[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 20th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 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
237/06:36:20
931 0
4 1
1 1
1
N/A 0
9 -0
0 221
6
000/00:02:41
861 0
3 0
0 215
1
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
7
Coasting Arc #1 (Orbit 3112)
---------------------------------------
Vector Time (GMT): 2017/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3178453
40 A = 6780151
48 meter
Y = -3808704
55 meter E =
0010434
Z = 4612597
31 I = 52
00400
XDOT = 3137
782321 Wp = 93
42065
YDOT = -6308
785821 meter/sec RA = 96
73572 deg
ZDOT = -3041
794277 TA = 26
80129
MA = 26
74741
Ha = 222
366 n
mi
Hp = 213
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10427996
73 X = -3158032
82
Y = -12495749
85 feet Y = -3844134
10 meter
Z = 15133193
27 Z = 4597206
99
XDOT = 10294
561420 XDOT = 3222
871074
YDOT = -20698
116210 feet/sec YDOT = -6273
221184 meter/sec
ZDOT = -9979
640017 ZDOT = -3026
345463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1231032
11 X = 375218
59
Y = 16291476
63 feet Y = 4965642
08 meter
Z = 15065615
42 Z = 4591999
58
XDOT = -19321
254081 XDOT = -5889
118244
YDOT = 10640
634615 feet/sec YDOT = 3243
265431 meter/sec
ZDOT = -9910
219604 ZDOT = -3020
634935
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 17228
54286976
00016717 00000-0 10270-3 0 9004
2 25544 51
6416 97
4490 0004886 146
9684 213
1774 15
54202015 31130
Satellite: ISS
Catalog Number: 25544
Epoch time: 17228
54286976 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 97
4490 deg
Eccentricity:
0004886
Arg of perigee: 146
9684 deg
Mean anomaly: 213
1774 deg
Mean motion: 15
54202015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3113
Checksum: 318
Coasting Arc #2 (Orbit 3127)
---------------------------------------
Vector Time (GMT): 2017/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2594761
72 A = 6784015
31 meter
Y = 5188985
55 meter E =
0008842
Z = -3527398
46 I = 52
01861
XDOT = -3699
792088 Wp = 122
20252
YDOT = 4934
391421 meter/sec RA = 91
77295 deg
ZDOT = 4540
889653 TA = 196
56550
MA = 196
59440
Ha = 222
271 n
mi
Hp = 213
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8512997
77 X = 2553678
45
Y = 17024230
81 feet Y = 5217772
32 meter
Z = -11572829
60 Z = -3514893
70
XDOT = -12138
425484 XDOT = -3776
751964
YDOT = 16188
948230 feet/sec YDOT = 4892
587407 meter/sec
ZDOT = 14897
931932 ZDOT = 4522
730601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2665541
74 X = 812457
12
Y = -18879899
77 feet Y = -5754593
45 meter
Z = -11518256
05 Z = -3510764
44
XDOT = 17911
523832 XDOT = 5459
432464
YDOT = -6503
078519 feet/sec YDOT = -1982
138333 meter/sec
ZDOT = 14816
705731 ZDOT = 4516
131907
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 17229
50738474
00016717 00000-0 10270-3 0 9017
2 25544 51
6409 92
6408 0004965 151
0911 209
0517 15
54161015 31285
Satellite: ISS
Catalog Number: 25544
Epoch time: 17229
50738474 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 92
6408 deg
Eccentricity:
0004965
Arg of perigee: 151
0911 deg
Mean anomaly: 209
0517 deg
Mean motion: 15
54161015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 296
Coasting Arc #3 (Orbit 3143)
---------------------------------------
Vector Time (GMT): 2017/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1936339
78 A = 6787442
64 meter
Y = -6166729
16 meter E =
0017803
Z = 2039113
76 I = 52
03114
XDOT = 4192
771393 Wp = 121
99595
YDOT = -3173
582558 meter/sec RA = 86
82069 deg
ZDOT = -5589
784615 TA = 35
56903
MA = 35
45049
Ha = 222
198 n
mi
Hp = 213
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6352820
79 X = -1877142
73
Y = -20232051
06 feet Y = -6188051
68 meter
Z = 6690005
79 Z = 2029851
43
XDOT = 13755
811657 XDOT = 4255
099645
YDOT = -10412
016265 feet/sec YDOT = -3126
347530 meter/sec
ZDOT = -18339
188370 ZDOT = -5569
266413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5947301
44 X = -1812737
48
Y = 20368064
68 feet Y = 6208186
12 meter
Z = 6649958
34 Z = 2026907
30
XDOT = -15838
598863 XDOT = -4827
604933
YDOT = 1361
396403 feet/sec YDOT = 414
953624 meter/sec
ZDOT = -18247
778946 ZDOT = -5561
923023
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 17230
53619678
00016717 00000-0 10270-3 0 9027
2 25544 51
6418 87
5119 0004855 154
3258 205
8136 15
54179596 31447
Satellite: ISS
Catalog Number: 25544
Epoch time: 17230
53619678 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 87
5119 deg
Eccentricity:
0004855
Arg of perigee: 154
3258 deg
Mean anomaly: 205
8136 deg
Mean motion: 15
54179596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3144
Checksum: 328
Coasting Arc #4 (Orbit 3158)
---------------------------------------
Vector Time (GMT): 2017/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1244653
56 A = 6789172
87 meter
Y = 6661496
08 meter E =
0010233
Z = -372395
82 I = 52
03244
XDOT = -4582
791855 Wp = 67
83961
YDOT = 1185
673602 meter/sec RA = 81
87448 deg
ZDOT = 6028
350515 TA = 288
16943
MA = 288
28082
Ha = 222
121 n
mi
Hp = 213
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4083509
06 X = 1171879
33
Y = 21855302
08 feet Y = 6675007
73 meter
Z = -1221771
05 Z = -366526
51
XDOT = -15035
406350 XDOT = -4624
991996
YDOT = 3890
005256 feet/sec YDOT = 1134
189726 meter/sec
ZDOT = 19778
052870 ZDOT = 6005
986656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8413300
52 X = 2564374
00
Y = -20581689
52 feet Y = -6273298
97 meter
Z = -1196842
01 Z = -364797
44
XDOT = 13351
043932 XDOT = 4069
398191
YDOT = 4339
691689 feet/sec YDOT = 1322
738027 meter/sec
ZDOT = 19678
778071 ZDOT = 5998
091556
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 17231
50070569
00016717 00000-0 10270-3 0 9036
2 25544 51
6402 82
7028 0004861 158
1485 201
9876 15
54160898 31596
Satellite: ISS
Catalog Number: 25544
Epoch time: 17231
50070569 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 82
7028 deg
Eccentricity:
0004861
Arg of perigee: 158
1485 deg
Mean anomaly: 201
9876 deg
Mean motion: 15
54160898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 316
Coasting Arc #5 (Orbit 3174)
---------------------------------------
Vector Time (GMT): 2017/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -435986
61 A = 6788460
07 meter
Y = -6626765
14 meter E =
0013390
Z = -1375517
60 I = 52
02340
XDOT = 4888
383310 Wp = 149
73608
YDOT = 883
948622 meter/sec RA = 76
93110 deg
ZDOT = -5843
867925 TA = 45
17365
MA = 45
06490
Ha = 222
086 n
mi
Hp = 213
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1430402
25 X = -355170
51
Y = -21741355
45 feet Y = -6631188
79 meter
Z = -4512853
01 Z = -1377439
04
XDOT = 16038
002987 XDOT = 4906
521510
YDOT = 2900
093903 feet/sec YDOT = 938
715164 meter/sec
ZDOT = -19172
795029 ZDOT = -5820
078126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10283620
44 X = -3134447
51
Y = 19207096
52 feet Y = 5854323
02 meter
Z = -4520290
22 Z = -1377784
46
XDOT = -10799
247218 XDOT = -3291
610552
YDOT = -10241
782698 feet/sec YDOT = -3121
695366 meter/sec
ZDOT = -19067
533910 ZDOT = -5811
784336
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 17232
52951416
00016717 00000-0 10270-3 0 9049
2 25544 51
6393 77
5743 0004939 163
1291 197
0027 15
54150129 31755
Satellite: ISS
Catalog Number: 25544
Epoch time: 17232
52951416 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 77
5743 deg
Eccentricity:
0004939
Arg of perigee: 163
1291 deg
Mean anomaly: 197
0027 deg
Mean motion: 15
54150129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3175
Checksum: 308
Coasting Arc #6 (Orbit 3190)
---------------------------------------
Vector Time (GMT): 2017/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -428698
61 A = 6785495
81 meter
Y = 6097990
51 meter E =
0014411
Z = 2936826
04 I = 52
00528
XDOT = -5053
468739 Wp = 101
85718
YDOT = -2796
241857 meter/sec RA = 71
98013 deg
ZDOT = 5044
675520 TA = 291
47514
MA = 291
62876
Ha = 221
900 n
mi
Hp = 214
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1406491
49 X = -511121
46
Y = 20006530
54 feet Y = 6092735
78 meter
Z = 9635256
04 Z = 2934543
16
XDOT = -16579
621846 XDOT = -5046
328898
YDOT = -9174
021841 feet/sec YDOT = -2852
713054 meter/sec
ZDOT = 16550
772702 ZDOT = 5020
145296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11525789
76 X = 3513060
72
Y = -16419793
87 feet Y = -5004753
17 meter
Z = 9624145
72 Z = 2933439
62
XDOT = 8421
105860 XDOT = 2566
753066
YDOT = 15594
327530 feet/sec YDOT = 4753
151031 meter/sec
ZDOT = 16442
542964 ZDOT = 5011
687095
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 17233
55831929
00016717 00000-0 10270-3 0 9050
2 25544 51
6390 72
4442 0004937 168
7220 191
4044 15
54193401 31918
Satellite: ISS
Catalog Number: 25544
Epoch time: 17233
55831929 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 72
4442 deg
Eccentricity:
0004937
Arg of perigee: 168
7220 deg
Mean anomaly: 191
4044 deg
Mean motion: 15
54193401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3191
Checksum: 302
Coasting Arc #7 (Orbit 3205)
---------------------------------------
Vector Time (GMT): 2017/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1421124
47 A = 6781651
09 meter
Y = -5113945
19 meter E =
0008704
Z = -4227150
62 I = 51
98016
XDOT = 5026
334706 Wp = 103
54548
YDOT = 4446
658229 meter/sec RA = 67
01877 deg
ZDOT = -3698
057737 TA = 128
71397
MA = 128
63612
Ha = 221
921 n
mi
Hp = 214
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4662481
86 X = 1498737
39
Y = -16778035
39 feet Y = -5097619
51 meter
Z = -13868604
41 Z = -4220058
54
XDOT = 16490
599430 XDOT = 4994
200453
YDOT = 14588
773717 feet/sec YDOT = 4502
686218 meter/sec
ZDOT = -12132
735358 ZDOT = -3673
720140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12480588
79 X = -3804083
46
Y = 12180719
61 feet Y = 3712683
34 meter
Z = -13836342
37 Z = -4217317
15
XDOT = -6211
467338 XDOT = -1893
255244
YDOT = -19993
342133 feet/sec YDOT = -6093
970682 meter/sec
ZDOT = -12025
634122 ZDOT = -3665
413280
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 17234
52282373
00016717 00000-0 10270-3 0 9062
2 25544 51
6379 67
6345 0004882 169
0676 191
0584 15
54177169 32066
Satellite: ISS
Catalog Number: 25544
Epoch time: 17234
52282373 = yrday
fracday
Element set: 906
Inclination: 51
6379 deg
RA of node: 67
6345 deg
Eccentricity:
0004882
Arg of perigee: 169
0676 deg
Mean anomaly: 191
0584 deg
Mean motion: 15
54177169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3206
Checksum: 332
Coasting Arc #8 (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 = -2437068
92 A = 6778597
46 meter
Y = 3820101
05 meter E =
0009739
Z = 5039214
47 I = 51
95541
XDOT = -4767
410083 Wp = 145
78216
YDOT = -5671
624459 meter/sec RA = 62
04748 deg
ZDOT = 1984
194549 TA = 284
98748
MA = 285
09526
Ha = 221
946 n
mi
Hp = 214
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7995632
93 X = -2504082
85
Y = 12533139
93 feet Y = 3792473
79 meter
Z = 16532855
88 Z = 5027213
06
XDOT = -15641
109197 XDOT = -4713
272256
YDOT = -18607
691795 feet/sec YDOT = -5724
634025 meter/sec
ZDOT = 6509
824636 ZDOT = 1961
168234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13151630
98 X = 4008617
12
Y = -7058363
79 feet Y = -2151389
28 meter
Z = 16479052
43 Z = 5022815
18
XDOT = 4225
365945 XDOT = 1287
891540
YDOT = 22909
944598 feet/sec YDOT = 6982
951114 meter/sec
ZDOT = 6408
743791 ZDOT = 1953
385108
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
55162709
00016717 00000-0 10270-3 0 9077
2 25544 51
6375 62
5051 0004883 172
7385 187
3840 15
54135756 32226
Satellite: ISS
Catalog Number: 25544
Epoch time: 17235
55162709 = yrday
fracday
Element set: 907
Inclination: 51
6375 deg
RA of node: 62
5051 deg
Eccentricity:
0004883
Arg of perigee: 172
7385 deg
Mean anomaly: 187
3840 deg
Mean motion: 15
54135756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3222
Checksum: 317
Coasting Arc #9 (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 = 3488755
29 A = 6777207
12 meter
Y = -2311508
65 meter E =
0016018
Z = -5343765
78 I = 51
93482
XDOT = 4190
190115 Wp = 107
93885
YDOT = 6409
124073 meter/sec RA = 57
06779 deg
ZDOT = -41
616075 TA = 161
69451
MA = 161
63679
Ha = 221
796 n
mi
Hp = 214
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11446047
53 X = 3540301
02
Y = -7583689
79 feet Y = -2272207
26 meter
Z = -17532039
98 Z = -5326693
28
XDOT = 13747
342896 XDOT = 4118
412316
YDOT = 21027
309951 feet/sec YDOT = 6455
580295 meter/sec
ZDOT = -136
535679 ZDOT = -21
436543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13766463
90 X = -4196018
20
Y = 1291765
36 feet Y = 393730
08 meter
Z = -17456018
86 Z = -5320594
55
XDOT = -2212
576455 XDOT = -674
393303
YDOT = -24012
774367 feet/sec YDOT = -7319
093627 meter/sec
ZDOT = -48
201702 ZDOT = -14
691879
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
51612648
00016717 00000-0 10270-3 0 9087
2 25544 51
6374 57
6957 0005039 176
1579 183
9613 15
54180629 32377
Satellite: ISS
Catalog Number: 25544
Epoch time: 17236
51612648 = yrday
fracday
Element set: 908
Inclination: 51
6374 deg
RA of node: 57
6957 deg
Eccentricity:
0005039
Arg of perigee: 176
1579 deg
Mean anomaly: 183
9613 deg
Mean motion: 15
54180629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3237
Checksum: 338
Coasting Arc #10 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2017/237/06:37:41
861
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4764109
73 A = 6779967
36 meter
Y = 45871
53 meter E =
0012858
Z = -4835731
00 I = 51
93286
XDOT = 2542
402033 Wp = 128
33506
YDOT = 6752
591799 meter/sec RA = 53
19854 deg
ZDOT = 2565
657174 TA = 166
86734
MA = 166
83383
Ha = 221
617 n
mi
Hp = 215
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15630281
26 X = 4786732
13
Y = 150497
14 feet Y = 99273
12 meter
Z = -15865259
18 Z = -4812533
67
XDOT = 8341
214020 XDOT = 2454
241198
YDOT = 22154
172570 feet/sec YDOT = 6780
529954 meter/sec
ZDOT = 8417
510412 ZDOT = 2577
792567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4930822
47 X = 1502914
69
Y = -14942067
26 feet Y = -4554342
10 meter
Z = -15762499
99 Z = -4804410
00
XDOT = 22536
080026 XDOT = 6868
997192
YDOT = -1509
352033 feet/sec YDOT = -460
050500 meter/sec
ZDOT = 8470
139442 ZDOT = 2581
698502
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
28772544
00016717 00000-0 10270-3 0 9095
2 25544 51
6423 53
8527 0004520 190
0459 170
0604 15
53991232 32498
Satellite: ISS
Catalog Number: 25544
Epoch time: 17237
28772544 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 53
8527 deg
Eccentricity:
0004520
Arg of perigee: 190
0459 deg
Mean anomaly: 170
0604 deg
Mean motion: 15
53991232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 307
Coasting Arc #11 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2017/238/06:37:41
861
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5363995
13 A = 6783417
79 meter
Y = -1436684
89 meter E =
0010642
Z = 3884903
21 I = 51
92392
XDOT = -1306
422675 Wp = 104
43021
YDOT = -6328
293087 meter/sec RA = 48
22963 deg
ZDOT = -4137
232237 TA = 28
83336
MA = 28
77460
Ha = 221
675 n
mi
Hp = 215
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17598409
21 X = -5366401
94
Y = -4713533
11 feet Y = -1496681
89 meter
Z = 12745745
44 Z = 3858840
98
XDOT = -4286
163631 XDOT = -1215
464378
YDOT = -20762
116426 feet/sec YDOT = -6342
394142 meter/sec
ZDOT = -13573
596577 ZDOT = -4143
356981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9603901
25 X = -2927269
10
Y = 15575945
24 feet Y = 4747548
11 meter
Z = 12630535
95 Z = 3849787
36
XDOT = -19956
628452 XDOT = -6082
780352
YDOT = -1258
578464 feet/sec YDOT = -383
614716 meter/sec
ZDOT = -13599
657398 ZDOT = -4145
175575
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
31665041
00016717 00000-0 10270-3 0 9105
2 25544 51
6421 48
7252 0004415 192
1859 167
9187 15
53997409 32655
Satellite: ISS
Catalog Number: 25544
Epoch time: 17238
31665041 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 48
7252 deg
Eccentricity:
0004415
Arg of perigee: 192
1859 deg
Mean anomaly: 167
9187 deg
Mean motion: 15
53997409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 324
Coasting Arc #12 (Orbit 3279)
---------------------------------------
Vector Time (GMT): 2017/239/06:37:41
861
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5714142
83 A = 6786963
33 meter
Y = 2611816
20 meter E =
0002817
Z = -2570773
58 I = 51
91358
XDOT = -156
711855 Wp = 108
37103
YDOT = 5543
176660 meter/sec RA = 43
26827 deg
ZDOT = 5287
223300 TA = 222
86853
MA = 222
89049
Ha = 221
385 n
mi
Hp = 215
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18747187
77 X = 5696999
65
Y = 8568950
78 feet Y = 2675619
61 meter
Z = -8434296
51 Z = -2543057
94
XDOT = -514
146507 XDOT = -244
368141
YDOT = 18186
275131 feet/sec YDOT = 5540
934442 meter/sec
ZDOT = 17346
533136 ZDOT = 5286
248768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13349715
67 X = 4068993
34
Y = -15770781
12 feet Y = -4806934
09 meter
Z = -8311972
02 Z = -2533489
07
XDOT = 16184
604954 XDOT = 4933
067590
YDOT = 4567
119349 feet/sec YDOT = 1392
057977 meter/sec
ZDOT = 17341
269084 ZDOT = 5285
618817
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
28126549
00016717 00000-0 10270-3 0 9118
2 25544 51
6423 43
9176 0004466 197
7916 162
3081 15
54005582 32802
Satellite: ISS
Catalog Number: 25544
Epoch time: 17239
28126549 = yrday
fracday
Element set: 911
Inclination: 51
6423 deg
RA of node: 43
9176 deg
Eccentricity:
0004466
Arg of perigee: 197
7916 deg
Mean anomaly: 162
3081 deg
Mean motion: 15
54005582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3280
Checksum: 314
Coasting Arc #13 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2017/240/06:37:41
861
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5705807
40 A = 6789436
16 meter
Y = -3529318
60 meter E =
0015279
Z = 979755
31 I = 51
89750
XDOT = 1775
250106 Wp = 141
29241
YDOT = -4527
961314 meter/sec RA = 38
31445 deg
ZDOT = -5934
096046 TA = 28
12626
MA = 28
04381
Ha = 221
430 n
mi
Hp = 215
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18719840
54 X = -5670676
71
Y = -11579129
28 feet Y = -3592928
34 meter
Z = 3214420
30 Z = 952123
85
XDOT = 5824
311372 XDOT = 1854
575892
YDOT = -14855
516123 feet/sec YDOT = -4507
666053 meter/sec
ZDOT = -19468
819050 ZDOT = -5925
279530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15972011
21 X = -4868269
02
Y = 15171407
92 feet Y = 4624245
13 meter
Z = 3092636
73 Z = 942635
67
XDOT = -11743
787391 XDOT = -3579
506397
YDOT = -8376
435099 feet/sec YDOT = -2553
137418 meter/sec
ZDOT = -19428
985981 ZDOT = -5921
954927
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
31018785
00016717 00000-0 10270-3 0 9127
2 25544 51
6428 38
7902 0004569 200
6274 159
4695 15
53963723 32965
Satellite: ISS
Catalog Number: 25544
Epoch time: 17240
31018785 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 38
7902 deg
Eccentricity:
0004569
Arg of perigee: 200
6274 deg
Mean anomaly: 159
4695 deg
Mean motion: 15
53963723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 326
Coasting Arc #14 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2017/241/06:37:41
861
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5326594
44 A = 6789431
44 meter
Y = 4148467
03 meter E =
0009472
Z = 682580
19 I = 51
87175
XDOT = -3405
026921 Wp = 63
97569
YDOT = 3378
118613 meter/sec RA = 33
36081 deg
ZDOT = 5980
332094 TA = 303
37096
MA = 303
46156
Ha = 221
112 n
mi
Hp = 215
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17475703
53 X = 5276493
66
Y = 13610456
13 feet Y = 4207752
54 meter
Z = 2239436
31 Z = 708333
18
XDOT = -11171
348165 XDOT = -3471
598312
YDOT = 11083
066317 feet/sec YDOT = 3339
669335 meter/sec
ZDOT = 19620
512121 ZDOT = 5963
629729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17377218
93 X = 5296576
33
Y = -13717014
41 feet Y = -4180945
99 meter
Z = 2352781
93 Z = 717127
93
XDOT = 7074
582856 XDOT = 2156
332855
YDOT = 12347
192452 feet/sec YDOT = 3763
424259 meter/sec
ZDOT = 19545
945909 ZDOT = 5957
604313
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
33910382
00016717 00000-0 10270-3 0 9135
2 25544 51
6426 33
6613 0004408 207
1231 152
9692 15
54018278 33124
Satellite: ISS
Catalog Number: 25544
Epoch time: 17241
33910382 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 33
6613 deg
Eccentricity:
0004408
Arg of perigee: 207
1231 deg
Mean anomaly: 152
9692 deg
Mean motion: 15
54018278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 283
Coasting Arc #15 (Orbit 3325)
---------------------------------------
Vector Time (GMT): 2017/242/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4885666
25 A = 6781208
98 meter
Y = -1373807
07 meter E =
0009684
Z = -4507118
18 I = 51
81709
XDOT = 4469
972192 Wp = 136
48671
YDOT = 5321
315594 meter/sec RA = 28
59476 deg
ZDOT = 3220
688950 TA = 165
86592
MA = 165
83880
Ha = 221
032 n
mi
Hp = 215
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16029088
73 X = 4922558
69
Y = -4507241
04 feet Y = -1318966
12 meter
Z = -14787133
14 Z = -4483295
56
XDOT = 14665
263097 XDOT = 4394
491146
YDOT = 17458
384496 feet/sec YDOT = 5370
879952 meter/sec
ZDOT = 10566
564797 ZDOT = 3242
219066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4091014
17 X = 1246941
12
Y = -16236590
81 feet Y = -4948912
88 meter
Z = -14681380
59 Z = -4474884
80
XDOT = 21217
607330 XDOT = 6467
126714
YDOT = -4301
950999 feet/sec YDOT = -1311
234665 meter/sec
ZDOT = 10660
992914 ZDOT = 3249
470640
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
23940701
00016717 00000-0 10270-3 0 9144
2 25544 51
6422 29
1747 0004370 210
2574 149
8327 15
54007055 33267
Satellite: ISS
Catalog Number: 25544
Epoch time: 17242
23940701 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 29
1747 deg
Eccentricity:
0004370
Arg of perigee: 210
2574 deg
Mean anomaly: 149
8327 deg
Mean motion: 15
54007055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3326
Checksum: 285
Coasting Arc #16 (Orbit 3341)
---------------------------------------
Vector Time (GMT): 2017/243/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925107
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5860354
29 A = 6784872
06 meter
Y = 347622
92 meter E =
0010824
Z = 3388807
02 I = 51
80061
XDOT = -3008
523576 Wp = 110
02574
YDOT = -5309
175900 meter/sec RA = 23
62118 deg
ZDOT = -4649
691417 TA = 30
46849
MA = 30
40564
Ha = 221
014 n
mi
Hp = 215
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19226884
15 X = -5880267
02
Y = 1140495
14 feet Y = 281977
23 meter
Z = 11118133
27 Z = 3360291
02
XDOT = -9870
484174 XDOT = -2926
345573
YDOT = -17418
556102 feet/sec YDOT = -5342
359934 meter/sec
ZDOT = -15254
893102 ZDOT = -4664
106028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8290149
45 X = -2526837
55
Y = 17465421
30 feet Y = 5323460
41 meter
Z = 10991777
45 Z = 3350293
77
XDOT = -18698
322728 XDOT = -5699
248768
YDOT = 782
398292 feet/sec YDOT = 238
474999 meter/sec
ZDOT = -15317
801315 ZDOT = -4668
865841
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
26832188
00016717 00000-0 10270-3 0 9158
2 25544 51
6425 24
0471 0004288 214
0883 145
9995 15
54023397 33424
Satellite: ISS
Catalog Number: 25544
Epoch time: 17243
26832188 = yrday
fracday
Element set: 915
Inclination: 51
6425 deg
RA of node: 24
0471 deg
Eccentricity:
0004288
Arg of perigee: 214
0883 deg
Mean anomaly: 145
9995 deg
Mean motion: 15
54023397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3342
Checksum: 316
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