[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 24th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 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
333/15:51:36
572 0
5 1
2 1
2
N/A -1
1 -0
1 221
5
000/00:03:13
144 0
3 -0
0 214
6
334/13:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 214
6
338/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 214
9
338/19:53:38
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
1
340/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 215
2
Coasting Arc #1 (Orbit 636)
---------------------------------------
Vector Time (GMT): 2017/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3733843
58 A = 6785764
08 meter
Y = 4911372
07 meter E =
0016694
Z = 2804522
85 I = 51
45541
XDOT = -5587
266051 Wp = 108
21937
YDOT = -1330
020529 meter/sec RA = 328
47687 deg
ZDOT = -5089
709712 TA = 39
83558
MA = 39
71315
Ha = 222
032 n
mi
Hp = 213
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12250142
97 X = -3802109
57
Y = 16113425
42 feet Y = 4869235
79 meter
Z = 9201190
44 Z = 2786219
22
XDOT = -18330
925363 XDOT = -5547
254425
YDOT = -4363
584412 feet/sec YDOT = -1392
277084 meter/sec
ZDOT = -16698
522678 ZDOT = -5116
754279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8059496
16 X = -2456534
43
Y = -18607968
29 feet Y = -5671708
74 meter
Z = 9119124
12 Z = 2779509
03
XDOT = 11343
511824 XDOT = 3457
502404
YDOT = -13187
280325 feet/sec YDOT = -4019
483043 meter/sec
ZDOT = -16818
240956 ZDOT = -5126
199844
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 17326
53782513
00016717 00000-0 10270-3 0 9000
2 25544 51
6398 328
9242 0003909 138
2726 221
8725 15
54228034 6371
Satellite: ISS
Catalog Number: 25544
Epoch time: 17326
53782513 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 328
9242 deg
Eccentricity:
0003909
Arg of perigee: 138
2726 deg
Mean anomaly: 221
8725 deg
Mean motion: 15
54228034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 637
Checksum: 315
Coasting Arc #2 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2017/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4731204
05 A = 6788372
21 meter
Y = -4711012
24 meter E =
0009121
Z = -1218641
78 I = 51
43649
XDOT = 4176
539975 Wp = 63
72377
YDOT = 2695
125116 meter/sec RA = 323
48965 deg
ZDOT = 5833
965678 TA = 283
00063
MA = 283
10245
Ha = 222
006 n
mi
Hp = 213
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15522323
01 X = 4789451
86
Y = -15456076
91 feet Y = -4657778
92 meter
Z = -3998168
57 Z = -1195517
57
XDOT = 13702
558973 XDOT = 4117
753022
YDOT = 8842
274001 feet/sec YDOT = 2741
500954 meter/sec
ZDOT = 19140
307344 ZDOT = 5854
111688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6267780
53 X = 1910419
51
Y = 21008662
98 feet Y = 6403440
48 meter
Z = -3894763
64 Z = -1187123
96
XDOT = -12680
242704 XDOT = -3864
937976
YDOT = 7324
245694 feet/sec YDOT = 2232
430088 meter/sec
ZDOT = 19229
184024 ZDOT = 5861
055290
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 17327
50230734
00016717 00000-0 10270-3 0 9012
2 25544 51
6393 324
1168 0004146 142
3636 217
7808 15
54249930 6522
Satellite: ISS
Catalog Number: 25544
Epoch time: 17327
50230734 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 324
1168 deg
Eccentricity:
0004146
Arg of perigee: 142
3636 deg
Mean anomaly: 217
7808 deg
Mean motion: 15
54249930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 652
Checksum: 298
Coasting Arc #3 (Orbit 667)
---------------------------------------
Vector Time (GMT): 2017/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5339464
29 A = 6788932
73 meter
Y = 4146242
38 meter E =
0014706
Z = -541661
34 I = 51
41150
XDOT = -2572
556284 Wp = 140
32713
YDOT = -4078
973275 meter/sec RA = 318
50390 deg
ZDOT = -5964
767002 TA = 45
53756
MA = 45
41738
Ha = 221
874 n
mi
Hp = 213
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17517927
46 X = -5382800
69
Y = 13603157
41 feet Y = 4086290
56 meter
Z = -1777104
15 Z = -567704
12
XDOT = -8440
145288 XDOT = -2497
778669
YDOT = -13382
458252 feet/sec YDOT = -4107
322901 meter/sec
ZDOT = -19569
445546 ZDOT = -5977
082442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4084447
69 X = -1244939
66
Y = -21790234
12 feet Y = -6641663
36 meter
Z = -1893345
51 Z = -577091
71
XDOT = 14114
921681 XDOT = 4302
228128
YDOT = -967
634818 feet/sec YDOT = -294
935092 meter/sec
ZDOT = -19623
348996 ZDOT = -5981
196774
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 17328
53108418
00016717 00000-0 10270-3 0 9020
2 25544 51
6384 318
9869 0003876 145
5281 214
6123 15
54216522 6685
Satellite: ISS
Catalog Number: 25544
Epoch time: 17328
53108418 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 318
9869 deg
Eccentricity:
0003876
Arg of perigee: 145
5281 deg
Mean anomaly: 214
6123 deg
Mean motion: 15
54216522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 668
Checksum: 319
Coasting Arc #4 (Orbit 683)
---------------------------------------
Vector Time (GMT): 2017/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5522889
16 A = 6786807
29 meter
Y = -3263042
89 meter E =
0015010
Z = 2201227
22 I = 51
38154
XDOT = 955
603063 Wp = 86
28913
YDOT = 5313
156623 meter/sec RA = 313
51536 deg
ZDOT = 5447
257077 TA = 298
25620
MA = 298
40763
Ha = 221
734 n
mi
Hp = 213
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18119715
08 X = 5548274
31
Y = -10705521
30 feet Y = -3201140
34 meter
Z = 7221874
09 Z = 2228117
49
XDOT = 3135
180654 XDOT = 869
658525
YDOT = 17431
616216 feet/sec YDOT = 5323
362029 meter/sec
ZDOT = 17871
578335 ZDOT = 5451
690648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1609065
29 X = 490443
10
Y = 20942729
60 feet Y = 6383343
98 meter
Z = 7341710
43 Z = 2237753
34
XDOT = -15443
082544 XDOT = -4707
051559
YDOT = -5120
452187 feet/sec YDOT = -1560
713827 meter/sec
ZDOT = 17890
313835 ZDOT = 5452
967657
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 17329
55985295
00016717 00000-0 10270-3 0 9030
2 25544 51
6389 313
8586 0003945 152
6597 207
4763 15
54266996 6844
Satellite: ISS
Catalog Number: 25544
Epoch time: 17329
55985295 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 313
8586 deg
Eccentricity:
0003945
Arg of perigee: 152
6597 deg
Mean anomaly: 207
4763 deg
Mean motion: 15
54266996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 684
Checksum: 368
Coasting Arc #5 (Orbit 698)
---------------------------------------
Vector Time (GMT): 2017/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5345485
42 A = 6783227
30 meter
Y = 2009169
31 meter E =
0007699
Z = -3665143
14 I = 51
34731
XDOT = 591
552720 Wp = 106
80560
YDOT = -6298
101421 meter/sec RA = 308
51538 deg
ZDOT = -4325
011269 TA = 116
95471
MA = 116
87605
Ha = 221
715 n
mi
Hp = 213
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17537681
84 X = -5349751
55
Y = 6591762
83 feet Y = 1949368
71 meter
Z = -12024747
84 Z = -3691120
42
XDOT = 1940
789764 XDOT = 682
944814
YDOT = -20663
062406 feet/sec YDOT = -6290
975126 meter/sec
ZDOT = -14189
669517 ZDOT = -4321
915889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1489813
57 X = 454095
18
Y = -18601331
40 feet Y = -5669685
81 meter
Z = -12140309
21 Z = -3700366
25
XDOT = 16463
720555 XDOT = 5018
142025
YDOT = 10549
283817 feet/sec YDOT = 3215
421708 meter/sec
ZDOT = -14174
852134 ZDOT = -4320
494930
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 17330
52432103
00016717 00000-0 10270-3 0 9045
2 25544 51
6387 309
0492 0003778 152
1327 208
0029 15
54230645 6995
Satellite: ISS
Catalog Number: 25544
Epoch time: 17330
52432103 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 309
0492 deg
Eccentricity:
0003778
Arg of perigee: 152
1327 deg
Mean anomaly: 208
0029 deg
Mean motion: 15
54230645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 699
Checksum: 294
Coasting Arc #6 (Orbit 714)
---------------------------------------
Vector Time (GMT): 2017/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4858042
51 A = 6779448
88 meter
Y = -527725
84 meter E =
0010820
Z = 4695103
64 I = 51
31469
XDOT = -1922
195893 Wp = 130
24980
YDOT = 6897
083136 meter/sec RA = 303
50496 deg
ZDOT = 2753
052878 TA = 292
32062
MA = 292
43528
Ha = 221
474 n
mi
Hp = 213
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15938459
69 X = 4840775
84
Y = -1731383
99 feet Y = -473496
53 meter
Z = 15403883
33 Z = 4718660
84
XDOT = -6306
416972 XDOT = -2012
551203
YDOT = 22628
225512 feet/sec YDOT = 6875
082561 meter/sec
ZDOT = 9032
325716 ZDOT = 2743
496020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4933894
72 X = -1503851
11
Y = 15147819
24 feet Y = 4617055
30 meter
Z = 15508451
39 Z = 4726975
98
XDOT = -16906
385758 XDOT = -5153
066379
YDOT = -14746
408198 feet/sec YDOT = -4494
705219 meter/sec
ZDOT = 8988
761434 ZDOT = 2739
774485
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 17331
55307903
00016717 00000-0 10270-3 0 9059
2 25544 51
6380 303
9209 0003699 159
3939 200
7363 15
54263818 7154
Satellite: ISS
Catalog Number: 25544
Epoch time: 17331
55307903 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 303
9209 deg
Eccentricity:
0003699
Arg of perigee: 159
3939 deg
Mean anomaly: 200
7363 deg
Mean motion: 15
54263818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 715
Checksum: 317
Coasting Arc #7 (Orbit 729)
---------------------------------------
Vector Time (GMT): 2017/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4156213
09 A = 6777256
16 meter
Y = -1148773
70 meter E =
0015736
Z = -5241874
51 I = 51
29023
XDOT = 3009
198081 Wp = 96
58690
YDOT = -6988
834719 meter/sec RA = 298
48216 deg
ZDOT = -858
325505 TA = 165
17728
MA = 165
13110
Ha = 221
583 n
mi
Hp = 213
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13635869
72 X = -4117595
47
Y = -3768942
59 feet Y = -1195035
31 meter
Z = -17197751
03 Z = -5261970
62
XDOT = 9872
697115 XDOT = 3091
294838
YDOT = -22929
247765 feet/sec YDOT = -6954
724765 meter/sec
ZDOT = -2816
028560 ZDOT = -843
508241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8809813
56 X = 2685231
17
Y = -10929881
80 feet Y = -3331427
97 meter
Z = -17286682
18 Z = -5268980
73
XDOT = 16353
274624 XDOT = 4984
478105
YDOT = 17508
618023 feet/sec YDOT = 5336
626773 meter/sec
ZDOT = -2749
133066 ZDOT = -837
935758
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 17332
51753578
00016717 00000-0 10270-3 0 9060
2 25544 51
6384 299
1113 0003704 161
0893 199
0398 15
54242988 7304
Satellite: ISS
Catalog Number: 25544
Epoch time: 17332
51753578 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 299
1113 deg
Eccentricity:
0003704
Arg of perigee: 161
0893 deg
Mean anomaly: 199
0398 deg
Mean motion: 15
54242988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 730
Checksum: 328
Coasting Arc #8 (Orbit 745)
---------------------------------------
Vector Time (GMT): 2017/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3314627
16 A = 6777409
17 meter
Y = 2819534
93 meter E =
0004412
Z = 5191962
08 I = 51
27656
XDOT = -3823
815202 Wp = 107
10821
YDOT = 6556
596495 meter/sec RA = 293
45635 deg
ZDOT = -1119
915210 TA = 353
67239
MA = 353
67796
Ha = 221
370 n
mi
Hp = 214
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10874761
01 X = 3257631
55
Y = 9250442
69 feet Y = 2856282
59 meter
Z = 17033996
33 Z = 5207925
42
XDOT = -12545
325465 XDOT = -3891
408529
YDOT = 21511
143356 feet/sec YDOT = 6513
458062 meter/sec
ZDOT = -3674
262499 ZDOT = -1138
654515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12644371
58 X = -3854004
46
Y = 6445949
82 feet Y = 1964725
51 meter
Z = 17104319
52 Z = 5213396
59
XDOT = -14679
292416 XDOT = -4474
248328
YDOT = -18826
025101 feet/sec YDOT = -5738
172451 meter/sec
ZDOT = -3758
466159 ZDOT = -1145
580485
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 17333
54628209
00016717 00000-0 10270-3 0 9077
2 25544 51
6388 293
9821 0003607 164
7409 195
3854 15
54255193 7466
Satellite: ISS
Catalog Number: 25544
Epoch time: 17333
54628209 = yrday
fracday
Element set: 907
Inclination: 51
6388 deg
RA of node: 293
9821 deg
Eccentricity:
0003607
Arg of perigee: 164
7409 deg
Mean anomaly: 195
3854 deg
Mean motion: 15
54255193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 746
Checksum: 337
Coasting Arc #9 (Orbit 747)
---------------------------------------
Vector Time (GMT): 2017/333/15:53:13
144
Vector Time (MET): N/A
Weight (LBS) : 933686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2943983
43 A = 6778699
16 meter
Y = -3454526
49 meter E =
0014228
Z = -5047702
32 I = 51
27966
XDOT = 4146
983170 Wp = 116
36284
YDOT = -6178
384123 meter/sec RA = 292
64016 deg
ZDOT = 1807
453448 TA = 171
25931
MA = 171
23451
Ha = 221
462 n
mi
Hp = 214
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9658738
28 X = -2880615
47
Y = -11333748
33 feet Y = -3487093
72 meter
Z = -16560703
15 Z = -5061849
70
XDOT = 13605
587827 XDOT = 4206
983418
YDOT = -20270
289119 feet/sec YDOT = -6131
674275 meter/sec
ZDOT = 5929
965380 ZDOT = 1827
744199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3517007
97 X = 1071984
03
Y = -14398364
70 feet Y = -4388621
56 meter
Z = -16622867
20 Z = -5066649
92
XDOT = 23320
015990 XDOT = 7107
940874
YDOT = -1263
371842 feet/sec YDOT = -385
075737 meter/sec
ZDOT = 6020
984369 ZDOT = 1835
196036
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 17333
67487486
00016717 00000-0 10270-3 0 9082
2 25544 51
6418 293
3417 0003244 180
3515 179
7636 15
54051385 7487
Satellite: ISS
Catalog Number: 25544
Epoch time: 17333
67487486 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 293
3417 deg
Eccentricity:
0003244
Arg of perigee: 180
3515 deg
Mean anomaly: 179
7636 deg
Mean motion: 15
54051385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 748
Checksum: 333
Coasting Arc #10 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2017/334/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4045103
82 A = 6777592
22 meter
Y = -1294985
42 meter E =
0015017
Z = -5294406
00 I = 51
26306
XDOT = 2364
935551 Wp = 102
15068
YDOT = -7283
238059 meter/sec RA = 288
16088 deg
ZDOT = -28
618318 TA = 167
59332
MA = 167
55631
Ha = 221
392 n
mi
Hp = 214
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13271338
00 X = -4004604
13
Y = -4248639
83 feet Y = -1339993
92 meter
Z = -17370098
43 Z = -5313957
95
XDOT = 7758
974906 XDOT = 2446
341920
YDOT = -23895
137990 feet/sec YDOT = -7256
336562 meter/sec
ZDOT = -93
892118 ZDOT = -16
932446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4252583
22 X = 1296187
37
Y = -13156085
10 feet Y = -4009974
74 meter
Z = -17456592
83 Z = -5320769
49
XDOT = 22934
333999 XDOT = 6990
385003
YDOT = 7453
787116 feet/sec YDOT = 2271
914313 meter/sec
ZDOT = -40
859371 ZDOT = -12
453936
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 17334
57514885
00016717 00000-0 10270-3 0 9097
2 25544 51
6395 288
8532 0003230 183
6633 176
4497 15
54047996 7628
Satellite: ISS
Catalog Number: 25544
Epoch time: 17334
57514885 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 288
8532 deg
Eccentricity:
0003230
Arg of perigee: 183
6633 deg
Mean anomaly: 176
4497 deg
Mean motion: 15
54047996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 349
Coasting Arc #11 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2017/335/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3448105
26 A = 6778699
11 meter
Y = 2963146
11 meter E =
0004137
Z = 5024424
96 I = 51
25829
XDOT = -3107
255279 Wp = 90
55319
YDOT = 6763
953513 meter/sec RA = 283
13704 deg
ZDOT = -1855
330507 TA = 17
51798
MA = 17
50371
Ha = 221
156 n
mi
Hp = 214
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11312681
29 X = 3390307
53
Y = 9721607
98 feet Y = 3001381
75 meter
Z = 16484333
86 Z = 5041034
95
XDOT = -10194
407083 XDOT = -3173
648185
YDOT = 22191
448533 feet/sec YDOT = 6728
834934 meter/sec
ZDOT = -6087
042346 ZDOT = -1870
585846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9530980
37 X = -2905042
82
Y = 11367893
43 feet Y = 3464933
92 meter
Z = 16557508
70 Z = 5046728
65
XDOT = -21531
519571 XDOT = -6562
807165
YDOT = -9080
129567 feet/sec YDOT = -2767
623492 meter/sec
ZDOT = -6155
811263 ZDOT = -1876
291273
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 17335
60402762
00016717 00000-0 10270-3 0 9104
2 25544 51
6401 283
7258 0003240 188
7762 171
3334 15
54063696 7781
Satellite: ISS
Catalog Number: 25544
Epoch time: 17335
60402762 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 283
7258 deg
Eccentricity:
0003240
Arg of perigee: 188
7762 deg
Mean anomaly: 171
3334 deg
Mean motion: 15
54063696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 309
Coasting Arc #12 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2017/336/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2812109
35 A = 6781729
61 meter
Y = -4476373
33 meter E =
0009334
Z = -4258134
89 I = 51
26287
XDOT = 3689
595659 Wp = 130
01734
YDOT = -5696
109659 meter/sec RA = 278
11648 deg
ZDOT = 3550
699754 TA = 176
44925
MA = 176
44262
Ha = 221
199 n
mi
Hp = 214
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9226080
53 X = -2741159
93
Y = -14686264
21 feet Y = -4507423
22 meter
Z = -13970258
84 Z = -4271623
60
XDOT = 12104
972634 XDOT = 3735
768909
YDOT = -18688
023815 feet/sec YDOT = -5654
592193 meter/sec
ZDOT = 11649
277409 ZDOT = 3568
734777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14366382
90 X = 4378873
51
Y = -9631171
25 feet Y = -2935581
00 meter
Z = -14029349
00 Z = -4276145
57
XDOT = 18385
258517 XDOT = 5603
826796
YDOT = 10334
183613 feet/sec YDOT = 3149
859165 meter/sec
ZDOT = 11730
194277 ZDOT = 3575
363216
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 17336
56859349
00016717 00000-0 10270-3 0 9118
2 25544 51
6409 278
9169 0003206 191
7110 168
3969 15
54080785 7934
Satellite: ISS
Catalog Number: 25544
Epoch time: 17336
56859349 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 278
9169 deg
Eccentricity:
0003206
Arg of perigee: 191
7110 deg
Mean anomaly: 168
3969 deg
Mean motion: 15
54080785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 793
Checksum: 346
Coasting Arc #13 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2017/337/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2128173
98 A = 6785529
64 meter
Y = 5675773
64 meter E =
0012979
Z = 3033454
93 I = 51
27199
XDOT = -4162
769734 Wp = 110
10102
YDOT = 4186
593555 meter/sec RA = 273
10715 deg
ZDOT = -4900
183608 TA = 34
89331
MA = 34
80830
Ha = 221
066 n
mi
Hp = 214
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6982198
11 X = 2049812
46
Y = 18621304
59 feet Y = 5699133
87 meter
Z = 9952279
95 Z = 3043603
40
XDOT = -13657
381018 XDOT = -4185
472800
YDOT = 13735
543159 feet/sec YDOT = 4139
916190 meter/sec
ZDOT = -16076
717873 ZDOT = -4920
460163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18242054
80 X = -5560178
30
Y = 7864603
22 feet Y = 2397131
06 meter
Z = 9996369
55 Z = 3046893
44
XDOT = -13839
010640 XDOT = -4218
130443
YDOT = -11497
362621 feet/sec YDOT = -3504
396127 meter/sec
ZDOT = -16167
329394 ZDOT = -4927
801999
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 17337
59745725
00016717 00000-0 10270-3 0 9125
2 25544 51
6409 273
7893 0003174 194
9195 165
1864 15
54080922 8093
Satellite: ISS
Catalog Number: 25544
Epoch time: 17337
59745725 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 273
7893 deg
Eccentricity:
0003174
Arg of perigee: 194
9195 deg
Mean anomaly: 165
1864 deg
Mean motion: 15
54080922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 342
Coasting Arc #14 (Orbit 823)
---------------------------------------
Vector Time (GMT): 2017/338/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 919252
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4156363
73 A = 6778260
89 meter
Y = -1636721
09 meter E =
0013520
Z = -5110084
26 I = 51
24739
XDOT = 1010
475535 Wp = 115
28162
YDOT = -7430
254967 meter/sec RA = 268
15971 deg
ZDOT = 1555
537044 TA = 169
82918
MA = 169
80180
Ha = 220
999 n
mi
Hp = 214
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13636363
94 X = -4112929
93
Y = -5369819
84 feet Y = -1682956
92 meter
Z = -16765368
31 Z = -5130169
58
XDOT = 3315
208449 XDOT = 1085
931394
YDOT = -24377
476926 feet/sec YDOT = -7418
533425 meter/sec
ZDOT = 5103
467991 ZDOT = 1560
628081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5330762
57 X = 1624816
43
Y = -13541861
37 feet Y = -4127559
34 meter
Z = -16854195
99 Z = -5137158
94
XDOT = 23399
260703 XDOT = 7132
094662
YDOT = 2819
889586 feet/sec YDOT = 859
502346 meter/sec
ZDOT = 5127
245436 ZDOT = 1562
784409
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 17338
56201078
00016717 00000-0 10270-3 0 9132
2 25544 51
6413 268
9813 0003172 200
1021 160
0007 15
54096346 8249
Satellite: ISS
Catalog Number: 25544
Epoch time: 17338
56201078 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 268
9813 deg
Eccentricity:
0003172
Arg of perigee: 200
1021 deg
Mean anomaly: 160
0007 deg
Mean motion: 15
54096346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 824
Checksum: 275
Coasting Arc #15 (Orbit 828)
---------------------------------------
Vector Time (GMT): 2017/338/19:53:38
000
Vector Time (MET): N/A
Weight (LBS) : 919252
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3217457
48 A = 6781478
41 meter
Y = -4145281
48 meter E =
0010159
Z = 4292661
23 I = 51
25492
XDOT = 3143
262408 Wp = 128
09750
YDOT = 6063
609663 meter/sec RA = 266
78868 deg
ZDOT = 3487
660064 TA = 286
17766
MA = 286
28944
Ha = 220
928 n
mi
Hp = 215
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10555962
88 X = 3242720
11
Y = -13600004
85 feet Y = -4109160
94 meter
Z = 14083534
22 Z = 4308351
70
XDOT = 10312
540709 XDOT = 3058
282335
YDOT = 19893
732490 feet/sec YDOT = 6098
284197 meter/sec
ZDOT = 11442
454279 ZDOT = 3502
723576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7580618
57 X = 2310572
54
Y = -15392811
35 feet Y = -4691728
90 meter
Z = 14153798
13 Z = 4314077
67
XDOT = 12831
595048 XDOT = 3911
070171
YDOT = 16936
700765 feet/sec YDOT = 5162
306393 meter/sec
ZDOT = 11508
299430 ZDOT = 3507
729666
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 17338
88352558
00016717 00000-0 10270-3 0 9148
2 25544 51
6376 267
3749 0003535 201
5803 158
5201 15
54113792 8292
Satellite: ISS
Catalog Number: 25544
Epoch time: 17338
88352558 = yrday
fracday
Element set: 914
Inclination: 51
6376 deg
RA of node: 267
3749 deg
Eccentricity:
0003535
Arg of perigee: 201
5803 deg
Mean anomaly: 158
5201 deg
Mean motion: 15
54113792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 829
Checksum: 324
Coasting Arc #16 (Orbit 843)
---------------------------------------
Vector Time (GMT): 2017/339/19:53:38
000
Vector Time (MET): N/A
Weight (LBS) : 919252
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3734399
16 A = 6778407
37 meter
Y = 2550067
76 meter E =
0011731
Z = -5059729
08 I = 51
24878
XDOT = -2440
992333 Wp = 90
84427
YDOT = -7045
681120 meter/sec RA = 261
76818 deg
ZDOT = -1753
073375 TA = 162
11086
MA = 162
06953
Ha = 220
950 n
mi
Hp = 214
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12251965
74 X = -3738059
32
Y = 8366364
03 feet Y = 2508287
29 meter
Z = -16600161
01 Z = -5077878
33
XDOT = -8008
505030 XDOT = -2353
508597
YDOT = -23115
751707 feet/sec YDOT = -7072
488606 meter/sec
ZDOT = -5751
553069 ZDOT = -1764
719377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10074011
90 X = -3070558
83
Y = 10766984
83 feet Y = 3281776
98 meter
Z = -16681078
48 Z = -5084392
72
XDOT = -11942
073013 XDOT = -3639
943854
YDOT = -20143
804818 feet/sec YDOT = -6139
831709 meter/sec
ZDOT = -5802
100743 ZDOT = -1768
480307
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 17339
84807112
00016717 00000-0 10270-3 0 9157
2 25544 51
6388 262
5672 0003409 200
1173 159
9846 15
54121992 8440
Satellite: ISS
Catalog Number: 25544
Epoch time: 17339
84807112 = yrday
fracday
Element set: 915
Inclination: 51
6388 deg
RA of node: 262
5672 deg
Eccentricity:
0003409
Arg of perigee: 200
1173 deg
Mean anomaly: 159
9846 deg
Mean motion: 15
54121992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 844
Checksum: 321
Coasting Arc #17 (Orbit 853)
---------------------------------------
Vector Time (GMT): 2017/340/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940422
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1567437
86 A = 6789356
48 meter
Y = 6591401
50 meter E =
0013753
Z = 291619
30 I = 51
28970
XDOT = -4610
729970 Wp = 144
31187
YDOT = 1366
680714 meter/sec RA = 258
60035 deg
ZDOT = -5976
567494 TA = 32
52904
MA = 32
44437
Ha = 220
808 n
mi
Hp = 215
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5142512
67 X = 1492198
00
Y = 21625333
02 feet Y = 6608508
94 meter
Z = 956756
22 Z = 299051
42
XDOT = -15127
066832 XDOT = -4596
638571
YDOT = 4483
860609 feet/sec YDOT = 1315
199824 meter/sec
ZDOT = -19608
161068 ZDOT = -5998
930680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21245995
86 X = -6475779
54
Y = -6530389
82 feet Y = -1990462
82 meter
Z = 988694
03 Z = 301353
94
XDOT = 3259
540858 XDOT = 993
508054
YDOT = -13651
647989 feet/sec YDOT = -4161
022307 meter/sec
ZDOT = -19707
588993 ZDOT = -6006
873125
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 17340
49109733
00016717 00000-0 10270-3 0 9165
2 25544 51
6400 259
3650 0003101 207
3099 152
7891 15
54106898 8540
Satellite: ISS
Catalog Number: 25544
Epoch time: 17340
49109733 = yrday
fracday
Element set: 916
Inclination: 51
6400 deg
RA of node: 259
3650 deg
Eccentricity:
0003101
Arg of perigee: 207
3099 deg
Mean anomaly: 152
7891 deg
Mean motion: 15
54106898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 854
Checksum: 309
Coasting Arc #18 (Orbit 868)
---------------------------------------
Vector Time (GMT): 2017/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940422
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -775832
37 A = 6788524
19 meter
Y = -6593796
84 meter E =
0011175
Z = 1393540
88 I = 51
29359
XDOT = 5008
220572 Wp = 68
26764
YDOT = 637
467302 meter/sec RA = 253
60650 deg
ZDOT = 5771
248669 TA = 306
99439
MA = 307
09662
Ha = 220
714 n
mi
Hp = 215
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2545381
81 X = -708810
24
Y = -21633191
72 feet Y = -6602098
10 meter
Z = 4571984
50 Z = 1389934
32
XDOT = 16431
169857 XDOT = 4972
686147
YDOT = 2091
428156 feet/sec YDOT = 693
273445 meter/sec
ZDOT = 18934
542878 ZDOT = 5795
490788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20102184
56 X = 6127145
85
Y = 8397196
75 feet Y = 2559465
57 meter
Z = 4557000
93 Z = 1388973
88
XDOT = -9229
943520 XDOT = -2813
286785
YDOT = 11702
496719 feet/sec YDOT = 3566
921000 meter/sec
ZDOT = 19042
004027 ZDOT = 5804
002827
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 17341
51993356
00016717 00000-0 10270-3 0 9172
2 25544 51
6390 254
2370 0003141 212
1356 147
9605 15
54124788 8698
Satellite: ISS
Catalog Number: 25544
Epoch time: 17341
51993356 = yrday
fracday
Element set: 917
Inclination: 51
6390 deg
RA of node: 254
2370 deg
Eccentricity:
0003141
Arg of perigee: 212
1356 deg
Mean anomaly: 147
9605 deg
Mean motion: 15
54124788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 869
Checksum: 314
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