[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 24th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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
239/04:51:15
873 0
7 1
0 1
0
N/A 0
7 -0
1 221
5
000/00:02:31
746 0
2 -0
0 215
2
242/05:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
6
246/10:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 215
8
Coasting Arc #1 (Orbit 3221)
---------------------------------------
Vector Time (GMT): 2017/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2447772
49 A = 6778547
11 meter
Y = 3807281
09 meter E =
0009675
Z = 5043613
82 I = 51
95512
XDOT = -4760
497062 Wp = 145
52006
YDOT = -5682
583625 meter/sec RA = 62
04646 deg
ZDOT = 1969
640796 TA = 285
39622
MA = 285
50308
Ha = 221
925 n
mi
Hp = 214
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8030749
62 X = -2514663
63
Y = 12491079
68 feet Y = 3779534
82 meter
Z = 16547289
42 Z = 5031560
70
XDOT = -15618
428681 XDOT = -4706
166506
YDOT = -18643
647063 feet/sec YDOT = -5735
514808 meter/sec
ZDOT = 6462
076104 ZDOT = 1946
648531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13162135
31 X = 4011818
84
Y = -7004526
95 feet Y = -2134979
82 meter
Z = 16493259
06 Z = 5027145
36
XDOT = 4191
785765 XDOT = 1277
656301
YDOT = 22929
551181 feet/sec YDOT = 6988
927200 meter/sec
ZDOT = 6361
147931 ZDOT = 1938
877889
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 17235
55160075
00016717 00000-0 10270-3 0 9004
2 25544 51
6372 62
5046 0004823 172
2324 187
8904 15
54146595 32228
Satellite: ISS
Catalog Number: 25544
Epoch time: 17235
55160075 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 62
5046 deg
Eccentricity:
0004823
Arg of perigee: 172
2324 deg
Mean anomaly: 187
8904 deg
Mean motion: 15
54146595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3222
Checksum: 296
Coasting Arc #2 (Orbit 3236)
---------------------------------------
Vector Time (GMT): 2017/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3500789
65 A = 6777171
75 meter
Y = -2293089
17 meter E =
0016046
Z = -5343832
02 I = 51
93459
XDOT = 4177
458954 Wp = 107
81393
YDOT = 6417
502133 meter/sec RA = 57
06660 deg
ZDOT = -21
950872 TA = 162
00589
MA = 161
94903
Ha = 221
770 n
mi
Hp = 214
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11485530
35 X = 3552128
84
Y = -7523258
44 feet Y = -2253654
37 meter
Z = -17532257
29 Z = -5326701
56
XDOT = 13705
573996 XDOT = 4105
492893
YDOT = 21054
797025 feet/sec YDOT = 6463
814936 meter/sec
ZDOT = -72
017297 ZDOT = -1
833641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13773069
18 X = -4198031
49
Y = 1219881
73 feet Y = 371819
95 meter
Z = -17455982
49 Z = -5320583
46
XDOT = -2167
666257 XDOT = -660
704675
YDOT = -24016
839463 feet/sec YDOT = -7320
332668 meter/sec
ZDOT = 16
039268 ZDOT = 4
888769
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 17236
51609294
00016717 00000-0 10270-3 0 9013
2 25544 51
6371 57
6951 0004978 175
6836 184
4360 15
54192823 32373
Satellite: ISS
Catalog Number: 25544
Epoch time: 17236
51609294 = yrday
fracday
Element set: 901
Inclination: 51
6371 deg
RA of node: 57
6951 deg
Eccentricity:
0004978
Arg of perigee: 175
6836 deg
Mean anomaly: 184
4360 deg
Mean motion: 15
54192823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3237
Checksum: 330
Coasting Arc #3 (Orbit 3252)
---------------------------------------
Vector Time (GMT): 2017/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4448512
70 A = 6778479
21 meter
Y = 736177
21 meter E =
0005098
Z = 5056651
50 I = 51
92079
XDOT = -3283
883769 Wp = 109
52864
YDOT = -6663
141507 meter/sec RA = 52
08630 deg
ZDOT = -1918
979217 TA = 358
99767
MA = 358
99870
Ha = 221
837 n
mi
Hp = 214
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14594857
95 X = -4480976
77
Y = 2415279
55 feet Y = 686249
82 meter
Z = 16590063
96 Z = 5034963
24
XDOT = -10773
896880 XDOT = -3199
809295
YDOT = -21860
700482 feet/sec YDOT = -6699
394206 meter/sec
ZDOT = -6295
863574 ZDOT = -1934
726423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14203888
10 X = 4329345
09
Y = 4502868
35 feet Y = 1372474
27 meter
Z = 16493859
94 Z = 5027328
51
XDOT = -1
186708 XDOT = -
361709
YDOT = 23315
610900 feet/sec YDOT = 7106
598202 meter/sec
ZDOT = -6364
505238 ZDOT = -1939
901196
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 17237
54488269
00016717 00000-0 10270-3 0 9025
2 25544 51
6378 52
5655 0004946 179
8104 180
3052 15
54166291 32535
Satellite: ISS
Catalog Number: 25544
Epoch time: 17237
54488269 = yrday
fracday
Element set: 902
Inclination: 51
6378 deg
RA of node: 52
5655 deg
Eccentricity:
0004946
Arg of perigee: 179
8104 deg
Mean anomaly: 180
3052 deg
Mean motion: 15
54166291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3253
Checksum: 324
Coasting Arc #4 (Orbit 3267)
---------------------------------------
Vector Time (GMT): 2017/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5241608
17 A = 6781605
25 meter
Y = 749850
72 meter E =
0010690
Z = -4248610
37 I = 51
91084
XDOT = 2046
463265 Wp = 136
01295
YDOT = 6411
700099 meter/sec RA = 47
11078 deg
ZDOT = 3654
412933 TA = 171
31705
MA = 171
29854
Ha = 221
616 n
mi
Hp = 214
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17196877
20 X = 5253471
15
Y = 2460140
15 feet Y = 808531
96 meter
Z = -13939010
41 Z = -4223119
62
XDOT = 6714
118324 XDOT = 1956
862567
YDOT = 21035
761479 feet/sec YDOT = 6434
084336 meter/sec
ZDOT = 11989
543743 ZDOT = 3664
135858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14470915
80 X = -4410735
14
Y = -9772879
87 feet Y = -2978773
78 meter
Z = -13826217
88 Z = -4214231
21
XDOT = 2521
666888 XDOT = 768
604068
YDOT = -20764
786068 feet/sec YDOT = -6329
106794 meter/sec
ZDOT = 12031
527141 ZDOT = 3667
209472
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 17238
50936973
00016717 00000-0 10270-3 0 9033
2 25544 51
6379 47
7564 0005024 181
3519 178
7621 15
54200603 32682
Satellite: ISS
Catalog Number: 25544
Epoch time: 17238
50936973 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 47
7564 deg
Eccentricity:
0005024
Arg of perigee: 181
3519 deg
Mean anomaly: 178
7621 deg
Mean motion: 15
54200603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3268
Checksum: 319
Coasting Arc #5 (Orbit 3278)
---------------------------------------
Vector Time (GMT): 2017/239/04:52:31
746
Vector Time (MET): N/A
Weight (LBS) : 925114
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4003275
53 A = 6778414
27 meter
Y = -1796411
52 meter E =
0014151
Z = -5178677
31 I = 51
88590
XDOT = 4579
773593 Wp = 120
07366
YDOT = 5959
160902 meter/sec RA = 43
63497 deg
ZDOT = 1469
248874 TA = 164
06263
MA = 164
01806
Ha = 221
464 n
mi
Hp = 215
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13134106
06 X = 4048221
35
Y = -5893738
57 feet Y = -1751393
21 meter
Z = -16990411
12 Z = -5159121
41
XDOT = 15025
503915 XDOT = 4505
659430
YDOT = 19551
052828 feet/sec YDOT = 6009
960752 meter/sec
ZDOT = 4820
370322 ZDOT = 1491
315505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4508827
45 X = 1374290
61
Y = -13778892
07 feet Y = -4199806
30 meter
Z = -16903478
19 Z = -5152180
15
XDOT = 23553
615488 XDOT = 7179
142001
YDOT = 1659
450402 feet/sec YDOT = 505
800482 meter/sec
ZDOT = 4917
100769 ZDOT = 1498
732314
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 17239
21665962
00016717 00000-0 10270-3 0 9040
2 25544 51
6413 44
2346 0004625 195
4755 164
6257 15
54021809 32795
Satellite: ISS
Catalog Number: 25544
Epoch time: 17239
21665962 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 44
2346 deg
Eccentricity:
0004625
Arg of perigee: 195
4755 deg
Mean anomaly: 164
6257 deg
Mean motion: 15
54021809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 319
Coasting Arc #6 (Orbit 3294)
---------------------------------------
Vector Time (GMT): 2017/240/04:52:31
746
Vector Time (MET): N/A
Weight (LBS) : 925114
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5036133
04 A = 6781119
94 meter
Y = 501412
61 meter E =
0006962
Z = 4506783
49 I = 51
87078
XDOT = -3486
019803 Wp = 98
19686
YDOT = -6026
966528 meter/sec RA = 38
65819 deg
ZDOT = -3221
654930 TA = 24
08539
MA = 24
05285
Ha = 221
471 n
mi
Hp = 215
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16522746
19 X = -5063257
36
Y = 1645054
48 feet Y = 444943
73 meter
Z = 14786035
07 Z = 4482253
67
XDOT = -11437
072845 XDOT = -3402
716394
YDOT = -19773
512232 feet/sec YDOT = -6065
483981 meter/sec
ZDOT = -10569
734022 ZDOT = -3238
386220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9690885
15 X = -2953781
79
Y = 13601394
83 feet Y = 4145705
14 meter
Z = 14677294
80 Z = 4473639
45
XDOT = -21380
115304 XDOT = -6516
659145
YDOT = -3736
804258 feet/sec YDOT = -1138
977938 meter/sec
ZDOT = -10642
806113 ZDOT = -3243
927303
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 17240
24556185
00016717 00000-0 10270-3 0 9052
2 25544 51
6414 39
1073 0004611 199
8285 160
2689 15
54028731 32957
Satellite: ISS
Catalog Number: 25544
Epoch time: 17240
24556185 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 39
1073 deg
Eccentricity:
0004611
Arg of perigee: 199
8285 deg
Mean anomaly: 160
2689 deg
Mean motion: 15
54028731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3295
Checksum: 313
Coasting Arc #7 (Orbit 3309)
---------------------------------------
Vector Time (GMT): 2017/241/04:52:31
746
Vector Time (MET): N/A
Weight (LBS) : 925114
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5835792
09 A = 6784780
06 meter
Y = 681590
66 meter E =
0004958
Z = -3399678
21 I = 51
85821
XDOT = 2035
967527 Wp = 143
13504
YDOT = 5741
445055 meter/sec RA = 33
68676 deg
ZDOT = 4645
612842 TA = 177
31204
MA = 177
30937
Ha = 221
182 n
mi
Hp = 215
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19146299
50 X = 5844250
56
Y = 2236189
82 feet Y = 746897
59 meter
Z = -11153799
91 Z = -3371309
31
XDOT = 6679
683489 XDOT = 1949
047800
YDOT = 18836
761990 feet/sec YDOT = 5763
726849 meter/sec
ZDOT = 15241
511950 ZDOT = 4655
291532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14098725
65 X = 4297291
58
Y = -13251109
06 feet Y = -4038938
04 meter
Z = -11028264
86 Z = -3361415
13
XDOT = 17676
339671 XDOT = 5387
748332
YDOT = 6086
406343 feet/sec YDOT = 1855
136653 meter/sec
ZDOT = 15283
384107 ZDOT = 4658
375476
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 17241
21015330
00016717 00000-0 10270-3 0 9063
2 25544 51
6425 34
2989 0004564 203
4817 156
6128 15
54046859 33107
Satellite: ISS
Catalog Number: 25544
Epoch time: 17241
21015330 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 34
2989 deg
Eccentricity:
0004564
Arg of perigee: 203
4817 deg
Mean anomaly: 156
6128 deg
Mean motion: 15
54046859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3310
Checksum: 294
Coasting Arc #8 (Orbit 3325)
---------------------------------------
Vector Time (GMT): 2017/242/04:52:31
746
Vector Time (MET): N/A
Weight (LBS) : 925114
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6270469
74 A = 6788159
66 meter
Y = -1704292
85 meter E =
0014462
Z = 1933243
28 I = 51
84057
XDOT = -321
644063 Wp = 131
32188
YDOT = -5212
833620 meter/sec RA = 28
72525 deg
ZDOT = -5620
846160 TA = 27
41408
MA = 27
33785
Ha = 221
247 n
mi
Hp = 215
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20572407
28 X = -6260336
56
Y = -5591511
99 feet Y = -1774356
78 meter
Z = 6342661
67 Z = 1902808
08
XDOT = -1055
262675 XDOT = -236
025661
YDOT = -17102
472507 feet/sec YDOT = -5215
951961 meter/sec
ZDOT = -18441
096324 ZDOT = -5622
200444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17351405
25 X = -5288708
32
Y = 12454147
75 feet Y = 3796024
23 meter
Z = 6208159
49 Z = 1892247
01
XDOT = -12944
870958 XDOT = -3945
596668
YDOT = -8810
118438 feet/sec YDOT = -2685
324100 meter/sec
ZDOT = -18446
183064 ZDOT = -5622
396598
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 17242
23905004
00016717 00000-0 10270-3 0 9073
2 25544 51
6417 29
1717 0004618 206
2996 153
7922 15
54009666 33261
Satellite: ISS
Catalog Number: 25544
Epoch time: 17242
23905004 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 29
1717 deg
Eccentricity:
0004618
Arg of perigee: 206
2996 deg
Mean anomaly: 153
7922 deg
Mean motion: 15
54009666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3326
Checksum: 308
Coasting Arc #9 (Orbit 3325)
---------------------------------------
Vector Time (GMT): 2017/242/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925114
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5021056
35 A = 6781504
91 meter
Y = -1208443
37 meter E =
0009292
Z = -4404560
50 I = 51
81815
XDOT = 4275
061157 Wp = 139
08346
YDOT = 5371
943605 meter/sec RA = 28
58889 deg
ZDOT = 3396
784397 TA = 165
27392
MA = 165
24683
Ha = 221
033 n
mi
Hp = 215
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16473281
98 X = 5055591
42
Y = -3964709
23 feet Y = -1152101
57 meter
Z = -14450657
81 Z = -4380085
94
XDOT = 14025
791198 XDOT = 4198
173080
YDOT = 17624
486892 feet/sec YDOT = 5419
320474 meter/sec
ZDOT = 11144
305765 ZDOT = 3417
364280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4781405
59 X = 1457372
42
Y = -16350942
12 feet Y = -4983767
16 meter
Z = -14342046
65 Z = -4371455
82
XDOT = 21034
195714 XDOT = 6411
222854
YDOT = -3711
421313 feet/sec YDOT = -1131
241216 meter/sec
ZDOT = 11234
516351 ZDOT = 3424
280584
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 17242
23904851
00016717 00000-0 10270-3 0 9083
2 25544 51
6420 29
1715 0004556 209
3482 150
7415 15
54038185 33260
Satellite: ISS
Catalog Number: 25544
Epoch time: 17242
23904851 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 29
1715 deg
Eccentricity:
0004556
Arg of perigee: 209
3482 deg
Mean anomaly: 150
7415 deg
Mean motion: 15
54038185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3326
Checksum: 297
Coasting Arc #10 (Orbit 3341)
---------------------------------------
Vector Time (GMT): 2017/243/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925114
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5954717
74 A = 6785220
14 meter
Y = 173832
38 meter E =
0011352
Z = 3234050
30 I = 51
80182
XDOT = -2761
113420 Wp = 113
44473
YDOT = -5320
063090 meter/sec RA = 23
61618 deg
ZDOT = -4789
072284 TA = 29
17526
MA = 29
11189
Ha = 221
022 n
mi
Hp = 215
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19536475
53 X = -5971928
36
Y = 570316
21 feet Y = 107146
55 meter
Z = 10610401
26 Z = 3205082
49
XDOT = -9058
771064 XDOT = -2678
155022
YDOT = -17454
275230 feet/sec YDOT = -5350
476057 meter/sec
ZDOT = -15712
179410 ZDOT = -4802
283164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8937381
38 X = -2724113
85
Y = 17459354
82 feet Y = 5321611
35 meter
Z = 10482074
93 Z = 3194936
44
XDOT = -18337
917262 XDOT = -5589
397181
YDOT = 98
300471 feet/sec YDOT = 29
961984 meter/sec
ZDOT = -15769
754484 ZDOT = -4806
621167
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 17243
26794154
00016717 00000-0 10270-3 0 9091
2 25544 51
6422 24
0437 0004480 212
8510 147
2364 15
54052188 33425
Satellite: ISS
Catalog Number: 25544
Epoch time: 17243
26794154 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 24
0437 deg
Eccentricity:
0004480
Arg of perigee: 212
8510 deg
Mean anomaly: 147
2364 deg
Mean motion: 15
54052188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3342
Checksum: 290
Coasting Arc #11 (Orbit 3356)
---------------------------------------
Vector Time (GMT): 2017/244/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925114
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6514544
65 A = 6788290
69 meter
Y = 740882
99 meter E =
0003139
Z = -1754090
56 I = 51
78214
XDOT = 954
984817 Wp = 37
56651
YDOT = 5048
443825 meter/sec RA = 18
64943 deg
ZDOT = 5686
851750 TA = 303
22846
MA = 303
25854
Ha = 220
739 n
mi
Hp = 215
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21373177
98 X = 6514296
17
Y = 2430718
46 feet Y = 813731
61 meter
Z = -5754890
29 Z = -1722445
81
XDOT = 3133
152286 XDOT = 870
837087
YDOT = 16563
135910 feet/sec YDOT = 5058
652817 meter/sec
ZDOT = 18657
650099 ZDOT = 5691
286175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12132476
11 X = 3697978
72
Y = -17807753
84 feet Y = -5427803
37 meter
Z = -5614874
72 Z = -1711413
82
XDOT = 14759
249011 XDOT = 4498
619098
YDOT = 4175
011620 feet/sec YDOT = 1272
543542 meter/sec
ZDOT = 18676
399687 ZDOT = 5692
566625
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 17244
23252360
00016717 00000-0 10270-3 0 9109
2 25544 51
6425 19
2350 0004497 218
1845 141
8989 15
54057047 33574
Satellite: ISS
Catalog Number: 25544
Epoch time: 17244
23252360 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 19
2350 deg
Eccentricity:
0004497
Arg of perigee: 218
1845 deg
Mean anomaly: 141
8989 deg
Mean motion: 15
54057047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3357
Checksum: 307
Coasting Arc #12 (Orbit 3372)
---------------------------------------
Vector Time (GMT): 2017/245/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925114
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6602409
45 A = 6789665
59 meter
Y = -1546360
14 meter E =
0013303
Z = 76011
41 I = 51
75435
XDOT = 1012
973049 Wp = 153
76069
YDOT = -4640
337971 meter/sec RA = 13
68796 deg
ZDOT = -6024
067757 TA = 25
42156
MA = 25
35618
Ha = 220
743 n
mi
Hp = 215
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21661448
31 X = -6584996
16
Y = -5073360
03 feet Y = -1620095
41 meter
Z = 249381
28 Z = 43981
65
XDOT = 3323
402392 XDOT = 1094
048919
YDOT = -15224
205943 feet/sec YDOT = -4628
557152 meter/sec
ZDOT = -19764
001827 ZDOT = -6018
949982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14297171
13 X = -4357777
76
Y = 17046958
41 feet Y = 5195912
92 meter
Z = 107808
87 Z = 32860
14
XDOT = -10789
547912 XDOT = -3288
654203
YDOT = -8905
542515 feet/sec YDOT = -2714
409359 meter/sec
ZDOT = -19740
519873 ZDOT = -6016
910457
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 17245
26140950
00016717 00000-0 10270-3 0 9115
2 25544 51
6417 14
1068 0004579 220
2239 139
8575 15
54013652 33737
Satellite: ISS
Catalog Number: 25544
Epoch time: 17245
26140950 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 14
1068 deg
Eccentricity:
0004579
Arg of perigee: 220
2239 deg
Mean anomaly: 139
8575 deg
Mean motion: 15
54013652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3373
Checksum: 296
Coasting Arc #13 (Orbit 3388)
---------------------------------------
Vector Time (GMT): 2017/246/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 909883
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6211207
28 A = 6788353
06 meter
Y = 2220486
54 meter E =
0009625
Z = 1587260
75 I = 51
71831
XDOT = -2951
843408 Wp = 70
93738
YDOT = 4133
156615 meter/sec RA = 8
72394 deg
ZDOT = 5743
617238 TA = 306
40262
MA = 306
49136
Ha = 220
449 n
mi
Hp = 215
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20377976
62 X = 6178205
54
Y = 7285060
81 feet Y = 2289760
05 meter
Z = 5207548
40 Z = 1617352
22
XDOT = -9684
525618 XDOT = -3025
741417
YDOT = 13560
225114 feet/sec YDOT = 4099
734232 meter/sec
ZDOT = 18843
888577 ZDOT = 5729
098550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15418566
82 X = 4699579
17
Y = -15139365
90 feet Y = -4614478
73 meter
Z = 5340412
00 Z = 1627757
58
XDOT = 6832
208908 XDOT = 2082
457275
YDOT = 13611
090100 feet/sec YDOT = 4148
660262 meter/sec
ZDOT = 18778
868289 ZDOT = 5723
799054
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 17246
29028935
00016717 00000-0 10270-3 0 9128
2 25544 51
6413 8
9781 0004594 226
6711 133
4059 15
54078464 33894
Satellite: ISS
Catalog Number: 25544
Epoch time: 17246
29028935 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 8
9781 deg
Eccentricity:
0004594
Arg of perigee: 226
6711 deg
Mean anomaly: 133
4059 deg
Mean motion: 15
54078464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3389
Checksum: 326
Coasting Arc #14 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2017/246/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909883
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6680892
34 A = 6788956
47 meter
Y = -40991
56 meter E =
0004551
Z = -1194112
93 I = 51
71237
XDOT = 1074
944007 Wp = 35
15152
YDOT = 4817
924471 meter/sec RA = 7
75947 deg
ZDOT = 5863
523306 TA = 311
89511
MA = 311
93392
Ha = 220
689 n
mi
Hp = 215
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21918938
13 X = 6686654
53
Y = -134486
73 feet Y = 33750
88 meter
Z = -3917693
34 Z = -1161645
63
XDOT = 3526
719183 XDOT = 992
507033
YDOT = 15806
838817 feet/sec YDOT = 4829
484651 meter/sec
ZDOT = 19237
281189 ZDOT = 5868
544470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14745453
48 X = -4494414
22
Y = -16252244
21 feet Y = -4953684
03 meter
Z = -3773912
63 Z = -1150288
57
XDOT = 8318
256977 XDOT = 2535
404727
YDOT = -12007
410443 feet/sec YDOT = -3659
858703 meter/sec
ZDOT = 19258
669046 ZDOT = 5870
042325
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 17246
41890150
00016717 00000-0 10270-3 0 9139
2 25544 51
6397 8
3321 0004778 220
4391 139
6407 15
54062043 33913
Satellite: ISS
Catalog Number: 25544
Epoch time: 17246
41890150 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 8
3321 deg
Eccentricity:
0004778
Arg of perigee: 220
4391 deg
Mean anomaly: 139
6407 deg
Mean motion: 15
54062043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 296
Coasting Arc #15 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2017/247/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909883
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6723130
57 A = 6789316
82 meter
Y = -730804
41 meter E =
0012072
Z = -509055
70 I = 51
68142
XDOT = 959
882183 Wp = 160
85237
YDOT = -4693
275447 meter/sec RA = 2
79332 deg
ZDOT = -5990
891685 TA = 24
63759
MA = 24
57997
Ha = 220
424 n
mi
Hp = 215
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22057514
99 X = -6711986
13
Y = -2397652
27 feet Y = -805924
77 meter
Z = -1670130
26 Z = -541687
05
XDOT = 3149
219760 XDOT = 1041
392745
YDOT = -15397
885326 feet/sec YDOT = -4682
086117 meter/sec
ZDOT = -19655
156447 ZDOT = -5986
030585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13235439
17 X = 4034161
86
Y = 17793335
95 feet Y = 5423408
80 meter
Z = -1814492
99 Z = -553057
46
XDOT = -12221
647849 XDOT = -3725
158264
YDOT = 7104
725399 feet/sec YDOT = 2165
520302 meter/sec
ZDOT = -19632
809412 ZDOT = -5984
080309
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 17247
44777745
00016717 00000-0 10270-3 0 9148
2 25544 51
6397 3
2031 0004623 225
8639 134
2134 15
54088693 34073
Satellite: ISS
Catalog Number: 25544
Epoch time: 17247
44777745 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 3
2031 deg
Eccentricity:
0004623
Arg of perigee: 225
8639 deg
Mean anomaly: 134
2134 deg
Mean motion: 15
54088693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 315
Coasting Arc #16 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2017/248/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909883
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6270980
94 A = 6787391
96 meter
Y = 1455822
50 meter E =
0009687
Z = 2139214
60 I = 51
64340
XDOT = -2921
442813 Wp = 81
34400
YDOT = 4468
901448 meter/sec RA = 357
82393 deg
ZDOT = 5502
884516 TA = 302
36762
MA = 302
46134
Ha = 220
368 n
mi
Hp = 215
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20574084
44 X = 6243844
33
Y = 4776320
55 feet Y = 1525797
37 meter
Z = 7018420
59 Z = 2169610
68
XDOT = -9584
786132 XDOT = -2997
928143
YDOT = 14661
750158 feet/sec YDOT = 4435
804768 meter/sec
ZDOT = 18054
083059 ZDOT = 5488
507008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10771760
49 X = -3283232
60
Y = -18115511
66 feet Y = -5521607
96 meter
Z = 7152749
77 Z = 2180158
13
XDOT = 15976
163694 XDOT = 4869
534694
YDOT = -2371
345923 feet/sec YDOT = -722
786237 meter/sec
ZDOT = 17989
645381 ZDOT = 5483
243912
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 17248
47664852
00016717 00000-0 10270-3 0 9157
2 25544 51
6405 358
0753 0004761 228
0289 132
0459 15
54102511 34234
Satellite: ISS
Catalog Number: 25544
Epoch time: 17248
47664852 = yrday
fracday
Element set: 915
Inclination: 51
6405 deg
RA of node: 358
0753 deg
Eccentricity:
0004761
Arg of perigee: 228
0289 deg
Mean anomaly: 132
0459 deg
Mean motion: 15
54102511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 305
Coasting Arc #17 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2017/249/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909883
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5336834
35 A = 6783963
75 meter
Y = -2184169
66 meter E =
0002652
Z = -3572856
66 I = 51
59902
XDOT = 4670
946353 Wp = 142
74394
YDOT = -4140
804714 meter/sec RA = 352
84471 deg
ZDOT = -4449
494062 TA = 79
48288
MA = 79
45300
Ha = 220
185 n
mi
Hp = 216
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17509299
04 X = -5294658
70
Y = -7165910
97 feet Y = -2243614
36 meter
Z = -11721970
66 Z = -3598678
44
XDOT = 15324
627141 XDOT = 4738
516055
YDOT = -13585
317304 feet/sec YDOT = -4088
193699 meter/sec
ZDOT = -14598
077631 ZDOT = -4426
639672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7204490
55 X = 2195928
72
Y = 17416570
81 feet Y = 5308570
78 meter
Z = -11835911
71 Z = -3607585
89
XDOT = -19236
538436 XDOT = -5863
296915
YDOT = -1885
565064 feet/sec YDOT = -574
720231 meter/sec
ZDOT = -14496
176870 ZDOT = -4418
434710
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 17249
44121329
00016717 00000-0 10270-3 0 9163
2 25544 51
6404 353
2680 0004712 232
7098 127
3626 15
54075690 34381
Satellite: ISS
Catalog Number: 25544
Epoch time: 17249
44121329 = yrday
fracday
Element set: 916
Inclination: 51
6404 deg
RA of node: 353
2680 deg
Eccentricity:
0004712
Arg of perigee: 232
7098 deg
Mean anomaly: 127
3626 deg
Mean motion: 15
54075690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 308
Coasting Arc #18 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2017/250/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909883
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4033115
09 A = 6780205
90 meter
Y = 2886131
42 meter E =
0006986
Z = 4623295
89 I = 51
55580
XDOT = -6035
672342 Wp = 150
07611
YDOT = 3695
147632 meter/sec RA = 347
85256 deg
ZDOT = 2950
613983 TA = 270
45519
MA = 270
53525
Ha = 219
970 n
mi
Hp = 216
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13232004
90 X = 3978084
25
Y = 9468935
12 feet Y = 2930925
32 meter
Z = 15168293
61 Z = 4642753
42
XDOT = -19802
074613 XDOT = -6090
876453
YDOT = 12123
187768 feet/sec YDOT = 3627
344315 meter/sec
ZDOT = 9680
492070 ZDOT = 2921
160175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2814482
79 X = -857854
35
Y = -15944280
69 feet Y = -4859816
76 meter
Z = 15253931
19 Z = 4649398
23
XDOT = 21531
926135 XDOT = 6562
931086
YDOT = 5359
701858 feet/sec YDOT = 1633
637126 meter/sec
ZDOT = 9549
466345 ZDOT = 2910
677342
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 17250
47007496
00016717 00000-0 10270-3 0 9177
2 25544 51
6417 348
1395 0004734 237
5431 122
5264 15
54113424 34540
Satellite: ISS
Catalog Number: 25544
Epoch time: 17250
47007496 = yrday
fracday
Element set: 917
Inclination: 51
6417 deg
RA of node: 348
1395 deg
Eccentricity:
0004734
Arg of perigee: 237
5431 deg
Mean anomaly: 122
5264 deg
Mean motion: 15
54113424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 301
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