[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 18th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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
294/08:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
3
299/12:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 212
8
303/19:34:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 212
6
306/03:16:27
095 0
6 1
1 1
1
N/A 1
0 -0
1 222
6
000/00:02:54
191 -0
1 0
0 213
3
Coasting Arc #1 (Orbit 92)
---------------------------------------
Vector Time (GMT): 2017/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5907035
44 A = 6785776
16 meter
Y = 1721027
12 meter E =
0017086
Z = 2839403
06 I = 51
87215
XDOT = 810
531237 Wp = 66
76887
YDOT = -5672
132466 meter/sec RA = 142
51985 deg
ZDOT = 5106
483340 TA = 325
41781
MA = 325
52883
Ha = 222
344 n
mi
Hp = 213
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19380037
52 X = -5939634
09
Y = 5646414
42 feet Y = 1654788
66 meter
Z = 9315626
85 Z = 2810628
59
XDOT = 2659
223217 XDOT = 849
093015
YDOT = -18609
358485 feet/sec YDOT = -5662
852364 meter/sec
ZDOT = 16753
554265 ZDOT = 5110
515029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14926325
64 X = 4549544
05
Y = -13676193
12 feet Y = -4168503
66 meter
Z = 9187779
84 Z = 2800435
30
XDOT = 4961
967544 XDOT = 1512
407708
YDOT = 16722
864769 feet/sec YDOT = 5097
129182 meter/sec
ZDOT = 16772
174737 ZDOT = 5112
158860
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 17291
55862804
00016717 00000-0 10270-3 0 9005
2 25544 51
6388 143
3110 0005129 28
8249 331
3187 15
54206883 936
Satellite: ISS
Catalog Number: 25544
Epoch time: 17291
55862804 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 143
3110 deg
Eccentricity:
0005129
Arg of perigee: 28
8249 deg
Mean anomaly: 331
3187 deg
Mean motion: 15
54206883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 93
Checksum: 305
Coasting Arc #2 (Orbit 107)
---------------------------------------
Vector Time (GMT): 2017/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5346439
28 A = 6781915
38 meter
Y = -467731
00 meter E =
0011859
Z = -4159327
62 I = 51
88355
XDOT = -2396
994272 Wp = 55
66931
YDOT = 6212
441587 meter/sec RA = 137
55241 deg
ZDOT = -3780
904018 TA = 175
46362
MA = 175
45286
Ha = 222
276 n
mi
Hp = 213
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17540811
29 X = 5371476
66
Y = -1534550
52 feet Y = -407803
91 meter
Z = -13646087
99 Z = -4133294
82
XDOT = -7864
154436 XDOT = -2447
919098
YDOT = 20382
026204 feet/sec YDOT = 6185
351627 meter/sec
ZDOT = -12404
540741 ZDOT = -3792
672480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14964386
71 X = -4561145
07
Y = 9446789
96 feet Y = 2879381
58 meter
Z = -13530554
81 Z = -4124113
11
XDOT = -1737
606004 XDOT = -529
622310
YDOT = -20589
783714 feet/sec YDOT = -6275
766076 meter/sec
ZDOT = -12457
560877 ZDOT = -3797
064555
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 17292
52311250
00016717 00000-0 10270-3 0 9018
2 25544 51
6378 138
5024 0005047 31
8627 328
2830 15
54203870 1088
Satellite: ISS
Catalog Number: 25544
Epoch time: 17292
52311250 = yrday
fracday
Element set: 901
Inclination: 51
6378 deg
RA of node: 138
5024 deg
Eccentricity:
0005047
Arg of perigee: 31
8627 deg
Mean anomaly: 328
2830 deg
Mean motion: 15
54203870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 108
Checksum: 280
Coasting Arc #3 (Orbit 123)
---------------------------------------
Vector Time (GMT): 2017/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4463278
79 A = 6778641
88 meter
Y = -944906
40 meter E =
0008222
Z = 5006318
24 I = 51
89617
XDOT = 3681
572764 Wp = 84
65875
YDOT = -6407
353569 meter/sec RA = 132
57525 deg
ZDOT = 2070
719676 TA = 345
27589
MA = 345
29982
Ha = 222
561 n
mi
Hp = 213
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14643303
13 X = -4476699
74
Y = -3100086
62 feet Y = -994892
43 meter
Z = 16424928
61 Z = 4984603
95
XDOT = 12078
650801 XDOT = 3742
889078
YDOT = -21021
501210 feet/sec YDOT = -6365
840682 meter/sec
ZDOT = 6793
699725 ZDOT = 2088
753579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14458958
81 X = 4407090
64
Y = -4257485
03 feet Y = -1297681
44 meter
Z = 16328731
57 Z = 4976997
38
XDOT = -952
429055 XDOT = -290
300376
YDOT = 23158
856253 feet/sec YDOT = 7058
819386 meter/sec
ZDOT = 6874
555951 ZDOT = 2095
364654
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 17293
55189272
00016717 00000-0 10270-3 0 9020
2 25544 51
6381 133
3721 0005157 36
3536 323
7966 15
54181738 1246
Satellite: ISS
Catalog Number: 25544
Epoch time: 17293
55189272 = yrday
fracday
Element set: 902
Inclination: 51
6381 deg
RA of node: 133
3721 deg
Eccentricity:
0005157
Arg of perigee: 36
3536 deg
Mean anomaly: 323
7966 deg
Mean motion: 15
54181738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 124
Checksum: 310
Coasting Arc #4 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2017/294/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3329340
87 A = 6777047
54 meter
Y = 2541402
99 meter E =
0018657
Z = -5343477
17 I = 51
91227
XDOT = -4703
739879 Wp = 77
20964
YDOT = 6039
376170 meter/sec RA = 128
23282 deg
ZDOT = -54
506396 TA = 192
24930
MA = 192
29473
Ha = 222
398 n
mi
Hp = 213
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10923034
36 X = 3326631
47
Y = 8337936
33 feet Y = 2578618
41 meter
Z = -17531093
07 Z = -5327310
60
XDOT = -15432
217450 XDOT = -4770
659428
YDOT = 19814
226281 feet/sec YDOT = 5986
401565 meter/sec
ZDOT = -178
826758 ZDOT = -77
519308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8094721
44 X = -2467271
09
Y = -11216361
71 feet Y = -3418747
05 meter
Z = -17459719
38 Z = -5321722
47
XDOT = 19761
857264 XDOT = 6023
414094
YDOT = -13803
565306 feet/sec YDOT = -4207
326705 meter/sec
ZDOT = -281
739493 ZDOT = -85
874197
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 17294
38777204
00016717 00000-0 10270-3 0 9031
2 25544 51
6402 129
2064 0005225 39
2528 320
9003 15
54236853 1377
Satellite: ISS
Catalog Number: 25544
Epoch time: 17294
38777204 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 129
2064 deg
Eccentricity:
0005225
Arg of perigee: 39
2528 deg
Mean anomaly: 320
9003 deg
Mean motion: 15
54236853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 137
Checksum: 292
Coasting Arc #5 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2017/295/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2136137
42 A = 6778116
85 meter
Y = -3967052
26 meter E =
0010648
Z = 5058855
39 I = 51
93536
XDOT = 5241
567901 Wp = 49
33982
YDOT = -5268
265271 meter/sec RA = 123
25213 deg
ZDOT = -1908
592602 TA = 59
13042
MA = 59
02573
Ha = 222
416 n
mi
Hp = 213
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7008324
86 X = -2116192
12
Y = -13015263
33 feet Y = -3990828
21 meter
Z = 16597294
58 Z = 5048527
08
XDOT = 17196
745083 XDOT = 5309
360741
YDOT = -17284
334878 feet/sec YDOT = -5209
271534 meter/sec
ZDOT = -6261
786753 ZDOT = -1882
965043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3220329
95 X = 981556
57
Y = 14479087
65 feet Y = 4413225
92 meter
Z = 16552020
43 Z = 5045055
83
XDOT = -20306
006233 XDOT = -6189
270700
YDOT = 11579
065152 feet/sec YDOT = 3529
299058 meter/sec
ZDOT = -6147
357367 ZDOT = -1873
714525
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 17295
41654317
00016717 00000-0 10270-3 0 9046
2 25544 51
6399 124
0773 0005128 41
9960 318
1585 15
54264708 1536
Satellite: ISS
Catalog Number: 25544
Epoch time: 17295
41654317 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 124
0773 deg
Eccentricity:
0005128
Arg of perigee: 41
9960 deg
Mean anomaly: 318
1585 deg
Mean motion: 15
54264708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 153
Checksum: 316
Coasting Arc #6 (Orbit 167)
---------------------------------------
Vector Time (GMT): 2017/296/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 992355
81 A = 6781347
17 meter
Y = 5189748
84 meter E =
0011335
Z = -4259930
28 I = 51
96332
XDOT = -5403
943661 Wp = 86
11568
YDOT = 4020
591869 meter/sec RA = 118
27862 deg
ZDOT = 3648
407071 TA = 221
04975
MA = 221
13510
Ha = 222
443 n
mi
Hp = 213
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3255760
53 X = 954942
09
Y = 17026735
03 feet Y = 5200636
67 meter
Z = -13976149
22 Z = -4255200
69
XDOT = -17729
473953 XDOT = -5466
223992
YDOT = 13190
918206 feet/sec YDOT = 3959
813201 meter/sec
ZDOT = 11969
839472 ZDOT = 3622
004266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1218133
77 X = 371287
17
Y = -17308714
32 feet Y = -5275696
13 meter
Z = -13955894
38 Z = -4253756
61
XDOT = 19374
066400 XDOT = 5905
215439
YDOT = -8168
709605 feet/sec YDOT = -2489
822688 meter/sec
ZDOT = 11852
123259 ZDOT = 3612
527169
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 17296
38101475
00016717 00000-0 10270-3 0 9056
2 25544 51
6402 119
2683 0005127 44
9260 315
2306 15
54238124 1680
Satellite: ISS
Catalog Number: 25544
Epoch time: 17296
38101475 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 119
2683 deg
Eccentricity:
0005127
Arg of perigee: 44
9260 deg
Mean anomaly: 315
2306 deg
Mean motion: 15
54238124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 168
Checksum: 290
Coasting Arc #7 (Orbit 183)
---------------------------------------
Vector Time (GMT): 2017/297/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 108657
46 A = 6785209
92 meter
Y = -6098188
76 meter E =
0017094
Z = 2960764
63 I = 51
99154
XDOT = 5293
401792 Wp = 83
99470
YDOT = -2358
565666 meter/sec RA = 113
31616 deg
ZDOT = -5025
548356 TA = 62
34636
MA = 62
17295
Ha = 222
481 n
mi
Hp = 212
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 356487
74 X = 162458
67
Y = -20007180
99 feet Y = -6096672
77 meter
Z = 9713794
72 Z = 2961423
33
XDOT = 17366
803779 XDOT = 5343
794727
YDOT = -7738
076331 feet/sec YDOT = -2299
089620 meter/sec
ZDOT = -16488
019541 ZDOT = -4999
711557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5179066
64 X = -1578579
51
Y = 19326610
90 feet Y = 5890751
00 meter
Z = 9717590
35 Z = 2961921
54
XDOT = -17427
868490 XDOT = -5312
014316
YDOT = 3606
076895 feet/sec YDOT = 1099
132238 meter/sec
ZDOT = -16373
033077 ZDOT = -4990
500482
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 17297
40977831
00016717 00000-0 10270-3 0 9068
2 25544 51
6406 114
1384 0005297 47
6784 312
4817 15
54266687 1844
Satellite: ISS
Catalog Number: 25544
Epoch time: 17297
40977831 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 114
1384 deg
Eccentricity:
0005297
Arg of perigee: 47
6784 deg
Mean anomaly: 312
4817 deg
Mean motion: 15
54266687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 184
Checksum: 336
Coasting Arc #8 (Orbit 198)
---------------------------------------
Vector Time (GMT): 2017/298/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1037020
99 A = 6788217
04 meter
Y = 6558716
29 meter E =
0013749
Z = -1385781
04 I = 52
01178
XDOT = -4951
347085 Wp = 42
93364
YDOT = 441
613212 meter/sec RA = 108
36487 deg
ZDOT = 5839
051418 TA = 302
04307
MA = 302
17655
Ha = 222
560 n
mi
Hp = 212
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3402299
83 X = -1103553
64
Y = 21518098
07 feet Y = 6546747
58 meter
Z = -4546525
72 Z = -1390980
43
XDOT = -16244
577052 XDOT = -4984
281200
YDOT = 1448
862243 feet/sec YDOT = 386
059858 meter/sec
ZDOT = 19156
992841 ZDOT = 5814
918775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8188965
18 X = 2495996
59
Y = -20182318
54 feet Y = -6151570
69 meter
Z = -4570552
75 Z = -1393104
48
XDOT = 14797
861210 XDOT = 4510
388097
YDOT = 1722
447469 feet/sec YDOT = 525
001989 meter/sec
ZDOT = 19049
832774 ZDOT = 5806
389030
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 17298
37424213
00016717 00000-0 10270-3 0 9077
2 25544 51
6392 109
3298 0005231 51
2671 308
8949 15
54226620 1996
Satellite: ISS
Catalog Number: 25544
Epoch time: 17298
37424213 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 109
3298 deg
Eccentricity:
0005231
Arg of perigee: 51
2671 deg
Mean anomaly: 308
8949 deg
Mean motion: 15
54226620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 199
Checksum: 317
Coasting Arc #9 (Orbit 214)
---------------------------------------
Vector Time (GMT): 2017/299/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1868973
70 A = 6788995
32 meter
Y = -6511523
47 meter E =
0013045
Z = -392854
96 I = 52
02436
XDOT = 4447
795975 Wp = 115
16213
YDOT = 1630
533309 meter/sec RA = 103
42030 deg
ZDOT = -6027
122021 TA = 69
04967
MA = 68
91012
Ha = 222
558 n
mi
Hp = 212
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6131803
49 X = 1943556
72
Y = -21363265
98 feet Y = -6490206
32 meter
Z = -1288894
22 Z = -383594
59
XDOT = 14592
506479 XDOT = 4458
509723
YDOT = 5349
518730 feet/sec YDOT = 1680
331377 meter/sec
ZDOT = -19774
022380 ZDOT = -6005
489595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10513317
71 X = -3204459
24
Y = 19584814
20 feet Y = 5969451
37 meter
Z = -1246835
63 Z = -380035
50
XDOT = -11832
394770 XDOT = -3606
513926
YDOT = -7569
714954 feet/sec YDOT = -2307
249118 meter/sec
ZDOT = -19678
254898 ZDOT = -5997
932093
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 17299
40300024
00016717 00000-0 10270-3 0 9086
2 25544 51
6399 104
2007 0005053 56
0661 304
0972 15
54221099 2157
Satellite: ISS
Catalog Number: 25544
Epoch time: 17299
40300024 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 104
2007 deg
Eccentricity:
0005053
Arg of perigee: 56
0661 deg
Mean anomaly: 304
0972 deg
Mean motion: 15
54221099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 215
Checksum: 277
Coasting Arc #10 (Orbit 216)
---------------------------------------
Vector Time (GMT): 2017/299/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2970068
71 A = 6787089
33 meter
Y = -5736523
31 meter E =
0009061
Z = -2085024
52 I = 52
01726
XDOT = 3578
021746 Wp = 104
79176
YDOT = 3866
762654 meter/sec RA = 102
77575 deg
ZDOT = -5564
186474 TA = 98
14449
MA = 98
04169
Ha = 222
564 n
mi
Hp = 212
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9744319
90 X = 3044123
52
Y = -18820614
53 feet Y = -5702895
95 meter
Z = -6840631
62 Z = -2070416
57
XDOT = 11738
916491 XDOT = 3561
545259
YDOT = 12686
229180 feet/sec YDOT = 3906
682292 meter/sec
ZDOT = -18255
204966 ZDOT = -5546
845319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2937431
78 X = 895329
21
Y = 21010308
53 feet Y = 6403942
04 meter
Z = -6774951
85 Z = -2065005
32
XDOT = -15484
412365 XDOT = -4719
648889
YDOT = -3673
145248 feet/sec YDOT = -1119
574672 meter/sec
ZDOT = -18178
812678 ZDOT = -5540
902104
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 17299
53159478
00016717 00000-0 10270-3 0 9096
2 25544 51
6376 103
5550 0005217 59
4684 300
6983 15
54275207 2177
Satellite: ISS
Catalog Number: 25544
Epoch time: 17299
53159478 = yrday
fracday
Element set: 909
Inclination: 51
6376 deg
RA of node: 103
5550 deg
Eccentricity:
0005217
Arg of perigee: 59
4684 deg
Mean anomaly: 300
6983 deg
Mean motion: 15
54275207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 217
Checksum: 327
Coasting Arc #11 (Orbit 232)
---------------------------------------
Vector Time (GMT): 2017/300/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3435985
73 A = 6783632
58 meter
Y = 4635453
37 meter E =
0016860
Z = 3551047
41 I = 52
01196
XDOT = -2796
124010 Wp = 84
26474
YDOT = -5542
590209 meter/sec RA = 97
82155 deg
ZDOT = 4512
957673 TA = 317
41872
MA = 317
54933
Ha = 222
647 n
mi
Hp = 212
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11272919
07 X = -3504814
78
Y = 15208180
34 feet Y = 4596645
07 meter
Z = 11650418
00 Z = 3534188
87
XDOT = -9173
635204 XDOT = -2755
859583
YDOT = -18184
351079 feet/sec YDOT = -5573
633130 meter/sec
ZDOT = 14806
291577 ZDOT = 4499
472674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 101615
50 X = 30972
40
Y = -18976593
14 feet Y = -5784065
59 meter
Z = 11574898
70 Z = 3528029
12
XDOT = 16872
067660 XDOT = 5142
606223
YDOT = 9119
147452 feet/sec YDOT = 2779
516143 meter/sec
ZDOT = 14747
267732 ZDOT = 4494
967205
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 17300
56034714
00016717 00000-0 10270-3 0 9109
2 25544 51
6377 98
4252 0005105 65
1773 294
9911 15
54270419 2332
Satellite: ISS
Catalog Number: 25544
Epoch time: 17300
56034714 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 98
4252 deg
Eccentricity:
0005105
Arg of perigee: 65
1773 deg
Mean anomaly: 294
9911 deg
Mean motion: 15
54270419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 233
Checksum: 295
Coasting Arc #12 (Orbit 247)
---------------------------------------
Vector Time (GMT): 2017/301/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3810717
98 A = 6779794
54 meter
Y = -3123083
72 meter E =
0015671
Z = -4672563
77 I = 52
00287
XDOT = 1961
693545 Wp = 69
65641
YDOT = 6790
447488 meter/sec RA = 92
85849 deg
ZDOT = -2941
466393 TA = 171
17716
MA = 171
14959
Ha = 222
640 n
mi
Hp = 212
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12502355
57 X = 3868055
29
Y = -10246337
65 feet Y = -3080149
24 meter
Z = -15329933
61 Z = -4653912
81
XDOT = 6436
002445 XDOT = 1899
903576
YDOT = 22278
371024 feet/sec YDOT = 6812
038892 meter/sec
ZDOT = -9650
480293 ZDOT = -2932
087265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3785066
47 X = -1153688
26
Y = 15796055
17 feet Y = 4814637
62 meter
Z = -15246675
29 Z = -4647186
63
XDOT = -17544
303186 XDOT = -5347
503611
YDOT = -13471
105344 feet/sec YDOT = -4105
992909 meter/sec
ZDOT = -9609
876784 ZDOT = -2929
090444
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 17301
52479968
00016717 00000-0 10270-3 0 9111
2 25544 51
6380 93
6175 0005251 68
4946 291
6766 15
54267829 2486
Satellite: ISS
Catalog Number: 25544
Epoch time: 17301
52479968 = yrday
fracday
Element set: 911
Inclination: 51
6380 deg
RA of node: 93
6175 deg
Eccentricity:
0005251
Arg of perigee: 68
4946 deg
Mean anomaly: 291
6766 deg
Mean motion: 15
54267829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 248
Checksum: 341
Coasting Arc #13 (Orbit 263)
---------------------------------------
Vector Time (GMT): 2017/302/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4056516
68 A = 6777314
05 meter
Y = 1351432
74 meter E =
0007992
Z = 5251549
09 I = 51
99538
XDOT = -1115
369471 Wp = 92
74381
YDOT = -7517
581343 meter/sec RA = 87
88436 deg
ZDOT = 1071
242886 TA = 347
04300
MA = 347
06352
Ha = 222
763 n
mi
Hp = 212
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13308781
76 X = -4096837
12
Y = 4433834
45 feet Y = 1305844
81 meter
Z = 17229491
78 Z = 5231745
49
XDOT = -3659
348659 XDOT = -1036
426625
YDOT = -24663
980783 feet/sec YDOT = -7529
612716 meter/sec
ZDOT = 3514
576397 ZDOT = 1066
016799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7764515
24 X = 2366624
24
Y = -11811999
72 feet Y = -3600297
51 meter
Z = 17141380
12 Z = 5224692
66
XDOT = 17342
775283 XDOT = 5286
077906
YDOT = 16476
903494 feet/sec YDOT = 5022
160185 meter/sec
ZDOT = 3492
528975 ZDOT = 1064
522832
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 17302
55354472
00016717 00000-0 10270-3 0 9128
2 25544 51
6381 88
4871 0005116 71
4015 288
7693 15
54267114 2644
Satellite: ISS
Catalog Number: 25544
Epoch time: 17302
55354472 = yrday
fracday
Element set: 912
Inclination: 51
6381 deg
RA of node: 88
4871 deg
Eccentricity:
0005116
Arg of perigee: 71
4015 deg
Mean anomaly: 288
7693 deg
Mean motion: 15
54267114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 264
Checksum: 306
Coasting Arc #14 (Orbit 278)
---------------------------------------
Vector Time (GMT): 2017/303/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4228479
96 A = 6777194
91 meter
Y = 521340
01 meter E =
0019378
Z = -5287265
32 I = 51
99396
XDOT = 216
744068 Wp = 91
29428
YDOT = 7595
216308 meter/sec RA = 82
90795 deg
ZDOT = 924
746199 TA = 187
51091
MA = 187
53998
Ha = 222
642 n
mi
Hp = 212
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13872965
76 X = 4248019
30
Y = 1710433
11 feet Y = 568734
68 meter
Z = -17346671
00 Z = -5266676
91
XDOT = 711
102585 XDOT = 127
304182
YDOT = 24918
688675 feet/sec YDOT = 7597
140059 meter/sec
ZDOT = 3033
944221 ZDOT = 925
581366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11895194
33 X = -3625655
23
Y = 7553052
03 feet Y = 2302170
26 meter
Z = -17255361
84 Z = -5259434
29
XDOT = -15793
737231 XDOT = -4813
931108
YDOT = -17955
133401 feet/sec YDOT = -5472
724661 meter/sec
ZDOT = 3036
476286 ZDOT = 925
517972
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 17303
51798858
00016717 00000-0 10270-3 0 9136
2 25544 51
6392 83
6790 0005227 75
2463 284
9269 15
54282779 2792
Satellite: ISS
Catalog Number: 25544
Epoch time: 17303
51798858 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 83
6790 deg
Eccentricity:
0005227
Arg of perigee: 75
2463 deg
Mean anomaly: 284
9269 deg
Mean motion: 15
54282779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 279
Checksum: 352
Coasting Arc #15 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2017/303/19:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2309991
43 A = 6782504
58 meter
Y = -5059592
07 meter E =
0011777
Z = -3893995
45 I = 52
01242
XDOT = 4031
761211 Wp = 73
92487
YDOT = 5023
191745 meter/sec RA = 81
39561 deg
ZDOT = -4142
279196 TA = 152
76806
MA = 152
70626
Ha = 222
697 n
mi
Hp = 212
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7578712
03 X = 2385312
90
Y = -16599711
50 feet Y = -5033339
28 meter
Z = -12775575
63 Z = -3882590
74
XDOT = 13227
563029 XDOT = 3995
412400
YDOT = 16480
287877 feet/sec YDOT = 5068
074134 meter/sec
ZDOT = -13590
154844 ZDOT = -4122
782439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14546894
13 X = 4433893
33
Y = -11076376
21 feet Y = -3376079
47 meter
Z = -12724165
67 Z = -3878325
70
XDOT = 3236
517849 XDOT = 986
490641
YDOT = 19736
731825 feet/sec YDOT = 6015
755860 meter/sec
ZDOT = -13504
390503 ZDOT = -4116
138225
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 17303
83946790
00016717 00000-0 10270-3 0 9142
2 25544 51
6411 82
0792 0005404 73
2928 286
8818 15
54285842 2841
Satellite: ISS
Catalog Number: 25544
Epoch time: 17303
83946790 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 82
0792 deg
Eccentricity:
0005404
Arg of perigee: 73
2928 deg
Mean anomaly: 286
8818 deg
Mean motion: 15
54285842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 327
Coasting Arc #16 (Orbit 299)
---------------------------------------
Vector Time (GMT): 2017/304/19:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3036163
13 A = 6778925
65 meter
Y = 3609050
94 meter E =
0011728
Z = 4860300
69 I = 51
99258
XDOT = -3534
779499 Wp = 101
09536
YDOT = -6340
614374 meter/sec RA = 76
42818 deg
ZDOT = 2492
867537 TA = 324
52259
MA = 324
60053
Ha = 222
873 n
mi
Hp = 212
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9961165
13 X = -3099904
29
Y = 11840718
32 feet Y = 3574742
46 meter
Z = 15945868
40 Z = 4845396
56
XDOT = -11597
045601 XDOT = -3475
723717
YDOT = -20802
540598 feet/sec YDOT = -6379
812306 meter/sec
ZDOT = 8178
699269 ZDOT = 2475
840238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14339619
44 X = -4370716
01
Y = 5993850
66 feet Y = 1826925
68 meter
Z = 15879143
82 Z = 4839963
04
XDOT = -520
036992 XDOT = -158
507275
YDOT = -22777
343202 feet/sec YDOT = -6942
534208 meter/sec
ZDOT = 8104
113631 ZDOT = 2470
133835
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 17304
86820306
00016717 00000-0 10270-3 0 9151
2 25544 51
6391 76
9494 0005525 76
8822 283
2947 15
54280212 3004
Satellite: ISS
Catalog Number: 25544
Epoch time: 17304
86820306 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 76
9494 deg
Eccentricity:
0005525
Arg of perigee: 76
8822 deg
Mean anomaly: 283
2947 deg
Mean motion: 15
54280212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 300
Checksum: 309
Coasting Arc #17 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2017/305/19:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3752031
44 A = 6777044
03 meter
Y = -1911912
91 meter E =
0019998
Z = -5327198
04 I = 51
97831
XDOT = 2831
879040 Wp = 84
13495
YDOT = 7089
423691 meter/sec RA = 71
45272 deg
ZDOT = -549
615294 TA = 180
63379
MA = 180
63633
Ha = 222
698 n
mi
Hp = 212
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12309814
42 X = 3799009
65
Y = -6272680
16 feet Y = -1869692
84 meter
Z = -17477683
87 Z = -5308857
15
XDOT = 9290
941731 XDOT = 2755
062564
YDOT = 23259
264077 feet/sec YDOT = 7120
662150 meter/sec
ZDOT = -1803
199782 ZDOT = -536
045656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13917160
09 X = 4241950
40
Y = -201059
94 feet Y = -61283
07 meter
Z = -17395968
23 Z = -5302291
12
XDOT = -1834
667181 XDOT = -559
206557
YDOT = 23969
383721 feet/sec YDOT = 7305
868158 meter/sec
ZDOT = -1744
096065 ZDOT = -531
600481
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 17305
83263862
00016717 00000-0 10270-3 0 9168
2 25544 51
6400 72
1412 0005291 79
9142 280
2607 15
54269850 3153
Satellite: ISS
Catalog Number: 25544
Epoch time: 17305
83263862 = yrday
fracday
Element set: 916
Inclination: 51
6400 deg
RA of node: 72
1412 deg
Eccentricity:
0005291
Arg of perigee: 79
9142 deg
Mean anomaly: 280
2607 deg
Mean motion: 15
54269850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 295
Coasting Arc #18 (Orbit 319)
---------------------------------------
Vector Time (GMT): 2017/306/03:17:54
191
Vector Time (MET): N/A
Weight (LBS) : 919921
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3780901
11 A = 6777501
61 meter
Y = -1817084
36 meter E =
0019081
Z = -5339748
20 I = 51
97648
XDOT = 2894
443378 Wp = 84
96687
YDOT = 7076
882928 meter/sec RA = 69
85503 deg
ZDOT = -358
232823 TA = 181
62402
MA = 181
63023
Ha = 222
613 n
mi
Hp = 213
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12404531
18 X = 3826877
77
Y = -5961562
87 feet Y = -1774547
04 meter
Z = -17518858
91 Z = -5321269
48
XDOT = 9496
205309 XDOT = 2816
832824
YDOT = 23218
119844 feet/sec YDOT = 7108
816600 meter/sec
ZDOT = -1175
304536 ZDOT = -344
361146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6007203
14 X = -1830995
52
Y = -12498136
66 feet Y = -3809432
05 meter
Z = -17436545
93 Z = -5314659
20
XDOT = 22272
929307 XDOT = 6788
788853
YDOT = -9147
629574 feet/sec YDOT = -2788
197494 meter/sec
ZDOT = -1114
863831 ZDOT = -339
810496
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 17306
15411765
00016717 00000-0 10270-3 0 9172
2 25544 51
6417 70
5389 0004316 77
5146 282
6490 15
54093233 3203
Satellite: ISS
Catalog Number: 25544
Epoch time: 17306
15411765 = yrday
fracday
Element set: 917
Inclination: 51
6417 deg
RA of node: 70
5389 deg
Eccentricity:
0004316
Arg of perigee: 77
5146 deg
Mean anomaly: 282
6490 deg
Mean motion: 15
54093233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 320
Checksum: 299
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