[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 14th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 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
027/19:27:44
236 2
4 2
8 2
8
N/A 1
5 -0
2 222
4
000/00:09:28
472 -0
3 0
0 213
1
Coasting Arc #1 (Orbit 2076)
---------------------------------------
Vector Time (GMT): 2016/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4374325
32 A = 6784740
88 meter
Y = 4236869
48 meter E =
0016177
Z = 2969298
16 I = 51
98500
XDOT = -1895
081762 Wp = 62
82543
YDOT = -5486
160637 meter/sec RA = 113
50966 deg
ZDOT = 5022
628115 TA = 330
97340
MA = 331
06325
Ha = 221
867 n
mi
Hp = 213
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14351461
04 X = -4435801
29
Y = 13900490
42 feet Y = 4187609
10 meter
Z = 9741791
85 Z = 2947899
85
XDOT = -6217
459848 XDOT = -1857
990718
YDOT = -17999
214687 feet/sec YDOT = -5507
145385 meter/sec
ZDOT = 16478
438696 ZDOT = 5013
512421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18226213
56 X = -5555349
89
Y = -8295009
61 feet Y = -2528318
93 meter
Z = 9648239
80 Z = 2940783
49
XDOT = 13808
803349 XDOT = 4208
923261
YDOT = -11166
619065 feet/sec YDOT = -3403
585491 meter/sec
ZDOT = 16439
913494 ZDOT = 5010
885633
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
55829853
00016717 00000-0 10270-3 0 9003
2 25544 51
6425 114
1607 0005774 12
8575 347
2724 15
54444482 20772
Satellite: ISS
Catalog Number: 25544
Epoch time: 16013
55829853 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 114
1607 deg
Eccentricity:
0005774
Arg of perigee: 12
8575 deg
Mean anomaly: 347
2724 deg
Mean motion: 15
54444482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2077
Checksum: 309
Coasting Arc #2 (Orbit 2091)
---------------------------------------
Vector Time (GMT): 2016/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4471706
42 A = 6780690
12 meter
Y = -2754777
47 meter E =
0012585
Z = -4302097
69 I = 51
98298
XDOT = 697
079696 Wp = 47
94033
YDOT = 6731
000451 meter/sec RA = 108
54683 deg
ZDOT = -3584
036380 TA = 185
60476
MA = 185
61886
Ha = 221
840 n
mi
Hp = 213
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14670952
84 X = 4523076
16
Y = -9037983
81 feet Y = -2704484
65 meter
Z = -14114493
72 Z = -4280250
76
XDOT = 2287
006876 XDOT = 639
169673
YDOT = 22083
334814 feet/sec YDOT = 6738
471869 meter/sec
ZDOT = -11758
649541 ZDOT = -3580
790827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14009150
94 X = 4269989
21
Y = 10165875
83 feet Y = 3098558
95 meter
Z = -14019258
19 Z = -4273069
90
XDOT = -18746
485200 XDOT = -5713
928689
YDOT = 9628
873771 feet/sec YDOT = 2934
880725 meter/sec
ZDOT = -11745
809652 ZDOT = -3580
122782
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
52263524
00016717 00000-0 10270-3 0 9019
2 25544 51
6421 109
3517 0005803 15
5722 344
5609 15
54443270 20924
Satellite: ISS
Catalog Number: 25544
Epoch time: 16014
52263524 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 109
3517 deg
Eccentricity:
0005803
Arg of perigee: 15
5722 deg
Mean anomaly: 344
5609 deg
Mean motion: 15
54443270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2092
Checksum: 277
Coasting Arc #3 (Orbit 2107)
---------------------------------------
Vector Time (GMT): 2016/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4340478
67 A = 6777240
42 meter
Y = 952041
77 meter E =
0006770
Z = 5111063
74 I = 51
98150
XDOT = 405
933715 Wp = 67
76919
YDOT = -7464
327226 meter/sec RA = 103
57209 deg
ZDOT = 1735
783205 TA = 5
54996
MA = 5
54247
Ha = 222
008 n
mi
Hp = 213
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14240415
57 X = -4375629
16
Y = 3123496
62 feet Y = 903307
15 meter
Z = 16768581
83 Z = 5089893
59
XDOT = 1331
803526 XDOT = 480
939879
YDOT = -24489
262551 feet/sec YDOT = -7459
368414 meter/sec
ZDOT = 5694
826787 ZDOT = 1737
937323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8594616
66 X = -2619639
16
Y = -11906065
15 feet Y = -3628968
66 meter
Z = 16676605
78 Z = 5083029
44
XDOT = 22100
412351 XDOT = 6736
205684
YDOT = -7965
019229 feet/sec YDOT = -2427
737861 meter/sec
ZDOT = 5705
545844 ZDOT = 1739
050373
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
55124256
00016717 00000-0 10270-3 0 9022
2 25544 51
6422 104
2205 0005911 19
4096 340
7281 15
54506720 21082
Satellite: ISS
Catalog Number: 25544
Epoch time: 16015
55124256 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 104
2205 deg
Eccentricity:
0005911
Arg of perigee: 19
4096 deg
Mean anomaly: 340
7281 deg
Mean motion: 15
54506720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2108
Checksum: 268
Coasting Arc #4 (Orbit 2122)
---------------------------------------
Vector Time (GMT): 2016/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4073060
13 A = 6776329
94 meter
Y = 984184
83 meter E =
0017844
Z = -5339947
86 I = 51
98426
XDOT = -1395
456651 Wp = 73
85443
YDOT = 7521
306717 meter/sec RA = 98
59251 deg
ZDOT = 327
562137 TA = 199
22465
MA = 199
29207
Ha = 222
013 n
mi
Hp = 213
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13363058
15 X = 4087691
02
Y = 3228952
85 feet Y = 1029814
29 meter
Z = -17519513
98 Z = -5320126
54
XDOT = -4578
269853 XDOT = -1481
049188
YDOT = 24676
203139 feet/sec YDOT = 7505
223221 meter/sec
ZDOT = 1074
678927 ZDOT = 320
575504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2656615
46 X = 809736
39
Y = 13599185
20 feet Y = 4145031
65 meter
Z = -17433742
75 Z = -5313804
79
XDOT = -23361
845314 XDOT = -7120
690452
YDOT = 5876
619361 feet/sec YDOT = 1791
193581 meter/sec
ZDOT = 1042
979598 ZDOT = 317
900181
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
51554851
00016717 00000-0 10270-3 0 9038
2 25544 51
6416 99
4111 0006079 22
4824 337
6594 15
54493058 21233
Satellite: ISS
Catalog Number: 25544
Epoch time: 16016
51554851 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 99
4111 deg
Eccentricity:
0006079
Arg of perigee: 22
4824 deg
Mean anomaly: 337
6594 deg
Mean motion: 15
54493058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2123
Checksum: 305
Coasting Arc #5 (Orbit 2138)
---------------------------------------
Vector Time (GMT): 2016/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3658354
85 A = 6777931
40 meter
Y = -2905664
32 meter E =
0012425
Z = 4906593
97 I = 51
99472
XDOT = 2297
005042 Wp = 43
24796
YDOT = -6923
911945 meter/sec RA = 93
61277 deg
ZDOT = -2375
305849 TA = 69
95569
MA = 69
82198
Ha = 222
062 n
mi
Hp = 212
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12002476
56 X = -3649425
13
Y = -9533019
42 feet Y = -2946524
60 meter
Z = 16097749
25 Z = 4888844
32
XDOT = 7536
105781 XDOT = 2385
797379
YDOT = -22716
246540 feet/sec YDOT = -6897
728818 meter/sec
ZDOT = -7792
998192 ZDOT = -2363
932039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3389383
51 X = 1033084
09
Y = -15030127
35 feet Y = -4581182
82 meter
Z = 16021322
82 Z = 4883299
20
XDOT = 22673
415550 XDOT = 6910
857060
YDOT = -3183
396274 feet/sec YDOT = -970
299184 meter/sec
ZDOT = -7742
369213 ZDOT = -2359
874136
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
54412325
00016717 00000-0 10270-3 0 9042
2 25544 51
6421 94
2796 0006153 25
8783 334
2677 15
54564257 21397
Satellite: ISS
Catalog Number: 25544
Epoch time: 16017
54412325 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 94
2796 deg
Eccentricity:
0006153
Arg of perigee: 25
8783 deg
Mean anomaly: 334
2677 deg
Mean motion: 15
54564257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2139
Checksum: 313
Coasting Arc #6 (Orbit 2153)
---------------------------------------
Vector Time (GMT): 2016/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3163786
15 A = 6781604
97 meter
Y = 4552177
78 meter E =
0010108
Z = -3911415
06 I = 52
00753
XDOT = -3085
789375 Wp = 69
10539
YDOT = 5675
767926 meter/sec RA = 88
64313 deg
ZDOT = 4121
663374 TA = 243
87984
MA = 243
98388
Ha = 222
126 n
mi
Hp = 212
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10379875
81 X = 3131647
33
Y = 14934966
47 feet Y = 4587377
74 meter
Z = -12832726
57 Z = -3896124
17
XDOT = -10123
980890 XDOT = -3169
049050
YDOT = 18621
285846 feet/sec YDOT = 5640
794938 meter/sec
ZDOT = 13522
517630 ZDOT = 4106
471377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8698439
06 X = -2651284
23
Y = 16025218
68 feet Y = 4884486
65 meter
Z = -12767280
07 Z = -3891466
97
XDOT = -20053
196802 XDOT = -6112
214385
YDOT = -196
495641 feet/sec YDOT = -59
891871 meter/sec
ZDOT = 13455
550406 ZDOT = 4101
251764
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
50839915
00016717 00000-0 10270-3 0 9058
2 25544 51
6413 89
4701 0006249 31
2447 328
9076 15
54576246 21545
Satellite: ISS
Catalog Number: 25544
Epoch time: 16018
50839915 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 89
4701 deg
Eccentricity:
0006249
Arg of perigee: 31
2447 deg
Mean anomaly: 328
9076 deg
Mean motion: 15
54576246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2154
Checksum: 317
Coasting Arc #7 (Orbit 2169)
---------------------------------------
Vector Time (GMT): 2016/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2525149
56 A = 6785548
76 meter
Y = -5820297
45 meter E =
0016857
Z = 2394615
43 I = 52
01988
XDOT = 3811
357668 Wp = 84
94299
YDOT = -3889
345650 meter/sec RA = 83
68419 deg
ZDOT = -5400
206104 TA = 68
44203
MA = 68
26246
Ha = 222
159 n
mi
Hp = 212
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8284611
40 X = -2471509
82
Y = -19095464
08 feet Y = -5848235
53 meter
Z = 7856349
85 Z = 2382479
00
XDOT = 12504
454291 XDOT = 3880
797732
YDOT = -12760
320373 feet/sec YDOT = -3846
336035 meter/sec
ZDOT = -17717
211626 ZDOT = -5381
523101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13094532
23 X = 3991213
42
Y = -16205293
62 feet Y = -4939373
49 meter
Z = 7804835
17 Z = 2378913
76
XDOT = 15962
648827 XDOT = 4865
415363
YDOT = 4350
719926 feet/sec YDOT = 1326
099434 meter/sec
ZDOT = -17635
432509 ZDOT = -5375
279829
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
53694244
00016717 00000-0 10270-3 0 9067
2 25544 51
6419 84
3387 0006441 33
6855 326
4706 15
54604598 21701
Satellite: ISS
Catalog Number: 25544
Epoch time: 16019
53694244 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 84
3387 deg
Eccentricity:
0006441
Arg of perigee: 33
6855 deg
Mean anomaly: 326
4706 deg
Mean motion: 15
54604598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2170
Checksum: 322
Coasting Arc #8 (Orbit 2184)
---------------------------------------
Vector Time (GMT): 2016/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1794337
00 A = 6787926
39 meter
Y = 6507953
38 meter E =
0017355
Z = -625703
09 I = 52
02255
XDOT = -4425
402320 Wp = 39
19513
YDOT = 1787
733455 meter/sec RA = 78
73499 deg
ZDOT = 6006
994318 TA = 314
08113
MA = 314
22387
Ha = 222
354 n
mi
Hp = 212
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5886932
43 X = 1724469
47
Y = 21351553
08 feet Y = 6527628
22 meter
Z = -2052831
68 Z = -617156
11
XDOT = -14519
036483 XDOT = -4474
243394
YDOT = 5865
267241 feet/sec YDOT = 1737
972287 meter/sec
ZDOT = 19707
986609 ZDOT = 5985
378495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15958168
98 X = -4864049
91
Y = 15363181
69 feet Y = 4682697
78 meter
Z = -2017027
81 Z = -614790
08
XDOT = -11017
691153 XDOT = -3358
192263
YDOT = -8914
665680 feet/sec YDOT = -2717
190099 meter/sec
ZDOT = 19613
884146 ZDOT = 5978
311888
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
50118779
00016717 00000-0 10270-3 0 9071
2 25544 51
6416 79
5286 0006606 36
8938 323
2668 15
54556203 21859
Satellite: ISS
Catalog Number: 25544
Epoch time: 16020
50118779 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 79
5286 deg
Eccentricity:
0006606
Arg of perigee: 36
8938 deg
Mean anomaly: 323
2668 deg
Mean motion: 15
54556203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2185
Checksum: 324
Coasting Arc #9 (Orbit 2200)
---------------------------------------
Vector Time (GMT): 2016/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -880689
05 A = 6787143
43 meter
Y = -6607260
14 meter E =
0010138
Z = -1279355
91 I = 52
01412
XDOT = 4908
156060 Wp = 101
97748
YDOT = 473
648696 meter/sec RA = 73
78793 deg
ZDOT = -5866
063153 TA = 91
85904
MA = 91
74293
Ha = 222
286 n
mi
Hp = 212
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2889399
76 X = -800525
11
Y = -21677362
66 feet Y = -6616660
30 meter
Z = -4197361
93 Z = -1283439
66
XDOT = 16102
874212 XDOT = 4930
989226
YDOT = 1553
965538 feet/sec YDOT = 528
662918 meter/sec
ZDOT = -19245
614020 ZDOT = -5842
165411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17469240
02 X = 5324624
36
Y = -13150827
25 feet Y = -4008372
14 meter
Z = -4213778
07 Z = -1284359
56
XDOT = 5667
265253 XDOT = 1727
382449
YDOT = 13618
601413 feet/sec YDOT = 4150
949711 meter/sec
ZDOT = -19142
049787 ZDOT = -5834
496775
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
52969997
00016717 00000-0 10270-3 0 9081
2 25544 51
6420 74
3970 0006641 42
0677 318
0985 15
54637472 22016
Satellite: ISS
Catalog Number: 25544
Epoch time: 16021
52969997 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 74
3970 deg
Eccentricity:
0006641
Arg of perigee: 42
0677 deg
Mean anomaly: 318
0985 deg
Mean motion: 15
54637472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2201
Checksum: 321
Coasting Arc #10 (Orbit 2216)
---------------------------------------
Vector Time (GMT): 2016/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -145715
11 A = 6784085
83 meter
Y = 6079779
89 meter E =
0019046
Z = 2982908
23 I = 51
99323
XDOT = -5204
480035 Wp = 70
37444
YDOT = -2593
541257 meter/sec RA = 68
83449 deg
ZDOT = 5012
260450 TA = 323
60437
MA = 323
73371
Ha = 222
429 n
mi
Hp = 211
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -478067
93 X = -228179
29
Y = 19946784
42 feet Y = 6077689
18 meter
Z = 9786444
32 Z = 2982000
39
XDOT = -17075
065730 XDOT = -5199
438573
YDOT = -8508
993625 feet/sec YDOT = -2651
713241 meter/sec
ZDOT = 16444
424047 ZDOT = 4986
990967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17472804
60 X = -5325710
84
Y = 9638694
31 feet Y = 2937874
02 meter
Z = 9781304
70 Z = 2981341
67
XDOT = -665
117411 XDOT = -202
727787
YDOT = -17848
250858 feet/sec YDOT = -5440
146862 meter/sec
ZDOT = 16335
324632 ZDOT = 4979
006948
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 16022
55819605
00016717 00000-0 10270-3 0 9096
2 25544 51
6412 69
2657 0006783 46
3453 313
8261 15
54634656 22176
Satellite: ISS
Catalog Number: 25544
Epoch time: 16022
55819605 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 69
2657 deg
Eccentricity:
0006783
Arg of perigee: 46
3453 deg
Mean anomaly: 313
8261 deg
Mean motion: 15
54634656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2217
Checksum: 316
Coasting Arc #11 (Orbit 2231)
---------------------------------------
Vector Time (GMT): 2016/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1328076
94 A = 6779746
47 meter
Y = -5033979
83 meter E =
0015217
Z = -4358831
35 I = 51
96753
XDOT = 5202
319721 Wp = 60
71574
YDOT = 4397
177077 meter/sec RA = 63
86830 deg
ZDOT = -3495
128755 TA = 173
87212
MA = 173
85349
Ha = 222
370 n
mi
Hp = 211
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4357207
80 X = 1405442
31
Y = -16515681
87 feet Y = -5018695
67 meter
Z = -14300627
79 Z = -4352192
29
XDOT = 17067
978088 XDOT = 5169
740229
YDOT = 14426
433980 feet/sec YDOT = 4455
170816 meter/sec
ZDOT = -11466
957856 ZDOT = -3469
936701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16414210
17 X = 5003051
26
Y = -4814366
17 feet Y = -1467418
81 meter
Z = -14270828
48 Z = -4349748
52
XDOT = -3724
774869 XDOT = -1135
311380
YDOT = 20950
977883 feet/sec YDOT = 6385
858059 meter/sec
ZDOT = -11358
551901 ZDOT = -3462
086619
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 16023
52239531
00016717 00000-0 10270-3 0 9100
2 25544 51
6420 64
4546 0006743 49
8994 310
2750 15
54672219 22321
Satellite: ISS
Catalog Number: 25544
Epoch time: 16023
52239531 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 64
4546 deg
Eccentricity:
0006743
Arg of perigee: 49
8994 deg
Mean anomaly: 310
2750 deg
Mean motion: 15
54672219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2232
Checksum: 295
Coasting Arc #12 (Orbit 2247)
---------------------------------------
Vector Time (GMT): 2016/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2553759
43 A = 6776426
24 meter
Y = 3574286
92 meter E =
0009495
Z = 5151323
42 I = 51
94060
XDOT = -4874
673915 Wp = 81
56563
YDOT = -5723
364746 meter/sec RA = 58
88934 deg
ZDOT = 1553
513915 TA = 353
53529
MA = 353
54753
Ha = 222
516 n
mi
Hp = 211
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8378475
81 X = -2618560
52
Y = 11726663
13 feet Y = 3545366
69 meter
Z = 16900667
37 Z = 5138760
84
XDOT = -15993
024656 XDOT = -4817
857674
YDOT = -18777
443393 feet/sec YDOT = -5777
558924 meter/sec
ZDOT = 5096
830430 ZDOT = 1529
972417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14450019
12 X = -4404365
83
Y = -879484
03 feet Y = -268066
73 meter
Z = 16845459
27 Z = 5134495
99
XDOT = 7199
985762 XDOT = 2194
555660
YDOT = -22539
103630 feet/sec YDOT = -6869
918786 meter/sec
ZDOT = 4995
850913 ZDOT = 1522
735358
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 16024
55085831
00016717 00000-0 10270-3 0 9117
2 25544 51
6408 59
3228 0006866 53
6378 306
5408 15
54706069 22488
Satellite: ISS
Catalog Number: 25544
Epoch time: 16024
55085831 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 59
3228 deg
Eccentricity:
0006866
Arg of perigee: 53
6378 deg
Mean anomaly: 306
5408 deg
Mean motion: 15
54706069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2248
Checksum: 319
Coasting Arc #13 (Orbit 2262)
---------------------------------------
Vector Time (GMT): 2016/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3762896
96 A = 6775813
31 meter
Y = -1911375
58 meter E =
0020460
Z = -5318086
19 I = 51
92217
XDOT = 4107
771095 Wp = 82
58699
YDOT = 6431
148201 meter/sec RA = 53
90279 deg
ZDOT = 599
637412 TA = 193
09772
MA = 193
15093
Ha = 222
426 n
mi
Hp = 211
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12345462
47 X = 3809823
14
Y = -6270917
25 feet Y = -1869034
02 meter
Z = -17447789
34 Z = -5299693
42
XDOT = 13476
939289 XDOT = 4032
638402
YDOT = 21099
567590 feet/sec YDOT = 6476
663929 meter/sec
ZDOT = 1967
314344 ZDOT = 619
408956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12093177
14 X = 3686000
39
Y = 6948452
98 feet Y = 2117888
47 meter
Z = -17367621
23 Z = -5293650
95
XDOT = -9699
570748 XDOT = -2956
429164
YDOT = 21972
305896 feet/sec YDOT = 6697
158837 meter/sec
ZDOT = 2051
794372 ZDOT = 625
386925
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 16025
51502811
00016717 00000-0 10270-3 0 9127
2 25544 51
6419 54
5116 0006819 56
3846 303
7956 15
54704201 22631
Satellite: ISS
Catalog Number: 25544
Epoch time: 16025
51502811 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 54
5116 deg
Eccentricity:
0006819
Arg of perigee: 56
3846 deg
Mean anomaly: 303
7956 deg
Mean motion: 15
54704201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2263
Checksum: 292
Coasting Arc #14 (Orbit 2278)
---------------------------------------
Vector Time (GMT): 2016/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4808324
54 A = 6777933
65 meter
Y = 169767
87 meter E =
0014675
Z = 4766053
28 I = 51
90889
XDOT = -2918
872421 Wp = 61
01288
YDOT = -6565
745400 meter/sec RA = 48
91682 deg
ZDOT = -2697
695677 TA = 55
58226
MA = 55
44362
Ha = 222
542 n
mi
Hp = 211
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15775342
96 X = -4833016
48
Y = 556981
19 feet Y = 115860
05 meter
Z = 15636657
75 Z = 4742636
19
XDOT = -9576
353086 XDOT = -2832
131748
YDOT = -21541
159448 feet/sec YDOT = -6597
901235 meter/sec
ZDOT = -8850
707601 ZDOT = -2711
663673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9425009
06 X = -2872742
76
Y = -12787036
68 feet Y = -3897488
78 meter
Z = 15535045
43 Z = 4735081
85
XDOT = 11471
554363 XDOT = 3496
529770
YDOT = -19333
110978 feet/sec YDOT = -5892
732226 meter/sec
ZDOT = -8909
980203 ZDOT = -2715
761966
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 16026
54345876
00016717 00000-0 10270-3 0 9138
2 25544 51
6405 49
3790 0006962 60
2756 299
9089 15
54768575 22793
Satellite: ISS
Catalog Number: 25544
Epoch time: 16026
54345876 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 49
3790 deg
Eccentricity:
0006962
Arg of perigee: 60
2756 deg
Mean anomaly: 299
9089 deg
Mean motion: 15
54768575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2279
Checksum: 355
Coasting Arc #15 (Orbit 2293)
---------------------------------------
Vector Time (GMT): 2016/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5558492
21 A = 6781972
65 meter
Y = 1402607
48 meter E =
0011846
Z = -3631319
49 I = 51
90177
XDOT = 1339
737042 Wp = 77
80679
YDOT = 6109
488272 meter/sec RA = 43
94051 deg
ZDOT = 4425
154649 TA = 239
35099
MA = 239
46782
Ha = 222
500 n
mi
Hp = 211
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18236523
00 X = 5560033
83
Y = 4601730
58 feet Y = 1464774
70 meter
Z = -11913777
84 Z = -3604314
57
XDOT = 4395
462735 XDOT = 1249
824597
YDOT = 20044
252861 feet/sec YDOT = 6123
967543 meter/sec
ZDOT = 14518
223913 ZDOT = 4431
444004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6846999
64 X = 2086965
49
Y = 17596476
81 feet Y = 5363406
13 meter
Z = -11796923
23 Z = -3595702
20
XDOT = -12573
873990 XDOT = -3832
516792
YDOT = 14610
897469 feet/sec YDOT = 4453
401548 meter/sec
ZDOT = 14544
274830 ZDOT = 4433
094968
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 16027
50759842
00016717 00000-0 10270-3 0 9148
2 25544 51
6416 44
5681 0007027 63
6294 296
5579 15
54772694 22949
Satellite: ISS
Catalog Number: 25544
Epoch time: 16027
50759842 = yrday
fracday
Element set: 914
Inclination: 51
6416 deg
RA of node: 44
5681 deg
Eccentricity:
0007027
Arg of perigee: 63
6294 deg
Mean anomaly: 296
5579 deg
Mean motion: 15
54772694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2294
Checksum: 341
Coasting Arc #16 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2016/027/19:32:28
472
Vector Time (MET): N/A
Weight (LBS) : 922190
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3427335
59 A = 6777182
58 meter
Y = -2502840
38 meter E =
0018473
Z = -5299617
91 I = 51
87450
XDOT = 5212
259032 Wp = 85
90566
YDOT = 5556
230292 meter/sec RA = 42
39626 deg
ZDOT = 750
344292 TA = 191
23130
MA = 191
27259
Ha = 222
402 n
mi
Hp = 213
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11244539
32 X = 3480811
01
Y = -8211418
58 feet Y = -2464214
87 meter
Z = -17387197
88 Z = -5282839
10
XDOT = 17100
587376 XDOT = 5146
095731
YDOT = 18229
102009 feet/sec YDOT = 5614
147317 meter/sec
ZDOT = 2461
759487 ZDOT = 775
502723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1140607
92 X = -347657
29
Y = -13968145
40 feet Y = -4257490
72 meter
Z = -17313914
56 Z = -5277281
16
XDOT = 23425
040232 XDOT = 7139
952263
YDOT = -5083
698097 feet/sec YDOT = -1549
511180 meter/sec
ZDOT = 2569
765885 ZDOT = 783
264642
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 16027
82897720
00016717 00000-0 10270-3 0 9152
2 25544 51
6425 42
9638 0004813 55
3156 304
8450 15
54258561 22996
Satellite: ISS
Catalog Number: 25544
Epoch time: 16027
82897720 = yrday
fracday
Element set: 915
Inclination: 51
6425 deg
RA of node: 42
9638 deg
Eccentricity:
0004813
Arg of perigee: 55
3156 deg
Mean anomaly: 304
8450 deg
Mean motion: 15
54258561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 322
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