[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 1st 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
245/12:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
4
000/00:00:00
000 0
0 0
0 215
4
246/19:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 215
4
250/21:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 215
1
250/21:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 215
2
254/00:41:11
035 3
1 3
6 3
6
N/A -1
3 0
0 220
0
000/00:10:18
071 -1
3 -0
0 217
0
257/20:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 216
9
Coasting Arc #1 (Orbit 1669)
---------------------------------------
Vector Time (GMT): 2016/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5524215
17 A = 6788159
20 meter
Y = -3787980
63 meter E =
0011063
Z = 1063521
04 I = 51
90678
XDOT = 1930
801838 Wp = 132
30639
YDOT = -4485
275399 meter/sec RA = 41
58860 deg
ZDOT = -5914
329082 TA = 36
20038
MA = 36
12555
Ha = 219
471 n
mi
Hp = 215
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18124065
52 X = -5486612
48
Y = -12427757
98 feet Y = -3849545
76 meter
Z = 3489242
26 Z = 1036777
89
XDOT = 6334
651699 XDOT = 2009
542621
YDOT = -14715
470468 feet/sec YDOT = -4463
244138 meter/sec
ZDOT = -19403
966803 ZDOT = -5904
758237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12563715
63 X = 3829420
52
Y = 18052182
78 feet Y = 5502305
31 meter
Z = 3373051
66 Z = 1028106
15
XDOT = -9940
397396 XDOT = -3029
833126
YDOT = 10556
088742 feet/sec YDOT = 3217
495848 meter/sec
ZDOT = -19361
279253 ZDOT = -5901
317916
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 16244
53416214
00016717 00000-0 10270-3 0 9000
2 25544 51
6390 42
0660 0003140 271
3704 88
7089 15
54377339 16707
Satellite: ISS
Catalog Number: 25544
Epoch time: 16244
53416214 = yrday
fracday
Element set: 900
Inclination: 51
6390 deg
RA of node: 42
0660 deg
Eccentricity:
0003140
Arg of perigee: 271
3704 deg
Mean anomaly: 88
7089 deg
Mean motion: 15
54377339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1670
Checksum: 291
Coasting Arc #2 (Orbit 1685)
---------------------------------------
Vector Time (GMT): 2016/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5055729
89 A = 6788358
03 meter
Y = 4463179
05 meter E =
0011049
Z = 719763
41 I = 51
88500
XDOT = -3632
867910 Wp = 42
79541
YDOT = 3143
633328 meter/sec RA = 36
63492 deg
ZDOT = 5978
669632 TA = 324
95665
MA = 325
02930
Ha = 219
488 n
mi
Hp = 215
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16587040
33 X = 5001949
49
Y = 14642975
89 feet Y = 4519414
98 meter
Z = 2361428
52 Z = 744191
45
XDOT = -11918
857971 XDOT = -3696
792216
YDOT = 10313
757637 feet/sec YDOT = 3102
651369 meter/sec
ZDOT = 19615
057847 ZDOT = 5960
866724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10640837
95 X = -3243327
41
Y = -19385759
84 feet Y = -5908779
60 meter
Z = 2467362
48 Z = 752052
08
XDOT = 13411
271231 XDOT = 4087
755471
YDOT = -4856
568619 feet/sec YDOT = -1480
282115 meter/sec
ZDOT = 19536
640830 ZDOT = 5954
768125
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 16245
56284266
00016717 00000-0 10270-3 0 9015
2 25544 51
6411 36
9361 0003063 271
5798 88
5004 15
54380977 16864
Satellite: ISS
Catalog Number: 25544
Epoch time: 16245
56284266 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 36
9361 deg
Eccentricity:
0003063
Arg of perigee: 271
5798 deg
Mean anomaly: 88
5004 deg
Mean motion: 15
54380977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1686
Checksum: 323
Coasting Arc #3 (Orbit 1685)
---------------------------------------
Vector Time (GMT): 2016/245/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3698371
44 A = 6786027
07 meter
Y = 5133774
72 meter E =
0010787
Z = 2437876
11 I = 51
87700
XDOT = -5329
160109 Wp = 69
64066
YDOT = 1284
077297 meter/sec RA = 36
63138 deg
ZDOT = 5365
005423 TA = 317
55464
MA = 317
63801
Ha = 219
439 n
mi
Hp = 215
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12133764
56 X = 3628847
41
Y = 16843092
92 feet Y = 5174743
91 meter
Z = 7998281
19 Z = 2455672
22
XDOT = -17484
121094 XDOT = -5369
183442
YDOT = 4212
852025 feet/sec YDOT = 1224
259837 meter/sec
ZDOT = 17601
723830 ZDOT = 5339
020714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6106228
92 X = -1861178
58
Y = -19809020
16 feet Y = -6037789
34 meter
Z = 8075098
27 Z = 2461289
95
XDOT = 16580
447615 XDOT = 5053
720433
YDOT = 2038
448948 feet/sec YDOT = 621
319239 meter/sec
ZDOT = 17487
895044 ZDOT = 5330
310409
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 16245
56284263
00016717 00000-0 10270-3 0 9023
2 25544 51
6409 36
9361 0003117 271
7871 88
2925 15
54381347 16866
Satellite: ISS
Catalog Number: 25544
Epoch time: 16245
56284263 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 36
9361 deg
Eccentricity:
0003117
Arg of perigee: 271
7871 deg
Mean anomaly: 88
2925 deg
Mean motion: 15
54381347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1686
Checksum: 323
Coasting Arc #4 (Orbit 1700)
---------------------------------------
Vector Time (GMT): 2016/246/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2358323
15 A = 6782169
59 meter
Y = -5039399
28 meter E =
0003917
Z = -3882812
20 I = 51
83840
XDOT = 6451
714907 Wp = 55
28124
YDOT = 163
943397 meter/sec RA = 31
66411 deg
ZDOT = -4132
170734 TA = 171
42455
MA = 171
41786
Ha = 219
518 n
mi
Hp = 215
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7737280
67 X = -2282935
20
Y = -16533462
21 feet Y = -5065350
56 meter
Z = -12738885
16 Z = -3894084
53
XDOT = 21167
043659 XDOT = 6469
474243
YDOT = 537
872039 feet/sec YDOT = 236
189615 meter/sec
ZDOT = -13556
990598 ZDOT = -4100
787137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2317842
49 X = 706478
39
Y = 18072500
65 feet Y = 5508498
20 meter
Z = -12787196
97 Z = -3897537
64
XDOT = -18787
290391 XDOT = -5726
366111
YDOT = -7083
886312 feet/sec YDOT = -2159
168548 meter/sec
ZDOT = -13419
846566 ZDOT = -4090
369233
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 16246
52722539
00016717 00000-0 10270-3 0 9034
2 25544 51
6417 32
1273 0003023 278
6349 81
4461 15
54376705 17017
Satellite: ISS
Catalog Number: 25544
Epoch time: 16246
52722539 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 32
1273 deg
Eccentricity:
0003023
Arg of perigee: 278
6349 deg
Mean anomaly: 81
4461 deg
Mean motion: 15
54376705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1701
Checksum: 295
Coasting Arc #5 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2016/246/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 429125
38 A = 6777491
06 meter
Y = -4415482
05 meter E =
0010926
Z = -5133610
82 I = 51
81592
XDOT = 7026
160220 Wp = 70
44163
YDOT = 2580
096299 meter/sec RA = 30
03239 deg
ZDOT = -1631
105440 TA = 183
83733
MA = 183
84572
Ha = 219
574 n
mi
Hp = 215
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1407891
66 X = 503405
16
Y = -14486489
68 feet Y = -4410268
57 meter
Z = -16842555
20 Z = -5131345
32
XDOT = 23051
706759 XDOT = 7004
709865
YDOT = 8464
882870 feet/sec YDOT = 2658
547401 meter/sec
ZDOT = -5351
395799 ZDOT = -1597
026841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14525940
69 X = 4427506
72
Y = -1095147
71 feet Y = -333801
02 meter
Z = -16831812
33 Z = -5130336
40
XDOT = -4285
046917 XDOT = -1306
082300
YDOT = 23167
157074 feet/sec YDOT = 7061
349476 meter/sec
ZDOT = -5202
936033 ZDOT = -1585
854903
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 16246
84868432
00016717 00000-0 10270-3 0 9043
2 25544 51
6439 30
5281 0003051 284
5238 75
5576 15
54367614 17061
Satellite: ISS
Catalog Number: 25544
Epoch time: 16246
84868432 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 30
5281 deg
Eccentricity:
0003051
Arg of perigee: 284
5238 deg
Mean anomaly: 75
5576 deg
Mean motion: 15
54367614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1706
Checksum: 318
Coasting Arc #6 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2016/247/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2172345
60 A = 6776661
56 meter
Y = 3602619
61 meter E =
0001898
Z = 5313037
91 I = 51
78316
XDOT = -6802
472172 Wp = 353
21518
YDOT = -3519
585553 meter/sec RA = 25
04155 deg
ZDOT = -392
975985 TA = 100
53496
MA = 100
51358
Ha = 219
735 n
mi
Hp = 215
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7127118
10 X = -2238277
85
Y = 11819618
15 feet Y = 3577958
98 meter
Z = 17431226
72 Z = 5302324
68
XDOT = -22317
822088 XDOT = -6760
700803
YDOT = -11547
196696 feet/sec YDOT = -3595
421844 meter/sec
ZDOT = -1289
291291 ZDOT = -425
918617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13008411
84 X = -3964963
93
Y = -4788994
53 feet Y = -1459685
53 meter
Z = 17383716
62 Z = 5298556
83
XDOT = 6613
901662 XDOT = 2015
917227
YDOT = -23187
439342 feet/sec YDOT = -7067
531512 meter/sec
ZDOT = -1432
593201 ZDOT = -436
654408
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 16247
87735221
00016717 00000-0 10270-3 0 9057
2 25544 51
6422 25
3987 0002922 290
4489 69
6349 15
54385639 17225
Satellite: ISS
Catalog Number: 25544
Epoch time: 16247
87735221 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 25
3987 deg
Eccentricity:
0002922
Arg of perigee: 290
4489 deg
Mean anomaly: 69
6349 deg
Mean motion: 15
54385639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 336
Coasting Arc #7 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2016/248/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3833237
21 A = 6778563
57 meter
Y = -2709848
92 meter E =
0008719
Z = -4898076
73 I = 51
76082
XDOT = 5974
830930 Wp = 104
39939
YDOT = 4169
323795 meter/sec RA = 20
05064 deg
ZDOT = 2370
653151 TA = 188
79298
MA = 188
80827
Ha = 219
677 n
mi
Hp = 215
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12576237
56 X = 3887047
22
Y = -8890580
43 feet Y = -2666682
79 meter
Z = -16069805
55 Z = -4879324
86
XDOT = 19602
463682 XDOT = 5916
248847
YDOT = 13678
883841 feet/sec YDOT = 4235
811083 meter/sec
ZDOT = 7777
733434 ZDOT = 2399
534531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11381667
50 X = 3469132
25
Y = 10502641
95 feet Y = 3201205
27 meter
Z = -15987338
08 Z = -4872940
65
XDOT = -8450
166729 XDOT = -2575
610819
YDOT = 21180
637520 feet/sec YDOT = 6455
858316 meter/sec
ZDOT = 7903
148381 ZDOT = 2408
879627
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 16248
84172233
00016717 00000-0 10270-3 0 9064
2 25544 51
6434 20
5905 0003178 294
1989 65
8832 15
54372000 17374
Satellite: ISS
Catalog Number: 25544
Epoch time: 16248
84172233 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 20
5905 deg
Eccentricity:
0003178
Arg of perigee: 294
1989 deg
Mean anomaly: 65
8832 deg
Mean motion: 15
54372000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1737
Checksum: 312
Coasting Arc #8 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2016/249/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5250509
79 A = 6782098
80 meter
Y = 1775028
01 meter E =
0009083
Z = 3904162
75 I = 51
74169
XDOT = -4597
097469 Wp = 68
15679
YDOT = -4577
639865 meter/sec RA = 15
06506 deg
ZDOT = -4090
249320 TA = 64
67149
MA = 64
57744
Ha = 219
780 n
mi
Hp = 215
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17226081
97 X = -5288933
11
Y = 5823582
72 feet Y = 1716098
88 meter
Z = 12808932
92 Z = 3878563
57
XDOT = -15082
340777 XDOT = -4525
698800
YDOT = -15018
503493 feet/sec YDOT = -4628
648923 meter/sec
ZDOT = -13419
453148 ZDOT = -4112
406945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9635451
00 X = -2936885
47
Y = -15513605
11 feet Y = -4728546
84 meter
Z = 12696728
67 Z = 3869962
90
XDOT = 10053
231045 XDOT = 3064
224822
YDOT = -17334
977012 feet/sec YDOT = -5283
700993 meter/sec
ZDOT = -13515
395284 ZDOT = -4119
492483
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 16249
87037669
00016717 00000-0 10270-3 0 9072
2 25544 51
6425 15
4607 0003153 301
4452 58
6392 15
54430087 17535
Satellite: ISS
Catalog Number: 25544
Epoch time: 16249
87037669 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 15
4607 deg
Eccentricity:
0003153
Arg of perigee: 301
4452 deg
Mean anomaly: 58
6392 deg
Mean motion: 15
54430087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 311
Coasting Arc #9 (Orbit 1767)
---------------------------------------
Vector Time (GMT): 2016/250/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6253426
42 A = 6785954
09 meter
Y = -873711
88 meter E =
0005661
Z = -2478395
67 I = 51
72235
XDOT = 2774
223215 Wp = 15
45658
YDOT = 4764
425434 meter/sec RA = 10
08983 deg
ZDOT = 5328
369902 TA = 316
80502
MA = 316
84941
Ha = 219
861 n
mi
Hp = 215
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20516490
88 X = 6274770
72
Y = -2866508
81 feet Y = -803662
79 meter
Z = -8131219
38 Z = -2447966
11
XDOT = 9101
782203 XDOT = 2694
857044
YDOT = 15631
317041 feet/sec YDOT = 4795
005426 meter/sec
ZDOT = 17481
528551 ZDOT = 5341
653158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7835560
62 X = 2388278
88
Y = 19232642
71 feet Y = 5862109
50 meter
Z = -7998090
00 Z = -2437817
83
XDOT = -11541
074434 XDOT = -3517
719487
YDOT = 11984
294587 feet/sec YDOT = 3652
812990 meter/sec
ZDOT = 17538
648319 ZDOT = 5345
780007
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 16250
83473618
00016717 00000-0 10270-3 0 9089
2 25544 51
6417 10
6527 0003051 305
1526 54
9340 15
54421270 17686
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
83473618 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 10
6527 deg
Eccentricity:
0003051
Arg of perigee: 305
1526 deg
Mean anomaly: 54
9340 deg
Mean motion: 15
54421270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 289
Coasting Arc #10 (Orbit 1768)
---------------------------------------
Vector Time (GMT): 2016/250/21:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2223427
38 A = 6778700
36 meter
Y = -4241679
87 meter E =
0009979
Z = -4806888
56 I = 51
69528
XDOT = 7164
075198 Wp = 56
58940
YDOT = -824
035211 meter/sec RA = 9
88729 deg
ZDOT = -2585
111026 TA = 187
93348
MA = 187
94927
Ha = 219
814 n
mi
Hp = 215
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7294709
26 X = -2152480
75
Y = -13916272
54 feet Y = -4266147
52 meter
Z = -15770631
77 Z = -4817516
69
XDOT = 23504
183722 XDOT = 7185
314698
YDOT = -2703
527596 feet/sec YDOT = -743
803223 meter/sec
ZDOT = -8481
335387 ZDOT = -2550
258017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8043395
08 X = 2451626
82
Y = -13443892
77 feet Y = -4097698
51 meter
Z = -15816250
95 Z = -4820793
29
XDOT = 13725
363552 XDOT = 4183
490811
YDOT = 18016
169145 feet/sec YDOT = 5491
328355 meter/sec
ZDOT = -8328
887955 ZDOT = -2538
645049
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 16250
89902732
00016717 00000-0 10270-3 0 9090
2 25544 51
6404 10
3311 0003184 305
7719 54
3138 15
54400083 17696
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
89902732 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 10
3311 deg
Eccentricity:
0003184
Arg of perigee: 305
7719 deg
Mean anomaly: 54
3138 deg
Mean motion: 15
54400083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1769
Checksum: 290
Coasting Arc #11 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2016/250/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 894307
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1926597
71 A = 6778205
12 meter
Y = 4261108
74 meter E =
0003247
Z = 4904755
28 I = 51
69308
XDOT = -7283
545418 Wp = 118
67734
YDOT = 614
721685 meter/sec RA = 9
72352 deg
ZDOT = 2324
250042 TA = 308
59172
MA = 308
62079
Ha = 219
693 n
mi
Hp = 215
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6320858
63 X = 1854980
49
Y = 13980015
54 feet Y = 4282253
29 meter
Z = 16091716
79 Z = 4913939
85
XDOT = -23896
146383 XDOT = -7301
168288
YDOT = 2016
803428 feet/sec YDOT = 533
173895 meter/sec
ZDOT = 7625
492265 ZDOT = 2288
825481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5847533
09 X = -1782328
09
Y = 14139796
41 feet Y = 4309809
95 meter
Z = 16131024
51 Z = 4916736
27
XDOT = -16931
899589 XDOT = -5160
842995
YDOT = -15534
880199 feet/sec YDOT = -4735
031485 meter/sec
ZDOT = 7470
588254 ZDOT = 2277
035300
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 16250
96331737
00016717 00000-0 10270-3 0 9101
2 25544 51
6407 10
0109 0003355 304
5172 55
5664 15
54423841 17707
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
96331737 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 10
0109 deg
Eccentricity:
0003355
Arg of perigee: 304
5172 deg
Mean anomaly: 55
5664 deg
Mean motion: 15
54423841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 282
Coasting Arc #12 (Orbit 1784)
---------------------------------------
Vector Time (GMT): 2016/251/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 894307
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -23060
81 A = 6776551
64 meter
Y = -4219232
45 meter E =
0012545
Z = -5313462
96 I = 51
65568
XDOT = 7643
937741 Wp = 77
33902
YDOT = 372
335615 meter/sec RA = 4
72436 deg
ZDOT = -326
799531 TA = 189
53081
MA = 189
55464
Ha = 219
845 n
mi
Hp = 215
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -75658
83 X = 49932
01
Y = -13842626
16 feet Y = -4219082
68 meter
Z = -17432621
26 Z = -5313397
32
XDOT = 25078
535895 XDOT = 7640
793530
YDOT = 1221
573541 feet/sec YDOT = 457
797639 meter/sec
ZDOT = -1072
176939 ZDOT = -289
674785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9892530
98 X = 3015243
44
Y = -9685058
84 feet Y = -2952005
93 meter
Z = -17431516
67 Z = -5313126
28
XDOT = 16019
970197 XDOT = 4882
886916
YDOT = 18013
093189 feet/sec YDOT = 5490
390804 meter/sec
ZDOT = -910
045422 ZDOT = -277
381845
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 16251
92767008
00016717 00000-0 10270-3 0 9113
2 25544 51
6410 5
2014 0003310 309
1940 50
8919 15
54413441 17859
Satellite: ISS
Catalog Number: 25544
Epoch time: 16251
92767008 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 5
2014 deg
Eccentricity:
0003310
Arg of perigee: 309
1940 deg
Mean anomaly: 50
8919 deg
Mean motion: 15
54413441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1785
Checksum: 276
Coasting Arc #13 (Orbit 1800)
---------------------------------------
Vector Time (GMT): 2016/252/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 894307
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1917167
65 A = 6777493
74 meter
Y = 4041076
96 meter E =
0005726
Z = 5091792
37 I = 51
62744
XDOT = -7357
051477 Wp = 19
00919
YDOT = -1322
211067 meter/sec RA = 359
72225 deg
ZDOT = -1714
879282 TA = 87
59549
MA = 87
52994
Ha = 219
975 n
mi
Hp = 215
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6289920
12 X = -1986947
29
Y = 13258126
52 feet Y = 4019248
14 meter
Z = 16705355
53 Z = 5082309
43
XDOT = -24137
307997 XDOT = -7333
389226
YDOT = -4337
962818 feet/sec YDOT = -1404
350373 meter/sec
ZDOT = -5626
244364 ZDOT = -1750
560479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13854269
99 X = -4222781
49
Y = 4980848
95 feet Y = 1518162
76 meter
Z = 16663140
88 Z = 5078925
34
XDOT = -13796
701886 XDOT = -4205
234735
YDOT = -18968
444745 feet/sec YDOT = -5781
581958 meter/sec
ZDOT = -5781
875611 ZDOT = -1762
315686
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 16252
95630356
00016717 00000-0 10270-3 0 9123
2 25544 51
6417
0717 0003416 313
9128 46
1742 15
54432815 18014
Satellite: ISS
Catalog Number: 25544
Epoch time: 16252
95630356 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node:
0717 deg
Eccentricity:
0003416
Arg of perigee: 313
9128 deg
Mean anomaly: 46
1742 deg
Mean motion: 15
54432815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1801
Checksum: 281
Coasting Arc #14 (Orbit 1815)
---------------------------------------
Vector Time (GMT): 2016/253/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 894307
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3677154
83 A = 6780732
07 meter
Y = -3753838
96 meter E =
0005455
Z = -4290340
53 I = 51
60537
XDOT = 6415
106000 Wp = 91
95403
YDOT = 2232
008311 meter/sec RA = 354
72427 deg
ZDOT = 3549
067242 TA = 214
24800
MA = 214
28319
Ha = 220
060 n
mi
Hp = 215
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12064156
27 X = 3739698
54
Y = -12315744
63 feet Y = -3712369
14 meter
Z = -14075920
38 Z = -4272325
67
XDOT = 21046
935695 XDOT = 6372
430490
YDOT = 7322
861913 feet/sec YDOT = 2303
507951 meter/sec
ZDOT = 11643
921396 ZDOT = 3580
126414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17295175
90 X = 5271569
61
Y = -572824
22 feet Y = -174596
82 meter
Z = -13996489
91 Z = -4266130
13
XDOT = 10134
805344 XDOT = 3089
088669
YDOT = 18483
866261 feet/sec YDOT = 5633
882436 meter/sec
ZDOT = 11779
176233 ZDOT = 3590
292916
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 16253
92064010
00016717 00000-0 10270-3 0 9130
2 25544 51
6411 355
2627 0003493 318
7148 41
3740 15
54431849 18160
Satellite: ISS
Catalog Number: 25544
Epoch time: 16253
92064010 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 355
2627 deg
Eccentricity:
0003493
Arg of perigee: 318
7148 deg
Mean anomaly: 41
3740 deg
Mean motion: 15
54431849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1816
Checksum: 294
Coasting Arc #15 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2016/254/00:46:20
071
Vector Time (MET): N/A
Weight (LBS) : 893926
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1113307
09 A = 6778514
22 meter
Y = -4101640
08 meter E =
0010130
Z = -5289363
13 I = 51
59036
XDOT = 7532
248667 Wp = 75
24159
YDOT = -1257
088297 meter/sec RA = 354
15045 deg
ZDOT = -609
034260 TA = 188
92626
MA = 188
94429
Ha = 219
995 n
mi
Hp = 217
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3652582
32 X = -1041665
33
Y = -13456824
41 feet Y = -4113689
61 meter
Z = -17353553
59 Z = -5294597
02
XDOT = 24712
101925 XDOT = 7548
704360
YDOT = -4124
305436 feet/sec YDOT = -1172
765679 meter/sec
ZDOT = -1998
143899 ZDOT = -572
404440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3592031
67 X = -1094851
25
Y = -13444640
47 feet Y = -4097926
42 meter
Z = -17375622
41 Z = -5296089
71
XDOT = 23728
050967 XDOT = 7232
309935
YDOT = -3957
683982 feet/sec YDOT = -1206
302078 meter/sec
ZDOT = -1837
875860 ZDOT = -560
184562
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 16254
04922202
00016717 00000-0 10270-3 0 9141
2 25544 51
6437 354
6224 0005048 285
9866 74
0731 15
53765541 18187
Satellite: ISS
Catalog Number: 25544
Epoch time: 16254
04922202 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 354
6224 deg
Eccentricity:
0005048
Arg of perigee: 285
9866 deg
Mean anomaly: 74
0731 deg
Mean motion: 15
53765541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1818
Checksum: 312
Coasting Arc #16 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2016/255/00:46:20
071
Vector Time (MET): N/A
Weight (LBS) : 893926
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -543879
65 A = 6778820
02 meter
Y = 4310994
95 meter E =
0004342
Z = 5205186
24 I = 51
55953
XDOT = -7557
809216 Wp = 337
89924
YDOT = 487
105091 meter/sec RA = 349
15083 deg
ZDOT = -1189
511510 TA = 123
54720
MA = 123
50572
Ha = 220
053 n
mi
Hp = 217
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1784382
05 X = -617330
35
Y = 14143684
23 feet Y = 4304502
57 meter
Z = 17077382
67 Z = 5202365
54
XDOT = -24795
961996 XDOT = -7556
916318
YDOT = 1598
113817 feet/sec YDOT = 402
593522 meter/sec
ZDOT = -3902
596819 ZDOT = -1226
223215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1596640
62 X = -486656
06
Y = 14181952
71 feet Y = 4322659
19 meter
Z = 17064225
09 Z = 5201175
81
XDOT = -23696
910507 XDOT = -7222
818323
YDOT = 2235
247424 feet/sec YDOT = 681
303415 meter/sec
ZDOT = -4063
066179 ZDOT = -1238
422571
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 16255
07830164
00016717 00000-0 10270-3 0 9151
2 25544 51
6435 349
4962 0005287 289
1383 70
9197 15
53798184 18349
Satellite: ISS
Catalog Number: 25544
Epoch time: 16255
07830164 = yrday
fracday
Element set: 915
Inclination: 51
6435 deg
RA of node: 349
4962 deg
Eccentricity:
0005287
Arg of perigee: 289
1383 deg
Mean anomaly: 70
9197 deg
Mean motion: 15
53798184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 344
Coasting Arc #17 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2016/256/00:46:20
071
Vector Time (MET): N/A
Weight (LBS) : 893926
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2119791
68 A = 6781202
39 meter
Y = -4450918
39 meter E =
0005212
Z = -4661241
00 I = 51
53690
XDOT = 7092
197814 Wp = 105
31970
YDOT = 364
052852 meter/sec RA = 344
15145 deg
ZDOT = 2879
034050 TA = 193
34751
MA = 193
36130
Ha = 220
251 n
mi
Hp = 217
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6954697
11 X = 2192047
61
Y = -14602750
61 feet Y = -4426809
77 meter
Z = -15292785
43 Z = -4650767
83
XDOT = 23268
365530 XDOT = 7073
614743
YDOT = 1194
399120 feet/sec YDOT = 443
258856 meter/sec
ZDOT = 9445
649770 ZDOT = 2913
440821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6489797
55 X = 1978090
29
Y = -14863178
10 feet Y = -4530296
68 meter
Z = -15246176
18 Z = -4647034
50
XDOT = 22151
664490 XDOT = 6751
827337
YDOT = -166
402909 feet/sec YDOT = -50
719607 meter/sec
ZDOT = 9595
879343 ZDOT = 2924
824024
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 16256
04305765
00016717 00000-0 10270-3 0 9164
2 25544 51
6446 344
6894 0005258 293
6825 66
3776 15
53777681 18498
Satellite: ISS
Catalog Number: 25544
Epoch time: 16256
04305765 = yrday
fracday
Element set: 916
Inclination: 51
6446 deg
RA of node: 344
6894 deg
Eccentricity:
0005258
Arg of perigee: 293
6825 deg
Mean anomaly: 66
3776 deg
Mean motion: 15
53777681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1849
Checksum: 356
Coasting Arc #18 (Orbit 1864)
---------------------------------------
Vector Time (GMT): 2016/257/00:46:20
071
Vector Time (MET): N/A
Weight (LBS) : 893926
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3525700
20 A = 6784656
71 meter
Y = 4474255
82 meter E =
0008041
Z = 3682165
99 I = 51
51725
XDOT = -6194
941414 Wp = 64
71799
YDOT = -1316
887896 meter/sec RA = 339
15860 deg
ZDOT = -4320
771000 TA = 71
37515
MA = 71
28785
Ha = 220
449 n
mi
Hp = 216
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11567257
89 X = -3593356
68
Y = 14679316
98 feet Y = 4434451
09 meter
Z = 12080597
07 Z = 3664874
44
XDOT = -20324
610939 XDOT = -6158
766931
YDOT = -4320
498347 feet/sec YDOT = -1385
961981 meter/sec
ZDOT = -14175
757874 ZDOT = -4350
776272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10813570
51 X = -3295976
29
Y = 15303278
73 feet Y = 4664439
36 meter
Z = 12004206
78 Z = 3658882
23
XDOT = -19324
982527 XDOT = -5890
254674
YDOT = -2405
143147 feet/sec YDOT = -733
087631 meter/sec
ZDOT = -14306
572342 ZDOT = -4360
643250
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 16257
07212286
00016717 00000-0 10270-3 0 9174
2 25544 51
6441 339
5632 0005140 298
6562 61
4073 15
53784503 18654
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
07212286 = yrday
fracday
Element set: 917
Inclination: 51
6441 deg
RA of node: 339
5632 deg
Eccentricity:
0005140
Arg of perigee: 298
6562 deg
Mean anomaly: 61
4073 deg
Mean motion: 15
53784503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1865
Checksum: 312
Coasting Arc #19 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2016/257/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893926
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3539858
32 A = 6779256
32 meter
Y = 2797765
51 meter E =
0000434
Z = 5059969
44 I = 51
47287
XDOT = -6031
383768 Wp = 212
78630
YDOT = 4380
101982 meter/sec RA = 335
08052 deg
ZDOT = 1797
304030 TA = 219
77706
MA = 219
78024
Ha = 220
325 n
mi
Hp = 216
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11613708
40 X = 3483730
96
Y = 9179020
71 feet Y = 2837037
26 meter
Z = 16600949
62 Z = 5077028
44
XDOT = -19788
004489 XDOT = -6088
645373
YDOT = 14370
413328 feet/sec YDOT = 4312
335018 meter/sec
ZDOT = 5896
666764 ZDOT = 1767
865809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1966924
75 X = -599518
66
Y = 14587738
36 feet Y = 4446342
65 meter
Z = 16674929
35 Z = 5082518
47
XDOT = -21449
888861 XDOT = -6537
926125
YDOT = -9485
655941 feet/sec YDOT = -2891
227931 meter/sec
ZDOT = 5767
246334 ZDOT = 1757
856683
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 16257
90823131
00016717 00000-0 10270-3 0 9184
2 25544 51
6418 335
3964 0005317 300
2887 59
7739 15
53824292 18789
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
90823131 = yrday
fracday
Element set: 918
Inclination: 51
6418 deg
RA of node: 335
3964 deg
Eccentricity:
0005317
Arg of perigee: 300
2887 deg
Mean anomaly: 59
7739 deg
Mean motion: 15
53824292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1878
Checksum: 337
Coasting Arc #20 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2016/258/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893926
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2118138
09 A = 6778315
95 meter
Y = -3660900
59 meter E =
0010927
Z = -5305982
42 I = 51
44102
XDOT = 6636
380315 Wp = 73
96958
YDOT = -3826
258560 meter/sec RA = 330
07180 deg
ZDOT = -6
330777 TA = 195
95264
MA = 195
98708
Ha = 220
596 n
mi
Hp = 216
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6949271
96 X = -2051269
57
Y = -12010828
71 feet Y = -3684213
78 meter
Z = -17408078
82 Z = -5316108
87
XDOT = 21772
901296 XDOT = 6678
704034
YDOT = -12553
341732 feet/sec YDOT = -3751
809461 meter/sec
ZDOT = -20
770265 ZDOT = 26
010096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6587129
60 X = 2007757
10
Y = -12150901
42 feet Y = -3703594
75 meter
Z = -17451616
35 Z = -5319252
66
XDOT = 21275
236126 XDOT = 6484
691971
YDOT = 11373
283441 feet/sec YDOT = 3466
576793 meter/sec
ZDOT = 121
209208 ZDOT = 36
944567
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 16258
87296899
00016717 00000-0 10270-3 0 9197
2 25544 51
6423 330
5895 0005293 304
7575 55
3079 15
53798175 18937
Satellite: ISS
Catalog Number: 25544
Epoch time: 16258
87296899 = yrday
fracday
Element set: 919
Inclination: 51
6423 deg
RA of node: 330
5895 deg
Eccentricity:
0005293
Arg of perigee: 304
7575 deg
Mean anomaly: 55
3079 deg
Mean motion: 15
53798175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1893
Checksum: 368
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