[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 30th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
284/02:47:17
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 212
5
286/10:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 212
2
287/18:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 212
2
Coasting Arc #1 (Orbit 2135)
---------------------------------------
Vector Time (GMT): 2016/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2241736
96 A = 6789635
45 meter
Y = -6396577
11 meter E =
0018157
Z = -159612
94 I = 51
30433
XDOT = 4484
565124 Wp = 36
18598
YDOT = -1711
965351 meter/sec RA = 251
76738 deg
ZDOT = 5986
121585 TA = 322
08550
MA = 322
21322
Ha = 222
892 n
mi
Hp = 213
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7354780
06 X = -2169266
86
Y = -20986145
38 feet Y = -6421240
54 meter
Z = -523664
51 Z = -170325
85
XDOT = 14713
140171 XDOT = 4474
297222
YDOT = -5616
684221 feet/sec YDOT = -1661
872458 meter/sec
ZDOT = 19639
506512 ZDOT = 6007
881960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10478809
98 X = 3193941
28
Y = 19612639
40 feet Y = 5977932
49 meter
Z = -569411
44 Z = -173556
61
XDOT = -12123
442635 XDOT = -3695
225315
YDOT = 7018
566345 feet/sec YDOT = 2139
259022 meter/sec
ZDOT = 19734
815747 ZDOT = 6015
171840
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 16274
50033672
00016717 00000-0 10270-3 0 9003
2 25544 51
6383 252
7108 0006713 21
8902 338
2536 15
54019889 21364
Satellite: ISS
Catalog Number: 25544
Epoch time: 16274
50033672 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 252
7108 deg
Eccentricity:
0006713
Arg of perigee: 21
8902 deg
Mean anomaly: 338
2536 deg
Mean motion: 15
54019889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2136
Checksum: 301
Coasting Arc #2 (Orbit 2151)
---------------------------------------
Vector Time (GMT): 2016/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1448911
89 A = 6788713
03 meter
Y = 6457766
44 meter E =
0007901
Z = -1517567
86 I = 51
31346
XDOT = -5080
079430 Wp = 91
89621
YDOT = -200
813319 meter/sec RA = 246
77378 deg
ZDOT = -5730
979747 TA = 104
74180
MA = 104
65422
Ha = 223
078 n
mi
Hp = 213
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4753647
95 X = 1383963
60
Y = 21186897
78 feet Y = 6473605
78 meter
Z = -4978897
17 Z = -1510688
02
XDOT = -16666
927263 XDOT = -5049
617367
YDOT = -658
836348 feet/sec YDOT = -257
452685 meter/sec
ZDOT = -18802
426993 ZDOT = -5755
583761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8320636
88 X = -2536130
12
Y = -20063320
44 feet Y = -6115300
07 meter
Z = -4949888
69 Z = -1508726
07
XDOT = 14952
997403 XDOT = 4557
673609
YDOT = -1557
307904 feet/sec YDOT = -474
667449 meter/sec
ZDOT = -18909
847805 ZDOT = -5763
721611
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 16275
52925800
00016717 00000-0 10270-3 0 9010
2 25544 51
6397 247
5816 0006920 24
4526 335
6954 15
54006206 21520
Satellite: ISS
Catalog Number: 25544
Epoch time: 16275
52925800 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 247
5816 deg
Eccentricity:
0006920
Arg of perigee: 24
4526 deg
Mean anomaly: 335
6954 deg
Mean motion: 15
54006206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2152
Checksum: 304
Coasting Arc #3 (Orbit 2167)
---------------------------------------
Vector Time (GMT): 2016/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -515307
35 A = 6785736
61 meter
Y = -6049892
43 meter E =
0017845
Z = 3006313
53 I = 51
31798
XDOT = 5541
754545 Wp = 65
14476
YDOT = 1984
034186 meter/sec RA = 241
77715 deg
ZDOT = 4926
918293 TA = 329
49475
MA = 329
59843
Ha = 222
991 n
mi
Hp = 213
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1690640
91 X = -462221
20
Y = -19848728
43 feet Y = -6055357
70 meter
Z = 9863233
35 Z = 3003940
03
XDOT = 18181
609399 XDOT = 5495
223492
YDOT = 6509
298512 feet/sec YDOT = 2045
746309 meter/sec
ZDOT = 16164
430096 ZDOT = 4953
725847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5436297
28 X = 1656983
41
Y = 19169307
19 feet Y = 5842804
83 meter
Z = 9853831
39 Z = 3003447
81
XDOT = -17577
590694 XDOT = -5357
649643
YDOT = -3410
737148 feet/sec YDOT = -1039
592683 meter/sec
ZDOT = 16281
195118 ZDOT = 4962
508272
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 16276
55816902
00016717 00000-0 10270-3 0 9027
2 25544 51
6402 242
4542 0006765 27
7073 332
4439 15
54047924 21689
Satellite: ISS
Catalog Number: 25544
Epoch time: 16276
55816902 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 242
4542 deg
Eccentricity:
0006765
Arg of perigee: 27
7073 deg
Mean anomaly: 332
4439 deg
Mean motion: 15
54047924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2168
Checksum: 310
Coasting Arc #4 (Orbit 2182)
---------------------------------------
Vector Time (GMT): 2016/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -592418
05 A = 6782036
49 meter
Y = 5278565
43 meter E =
0014196
Z = -4232313
55 I = 51
32132
XDOT = -5759
251122 Wp = 52
25488
YDOT = -3532
703826 meter/sec RA = 236
77094 deg
ZDOT = -3599
641208 TA = 180
70829
MA = 180
71030
Ha = 223
187 n
mi
Hp = 213
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1943628
78 X = -630841
18
Y = 17318128
05 feet Y = 5271725
25 meter
Z = -13885543
15 Z = -4235285
41
XDOT = -18895
180846 XDOT = -5701
833681
YDOT = -11590
235649 feet/sec YDOT = -3596
787047 meter/sec
ZDOT = -11809
846483 ZDOT = -3627
478772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1716749
43 X = -523265
23
Y = -17331017
22 feet Y = -5282494
05 meter
Z = -13899358
77 Z = -4236524
55
XDOT = 19522
934618 XDOT = 5950
590472
YDOT = 7635
174536 feet/sec YDOT = 2327
201199 meter/sec
ZDOT = -11930
873653 ZDOT = -3636
530290
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 16277
52276915
00016717 00000-0 10270-3 0 9030
2 25544 51
6400 237
6461 0006973 31
1371 329
0193 15
54027554 21837
Satellite: ISS
Catalog Number: 25544
Epoch time: 16277
52276915 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 237
6461 deg
Eccentricity:
0006973
Arg of perigee: 31
1371 deg
Mean anomaly: 329
0193 deg
Mean motion: 15
54027554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2183
Checksum: 301
Coasting Arc #5 (Orbit 2198)
---------------------------------------
Vector Time (GMT): 2016/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1796452
45 A = 6778783
24 meter
Y = -4193009
06 meter E =
0008895
Z = 5006171
46 I = 51
33031
XDOT = 5710
520034 Wp = 74
47389
YDOT = 4751
041007 meter/sec RA = 231
75780 deg
ZDOT = 1929
588749 TA = 356
73876
MA = 356
74455
Ha = 223
012 n
mi
Hp = 213
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5893872
88 X = 1818887
96
Y = -13756591
41 feet Y = -4172793
92 meter
Z = 16424447
06 Z = 5014953
30
XDOT = 18735
301950 XDOT = 5647
594980
YDOT = 15587
404878 feet/sec YDOT = 4814
548254 meter/sec
ZDOT = 6330
671750 ZDOT = 1957
176154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2608314
67 X = -795014
31
Y = 14693365
68 feet Y = 4478537
86 meter
Z = 16463465
78 Z = 5018064
37
XDOT = -20602
281576 XDOT = -6279
575424
YDOT = -10886
674850 feet/sec YDOT = -3318
258494 meter/sec
ZDOT = 6450
426283 ZDOT = 1966
089931
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 16278
55166525
00016717 00000-0 10270-3 0 9040
2 25544 51
6409 232
5188 0006787 33
5816 326
5765 15
54072319 21992
Satellite: ISS
Catalog Number: 25544
Epoch time: 16278
55166525 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 232
5188 deg
Eccentricity:
0006787
Arg of perigee: 33
5816 deg
Mean anomaly: 326
5765 deg
Mean motion: 15
54072319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2199
Checksum: 336
Coasting Arc #6 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2016/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3044812
95 A = 6777601
57 meter
Y = 2953142
60 meter E =
0019905
Z = -5302838
87 I = 51
34718
XDOT = -5276
321729 Wp = 73
71664
YDOT = -5544
745281 meter/sec RA = 226
73810 deg
ZDOT = -52
968381 TA = 195
74463
MA = 195
80661
Ha = 223
239 n
mi
Hp = 212
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9989543
79 X = -3051850
06
Y = 9688788
04 feet Y = 2919053
58 meter
Z = -17397765
33 Z = -5317647
47
XDOT = -17310
766829 XDOT = -5213
669523
YDOT = -18191
421527 feet/sec YDOT = -5603
398346 meter/sec
ZDOT = -173
780776 ZDOT = -78
447175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7293549
97 X = 2223074
03
Y = -11755700
92 feet Y = -3583137
64 meter
Z = -17462916
77 Z = -5322697
03
XDOT = 20277
083101 XDOT = 6180
454929
YDOT = 13028
393220 feet/sec YDOT = 3971
054253 meter/sec
ZDOT = -284
214170 ZDOT = -86
628479
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 16279
51624793
00016717 00000-0 10270-3 0 9054
2 25544 51
6412 227
7105 0006930 37
4285 322
7349 15
54046756 22144
Satellite: ISS
Catalog Number: 25544
Epoch time: 16279
51624793 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 227
7105 deg
Eccentricity:
0006930
Arg of perigee: 37
4285 deg
Mean anomaly: 322
7349 deg
Mean motion: 15
54046756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2214
Checksum: 312
Coasting Arc #7 (Orbit 2229)
---------------------------------------
Vector Time (GMT): 2016/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4239031
61 A = 6778635
64 meter
Y = -1608888
92 meter E =
0012376
Z = 5033421
62 I = 51
37338
XDOT = 4467
014281 Wp = 47
82402
YDOT = 5959
254196 meter/sec RA = 221
72101 deg
ZDOT = -1846
112213 TA = 60
17460
MA = 60
05162
Ha = 223
183 n
mi
Hp = 212
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13907584
02 X = 4232256
94
Y = -5278506
95 feet Y = -1561522
67 meter
Z = 16513850
45 Z = 5053997
81
XDOT = 14655
558665 XDOT = 4409
012158
YDOT = 19551
358910 feet/sec YDOT = 6008
882878 meter/sec
ZDOT = -6056
798599 ZDOT = -1824
553592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12005993
99 X = -3659426
97
Y = 8611287
63 feet Y = 2624720
47 meter
Z = 16603994
07 Z = 5060897
39
XDOT = -18553
052580 XDOT = -5654
970426
YDOT = -14298
544794 feet/sec YDOT = -4358
196453 meter/sec
ZDOT = -5963
540584 ZDOT = -1817
687170
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 16280
54512568
00016717 00000-0 10270-3 0 9066
2 25544 51
6409 222
5831 0007008 41
4121 318
7561 15
54063132 22306
Satellite: ISS
Catalog Number: 25544
Epoch time: 16280
54512568 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 222
5831 deg
Eccentricity:
0007008
Arg of perigee: 41
4121 deg
Mean anomaly: 318
7561 deg
Mean motion: 15
54063132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2230
Checksum: 276
Coasting Arc #8 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2016/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5255036
96 A = 6781601
14 meter
Y = 344839
21 meter E =
0012974
Z = -4282629
06 I = 51
40800
XDOT = -3265
333728 Wp = 81
70503
YDOT = -5957
127195 meter/sec RA = 216
71105 deg
ZDOT = 3538
129986 TA = 224
47050
MA = 224
57473
Ha = 223
251 n
mi
Hp = 212
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17240934
90 X = -5237698
97
Y = 1131362
24 feet Y = 286170
48 meter
Z = -14050620
28 Z = -4308115
03
XDOT = -10713
037165 XDOT = -3215
663908
YDOT = -19544
380560 feet/sec YDOT = -5993
364357 meter/sec
ZDOT = 11608
038012 ZDOT = 3522
388661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16203036
08 X = 4938685
40
Y = -5731344
11 feet Y = -1746913
69 meter
Z = -14162028
92 Z = -4316586
42
XDOT = 15258
631388 XDOT = 4650
830847
YDOT = 14710
842877 feet/sec YDOT = 4483
864909 meter/sec
ZDOT = 11540
181514 ZDOT = 3517
447325
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 16281
50968947
00016717 00000-0 10270-3 0 9070
2 25544 51
6407 217
7757 0006905 44
5150 315
6556 15
54073099 22457
Satellite: ISS
Catalog Number: 25544
Epoch time: 16281
50968947 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 217
7757 deg
Eccentricity:
0006905
Arg of perigee: 44
5150 deg
Mean anomaly: 315
6556 deg
Mean motion: 15
54073099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 331
Coasting Arc #9 (Orbit 2260)
---------------------------------------
Vector Time (GMT): 2016/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5997348
51 A = 6785352
89 meter
Y = 852961
30 meter E =
0018417
Z = 3045331
26 I = 51
44809
XDOT = 1702
007338 Wp = 79
70105
YDOT = 5646
358557 meter/sec RA = 211
71183 deg
ZDOT = -4904
801960 TA = 65
24570
MA = 65
05416
Ha = 223
240 n
mi
Hp = 212
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19676340
24 X = 5972571
63
Y = 2798429
45 feet Y = 919889
35 meter
Z = 9991244
31 Z = 3074405
02
XDOT = 5584
013575 XDOT = 1662
567553
YDOT = 18524
798414 feet/sec YDOT = 5665
170674 meter/sec
ZDOT = -16091
869947 ZDOT = -4896
630123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19588761
77 X = -5970654
59
Y = 2952591
47 feet Y = 899949
88 meter
Z = 10118159
49 Z = 3084015
01
XDOT = -10554
381222 XDOT = -3216
975397
YDOT = -14680
049975 feet/sec YDOT = -4474
479232 meter/sec
ZDOT = -16057
029028 ZDOT = -4894
182448
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 16282
53854548
00016717 00000-0 10270-3 0 9086
2 25544 51
6415 212
6470 0006950 47
8428 312
3314 15
54110159 22619
Satellite: ISS
Catalog Number: 25544
Epoch time: 16282
53854548 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 212
6470 deg
Eccentricity:
0006950
Arg of perigee: 47
8428 deg
Mean anomaly: 312
3314 deg
Mean motion: 15
54110159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2261
Checksum: 299
Coasting Arc #10 (Orbit 2275)
---------------------------------------
Vector Time (GMT): 2016/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6349341
91 A = 6788318
70 meter
Y = -1826361
60 meter E =
0014932
Z = -1538012
07 I = 51
48522
XDOT = 79
988428 Wp = 44
53816
YDOT = -5078
649386 meter/sec RA = 206
72451 deg
ZDOT = 5744
892243 TA = 298
61764
MA = 298
76777
Ha = 223
301 n
mi
Hp = 212
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20831174
26 X = -6320976
09
Y = -5992000
01 feet Y = -1897205
71 meter
Z = -5045971
37 Z = -1568786
88
XDOT = 262
429225 XDOT = 108
866722
YDOT = -16662
235520 feet/sec YDOT = -5077
593013 meter/sec
ZDOT = 18848
071664 ZDOT = 5745
351325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21635632
50 X = 6594540
79
Y = -607261
67 feet Y = -185093
36 meter
Z = -5180188
37 Z = -1578921
42
XDOT = 4881
982793 XDOT = 1488
028355
YDOT = 14338
522575 feet/sec YDOT = 4370
381681 meter/sec
ZDOT = 18850
853846 ZDOT = 5745
740252
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 16283
50308634
00016717 00000-0 10270-3 0 9095
2 25544 51
6408 207
8395 0006993 51
4632 308
7147 15
54110916 22768
Satellite: ISS
Catalog Number: 25544
Epoch time: 16283
50308634 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 207
8395 deg
Eccentricity:
0006993
Arg of perigee: 51
4632 deg
Mean anomaly: 308
7147 deg
Mean motion: 15
54110916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2276
Checksum: 317
Coasting Arc #11 (Orbit 2285)
---------------------------------------
Vector Time (GMT): 2016/284/02:47:17
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5668325
55 A = 6788708
79 meter
Y = 3533879
08 meter E =
0011859
Z = -1208192
01 I = 51
50490
XDOT = -3453
419236 Wp = 107
60207
YDOT = 3559
280205 meter/sec RA = 203
67053 deg
ZDOT = -5842
229357 TA = 85
54275
MA = 85
40727
Ha = 223
310 n
mi
Hp = 212
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18596868
61 X = 5634256
46
Y = 11594091
48 feet Y = 3597075
52 meter
Z = -3963884
56 Z = -1180739
48
XDOT = -11330
115603 XDOT = -3464
584045
YDOT = 11677
428494 feet/sec YDOT = 3520
598872 meter/sec
ZDOT = -19167
419150 ZDOT = -5859
032756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19331878
53 X = 5892356
58
Y = -10367142
33 feet Y = -3159904
98 meter
Z = -3844436
52 Z = -1171784
25
XDOT = 3782
132035 XDOT = 1152
793844
YDOT = 14124
058740 feet/sec YDOT = 4305
013104 meter/sec
ZDOT = -19241
402418 ZDOT = -5864
779457
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 16284
14610683
00016717 00000-0 10270-3 0 9108
2 25544 51
6412 204
6330 0006783 56
1085 304
0712 15
54139426 22863
Satellite: ISS
Catalog Number: 25544
Epoch time: 16284
14610683 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 204
6330 deg
Eccentricity:
0006783
Arg of perigee: 56
1085 deg
Mean anomaly: 304
0712 deg
Mean motion: 15
54139426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2286
Checksum: 285
Coasting Arc #12 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2016/285/02:47:17
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4766172
35 A = 6786101
14 meter
Y = -3938175
77 meter E =
0019984
Z = 2772668
99 I = 51
52603
XDOT = 5111
863191 Wp = 73
03943
YDOT = -2565
252292 meter/sec RA = 198
68770 deg
ZDOT = 5118
823428 TA = 318
47208
MA = 318
62373
Ha = 223
363 n
mi
Hp = 212
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15637048
38 X = -4735248
97
Y = -12920524
19 feet Y = -3991301
15 meter
Z = 9096683
03 Z = 2749591
40
XDOT = 16771
204694 XDOT = 5115
303327
YDOT = -8416
182060 feet/sec YDOT = -2508
068305 meter/sec
ZDOT = 16794
040118 ZDOT = 5143
664369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18896890
83 X = -5759772
33
Y = 7495274
77 feet Y = 2284559
75 meter
Z = 8996401
64 Z = 2742103
22
XDOT = 1234
096948 XDOT = 376
152750
YDOT = -17275
721849 feet/sec YDOT = -5265
640020 meter/sec
ZDOT = 16903
011664 ZDOT = 5152
037955
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 16285
17493067
00016717 00000-0 10270-3 0 9118
2 25544 51
6412 199
5043 0006767 59
8963 300
2860 15
54142829 23025
Satellite: ISS
Catalog Number: 25544
Epoch time: 16285
17493067 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 199
5043 deg
Eccentricity:
0006767
Arg of perigee: 59
8963 deg
Mean anomaly: 300
2860 deg
Mean motion: 15
54142829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 317
Coasting Arc #13 (Orbit 2316)
---------------------------------------
Vector Time (GMT): 2016/286/02:47:17
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3433086
30 A = 6782190
47 meter
Y = 4187286
13 meter E =
0014073
Z = -4099051
38 I = 51
54509
XDOT = -6449
735532 Wp = 67
89261
YDOT = 1551
994586 meter/sec RA = 193
69734 deg
ZDOT = -3821
823488 TA = 162
52889
MA = 162
48042
Ha = 223
340 n
mi
Hp = 212
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11263406
49 X = 3405919
43
Y = 13737815
38 feet Y = 4225524
86 meter
Z = -13448331
29 Z = -4082440
61
XDOT = -21160
549646 XDOT = -6448
046044
YDOT = 5091
845753 feet/sec YDOT = 1479
878348 meter/sec
ZDOT = -12538
790972 ZDOT = -3853
151008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17452325
29 X = 5319468
75
Y = -3597124
86 feet Y = -1096403
66 meter
Z = -13376342
80 Z = -4077109
28
XDOT = -5634
036354 XDOT = -1717
254281
YDOT = 19736
429493 feet/sec YDOT = 6015
663709 meter/sec
ZDOT = -12675
977170 ZDOT = -3863
637841
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 16286
13944078
00016717 00000-0 10270-3 0 9129
2 25544 51
6422 194
6959 0006836 63
2945 296
8907 15
54165829 23177
Satellite: ISS
Catalog Number: 25544
Epoch time: 16286
13944078 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 194
6959 deg
Eccentricity:
0006836
Arg of perigee: 63
2945 deg
Mean anomaly: 296
8907 deg
Mean motion: 15
54165829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2317
Checksum: 350
Coasting Arc #14 (Orbit 2321)
---------------------------------------
Vector Time (GMT): 2016/286/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 907704
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6016318
46 A = 6785438
52 meter
Y = 1108817
46 meter E =
0011444
Z = -2938019
64 I = 51
56636
XDOT = -3312
875194 Wp = 64
88819
YDOT = -4762
759434 meter/sec RA = 191
95953 deg
ZDOT = 5006
489628 TA = 261
56191
MA = 261
69164
Ha = 223
289 n
mi
Hp = 212
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19738577
62 X = -6013998
63
Y = 3637852
56 feet Y = 1041551
59 meter
Z = -9639172
06 Z = -2967240
15
XDOT = -10869
013103 XDOT = -3283
690167
YDOT = -15625
851162 feet/sec YDOT = -4799
642475 meter/sec
ZDOT = 16425
490907 ZDOT = 4990
467802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19343829
10 X = 5895999
11
Y = -5116579
30 feet Y = -1559533
37 meter
Z = -9767084
92 Z = -2977007
48
XDOT = 11753
733346 XDOT = 3582
537924
YDOT = 13337
822903 feet/sec YDOT = 4065
368421 meter/sec
ZDOT = 16356
159355 ZDOT = 4985
357372
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 16286
46094216
00016717 00000-0 10270-3 0 9136
2 25544 51
6416 193
0946 0006919 61
9143 298
2709 15
54172795 23228
Satellite: ISS
Catalog Number: 25544
Epoch time: 16286
46094216 = yrday
fracday
Element set: 913
Inclination: 51
6416 deg
RA of node: 193
0946 deg
Eccentricity:
0006919
Arg of perigee: 61
9143 deg
Mean anomaly: 298
2709 deg
Mean motion: 15
54172795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2322
Checksum: 328
Coasting Arc #15 (Orbit 2337)
---------------------------------------
Vector Time (GMT): 2016/287/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 907704
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6647413
42 A = 6788373
65 meter
Y = -243472
00 meter E =
0018736
Z = 1324698
86 I = 51
60857
XDOT = 1348
810703 Wp = 103
01480
YDOT = 4810
319230 meter/sec RA = 186
98123 deg
ZDOT = -5819
063091 TA = 62
55563
MA = 62
36521
Ha = 223
331 n
mi
Hp = 212
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21809099
16 X = 6643207
05
Y = -798792
65 feet Y = -169159
51 meter
Z = 4346124
87 Z = 1356980
50
XDOT = 4425
231965 XDOT = 1323
187061
YDOT = 15781
887238 feet/sec YDOT = 4825
258523 meter/sec
ZDOT = -19091
414342 ZDOT = -5812
573687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21612225
98 X = -6587406
48
Y = 2817705
26 feet Y = 858836
56 meter
Z = 4487304
58 Z = 1367730
44
XDOT = -5789
125669 XDOT = -1764
525504
YDOT = -13713
573530 feet/sec YDOT = -4179
897212 meter/sec
ZDOT = -19063
757741 ZDOT = -5810
633359
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 16287
48973748
00016717 00000-0 10270-3 0 9146
2 25544 51
6423 187
9660 0006892 66
1018 294
0857 15
54185620 23385
Satellite: ISS
Catalog Number: 25544
Epoch time: 16287
48973748 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 187
9660 deg
Eccentricity:
0006892
Arg of perigee: 66
1018 deg
Mean anomaly: 294
0857 deg
Mean motion: 15
54185620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2338
Checksum: 345
Coasting Arc #16 (Orbit 2342)
---------------------------------------
Vector Time (GMT): 2016/287/18:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907704
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5981551
04 A = 6787041
80 meter
Y = 2324330
63 meter E =
0010815
Z = -2214379
67 I = 51
61227
XDOT = -3572
224976 Wp = 102
36155
YDOT = 4011
631895 meter/sec RA = 185
37009 deg
ZDOT = -5463
414878 TA = 102
23038
MA = 102
10924
Ha = 223
312 n
mi
Hp = 212
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19624511
29 X = 5965871
86
Y = 7625756
67 feet Y = 2391132
39 meter
Z = -7265025
17 Z = -2185360
83
XDOT = -11719
898216 XDOT = -3590
279323
YDOT = 13161
521966 feet/sec YDOT = 3971
583215 meter/sec
ZDOT = -17924
589495 ZDOT = -5480
812442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4643427
97 X = 1415316
84
Y = 20579959
69 feet Y = 6272771
71 meter
Z = -7138489
68 Z = -2175811
66
XDOT = -15894
142832 XDOT = -4844
534735
YDOT = -2629
090953 feet/sec YDOT = -801
346922 meter/sec
ZDOT = -18001
255417 ZDOT = -5486
782651
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 16287
81123242
00016717 00000-0 10270-3 0 9150
2 25544 51
6397 186
3590 0006823 69
8177 290
3709 15
54222955 23434
Satellite: ISS
Catalog Number: 25544
Epoch time: 16287
81123242 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 186
3590 deg
Eccentricity:
0006823
Arg of perigee: 69
8177 deg
Mean anomaly: 290
3709 deg
Mean motion: 15
54222955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2343
Checksum: 328
Coasting Arc #17 (Orbit 2358)
---------------------------------------
Vector Time (GMT): 2016/288/18:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907704
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4919199
66 A = 6783501
65 meter
Y = -2911617
00 meter E =
0018394
Z = 3635672
33 I = 51
63364
XDOT = 5284
408324 Wp = 87
24319
YDOT = -3433
277004 meter/sec RA = 180
38932 deg
ZDOT = 4382
204224 TA = 315
95117
MA = 316
09758
Ha = 223
315 n
mi
Hp = 212
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16139106
48 X = -4903936
43
Y = -9552549
22 feet Y = -2966540
97 meter
Z = 11928058
81 Z = 3611813
15
XDOT = 17337
297651 XDOT = 5301
120131
YDOT = -11264
032164 feet/sec YDOT = -3374
089177 meter/sec
ZDOT = 14377
310445 ZDOT = 4407
916034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1440335
33 X = -439014
21
Y = -18764732
58 feet Y = -5719490
49 meter
Z = 11824161
16 Z = 3604004
32
XDOT = 17733
220517 XDOT = 5405
085614
YDOT = 7807
634211 feet/sec YDOT = 2379
766908 meter/sec
ZDOT = 14490
252883 ZDOT = 4416
629079
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 16288
84001224
00016717 00000-0 10270-3 0 9160
2 25544 51
6406 181
2299 0006652 74
7338 285
4550 15
54236047 23592
Satellite: ISS
Catalog Number: 25544
Epoch time: 16288
84001224 = yrday
fracday
Element set: 916
Inclination: 51
6406 deg
RA of node: 181
2299 deg
Eccentricity:
0006652
Arg of perigee: 74
7338 deg
Mean anomaly: 285
4550 deg
Mean motion: 15
54236047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2359
Checksum: 316
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