[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 6th 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
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
3
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
0
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
1
254/00:41:33
991 3
4 3
8 3
9
N/A -1
5 -0
4 220
0
000/00:11:03
983 -0
9 0
1 217
1
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
8
Coasting Arc #1 (Orbit 1700)
---------------------------------------
Vector Time (GMT): 2016/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909415
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4119186
39 A = 6785937
52 meter
Y = -4802336
93 meter E =
0003257
Z = -2449264
42 I = 51
85111
XDOT = 5202
780504 Wp = 158
91794
YDOT = -1733
469033 meter/sec RA = 31
67643 deg
ZDOT = -5356
378118 TA = 48
40868
MA = 48
38077
Ha = 219
511 n
mi
Hp = 215
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13514391
03 X = -4053281
94
Y = -15755698
60 feet Y = -4848032
22 meter
Z = -8035644
42 Z = -2469113
55
XDOT = 17069
489844 XDOT = 5247
796621
YDOT = -5687
234360 feet/sec YDOT = -1675
036976 meter/sec
ZDOT = -17573
419022 ZDOT = -5330
995045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7670579
44 X = 2337992
61
Y = 19252428
37 feet Y = 5868140
17 meter
Z = -8121489
86 Z = -2475430
11
XDOT = -16695
507201 XDOT = -5088
790595
YDOT = -707
342294 feet/sec YDOT = -215
597931 meter/sec
ZDOT = -17462
141797 ZDOT = -5322
460820
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
52721698
00016717 00000-0 10270-3 0 9006
2 25544 51
6415 32
1269 0002931 280
0688 80
0134 15
54400533 17019
Satellite: ISS
Catalog Number: 25544
Epoch time: 16246
52721698 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 32
1269 deg
Eccentricity:
0002931
Arg of perigee: 280
0688 deg
Mean anomaly: 80
0134 deg
Mean motion: 15
54400533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1701
Checksum: 279
Coasting Arc #2 (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 = 436476
07 A = 6777426
08 meter
Y = -4412765
73 meter E =
0011027
Z = -5135329
83 I = 51
81605
XDOT = 7025
549506 Wp = 70
45031
YDOT = 2585
976190 meter/sec RA = 30
03221 deg
ZDOT = -1624
223596 TA = 183
89650
MA = 183
90510
Ha = 219
576 n
mi
Hp = 215
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1432008
12 X = 510733
29
Y = -14477577
84 feet Y = -4407470
17 meter
Z = -16848195
00 Z = -5133028
68
XDOT = 23049
703103 XDOT = 7004
000017
YDOT = 8484
173853 feet/sec YDOT = 2664
419909 meter/sec
ZDOT = -5328
817573 ZDOT = -1590
148206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14521486
25 X = 4426149
01
Y = -1069792
04 feet Y = -326072
61 meter
Z = -16837296
82 Z = -5132008
07
XDOT = -4302
564665 XDOT = -1311
421710
YDOT = 23168
812545 feet/sec YDOT = 7061
854064 meter/sec
ZDOT = -5180
372949 ZDOT = -1578
977675
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
84867208
00016717 00000-0 10270-3 0 9010
2 25544 51
6441 30
5281 0002982 285
6684 74
4140 15
54387475 17065
Satellite: ISS
Catalog Number: 25544
Epoch time: 16246
84867208 = yrday
fracday
Element set: 901
Inclination: 51
6441 deg
RA of node: 30
5281 deg
Eccentricity:
0002982
Arg of perigee: 285
6684 deg
Mean anomaly: 74
4140 deg
Mean motion: 15
54387475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1706
Checksum: 319
Coasting Arc #3 (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 = -2188457
52 A = 6776585
81 meter
Y = 3594158
19 meter E =
0001965
Z = 5311990
77 I = 51
78333
XDOT = -6795
965989 Wp = 356
09208
YDOT = -3530
523213 meter/sec RA = 25
04114 deg
ZDOT = -409
131794 TA = 97
81244
MA = 97
79012
Ha = 219
726 n
mi
Hp = 215
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7179978
74 X = -2254288
88
Y = 11791857
58 feet Y = 3569317
95 meter
Z = 17427791
25 Z = 5301199
53
XDOT = -22296
476341 XDOT = -6753
994317
YDOT = -11583
081408 feet/sec YDOT = -3606
285630 meter/sec
ZDOT = -1342
295912 ZDOT = -442
042332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12991516
24 X = -3959814
15
Y = -4846239
51 feet Y = -1477133
80 meter
Z = 17379941
77 Z = 5297406
25
XDOT = 6649
164167 XDOT = 2026
665238
YDOT = -23174
418082 feet/sec YDOT = -7063
562632 meter/sec
ZDOT = -1485
455469 ZDOT = -452
766827
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
87732410
00016717 00000-0 10270-3 0 9021
2 25544 51
6424 25
3986 0002862 291
8435 68
2414 15
54413265 17220
Satellite: ISS
Catalog Number: 25544
Epoch time: 16247
87732410 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 25
3986 deg
Eccentricity:
0002862
Arg of perigee: 291
8435 deg
Mean anomaly: 68
2414 deg
Mean motion: 15
54413265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 305
Coasting Arc #4 (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 = 3857686
39 A = 6778501
09 meter
Y = -2692671
53 meter E =
0008722
Z = -4888248
13 I = 51
76111
XDOT = 5954
711104 Wp = 104
10910
YDOT = 4183
456216 meter/sec RA = 20
04998 deg
ZDOT = 2396
381168 TA = 189
34932
MA = 189
36557
Ha = 219
659 n
mi
Hp = 215
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12656451
40 X = 3911254
76
Y = -8834224
18 feet Y = -2649233
35 meter
Z = -16037559
48 Z = -4869378
08
XDOT = 19536
453754 XDOT = 5895
847508
YDOT = 13725
250051 feet/sec YDOT = 4249
716939 meter/sec
ZDOT = 7862
142941 ZDOT = 2425
164126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11343581
47 X = 3457523
63
Y = 10592788
41 feet Y = 3228681
91 meter
Z = -15954578
85 Z = -4862955
63
XDOT = -8503
041428 XDOT = -2591
727027
YDOT = 21128
224941 feet/sec YDOT = 6439
882962 meter/sec
ZDOT = 7987
125059 ZDOT = 2434
475718
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
84167451
00016717 00000-0 10270-3 0 9037
2 25544 51
6435 20
5903 0003124 295
6796 64
4034 15
54407519 17379
Satellite: ISS
Catalog Number: 25544
Epoch time: 16248
84167451 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 20
5903 deg
Eccentricity:
0003124
Arg of perigee: 295
6796 deg
Mean anomaly: 64
4034 deg
Mean motion: 15
54407519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1737
Checksum: 310
Coasting Arc #5 (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 = -5279349
73 A = 6782058
48 meter
Y = 1745997
85 meter E =
0009234
Z = 3878097
60 I = 51
74212
XDOT = -4554
649390 Wp = 68
74497
YDOT = -4591
874311 meter/sec RA = 15
06426 deg
ZDOT = -4121
833093 TA = 64
49384
MA = 64
39837
Ha = 219
749 n
mi
Hp = 215
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17320701
22 X = -5317319
68
Y = 5728339
41 feet Y = 1686748
75 meter
Z = 12723417
33 Z = 3852359
43
XDOT = -14943
075428 XDOT = -4482
941283
YDOT = -15065
204433 feet/sec YDOT = -4642
406960 meter/sec
ZDOT = -13523
074452 ZDOT = -4143
783764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9564285
53 X = -2915194
23
Y = -15626990
65 feet Y = -4763106
75 meter
Z = 12610611
31 Z = 3843714
33
XDOT = 10122
491289 XDOT = 3085
335345
YDOT = -17214
658234 feet/sec YDOT = -5247
027830 meter/sec
ZDOT = -13618
109498 ZDOT = -4150
799775
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
87030267
00016717 00000-0 10270-3 0 9046
2 25544 51
6427 15
4603 0003111 303
1355 56
9499 15
54473443 17530
Satellite: ISS
Catalog Number: 25544
Epoch time: 16249
87030267 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 15
4603 deg
Eccentricity:
0003111
Arg of perigee: 303
1355 deg
Mean anomaly: 56
9499 deg
Mean motion: 15
54473443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 300
Coasting Arc #6 (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 = 6277716
10 A = 6785899
50 meter
Y = -831175
88 meter E =
0005905
Z = -2430650
95 I = 51
72282
XDOT = 2702
760504 Wp = 15
81979
YDOT = 4774
176166 meter/sec RA = 10
08902 deg
ZDOT = 5356
553666 TA = 317
02010
MA = 317
06622
Ha = 219
818 n
mi
Hp = 215
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20596181
42 X = 6298351
02
Y = -2726954
98 feet Y = -760859
12 meter
Z = -7974576
62 Z = -2400105
13
XDOT = 8867
324487 XDOT = 2623
153703
YDOT = 15663
307631 feet/sec YDOT = 4803
955672 meter/sec
ZDOT = 17573
994966 ZDOT = 5369
489187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7719616
25 X = 2352939
03
Y = 19343213
61 feet Y = 5895811
51 meter
Z = -7840947
44 Z = -2389920
78
XDOT = -11621
810022 XDOT = -3542
327695
YDOT = 11772
777432 feet/sec YDOT = 3588
342561 meter/sec
ZDOT = 17629
593439 ZDOT = 5373
500080
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
83463265
00016717 00000-0 10270-3 0 9053
2 25544 51
6419 10
6522 0003012 306
9814 53
1063 15
54473738 17688
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
83463265 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 10
6522 deg
Eccentricity:
0003012
Arg of perigee: 306
9814 deg
Mean anomaly: 53
1063 deg
Mean motion: 15
54473738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 295
Coasting Arc #7 (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 = -2158273
21 A = 6778455
79 meter
Y = -4248855
61 meter E =
0010211
Z = -4830063
66 I = 51
69511
XDOT = 7189
405578 Wp = 57
11014
YDOT = -775
014730 meter/sec RA = 9
88582 deg
ZDOT = -2529
237988 TA = 188
00071
MA = 188
01701
Ha = 219
773 n
mi
Hp = 215
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7080948
84 X = -2087138
61
Y = -13939814
99 feet Y = -4272593
61 meter
Z = -15846665
57 Z = -4840374
83
XDOT = 23587
288642 XDOT = 7209
823628
YDOT = -2542
699245 feet/sec YDOT = -694
504068 meter/sec
ZDOT = -8298
024896 ZDOT = -2494
263931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8176244
99 X = 2492119
47
Y = -13274164
88 feet Y = -4045965
46 meter
Z = -15890898
42 Z = -4843545
84
XDOT = 13644
148873 XDOT = 4158
736576
YDOT = 18160
825749 feet/sec YDOT = 5535
419688 meter/sec
ZDOT = -8145
058027 ZDOT = -2482
613687
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
89892166
00016717 00000-0 10270-3 0 9066
2 25544 51
6405 10
3305 0003149 307
5908 52
4959 15
54452126 17696
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
89892166 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 10
3305 deg
Eccentricity:
0003149
Arg of perigee: 307
5908 deg
Mean anomaly: 52
4959 deg
Mean motion: 15
54452126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1769
Checksum: 316
Coasting Arc #8 (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 = 1859597
36 A = 6777970
70 meter
Y = 4266353
53 meter E =
0003148
Z = 4925682
59 I = 51
69292
XDOT = -7305
904919 Wp = 117
68319
YDOT = 564
790951 meter/sec RA = 9
72198 deg
ZDOT = 2266
477146 TA = 310
18194
MA = 310
20949
Ha = 219
657 n
mi
Hp = 215
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6101041
19 X = 1787824
81
Y = 13997222
86 feet Y = 4286747
98 meter
Z = 16160375
95 Z = 4934541
31
XDOT = -23969
504329 XDOT = -7322
687154
YDOT = 1852
988686 feet/sec YDOT = 482
997818 meter/sec
ZDOT = 7435
948642 ZDOT = 2230
946014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6011790
87 X = -1832393
86
Y = 13992050
68 feet Y = 4264777
05 meter
Z = 16198258
88 Z = 4937229
31
XDOT = -16873
660601 XDOT = -5143
091751
YDOT = -15688
071411 feet/sec YDOT = -4781
724166 meter/sec
ZDOT = 7280
588635 ZDOT = 2219
123416
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
96320960
00016717 00000-0 10270-3 0 9073
2 25544 51
6408 10
0103 0003317 306
2949 53
7897 15
54474660 17704
Satellite: ISS
Catalog Number: 25544
Epoch time: 16250
96320960 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 10
0103 deg
Eccentricity:
0003317
Arg of perigee: 306
2949 deg
Mean anomaly: 53
7897 deg
Mean motion: 15
54474660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 301
Coasting Arc #9 (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 = 71232
83 A = 6776357
85 meter
Y = -4214142
20 meter E =
0012638
Z = -5316897
86 I = 51
65576
XDOT = 7643
597512 Wp = 77
89431
YDOT = 438
487915 meter/sec RA = 4
72211 deg
ZDOT = -243
038385 TA = 189
77489
MA = 189
79950
Ha = 219
790 n
mi
Hp = 215
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 233703
51 X = 144178
40
Y = -13825925
84 feet Y = -4212938
23 meter
Z = -17443890
61 Z = -5316374
28
XDOT = 25077
419658 XDOT = 7639
306718
YDOT = 1438
608645 feet/sec YDOT = 523
939730 meter/sec
ZDOT = -797
370030 ZDOT = -205
918083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10097689
65 X = 3077775
80
Y = -9452819
84 feet Y = -2881219
49 meter
Z = -17440786
20 Z = -5315951
63
XDOT = 15880
180840 XDOT = 4840
279120
YDOT = 18148
334766 feet/sec YDOT = 5531
612437 meter/sec
ZDOT = -635
270756 ZDOT = -193
630526
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
92752660
00016717 00000-0 10270-3 0 9087
2 25544 51
6411 5
2006 0003285 311
0938 48
9931 15
54475499 17854
Satellite: ISS
Catalog Number: 25544
Epoch time: 16251
92752660 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 5
2006 deg
Eccentricity:
0003285
Arg of perigee: 311
0938 deg
Mean anomaly: 48
9931 deg
Mean motion: 15
54475499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1785
Checksum: 315
Coasting Arc #10 (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 = -2035255
67 A = 6777405
78 meter
Y = 4018975
84 meter E =
0006015
Z = 5063126
61 I = 51
62797
XDOT = -7316
586901 Wp = 21
29495
YDOT = -1405
001591 meter/sec RA = 359
71943 deg
ZDOT = -1819
677220 TA = 86
35568
MA = 86
28689
Ha = 219
907 n
mi
Hp = 214
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6677348
01 X = -2104640
15
Y = 13185616
28 feet Y = 3995828
69 meter
Z = 16611307
76 Z = 5053070
99
XDOT = -24004
550199 XDOT = -7291
492808
YDOT = -4609
585273 feet/sec YDOT = -1486
680398 meter/sec
ZDOT = -5970
069618 ZDOT = -1855
158365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14079514
61 X = -4291436
05
Y = 4658130
93 feet Y = 1419798
31 meter
Z = 16566595
41 Z = 5049498
28
XDOT = -13533
612334 XDOT = -4125
045039
YDOT = -19051
328247 feet/sec YDOT = -5806
844850 meter/sec
ZDOT = -6124
810777 ZDOT = -1866
842325
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
95611528
00016717 00000-0 10270-3 0 9099
2 25544 51
6418
0706 0003405 315
8830 44
2051 15
54506315 18011
Satellite: ISS
Catalog Number: 25544
Epoch time: 16252
95611528 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node:
0706 deg
Eccentricity:
0003405
Arg of perigee: 315
8830 deg
Mean anomaly: 44
2051 deg
Mean motion: 15
54506315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1801
Checksum: 274
Coasting Arc #11 (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 = 3806732
32 A = 6780757
46 meter
Y = -3707313
43 meter E =
0005207
Z = -4216726
02 I = 51
60637
XDOT = 6317
930180 Wp = 89
06141
YDOT = 2328
906065 meter/sec RA = 354
72135 deg
ZDOT = 3660
073733 TA = 218
46109
MA = 218
49821
Ha = 219
982 n
mi
Hp = 214
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12489279
25 X = 3868388
55
Y = -12163101
82 feet Y = -3664399
55 meter
Z = -13834402
97 Z = -4198083
87
XDOT = 20728
117390 XDOT = 6273
639136
YDOT = 7640
767930 feet/sec YDOT = 2399
309995 meter/sec
ZDOT = 12008
115922 ZDOT = 3690
656919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17497445
84 X = 5333221
49
Y = -170593
68 feet Y = -51996
95 meter
Z = -13752241
07 Z = -4191683
08
XDOT = 9712
318487 XDOT = 2960
314675
YDOT = 18478
802494 feet/sec YDOT = 5632
339000 meter/sec
ZDOT = 12141
272493 ZDOT = 3700
659856
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
92040360
00016717 00000-0 10270-3 0 9109
2 25544 51
6412 355
2613 0003489 320
8220 39
2680 15
54514493 18162
Satellite: ISS
Catalog Number: 25544
Epoch time: 16253
92040360 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 355
2613 deg
Eccentricity:
0003489
Arg of perigee: 320
8220 deg
Mean anomaly: 39
2680 deg
Mean motion: 15
54514493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1816
Checksum: 285
Coasting Arc #12 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2016/254/00:47:05
983
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -607044
21 A = 6778322
20 meter
Y = -4173836
55 meter E =
0010004
Z = -5314793
25 I = 51
58974
XDOT = 7605
620527 Wp = 79
29968
YDOT = -905
143611 meter/sec RA = 354
14025 deg
ZDOT = -156
300533 TA = 189
19915
MA = 189
21749
Ha = 219
950 n
mi
Hp = 217
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1991614
87 X = -534509
22
Y = -13693689
48 feet Y = -4180219
72 meter
Z = -17436985
73 Z = -5317565
66
XDOT = 24952
823250 XDOT = 7615
936047
YDOT = -2969
631271 feet/sec YDOT = -820
034801 meter/sec
ZDOT = -512
797024 ZDOT = -119
329228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1977299
04 X = -602680
75
Y = -13681363
11 feet Y = -4170079
48 meter
Z = -17448287
16 Z = -5318237
93
XDOT = 23935
936886 XDOT = 7295
673563
YDOT = -3005
018146 feet/sec YDOT = -915
929531 meter/sec
ZDOT = -351
105504 ZDOT = -107
016958
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
04897831
00016717 00000-0 10270-3 0 9117
2 25544 51
6435 354
6199 0005261 287
2984 72
7593 15
53796924 18189
Satellite: ISS
Catalog Number: 25544
Epoch time: 16254
04897831 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 354
6199 deg
Eccentricity:
0005261
Arg of perigee: 287
2984 deg
Mean anomaly: 72
7593 deg
Mean motion: 15
53796924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1818
Checksum: 350
Coasting Arc #13 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2016/255/00:47:05
983
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1063356
91 A = 6779144
63 meter
Y = 4331574
02 meter E =
0004974
Z = 5107266
67 I = 51
56073
XDOT = -7486
954394 Wp = 349
07284
YDOT = 106
852948 meter/sec RA = 349
14068 deg
ZDOT = -1644
925762 TA = 116
85132
MA = 116
80047
Ha = 220
046 n
mi
Hp = 217
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3488703
79 X = -1136523
48
Y = 14211200
84 feet Y = 4319274
08 meter
Z = 16756124
23 Z = 5101923
17
XDOT = -24563
498667 XDOT = -7479
602485
YDOT = 350
567414 feet/sec YDOT = 23
169810 meter/sec
ZDOT = -5396
738064 ZDOT = -1681
277560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3249205
82 X = -990357
93
Y = 14296215
11 feet Y = 4357486
37 meter
Z = 16731941
84 Z = 5099895
87
XDOT = -23469
733924 XDOT = -7153
574900
YDOT = 1185
326069 feet/sec YDOT = 361
287386 meter/sec
ZDOT = -5555
561465 ZDOT = -1693
335135
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
07803273
00016717 00000-0 10270-3 0 9129
2 25544 51
6433 349
4936 0005488 290
8269 69
2295 15
53838863 18342
Satellite: ISS
Catalog Number: 25544
Epoch time: 16255
07803273 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 349
4936 deg
Eccentricity:
0005488
Arg of perigee: 290
8269 deg
Mean anomaly: 69
2295 deg
Mean motion: 15
53838863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 345
Coasting Arc #14 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2016/256/00:47:05
983
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2620212
89 A = 6781906
50 meter
Y = -4410254
33 meter E =
0003708
Z = -4439642
05 I = 51
53953
XDOT = 6875
919752 Wp = 103
16299
YDOT = 768
551091 meter/sec RA = 344
14243 deg
ZDOT = 3296
101217 TA = 200
14579
MA = 200
16042
Ha = 220
236 n
mi
Hp = 217
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8596498
98 X = 2690900
49
Y = -14469338
35 feet Y = -4380558
43 meter
Z = -14565754
74 Z = -4426741
78
XDOT = 22558
791836 XDOT = 6850
803631
YDOT = 2521
493081 feet/sec YDOT = 845
302030 meter/sec
ZDOT = 10813
980370 ZDOT = 3329
441473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8081198
92 X = 2463149
43
Y = -14819545
53 feet Y = -4516997
48 meter
Z = -14508551
02 Z = -4422206
35
XDOT = 21493
152555 XDOT = 6551
112899
YDOT = 995
702598 feet/sec YDOT = 303
490152 meter/sec
ZDOT = 10959
472966 ZDOT = 3340
447360
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
04275874
00016717 00000-0 10270-3 0 9138
2 25544 51
6444 344
6865 0005461 295
2853 64
7733 15
53831620 18498
Satellite: ISS
Catalog Number: 25544
Epoch time: 16256
04275874 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 344
6865 deg
Eccentricity:
0005461
Arg of perigee: 295
2853 deg
Mean anomaly: 64
7733 deg
Mean motion: 15
53831620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1849
Checksum: 330
Coasting Arc #15 (Orbit 1864)
---------------------------------------
Vector Time (GMT): 2016/257/00:47:05
983
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3976269
80 A = 6785498
10 meter
Y = 4359958
32 meter E =
0008306
Z = 3345703
20 I = 51
52031
XDOT = -5836
142201 Wp = 73
42762
YDOT = -1739
116743 meter/sec RA = 339
15166 deg
ZDOT = -4657
824691 TA = 67
51834
MA = 67
43042
Ha = 220
410 n
mi
Hp = 216
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13045504
59 X = -4040980
30
Y = 14304325
19 feet Y = 4315131
47 meter
Z = 10976716
52 Z = 3326230
08
XDOT = -19147
448166 XDOT = -5793
635665
YDOT = -5705
763591 feet/sec YDOT = -1804
143118 meter/sec
ZDOT = -15281
577071 ZDOT = -4686
071604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12252850
76 X = -3734668
91
Y = 15051409
55 feet Y = 4587669
63 meter
Z = 10890818
77 Z = 3319521
56
XDOT = -18253
099536 XDOT = -5563
544739
YDOT = -3684
305306 feet/sec YDOT = -1122
976257 meter/sec
ZDOT = -15404
629758 ZDOT = -4695
331150
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
07178585
00016717 00000-0 10270-3 0 9144
2 25544 51
6439 339
5601 0005330 300
0835 59
9789 15
53840367 18656
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
07178585 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 339
5601 deg
Eccentricity:
0005330
Arg of perigee: 300
0835 deg
Mean anomaly: 59
9789 deg
Mean motion: 15
53840367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1865
Checksum: 334
Coasting Arc #16 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2016/257/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3344213
57 A = 6778827
20 meter
Y = 2936129
67 meter E =
0000771
Z = 5114119
06 I = 51
47185
XDOT = -6171
975584 Wp = 281
26655
YDOT = 4263
279948 meter/sec RA = 335
07367 deg
ZDOT = 1588
672156 TA = 153
37746
MA = 153
37350
Ha = 220
309 n
mi
Hp = 216
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10971829
29 X = 3286290
49
Y = 9632971
35 feet Y = 2973203
55 meter
Z = 16778605
84 Z = 5130223
29
XDOT = -20249
263727 XDOT = -6226
906971
YDOT = 13987
138937 feet/sec YDOT = 4193
953800 meter/sec
ZDOT = 5212
178989 ZDOT = 1558
556653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2686708
94 X = -818908
88
Y = 14269203
84 feet Y = 4349253
33 meter
Z = 16848388
82 Z = 5135388
91
XDOT = -21378
855367 XDOT = -6516
275116
YDOT = -10022
019979 feet/sec YDOT = -3054
711689 meter/sec
ZDOT = 5079
822504 ZDOT = 1548
329899
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
90785819
00016717 00000-0 10270-3 0 9151
2 25544 51
6416 335
3930 0005529 302
1411 57
9204 15
53892804 18780
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
90785819 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 335
3930 deg
Eccentricity:
0005529
Arg of perigee: 302
1411 deg
Mean anomaly: 57
9204 deg
Mean motion: 15
53892804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1878
Checksum: 325
Coasting Arc #17 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2016/258/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1876829
19 A = 6778111
30 meter
Y = -3795814
29 meter E =
0010748
Z = -5301550
07 I = 51
44085
XDOT = 6728
194997 Wp = 74
97149
YDOT = -3655
276798 meter/sec RA = 330
06384 deg
ZDOT = 238
364379 TA = 197
29065
MA = 197
32728
Ha = 220
554 n
mi
Hp = 216
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6157576
07 X = -1808491
49
Y = -12453458
94 feet Y = -3816420
79 meter
Z = -17393536
98 Z = -5310500
72
XDOT = 22074
130567 XDOT = 6767
411316
YDOT = -11992
377946 feet/sec YDOT = -3579
818311 meter/sec
ZDOT = 782
035365 ZDOT = 271
143693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7381153
69 X = 2249775
64
Y = -11712663
00 feet Y = -3570019
68 meter
Z = -17431913
46 Z = -5313247
22
XDOT = 20987
249572 XDOT = 6396
913670
YDOT = 11863
131609 feet/sec YDOT = 3615
882514 meter/sec
ZDOT = 925
897486 ZDOT = 282
213554
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
87254929
00016717 00000-0 10270-3 0 9162
2 25544 51
6420 330
5857 0005506 306
5722 53
4923 15
53877145 18935
Satellite: ISS
Catalog Number: 25544
Epoch time: 16258
87254929 = yrday
fracday
Element set: 916
Inclination: 51
6420 deg
RA of node: 330
5857 deg
Eccentricity:
0005506
Arg of perigee: 306
5722 deg
Mean anomaly: 53
4923 deg
Mean motion: 15
53877145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1893
Checksum: 331
Coasting Arc #18 (Orbit 1908)
---------------------------------------
Vector Time (GMT): 2016/259/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 363843
83 A = 6779504
06 meter
Y = 4590028
67 meter E =
0007092
Z = 4977401
02 I = 51
41822
XDOT = -6842
472947 Wp = 8
03422
YDOT = 2780
181270 meter/sec RA = 325
05385 deg
ZDOT = -2056
387471 TA = 102
07271
MA = 101
99324
Ha = 220
766 n
mi
Hp = 216
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1193713
36 X = 288311
98
Y = 15059149
18 feet Y = 4593675
77 meter
Z = 16330055
84 Z = 4978984
39
XDOT = -22449
058226 XDOT = -6863
064103
YDOT = 9121
329625 feet/sec YDOT = 2703
548735 meter/sec
ZDOT = -6746
678055 ZDOT = -2089
676699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12057684
41 X = -3675182
21
Y = 9089409
63 feet Y = 2770452
05 meter
Z = 16336111
19 Z = 4979246
69
XDOT = -19159
573005 XDOT = -5839
837852
YDOT = -12985
871933 feet/sec YDOT = -3958
093765 meter/sec
ZDOT = -6892
587877 ZDOT = -2100
860785
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 16259
90154025
00016717 00000-0 10270-3 0 9174
2 25544 51
6421 325
4590 0005515 311
7239 48
3441 15
53892355 19090
Satellite: ISS
Catalog Number: 25544
Epoch time: 16259
90154025 = yrday
fracday
Element set: 917
Inclination: 51
6421 deg
RA of node: 325
4590 deg
Eccentricity:
0005515
Arg of perigee: 311
7239 deg
Mean anomaly: 48
3441 deg
Mean motion: 15
53892355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1909
Checksum: 308
Coasting Arc #19 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2016/260/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1038574
38 A = 6782552
91 meter
Y = -5233106
92 meter E =
0003706
Z = -4190054
95 I = 51
40182
XDOT = 6524
405662 Wp = 68
83939
YDOT = -1641
950304 meter/sec RA = 320
04753 deg
ZDOT = 3671
811920 TA = 238
94702
MA = 238
98341
Ha = 220
875 n
mi
Hp = 216
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3407396
27 X = 1117368
59
Y = -17168985
97 feet Y = -5221052
94 meter
Z = -13746899
44 Z = -4184817
68
XDOT = 21405
530388 XDOT = 6524
445401
YDOT = -5386
976062 feet/sec YDOT = -1568
989265 meter/sec
ZDOT = 12046
627034 ZDOT = 3703
506139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16205745
09 X = 4939511
10
Y = -6664326
66 feet Y = -2031286
77 meter
Z = -13723055
39 Z = -4182787
28
XDOT = 15870
141419 XDOT = 4837
219105
YDOT = 13526
502192 feet/sec YDOT = 4122
877868 meter/sec
ZDOT = 12185
345173 ZDOT = 3714
093209
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 16260
86620877
00016717 00000-0 10270-3 0 9185
2 25544 51
6412 320
6522 0005555 315
3580 44
7125 15
53908399 19247
Satellite: ISS
Catalog Number: 25544
Epoch time: 16260
86620877 = yrday
fracday
Element set: 918
Inclination: 51
6412 deg
RA of node: 320
6522 deg
Eccentricity:
0005555
Arg of perigee: 315
3580 deg
Mean anomaly: 44
7125 deg
Mean motion: 15
53908399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1924
Checksum: 316
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