[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 9th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 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
254/00:50:05
163 3
7 3
8 3
8
N/A -0
3 -0
4 220
7
000/00:10:10
325 0
8 0
1 217
3
257/20:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 216
6
265/22:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 215
0
Coasting Arc #1 (Orbit 1809)
---------------------------------------
Vector Time (GMT): 2016/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893582
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6480302
65 A = 6787575
65 meter
Y = 1454900
31 meter E =
0010839
Z = 1375998
93 I = 51
64464
XDOT = -2244
747498 Wp = 116
92155
YDOT = -4476
822344 meter/sec RA = 356
78222 deg
ZDOT = -5807
700770 TA = 48
08524
MA = 47
99286
Ha = 219
827 n
mi
Hp = 214
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21260835
47 X = -6502774
10
Y = 4773294
97 feet Y = 1382307
67 meter
Z = 4514432
20 Z = 1344464
54
XDOT = -7364
657145 XDOT = -2166
308365
YDOT = -14687
737349 feet/sec YDOT = -4501
486448 meter/sec
ZDOT = -19054
136385 ZDOT = -5818
414362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21816350
53 X = 6649623
64
Y = -285818
72 feet Y = -87117
54 meter
Z = 4376382
66 Z = 1333921
44
XDOT = 4039
199351 XDOT = 1231
147962
YDOT = 14275
166439 feet/sec YDOT = 4351
070730 meter/sec
ZDOT = -19100
072221 ZDOT = -5821
702013
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
53476751
00016717 00000-0 10270-3 0 9002
2 25544 51
6439 357
1826 0003028 310
6236 49
4654 15
54472553 18109
Satellite: ISS
Catalog Number: 25544
Epoch time: 16253
53476751 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 357
1826 deg
Eccentricity:
0003028
Arg of perigee: 310
6236 deg
Mean anomaly: 49
4654 deg
Mean motion: 15
54472553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1810
Checksum: 305
Coasting Arc #2 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2016/254/00:55:10
325
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2930507
17 A = 6781380
35 meter
Y = -3995590
57 meter E =
0004420
Z = -4633651
88 I = 51
59994
XDOT = 6883
417321 Wp = 92
36816
YDOT = 1634
805961 meter/sec RA = 354
08975 deg
ZDOT = 2945
910305 TA = 206
99347
MA = 207
01647
Ha = 220
706 n
mi
Hp = 217
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9614524
83 X = 2997477
36
Y = -13108892
95 feet Y = -3962445
54 meter
Z = -15202269
96 Z = -4619253
29
XDOT = 22583
390160 XDOT = 6850
314954
YDOT = 5363
536619 feet/sec YDOT = 1711
596056 meter/sec
ZDOT = 9665
060055 ZDOT = 2979
267701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9146655
96 X = 2787900
74
Y = -13511214
22 feet Y = -4118218
10 meter
Z = -15138591
39 Z = -4614242
66
XDOT = 21742
797465 XDOT = 6627
204667
YDOT = 3735
378601 feet/sec YDOT = 1138
543397 meter/sec
ZDOT = 9810
470327 ZDOT = 2990
231356
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
04906591
00016717 00000-0 10270-3 0 9010
2 25544 51
6442 354
6202 0006164 302
1508 57
9052 15
53759898 18188
Satellite: ISS
Catalog Number: 25544
Epoch time: 16254
04906591 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 354
6202 deg
Eccentricity:
0006164
Arg of perigee: 302
1508 deg
Mean anomaly: 57
9052 deg
Mean motion: 15
53759898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1818
Checksum: 312
Coasting Arc #3 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2016/255/00:55:10
325
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4303840
28 A = 6784871
00 meter
Y = 3771465
83 meter E =
0008148
Z = 3643265
54 I = 51
57934
XDOT = -5819
711578 Wp = 57
51075
YDOT = -2409
066465 meter/sec RA = 349
10197 deg
ZDOT = -4369
644811 TA = 79
21602
MA = 79
12430
Ha = 220
835 n
mi
Hp = 217
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14120210
88 X = -4363391
26
Y = 12373575
55 feet Y = 3723004
67 meter
Z = 11952970
93 Z = 3622213
74
XDOT = -19093
541921 XDOT = -5771
114456
YDOT = -7903
761367 feet/sec YDOT = -2473
874936 meter/sec
ZDOT = -14336
105022 ZDOT = -4397
797242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13433376
68 X = -4094493
21
Y = 13199905
28 feet Y = 4023331
13 meter
Z = 11860275
41 Z = 3615011
95
XDOT = -18475
774491 XDOT = -5631
416065
YDOT = -5777
374557 feet/sec YDOT = -1760
943765 meter/sec
ZDOT = -14458
621910 ZDOT = -4406
987958
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
07814347
00016717 00000-0 10270-3 0 9022
2 25544 51
6439 349
4943 0006160 305
4428 54
6149 15
53757875 18343
Satellite: ISS
Catalog Number: 25544
Epoch time: 16255
07814347 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 349
4943 deg
Eccentricity:
0006160
Arg of perigee: 305
4428 deg
Mean anomaly: 54
6149 deg
Mean motion: 15
53757875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 329
Coasting Arc #4 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2016/256/00:55:10
325
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5352930
84 A = 6788040
82 meter
Y = -3449746
46 meter E =
0008195
Z = -2334954
02 I = 51
56032
XDOT = 4411
993014 Wp = 354
09346
YDOT = 3197
855368 meter/sec RA = 344
11897 deg
ZDOT = 5396
246085 TA = 339
83446
MA = 339
86681
Ha = 220
993 n
mi
Hp = 216
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17562109
07 X = 5402451
08
Y = -11318065
80 feet Y = -3389609
68 meter
Z = -7660610
30 Z = -2308830
44
XDOT = 14475
042697 XDOT = 4349
693376
YDOT = 10491
651470 feet/sec YDOT = 3246
845269 meter/sec
ZDOT = 17704
219438 ZDOT = 5417
526784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16689438
42 X = 5086940
83
Y = -12638605
89 feet Y = -3852247
08 meter
Z = -7545828
32 Z = -2299968
47
XDOT = 14202
470917 XDOT = 4328
913136
YDOT = 8141
681451 feet/sec YDOT = 2481
584506 meter/sec
ZDOT = 17796
563071 ZDOT = 5424
392424
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
04289205
00016717 00000-0 10270-3 0 9030
2 25544 51
6453 344
6871 0006304 309
2788 50
7805 15
53799495 18493
Satellite: ISS
Catalog Number: 25544
Epoch time: 16256
04289205 = yrday
fracday
Element set: 903
Inclination: 51
6453 deg
RA of node: 344
6871 deg
Eccentricity:
0006304
Arg of perigee: 309
2788 deg
Mean anomaly: 50
7805 deg
Mean motion: 15
53799495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1849
Checksum: 337
Coasting Arc #5 (Orbit 1864)
---------------------------------------
Vector Time (GMT): 2016/257/00:55:10
325
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6046622
63 A = 6790127
47 meter
Y = 2978575
38 meter E =
0007171
Z = 793733
34 I = 51
53584
XDOT = -2752
191834 Wp = 121
11450
YDOT = -3996
101898 meter/sec RA = 339
14282 deg
ZDOT = -5934
090006 TA = 50
29564
MA = 50
23244
Ha = 221
115 n
mi
Hp = 216
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19838000
74 X = -6083336
00
Y = 9772228
95 feet Y = 2910752
79 meter
Z = 2604112
00 Z = 764271
16
XDOT = -9029
500767 XDOT = -2678
476821
YDOT = -13110
570530 feet/sec YDOT = -4026
467084 meter/sec
ZDOT = -19468
799233 ZDOT = -5947
279984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18848097
81 X = -5744900
21
Y = 11595192
07 feet Y = 3534214
54 meter
Z = 2474845
70 Z = 754332
97
XDOT = -9250
757699 XDOT = -2819
630947
YDOT = -10843
063797 feet/sec YDOT = -3304
965845 meter/sec
ZDOT = -19525
648096 ZDOT = -5951
417540
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
07194931
00016717 00000-0 10270-3 0 9046
2 25544 51
6448 339
5610 0006181 313
2525 46
8111 15
53770308 18654
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
07194931 = yrday
fracday
Element set: 904
Inclination: 51
6448 deg
RA of node: 339
5610 deg
Eccentricity:
0006181
Arg of perigee: 313
2525 deg
Mean anomaly: 46
8111 deg
Mean motion: 15
53770308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1865
Checksum: 304
Coasting Arc #6 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2016/257/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3442275
79 A = 6779088
66 meter
Y = 2867246
39 meter E =
0001717
Z = 5087639
53 I = 51
47285
XDOT = -6102
468867 Wp = 349
42495
YDOT = 4323
206568 meter/sec RA = 335
07640 deg
ZDOT = 1694
215911 TA = 84
18008
MA = 84
16051
Ha = 221
078 n
mi
Hp = 216
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11293555
73 X = 3385244
32
Y = 9406976
36 feet Y = 2905421
86 meter
Z = 16691730
74 Z = 5104222
29
XDOT = -20021
223316 XDOT = -6158
588216
YDOT = 14183
748584 feet/sec YDOT = 4254
651059 meter/sec
ZDOT = 5558
451150 ZDOT = 1664
435159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2327260
44 X = -709348
98
Y = 14429639
02 feet Y = 4398153
97 meter
Z = 16763617
06 Z = 5109550
48
XDOT = -21419
896924 XDOT = -6528
784582
YDOT = -9753
495242 feet/sec YDOT = -2972
865350 meter/sec
ZDOT = 5427
545417 ZDOT = 1654
315843
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
90804893
00016717 00000-0 10270-3 0 9054
2 25544 51
6423 335
3943 0006394 316
1378 43
9267 15
53840896 18788
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
90804893 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 335
3943 deg
Eccentricity:
0006394
Arg of perigee: 316
1378 deg
Mean anomaly: 43
9267 deg
Mean motion: 15
53840896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1878
Checksum: 346
Coasting Arc #7 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2016/258/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2008757
81 A = 6778262
99 meter
Y = -3723158
16 meter E =
0011740
Z = -5305274
41 I = 51
44142
XDOT = 6679
720008 Wp = 66
36805
YDOT = -3748
389452 meter/sec RA = 330
06745 deg
ZDOT = 106
187921 TA = 204
61964
MA = 204
67573
Ha = 221
320 n
mi
Hp = 216
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6590412
76 X = -1941204
68
Y = -12215085
82 feet Y = -3745244
36 meter
Z = -17405755
92 Z = -5314867
84
XDOT = 21915
091890 XDOT = 6720
623191
YDOT = -12297
865657 feet/sec YDOT = -3673
463629 meter/sec
ZDOT = 348
385568 ZDOT = 138
735866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6950134
34 X = 2118400
95
Y = -11954147
49 feet Y = -3643624
15 meter
Z = -17446953
65 Z = -5317831
47
XDOT = 21146
505075 XDOT = 6445
454747
YDOT = 11600
499616 feet/sec YDOT = 3535
832283 meter/sec
ZDOT = 491
254743 ZDOT = 149
734446
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
87277498
00016717 00000-0 10270-3 0 9067
2 25544 51
6428 330
5873 0006392 320
4690 39
5996 15
53818626 18938
Satellite: ISS
Catalog Number: 25544
Epoch time: 16258
87277498 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 330
5873 deg
Eccentricity:
0006392
Arg of perigee: 320
4690 deg
Mean anomaly: 39
5996 deg
Mean motion: 15
53818626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1893
Checksum: 359
Coasting Arc #8 (Orbit 1908)
---------------------------------------
Vector Time (GMT): 2016/259/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 517282
63 A = 6779494
02 meter
Y = 4526236
77 meter E =
0008595
Z = 5022215
17 I = 51
41822
XDOT = -6829
658272 Wp = 7
28383
YDOT = 2911
410737 meter/sec RA = 325
05783 deg
ZDOT = -1911
718217 TA = 101
36628
MA = 101
26971
Ha = 221
536 n
mi
Hp = 216
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1697121
50 X = 442235
03
Y = 14849858
17 feet Y = 4531602
44 meter
Z = 16477083
91 Z = 5024545
09
XDOT = -22407
015329 XDOT = -6852
420559
YDOT = 9551
872496 feet/sec YDOT = 2834
909385 meter/sec
ZDOT = -6272
041394 ZDOT = -1944
950486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11609173
52 X = -3538476
09
Y = 9397772
20 feet Y = 2864440
97 meter
Z = 16486411
71 Z = 5025058
29
XDOT = -19477
549018 XDOT = -5936
756941
YDOT = -12752
105662 feet/sec YDOT = -3886
841806 meter/sec
ZDOT = -6417
727048 ZDOT = -1956
123204
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
90180647
00016717 00000-0 10270-3 0 9072
2 25544 51
6428 325
4609 0006433 325
3729 34
7004 15
53829371 19095
Satellite: ISS
Catalog Number: 25544
Epoch time: 16259
90180647 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 325
4609 deg
Eccentricity:
0006433
Arg of perigee: 325
3729 deg
Mean anomaly: 34
7004 deg
Mean motion: 15
53829371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1909
Checksum: 321
Coasting Arc #9 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2016/260/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 864090
61 A = 6782400
54 meter
Y = -5186714
57 meter E =
0005199
Z = -4286136
57 I = 51
40131
XDOT = 6556
901951 Wp = 59
05570
YDOT = -1818
281573 meter/sec RA = 320
05149 deg
ZDOT = 3528
015048 TA = 247
00080
MA = 247
05565
Ha = 221
644 n
mi
Hp = 216
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2834942
96 X = 942845
74
Y = -17016780
08 feet Y = -5176612
01 meter
Z = -14062127
85 Z = -4281747
00
XDOT = 21512
145507 XDOT = 6559
609557
YDOT = -5965
490725 feet/sec YDOT = -1744
942243 meter/sec
ZDOT = 11574
852520 ZDOT = 3559
873631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15761544
34 X = 4804118
71
Y = -7053173
62 feet Y = -2149807
32 meter
Z = -14041994
44 Z = -4279999
90
XDOT = 16383
307623 XDOT = 4993
632164
YDOT = 13327
575345 feet/sec YDOT = 4062
244965 meter/sec
ZDOT = 11714
321228 ZDOT = 3570
525110
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
86651613
00016717 00000-0 10270-3 0 9086
2 25544 51
6420 320
6545 0006466 328
8656 31
2113 15
53840844 19244
Satellite: ISS
Catalog Number: 25544
Epoch time: 16260
86651613 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 320
6545 deg
Eccentricity:
0006466
Arg of perigee: 328
8656 deg
Mean anomaly: 31
2113 deg
Mean motion: 15
53840844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1924
Checksum: 304
Coasting Arc #10 (Orbit 1939)
---------------------------------------
Vector Time (GMT): 2016/261/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2112296
93 A = 6785994
60 meter
Y = 5637823
26 meter E =
0010903
Z = 3127950
97 I = 51
38988
XDOT = -5932
071114 Wp = 64
57109
YDOT = 468
521900 meter/sec RA = 315
05220 deg
ZDOT = -4832
568942 TA = 79
27152
MA = 79
14878
Ha = 221
767 n
mi
Hp = 215
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6930108
05 X = -2190377
81
Y = 18496795
47 feet Y = 5613766
02 meter
Z = 10262306
35 Z = 3117499
46
XDOT = -19462
175572 XDOT = -5913
394735
YDOT = 1537
145341 feet/sec YDOT = 402
289225 meter/sec
ZDOT = -15854
884981 ZDOT = -4861
340262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19178152
05 X = -5845500
75
Y = 4828273
91 feet Y = 1471657
89 meter
Z = 10215626
59 Z = 3113722
99
XDOT = -11970
412702 XDOT = -3648
581791
YDOT = -13611
258357 feet/sec YDOT = -4148
711547 meter/sec
ZDOT = -15980
611073 ZDOT = -4870
890255
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 16261
89553240
00016717 00000-0 10270-3 0 9098
2 25544 51
6424 315
5275 0006527 332
3312 27
7492 15
53863289 19404
Satellite: ISS
Catalog Number: 25544
Epoch time: 16261
89553240 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 315
5275 deg
Eccentricity:
0006527
Arg of perigee: 332
3312 deg
Mean anomaly: 27
7492 deg
Mean motion: 15
53863289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1940
Checksum: 316
Coasting Arc #11 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2016/262/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3096679
78 A = 6788911
64 meter
Y = -5789609
60 meter E =
0012313
Z = -1697182
92 I = 51
37734
XDOT = 5050
887216 Wp = 9
64137
YDOT = 1042
247816 meter/sec RA = 310
05928 deg
ZDOT = 5678
308974 TA = 331
67580
MA = 331
74269
Ha = 221
911 n
mi
Hp = 215
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10159710
56 X = 3169434
76
Y = -18994782
15 feet Y = -5754573
88 meter
Z = -5568185
43 Z = -1681962
41
XDOT = 16571
152283 XDOT = 5011
274143
YDOT = 3419
448214 feet/sec YDOT = 1098
509503 meter/sec
ZDOT = 18629
622617 ZDOT = 5702
748751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21368596
48 X = 6513148
21
Y = -2855162
20 feet Y = -870253
44 meter
Z = -5500662
68 Z = -1676601
98
XDOT = 6649
083355 XDOT = 2026
640607
YDOT = 13781
036995 feet/sec YDOT = 4200
460076 meter/sec
ZDOT = 18736
149754 ZDOT = 5710
778445
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 16262
86022774
00016717 00000-0 10270-3 0 9101
2 25544 51
6422 310
7203 0006579 336
3760 23
7090 15
53861741 19555
Satellite: ISS
Catalog Number: 25544
Epoch time: 16262
86022774 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 310
7203 deg
Eccentricity:
0006579
Arg of perigee: 336
3760 deg
Mean anomaly: 23
7090 deg
Mean motion: 15
53861741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1955
Checksum: 300
Coasting Arc #12 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2016/263/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3849801
72 A = 6790076
89 meter
Y = 5590726
19 meter E =
0006998
Z = 77004
90 I = 51
36176
XDOT = -3982
782317 Wp = 109
08784
YDOT = -2654
001777 meter/sec RA = 305
07108 deg
ZDOT = -5985
413502 TA = 70
08006
MA = 70
00468
Ha = 222
022 n
mi
Hp = 215
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12630583
08 X = -3912406
58
Y = 18342277
53 feet Y = 5547325
09 meter
Z = 252640
73 Z = 58150
61
XDOT = -13066
871118 XDOT = -3923
733718
YDOT = -8707
354912 feet/sec YDOT = -2698
210469 meter/sec
ZDOT = -19637
183405 ZDOT = -6004
617322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22253775
80 X = -6782950
86
Y = 880569
64 feet Y = 268397
63 meter
Z = 169296
03 Z = 51601
43
XDOT = -718
767399 XDOT = -219
080303
YDOT = -13954
999668 feet/sec YDOT = -4253
483899 meter/sec
ZDOT = -19720
550901 ZDOT = -6010
823915
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 16263
88922959
00016717 00000-0 10270-3 0 9119
2 25544 51
6426 305
5928 0006528 340
5783 19
5120 15
53869316 19712
Satellite: ISS
Catalog Number: 25544
Epoch time: 16263
88922959 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 305
5928 deg
Eccentricity:
0006528
Arg of perigee: 340
5783 deg
Mean anomaly: 19
5120 deg
Mean motion: 15
53869316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1971
Checksum: 335
Coasting Arc #13 (Orbit 1986)
---------------------------------------
Vector Time (GMT): 2016/264/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4310056
35 A = 6789041
19 meter
Y = -5004312
45 meter E =
0016551
Z = 1526564
80 I = 51
34048
XDOT = 2859
623340 Wp = 39
19392
YDOT = 4219
470228 meter/sec RA = 300
08142 deg
ZDOT = 5736
806444 TA = 337
56814
MA = 337
64043
Ha = 222
076 n
mi
Hp = 215
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14140604
83 X = 4358280
04
Y = -16418347
94 feet Y = -4955844
73 meter
Z = 5008414
69 Z = 1547619
82
XDOT = 9381
966338 XDOT = 2784
360380
YDOT = 13843
406260 feet/sec YDOT = 4251
028204 meter/sec
ZDOT = 18821
543451 ZDOT = 5750
514700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21619629
70 X = 6589663
13
Y = 1082533
82 feet Y = 329956
31 meter
Z = 5101255
13 Z = 1554862
56
XDOT = -5183
658291 XDOT = -1579
979047
YDOT = 14226
587456 feet/sec YDOT = 4336
263856 meter/sec
ZDOT = 18880
632487 ZDOT = 5754
816782
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 16264
91822539
00016717 00000-0 10270-3 0 9128
2 25544 51
6424 300
4652 0006617 344
2847 15
8100 15
53877054 19871
Satellite: ISS
Catalog Number: 25544
Epoch time: 16264
91822539 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 300
4652 deg
Eccentricity:
0006617
Arg of perigee: 344
2847 deg
Mean anomaly: 15
8100 deg
Mean motion: 15
53877054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1987
Checksum: 313
Coasting Arc #14 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2016/265/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4552391
29 A = 6786081
56 meter
Y = 4039251
69 meter E =
0005713
Z = -3010552
10 I = 51
31691
XDOT = -1723
663114 Wp = 28
60608
YDOT = -5611
106298 meter/sec RA = 295
08572 deg
ZDOT = -4920
948522 TA = 186
00436
MA = 186
01121
Ha = 222
200 n
mi
Hp = 215
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14935666
97 X = -4582596
79
Y = 13252138
09 feet Y = 3988174
66 meter
Z = -9877139
44 Z = -3032740
38
XDOT = -5655
062711 XDOT = -1636
886122
YDOT = -18409
141396 feet/sec YDOT = -5629
896666 meter/sec
ZDOT = -16144
844231 ZDOT = -4929
110480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19645226
05 X = -5987864
90
Y = -3289480
30 feet Y = -1002633
60 meter
Z = -9974748
51 Z = -3040303
35
XDOT = 10632
567501 XDOT = 3240
806574
YDOT = -14427
680828 feet/sec YDOT = -4397
557116 meter/sec
ZDOT = -16179
470305 ZDOT = -4931
502549
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 16265
88290044
00016717 00000-0 10270-3 0 9136
2 25544 51
6438 295
6584 0006625 346
7830 13
3148 15
53899050 20027
Satellite: ISS
Catalog Number: 25544
Epoch time: 16265
88290044 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 295
6584 deg
Eccentricity:
0006625
Arg of perigee: 346
7830 deg
Mean anomaly: 13
3148 deg
Mean motion: 15
53899050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2002
Checksum: 317
Coasting Arc #15 (Orbit 2002)
---------------------------------------
Vector Time (GMT): 2016/265/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2925936
30 A = 6778891
14 meter
Y = -3402766
28 meter E =
0012091
Z = -5089804
36 I = 51
29173
XDOT = 4275
361528 Wp = 72
50600
YDOT = -6137
792463 meter/sec RA = 294
66224 deg
ZDOT = 1652
473097 TA = 213
50348
MA = 213
58001
Ha = 222
131 n
mi
Hp = 215
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9599528
53 X = -2862943
94
Y = -11163931
36 feet Y = -3435134
27 meter
Z = -16698833
22 Z = -5103864
67
XDOT = 14026
776668 XDOT = 4335
651055
YDOT = -20137
114381 feet/sec YDOT = -6089
645270 meter/sec
ZDOT = 5421
499663 ZDOT = 1673
388861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4280633
85 X = -1304737
20
Y = -14015239
02 feet Y = -4271844
85 meter
Z = -16759611
91 Z = -5108329
71
XDOT = 19811
925618 XDOT = 6038
674929
YDOT = -12618
060352 feet/sec YDOT = -3845
984795 meter/sec
ZDOT = 5513
930252 ZDOT = 1680
645941
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 16265
94721086
00016717 00000-0 10270-3 0 9149
2 25544 51
6436 295
3381 0006712 346
7322 13
3653 15
53919592 20036
Satellite: ISS
Catalog Number: 25544
Epoch time: 16265
94721086 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 295
3381 deg
Eccentricity:
0006712
Arg of perigee: 346
7322 deg
Mean anomaly: 13
3653 deg
Mean motion: 15
53919592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2003
Checksum: 309
Coasting Arc #16 (Orbit 2018)
---------------------------------------
Vector Time (GMT): 2016/266/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2033591
55 A = 6781623
55 meter
Y = 4756269
96 meter E =
0012555
Z = 4384669
40 I = 51
28835
XDOT = -4660
959869 Wp = 37
68771
YDOT = 5088
044517 meter/sec RA = 289
64509 deg
ZDOT = -3342
665763 TA = 86
35120
MA = 86
20763
Ha = 222
251 n
mi
Hp = 214
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6671888
29 X = 1958955
63
Y = 15604560
25 feet Y = 4778593
96 meter
Z = 14385398
31 Z = 4394366
50
XDOT = -15291
863087 XDOT = -4701
271936
YDOT = 16693
059439 feet/sec YDOT = 5035
696892 meter/sec
ZDOT = -10966
751190 ZDOT = -3365
405964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 136287
11 X = 41540
31
Y = 16935240
19 feet Y = 5161861
21 meter
Z = 14426889
61 Z = 4397315
95
XDOT = -19197
512073 XDOT = -5851
401680
YDOT = 9623
675143 feet/sec YDOT = 2933
296184 meter/sec
ZDOT = -11066
953130 ZDOT = -3373
207314
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 16266
97618975
00016717 00000-0 10270-3 0 9156
2 25544 51
6433 290
2103 0006859 350
4105 9
6915 15
53959847 20195
Satellite: ISS
Catalog Number: 25544
Epoch time: 16266
97618975 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 290
2103 deg
Eccentricity:
0006859
Arg of perigee: 350
4105 deg
Mean anomaly: 9
6915 deg
Mean motion: 15
53959847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2019
Checksum: 335
Coasting Arc #17 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2016/267/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1201695
60 A = 6785334
68 meter
Y = -5812628
89 meter E =
0008169
Z = -3283343
00 I = 51
28942
XDOT = 4841
538856 Wp = 28
44562
YDOT = -3646
406472 meter/sec RA = 284
63630 deg
ZDOT = 4695
270597 TA = 293
21494
MA = 293
30095
Ha = 222
361 n
mi
Hp = 214
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3942570
86 X = -1120658
89
Y = -19070304
74 feet Y = -5825614
20 meter
Z = -10772122
70 Z = -3288983
28
XDOT = 15884
313831 XDOT = 4859
146407
YDOT = -11963
275827 feet/sec YDOT = -3592
166335 meter/sec
ZDOT = 15404
431094 ZDOT = 4718
832679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3356642
77 X = 1023104
72
Y = -19168837
66 feet Y = -5842661
72 meter
Z = -10795722
65 Z = -3290536
26
XDOT = 17663
918832 XDOT = 5383
962460
YDOT = -5618
913140 feet/sec YDOT = -1712
644725 meter/sec
ZDOT = 15507
960289 ZDOT = 4726
826296
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 16267
94085419
00016717 00000-0 10270-3 0 9166
2 25544 51
6422 285
4032 0006751 353
7854 6
3214 15
53921886 20343
Satellite: ISS
Catalog Number: 25544
Epoch time: 16267
94085419 = yrday
fracday
Element set: 916
Inclination: 51
6422 deg
RA of node: 285
4032 deg
Eccentricity:
0006751
Arg of perigee: 353
7854 deg
Mean anomaly: 6
3214 deg
Mean motion: 15
53921886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2034
Checksum: 313
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