 X = -4650209
25
Y = -4845341
90 feet Y = -1528828
90 meter
Z = 15418414
51 Z = 4676957
52
XDOT = 15089
492048 XDOT = 4646
186948
YDOT = -17898
584111 feet/sec YDOT = -5403
794204 meter/sec
ZDOT = 9288
869899 ZDOT = 2853
703267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 803301
81 X = 244846
39
Y = -16062281
62 feet Y = -4895783
44 meter
Z = 15320872
58 Z = 4669801
96
XDOT = 19948
567874 XDOT = 6080
323488
YDOT = 9949
883770 feet/sec YDOT = 3032
724573 meter/sec
ZDOT = 9387
114006 ZDOT = 2861
192349
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 16006
55328283
00016717 00000-0 10270-3 0 9006
2 25544 51
6391 149
1236 0008524 6
2274 353
8984 15
55297043 19688
Satellite: ISS
Catalog Number: 25544
Epoch time: 16006
55328283 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 149
1236 deg
Eccentricity:
0008524
Arg of perigee: 6
2274 deg
Mean anomaly: 353
8984 deg
Mean motion: 15
55297043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1968
Checksum: 318
Coasting Arc #2 (Orbit 1982)
---------------------------------------
Vector Time (GMT): 2016/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3005275
76 A = 6774075
83 meter
Y = 2966794
94 meter E =
0018937
Z = -5311500
44 I = 51
83492
XDOT = -5851
182022 Wp = 59
52665
YDOT = 4908
079816 meter/sec RA = 143
32092 deg
ZDOT = -561
304638 TA = 205
07793
MA = 205
17002
Ha = 221
332 n
mi
Hp = 211
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9859828
61 X = 2997677
94
Y = 9733579
22 feet Y = 3000359
90 meter
Z = -17426182
54 Z = -5296919
77
XDOT = -19196
791410 XDOT = -5902
903931
YDOT = 16102
624069 feet/sec YDOT = 4842
358885 meter/sec
ZDOT = -1841
550650 ZDOT = -589
853409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6680887
77 X = -2036334
59
Y = 12227187
41 feet Y = 3726846
72 meter
Z = -17363532
16 Z = -5292404
60
XDOT = -19789
542732 XDOT = -6031
852625
YDOT = -13641
745314 feet/sec YDOT = -4158
003972 meter/sec
ZDOT = -1966
118054 ZDOT = -599
272783
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 16007
51710248
00016717 00000-0 10270-3 0 9010
2 25544 51
6400 144
3116 0008666 10
7746 349
3591 15
55298708 19834
Satellite: ISS
Catalog Number: 25544
Epoch time: 16007
51710248 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 144
3116 deg
Eccentricity:
0008666
Arg of perigee: 10
7746 deg
Mean anomaly: 349
3591 deg
Mean motion: 15
55298708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1983
Checksum: 308
Coasting Arc #3 (Orbit 1998)
---------------------------------------
Vector Time (GMT): 2016/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1124859
27 A = 6775077
46 meter
Y = -4337464
32 meter E =
0013245
Z = 5078948
60 I = 51
86380
XDOT = 6412
527329 Wp = 30
34643
YDOT = -3802
328460 meter/sec RA = 138
32190 deg
ZDOT = -1813
793945 TA = 77
21852
MA = 77
07053
Ha = 221
495 n
mi
Hp = 211
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3690483
17 X = -1100944
31
Y = -14230525
98 feet Y = -4349909
97 meter
Z = 16663217
18 Z = 5073542
04
XDOT = 21038
475489 XDOT = 6463
379899
YDOT = -12474
830906 feet/sec YDOT = -3730
334847 meter/sec
ZDOT = -5950
767537 ZDOT = -1782
520449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12546059
28 X = 3824038
87
Y = -7712227
86 feet Y = -2350687
05 meter
Z = 16640561
30 Z = 5072043
09
XDOT = 17425
137559 XDOT = 5311
181928
YDOT = 15707
110909 feet/sec YDOT = 4787
527405 meter/sec
ZDOT = -5814
566893 ZDOT = -1772
279989
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 16008
54516873
00016717 00000-0 10270-3 0 9023
2 25544 51
6405 139
1761 0008708 14
9033 345
2375 15
55268848 19993
Satellite: ISS
Catalog Number: 25544
Epoch time: 16008
54516873 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 139
1761 deg
Eccentricity:
0008708
Arg of perigee: 14
9033 deg
Mean anomaly: 345
2375 deg
Mean motion: 15
55268848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1999
Checksum: 330
Coasting Arc #4 (Orbit 2013)
---------------------------------------
Vector Time (GMT): 2016/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -666377
96 A = 6778842
89 meter
Y = 5372323
10 meter E =
0011275
Z = -4083996
00 I = 51
90086
XDOT = -6239
472652 Wp = 58
24410
YDOT = 2171
132558 meter/sec RA = 133
33540 deg
ZDOT = 3887
754913 TA = 251
82192
MA = 251
94471
Ha = 221
512 n
mi
Hp = 211
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2186279
38 X = -706564
95
Y = 17625731
95 feet Y = 5364646
86 meter
Z = -13398937
02 Z = -4087330
24
XDOT = -20470
710799 XDOT = -6282
171935
YDOT = 7123
138314 feet/sec YDOT = 2101
119583 meter/sec
ZDOT = 12755
101419 ZDOT = 3857
341842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17433205
85 X = -5313641
14
Y = 3334109
53 feet Y = 1016236
58 meter
Z = -13414350
71 Z = -4088694
10
XDOT = -12769
057009 XDOT = -3892
008576
YDOT = -16159
389545 feet/sec YDOT = -4925
381933 meter/sec
ZDOT = 12622
899876 ZDOT = 3847
459882
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 16009
50897071
00016717 00000-0 10270-3 0 9033
2 25544 51
6414 134
3636 0008751 17
1775 342
9673 15
55294507 20142
Satellite: ISS
Catalog Number: 25544
Epoch time: 16009
50897071 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 134
3636 deg
Eccentricity:
0008751
Arg of perigee: 17
1775 deg
Mean anomaly: 342
9673 deg
Mean motion: 15
55294507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2014
Checksum: 309
Coasting Arc #5 (Orbit 2029)
---------------------------------------
Vector Time (GMT): 2016/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2279243
02 A = 6783412
56 meter
Y = -5915610
09 meter E =
0017031
Z = 2406636
56 I = 51
93803
XDOT = 5458
581447 Wp = 75
41617
YDOT = -102
203456 meter/sec RA = 128
36427 deg
ZDOT = -5384
903951 TA = 77
79072
MA = 77
60003
Ha = 221
571 n
mi
Hp = 211
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7477831
44 X = 2333533
17
Y = -19408169
60 feet Y = -5889818
71 meter
Z = 7895789
25 Z = 2417839
87
XDOT = 17908
731783 XDOT = 5485
475840
YDOT = -335
313175 feet/sec YDOT = -41
011237 meter/sec
ZDOT = -17667
007714 ZDOT = -5358
322537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20762790
25 X = 6328498
47
Y = 845812
01 feet Y = 257803
50 meter
Z = 7945416
36 Z = 2421762
91
XDOT = 6131
783828 XDOT = 1868
967711
YDOT = 15457
915611 feet/sec YDOT = 4711
572678 meter/sec
ZDOT = -17551
768584 ZDOT = -5349
779064
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 16010
53701955
00016717 00000-0 10270-3 0 9044
2 25544 51
6419 129
2290 0008729 21
6893 338
4629 15
55309491 20300
Satellite: ISS
Catalog Number: 25544
Epoch time: 16010
53701955 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 129
2290 deg
Eccentricity:
0008729
Arg of perigee: 21
6893 deg
Mean anomaly: 338
4629 deg
Mean motion: 15
55309491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2030
Checksum: 308
Coasting Arc #6 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2016/011/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3623890
50 A = 6776851
50 meter
Y = 2116558
03 meter E =
0016581
Z = -5334400
97 I = 51
91846
XDOT = -4220
211791 Wp = 66
10099
YDOT = 6380
999942 meter/sec RA = 125
41310 deg
ZDOT = -329
422916 TA = 200
73231
MA = 200
79965
Ha = 221
862 n
mi
Hp = 214
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11889404
54 X = 3625865
15
Y = 6944088
02 feet Y = 2157094
13 meter
Z = -17501315
52 Z = -5316792
34
XDOT = -13845
839208 XDOT = -4289
651876
YDOT = 20935
039180 feet/sec YDOT = 6333
418500 meter/sec
ZDOT = -1080
783845 ZDOT = -350
091639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5782099
86 X = -1762384
04
Y = -12601520
39 feet Y = -3840943
42 meter
Z = -17425365
09 Z = -5311251
28
XDOT = 22473
394842 XDOT = 6849
890748
YDOT = -8665
631877 feet/sec YDOT = -2641
284596 meter/sec
ZDOT = -1171
532790 ZDOT = -357
083194
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 16011
11530132
00016717 00000-0 10270-3 0 9057
2 25544 51
6423 126
3441 0006078 3
2055 356
9135 15
54317200 20394
Satellite: ISS
Catalog Number: 25544
Epoch time: 16011
11530132 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 126
3441 deg
Eccentricity:
0006078
Arg of perigee: 3
2055 deg
Mean anomaly: 356
9135 deg
Mean motion: 15
54317200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 255
Coasting Arc #7 (Orbit 2054)
---------------------------------------
Vector Time (GMT): 2016/012/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2502904
18 A = 6777595
95 meter
Y = -3660272
73 meter E =
0010184
Z = 5123938
25 I = 51
93915
XDOT = 4864
587401 Wp = 27
80282
YDOT = -5688
457498 meter/sec RA = 120
43093 deg
ZDOT = -1677
200785 TA = 78
37796
MA = 78
26367
Ha = 221
921 n
mi
Hp = 213
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8211627
89 X = -2486677
59
Y = -12008768
80 feet Y = -3688171
34 meter
Z = 16810821
04 Z = 5111819
22
XDOT = 15959
932418 XDOT = 4935
982579
YDOT = -18662
918301 feet/sec YDOT = -5633
659201 meter/sec
ZDOT = -5502
627248 ZDOT = -1653
397034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 101406
46 X = 30908
69
Y = 14607279
20 feet Y = 4452298
70 meter
Z = 16758943
16 Z = 5108125
88
XDOT = -22667
591216 XDOT = -6909
081803
YDOT = 6389
147328 feet/sec YDOT = 1947
412106 meter/sec
ZDOT = -5398
398634 ZDOT = -1645
431904
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 16012
14401641
00016717 00000-0 10270-3 0 9064
2 25544 51
6423 121
2142 0006157 5
5241 354
5979 15
54352937 20550
Satellite: ISS
Catalog Number: 25544
Epoch time: 16012
14401641 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 121
2142 deg
Eccentricity:
0006157
Arg of perigee: 5
5241 deg
Mean anomaly: 354
5979 deg
Mean motion: 15
54352937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 278
Coasting Arc #8 (Orbit 2069)
---------------------------------------
Vector Time (GMT): 2016/013/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1403990
67 A = 6780700
00 meter
Y = 4998837
69 meter E =
0009693
Z = -4367094
39 I = 51
96490
XDOT = -5149
600590 Wp = 71
86218
YDOT = 4480
300782 meter/sec RA = 115
45577 deg
ZDOT = 3482
119893 TA = 233
32963
MA = 233
41875
Ha = 222
039 n
mi
Hp = 213
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4606268
59 X = 1369201
22
Y = 16400386
13 feet Y = 5014343
62 meter
Z = -14327737
51 Z = -4360358
65
XDOT = -16895
015059 XDOT = -5216
232066
YDOT = 14699
149546 feet/sec YDOT = 4422
341904 meter/sec
ZDOT = 11424
277863 ZDOT = 3456
943072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5086172
52 X = 1550265
38
Y = -16282851
37 feet Y = -4963013
10 meter
Z = -14299441
88 Z = -4358469
88
XDOT = 21067
027790 XDOT = 6421
230070
YDOT = -3328
801174 feet/sec YDOT = -1014
618598 meter/sec
ZDOT = 11314
302840 ZDOT = 3448
599506
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 16013
10843144
00016717 00000-0 10270-3 0 9070
2 25544 51
6424 116
4049 0006202 9
2171 350
9094 15
54327225 20704
Satellite: ISS
Catalog Number: 25544
Epoch time: 16013
10843144 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 116
4049 deg
Eccentricity:
0006202
Arg of perigee: 9
2171 deg
Mean anomaly: 350
9094 deg
Mean motion: 15
54327225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2070
Checksum: 268
Coasting Arc #9 (Orbit 2085)
---------------------------------------
Vector Time (GMT): 2016/014/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -322050
71 A = 6784677
32 meter
Y = -6029776
26 meter E =
0015243
Z = 3086892
42 I = 51
99098
XDOT = 5160
716636 Wp = 71
62842
YDOT = -2810
342331 meter/sec RA = 110
49171 deg
ZDOT = -4926
611131 TA = 73
08219
MA = 72
91514
Ha = 222
121 n
mi
Hp = 213
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1056596
81 X = -269594
92
Y = -19782730
52 feet Y = -6033084
37 meter
Z = 10127599
79 Z = 3085455
36
XDOT = 16931
485025 XDOT = 5215
690053
YDOT = -9220
283237 feet/sec YDOT = -2752
324376 meter/sec
ZDOT = -16163
422345 ZDOT = -4901
408496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9636800
12 X = -2937296
68
Y = 17312098
99 feet Y = 5276727
77 meter
Z = 10122470
69 Z = 3085329
07
XDOT = -18063
047805 XDOT = -5505
616971
YDOT = -621
047483 feet/sec YDOT = -189
295273 meter/sec
ZDOT = -16053
629380 ZDOT = -4893
146235
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 16014
13713225
00016717 00000-0 10270-3 0 9081
2 25544 51
6422 111
2748 0006284 13
9026 346
2299 15
54341328 20864
Satellite: ISS
Catalog Number: 25544
Epoch time: 16014
13713225 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 111
2748 deg
Eccentricity:
0006284
Arg of perigee: 13
9026 deg
Mean anomaly: 346
2299 deg
Mean motion: 15
54341328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2086
Checksum: 289
Coasting Arc #10 (Orbit 2100)
---------------------------------------
Vector Time (GMT): 2016/015/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -618328
34 A = 6787720
61 meter
Y = 6584773
65 meter E =
0014349
Z = -1495832
46 I = 52
01144
XDOT = -4941
589022 Wp = 28
42297
YDOT = 846
887085 meter/sec RA = 105
53809 deg
ZDOT = 5805
802101 TA = 315
32280
MA = 315
43831
Ha = 222
172 n
mi
Hp = 213
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2028636
28 X = -684648
91
Y = 21603588
08 feet Y = 6577488
26 meter
Z = -4907586
81 Z = -1498997
22
XDOT = -16212
562408 XDOT = -4978
893646
YDOT = 2778
500934 feet/sec YDOT = 791
418402 meter/sec
ZDOT = 19047
907157 ZDOT = 5781
706738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12948493
33 X = 3946700
77
Y = -17407472
30 feet Y = -5305797
56 meter
Z = -4922521
70 Z = -1500384
61
XDOT = 14125
501241 XDOT = 4305
452778
YDOT = 5182
807990 feet/sec YDOT = 1579
719875 meter/sec
ZDOT = 18943
268026 ZDOT = 5773
908094
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 16015
10153079
00016717 00000-0 10270-3 0 9095
2 25544 51
6421 106
4647 0006318 16
0018 344
1333 15
54352627 21018
Satellite: ISS
Catalog Number: 25544
Epoch time: 16015
10153079 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 106
4647 deg
Eccentricity:
0006318
Arg of perigee: 16
0018 deg
Mean anomaly: 344
1333 deg
Mean motion: 15
54352627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2101
Checksum: 267
Coasting Arc #11 (Orbit 2116)
---------------------------------------
Vector Time (GMT): 2016/016/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1484564
36 A = 6788718
90 meter
Y = -6615644
52 meter E =
0010293
Z = -311569
04 I = 52
02188
XDOT = 4547
640899 Wp = 104
80020
YDOT = 1296
619919 meter/sec RA = 100
59189 deg
ZDOT = -6031
337479 TA = 78
53838
MA = 78
42280
Ha = 222
243 n
mi
Hp = 213
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4870617
97 X = 1559945
24
Y = -21704870
48 feet Y = -6598621
66 meter
Z = -1022208
14 Z = -304174
34
XDOT = 14920
081689 XDOT = 4562
101219
YDOT = 4254
002359 feet/sec YDOT = 1347
555483 meter/sec
ZDOT = -19787
852622 ZDOT = -6009
211215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15183248
18 X = -4627854
05
Y = 16259159
14 feet Y = 4955791
71 meter
Z = -988913
49 Z = -301420
83
XDOT = -9645
285428 XDOT = -2939
882998
YDOT = -10170
011675 feet/sec YDOT = -3099
819559 meter/sec
ZDOT = -19692
144683 ZDOT = -6002
165699
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 16016
13021634
00016717 00000-0 10270-3 0 9102
2 25544 51
6418 101
3345 0006160 20
2150 339
9246 15
54323378 21175
Satellite: ISS
Catalog Number: 25544
Epoch time: 16016
13021634 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 101
3345 deg
Eccentricity:
0006160
Arg of perigee: 20
2150 deg
Mean anomaly: 339
9246 deg
Mean motion: 15
54323378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2117
Checksum: 261
Coasting Arc #12 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2016/017/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2204276
41 A = 6786847
51 meter
Y = 6072378
53 meter E =
0018880
Z = 2044873
37 I = 52
02065
XDOT = -4051
016168 Wp = 54
69561
YDOT = -3360
565521 meter/sec RA = 95
64350 deg
ZDOT = 5587
066960 TA = 327
81528
MA = 327
93038
Ha = 222
299 n
mi
Hp = 213
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7231878
00 X = -2281948
49
Y = 19922501
74 feet Y = 6047294
55 meter
Z = 6708902
14 Z = 2033976
98
XDOT = -13290
735459 XDOT = -4040
275858
YDOT = -11025
477430 feet/sec YDOT = -3405
806648 meter/sec
ZDOT = 18330
272180 ZDOT = 5567
414292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16115956
86 X = 4912143
65
Y = -13788728
89 feet Y = -4202804
57 meter
Z = 6660509
98 Z = 2030123
44
XDOT = 5266
814587 XDOT = 1605
325086
YDOT = 15009
895906 feet/sec YDOT = 4575
016272 meter/sec
ZDOT = 18245
677176 ZDOT = 5561
282403
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 16017
15889161
00016717 00000-0 10270-3 0 9113
2 25544 51
6413 96
2032 0006344 22
5504 337
5927 15
54382710 21330
Satellite: ISS
Catalog Number: 25544
Epoch time: 16017
15889161 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 96
2032 deg
Eccentricity:
0006344
Arg of perigee: 22
5504 deg
Mean anomaly: 337
5927 deg
Mean motion: 15
54382710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 287
Coasting Arc #13 (Orbit 2147)
---------------------------------------
Vector Time (GMT): 2016/018/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2861390
63 A = 6783232
15 meter
Y = -5005379
23 meter E =
0010143
Z = -3586488
12 I = 52
01009
XDOT = 3437
035152 Wp = 51
81941
YDOT = 5173
121090 meter/sec RA = 90
68831 deg
ZDOT = -4480
054124 TA = 170
26339
MA = 170
24372
Ha = 222
327 n
mi
Hp = 213
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9387764
54 X = 2934570
90
Y = -16421847
86 feet Y = -4972972
01 meter
Z = -11766693
32 Z = -3572410
62
XDOT = 11276
362047 XDOT = 3400
694680
YDOT = 16972
182055 feet/sec YDOT = 5211
353198 meter/sec
ZDOT = -14698
340302 ZDOT = -4463
446084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16136180
15 X = -4918307
71
Y = 9944150
87 feet Y = 3030977
18 meter
Z = -11704692
90 Z = -3567590
40
XDOT = -1203
318124 XDOT = -366
771364
YDOT = -19159
893314 feet/sec YDOT = -5839
935482 meter/sec
ZDOT = -14627
296593 ZDOT = -4458
400002
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 16018
12326935
00016717 00000-0 10270-3 0 9127
2 25544 51
6407 91
3933 0006325 25
8961 334
2507 15
54372288 21484
Satellite: ISS
Catalog Number: 25544
Epoch time: 16018
12326935 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 91
3933 deg
Eccentricity:
0006325
Arg of perigee: 25
8961 deg
Mean anomaly: 334
2507 deg
Mean motion: 15
54372288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2148
Checksum: 305
Coasting Arc #14 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2016/019/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3412926
79 A = 6779387
76 meter
Y = 3496591
33 meter E =
0010736
Z = 4689530
62 I = 51
99675
XDOT = -2751
249024 Wp = 78
80007
YDOT = -6559
313661 meter/sec RA = 85
72124 deg
ZDOT = 2884
903224 TA = 342
69336
MA = 342
72993
Ha = 222
613 n
mi
Hp = 212
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11197266
36 X = -3474552
48
Y = 11471756
35 feet Y = 3458080
98 meter
Z = 15385599
15 Z = 4672802
01
XDOT = -9026
407560 XDOT = -2691
710229
YDOT = -21520
057943 feet/sec YDOT = -6589
747155 meter/sec
ZDOT = 9464
905592 ZDOT = 2871
682781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15310175
31 X = 4666541
43
Y = -4982597
90 feet Y = -1518695
84 meter
Z = 15312376
66 Z = 4667212
41
XDOT = -2206
821705 XDOT = -672
639256
YDOT = 22169
802660 feet/sec YDOT = 6757
355851 meter/sec
ZDOT = 9408
827538 ZDOT = 2867
810634
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 16019
15193235
00016717 00000-0 10270-3 0 9137
2 25544 51
6408 86
2622 0006503 30
2753 329
8774 15
54361125 21642
Satellite: ISS
Catalog Number: 25544
Epoch time: 16019
15193235 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 86
2622 deg
Eccentricity:
0006503
Arg of perigee: 30
2753 deg
Mean anomaly: 329
8774 deg
Mean motion: 15
54361125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 293
Coasting Arc #15 (Orbit 2178)
---------------------------------------
Vector Time (GMT): 2016/020/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3904855
77 A = 6776836
78 meter
Y = -1714806
41 meter E =
0019229
Z = -5282932
96 I = 51
98422
XDOT = 1943
581247 Wp = 68
10696
YDOT = 7343
798415 meter/sec RA = 80
74451 deg
ZDOT = -942
938438 TA = 192
87324
MA = 192
92240
Ha = 222
442 n
mi
Hp = 212
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12811206
61 X = 3949402
94
Y = -5626005
30 feet Y = -1670890
40 meter
Z = -17332457
22 Z = -5263856
19
XDOT = 6376
578894 XDOT = 1865
896984
YDOT = 24093
826821 feet/sec YDOT = 7365
098514 meter/sec
ZDOT = -3093
630045 ZDOT = -933
685414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14076330
48 X = -4290465
53
Y = -713209
03 feet Y = -217386
11 meter
Z = -17249384
82 Z = -5257612
49
XDOT = 4945
998401 XDOT = 1507
540313
YDOT = -23395
478313 feet/sec YDOT = -7130
941790 meter/sec
ZDOT = -3054
921959 ZDOT = -931
140213
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 16020
11629441
00016717 00000-0 10270-3 0 9149
2 25544 51
6397 81
4517 0006409 33
6142 326
5417 15
54407975 21791
Satellite: ISS
Catalog Number: 25544
Epoch time: 16020
11629441 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 81
4517 deg
Eccentricity:
0006409
Arg of perigee: 33
6142 deg
Mean anomaly: 326
5417 deg
Mean motion: 15
54407975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2179
Checksum: 304
Coasting Arc #16 (Orbit 2194)
---------------------------------------
Vector Time (GMT): 2016/021/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4282171
60 A = 6776960
24 meter
Y = -206548
77 meter E =
0010094
Z = 5243661
04 I = 51
97902
XDOT = -1010
775916 Wp = 44
40709
YDOT = -7524
725887 meter/sec RA = 75
76462 deg
ZDOT = -1113
523569 TA = 56
25563
MA = 56
15949
Ha = 222
632 n
mi
Hp = 212
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14049119
43 X = -4305014
80
Y = -677653
45 feet Y = -254562
85 meter
Z = 17203612
33 Z = 5222804
08
XDOT = -3316
193949 XDOT = -921
148504
YDOT = -24687
420890 feet/sec YDOT = -7535
527857 meter/sec
ZDOT = -3653
292548 ZDOT = -1118
216308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12494902
51 X = 3808446
28
Y = 6694586
61 feet Y = 2040510
00 meter
Z = 17113187
01 Z = 5216099
40
XDOT = -7146
812826 XDOT = -2178
348549
YDOT = 22796
124253 feet/sec YDOT = 6948
258672 meter/sec
ZDOT = -3672
174355 ZDOT = -1119
278743
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 16021
14494160
00016717 00000-0 10270-3 0 9152
2 25544 51
6402 76
3214 0006371 37
4276 322
7319 15
54403905 21959
Satellite: ISS
Catalog Number: 25544
Epoch time: 16021
14494160 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 76
3214 deg
Eccentricity:
0006371
Arg of perigee: 37
4276 deg
Mean anomaly: 322
7319 deg
Mean motion: 15
54403905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2195
Checksum: 285
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