[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 31st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 568 ET - UTC (sec) : 67 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
There are no maneuvers
Coasting Arc #1 (Orbit 2512)
---------------------------------------
Vector Time (GMT): 2015/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6013219
92 A = 6783829
92 meter
Y = 2180167
73 meter E =
0009386
Z = -2247959
61 I = 51
67317
XDOT = -3515
273280 Wp = 25
41075
YDOT = -4088
316700 meter/sec RA = 176
20174 deg
ZDOT = 5454
940227 TA = 309
58678
MA = 309
66963
Ha = 219
697 n
mi
Hp = 212
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19728411
80 X = -6026232
25
Y = 7152781
28 feet Y = 2112851
33 meter
Z = -7375195
56 Z = -2277202
59
XDOT = -11533
048820 XDOT = -3495
793930
YDOT = -13413
112534 feet/sec YDOT = -4127
518138 meter/sec
ZDOT = 17896
785522 ZDOT = 5437
910571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1522226
45 X = -463974
62
Y = 20884976
42 feet Y = 6365740
81 meter
Z = -7501107
13 Z = -2286337
45
XDOT = -15478
701395 XDOT = -4717
908185
YDOT = 5254
291582 feet/sec YDOT = 1601
508074 meter/sec
ZDOT = 17824
363671 ZDOT = 5432
866047
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 15149
50454785
00016717 00000-0 10270-3 0 9005
2 25544 51
6427 177
3246 0004296 357
9989 2
1146 15
55255957 25132
Satellite: ISS
Catalog Number: 25544
Epoch time: 15149
50454785 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 177
3246 deg
Eccentricity:
0004296
Arg of perigee: 357
9989 deg
Mean anomaly: 2
1146 deg
Mean motion: 15
55255957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2513
Checksum: 331
Coasting Arc #2 (Orbit 2528)
---------------------------------------
Vector Time (GMT): 2015/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6673260
97 A = 6786082
04 meter
Y = -1197213
65 meter E =
0010288
Z = 209619
41 I = 51
71084
XDOT = 1029
352812 Wp = 113
49371
YDOT = 4644
505762 meter/sec RA = 171
22770 deg
ZDOT = -6013
284903 TA = 64
24981
MA = 64
14366
Ha = 219
911 n
mi
Hp = 212
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21893900
82 X = 6685134
25
Y = -3927866
31 feet Y = -1122522
51 meter
Z = 687727
74 Z = 242066
13
XDOT = 3377
141772 XDOT = 1006
551104
YDOT = 15237
879798 feet/sec YDOT = 4655
889552 meter/sec
ZDOT = -19728
625009 ZDOT = -6008
339509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4995511
36 X = 1522631
86
Y = -21670360
63 feet Y = -6605125
92 meter
Z = 827244
02 Z = 252143
98
XDOT = 13805
755813 XDOT = 4207
994372
YDOT = 2406
273208 feet/sec YDOT = 733
432074 meter/sec
ZDOT = -19708
177706 ZDOT = -6007
052565
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 15150
53265247
00016717 00000-0 10270-3 0 9014
2 25544 51
6415 172
1903 0004406 1
8956 358
2214 15
55236087 25295
Satellite: ISS
Catalog Number: 25544
Epoch time: 15150
53265247 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 172
1903 deg
Eccentricity:
0004406
Arg of perigee: 1
8956 deg
Mean anomaly: 358
2214 deg
Mean motion: 15
55236087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2529
Checksum: 293
Coasting Arc #3 (Orbit 2544)
---------------------------------------
Vector Time (GMT): 2015/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6522186
65 A = 6784743
69 meter
Y = 108486
80 meter E =
0016673
Z = 1830880
12 I = 51
73700
XDOT = 1512
444611 Wp = 52
28506
YDOT = -4962
842388 meter/sec RA = 166
25748 deg
ZDOT = 5656
716486 TA = 327
84608
MA = 327
94765
Ha = 220
051 n
mi
Hp = 212
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21398250
17 X = -6531808
91
Y = 355927
82 feet Y = 35497
49 meter
Z = 6006824
54 Z = 1799172
69
XDOT = 4962
088618 XDOT = 1540
349210
YDOT = -16282
291300 feet/sec YDOT = -4945
773689 meter/sec
ZDOT = 18558
781121 ZDOT = 5664
131142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7758364
92 X = -2364749
63
Y = 19985919
37 feet Y = 6091708
22 meter
Z = 5870650
45 Z = 1789374
26
XDOT = -11791
868282 XDOT = -3594
161452
YDOT = -10063
365324 feet/sec YDOT = -3067
313751 meter/sec
ZDOT = 18591
466056 ZDOT = 5666
678854
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 15151
56074953
00016717 00000-0 10270-3 0 9021
2 25544 51
6411 167
0565 0004533 5
3205 354
7996 15
55240819 25459
Satellite: ISS
Catalog Number: 25544
Epoch time: 15151
56074953 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 167
0565 deg
Eccentricity:
0004533
Arg of perigee: 5
3205 deg
Mean anomaly: 354
7996 deg
Mean motion: 15
55240819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2545
Checksum: 304
Coasting Arc #4 (Orbit 2559)
---------------------------------------
Vector Time (GMT): 2015/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5627540
84 A = 6780601
30 meter
Y = 1110471
46 meter E =
0007839
Z = -3625713
52 I = 51
75329
XDOT = -3820
199820 Wp = 49
61202
YDOT = 4965
024542 meter/sec RA = 161
27890 deg
ZDOT = -4410
056237 TA = 173
25779
MA = 173
24724
Ha = 220
043 n
mi
Hp = 212
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18463060
50 X = 5632317
67
Y = 3643279
06 feet Y = 1173429
38 meter
Z = -11895385
56 Z = -3598363
85
XDOT = -12533
463975 XDOT = -3854
013234
YDOT = 16289
450598 feet/sec YDOT = 4922
115959 meter/sec
ZDOT = -14468
688440 ZDOT = -4428
695955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10094831
99 X = 3076904
79
Y = -15969614
42 feet Y = -4867538
47 meter
Z = -11778118
07 Z = -3589970
39
XDOT = 9527
413733 XDOT = 2903
955706
YDOT = 16750
117348 feet/sec YDOT = 5105
435768 meter/sec
ZDOT = -14549
592009 ZDOT = -4434
715644
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 15152
52458274
00016717 00000-0 10270-3 0 9031
2 25544 51
6405 162
2427 0004504 8
3806 351
7421 15
55251945 25603
Satellite: ISS
Catalog Number: 25544
Epoch time: 15152
52458274 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 162
2427 deg
Eccentricity:
0004504
Arg of perigee: 8
3806 deg
Mean anomaly: 351
7421 deg
Mean motion: 15
55251945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2560
Checksum: 288
Coasting Arc #5 (Orbit 2575)
---------------------------------------
Vector Time (GMT): 2015/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4105839
90 A = 6776181
45 meter
Y = -2360908
67 meter E =
0007325
Z = 4839496
17 I = 51
76746
XDOT = 5601
988023 Wp = 83
07805
YDOT = -4612
145905 meter/sec RA = 156
28713 deg
ZDOT = 2500
366148 TA = 342
40641
MA = 342
43177
Ha = 220
247 n
mi
Hp = 212
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13470603
34 X = -4102643
28
Y = -7745763
35 feet Y = -2406805
55 meter
Z = 15877612
11 Z = 4819558
00
XDOT = 18379
225796 XDOT = 5640
999775
YDOT = -15131
712286 feet/sec YDOT = -4549
282979 meter/sec
ZDOT = 8203
301011 ZDOT = 2527
674119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11953616
55 X = -3643462
32
Y = 10063018
76 feet Y = 3067208
12 meter
Z = 15792380
29 Z = 4813517
51
XDOT = -7139
349955 XDOT = -2176
073866
YDOT = -21552
124239 feet/sec YDOT = -6569
087468 meter/sec
ZDOT = 8321
393594 ZDOT = 2536
360767
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 15153
55266465
00016717 00000-0 10270-3 0 9045
2 25544 51
6396 157
1079 0004607 12
1713 347
9551 15
55259931 25763
Satellite: ISS
Catalog Number: 25544
Epoch time: 15153
55266465 = yrday
fracday
Element set: 904
Inclination: 51
6396 deg
RA of node: 157
1079 deg
Eccentricity:
0004607
Arg of perigee: 12
1713 deg
Mean anomaly: 347
9551 deg
Mean motion: 15
55259931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2576
Checksum: 322
Coasting Arc #6 (Orbit 2590)
---------------------------------------
Vector Time (GMT): 2015/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2208405
07 A = 6774077
78 meter
Y = 3573108
57 meter E =
0016769
Z = -5328495
24 I = 51
78934
XDOT = -6640
365970 Wp = 73
33019
YDOT = 3810
510735 meter/sec RA = 151
28655 deg
ZDOT = -192
726098 TA = 194
80987
MA = 194
85904
Ha = 220
191 n
mi
Hp = 212
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7245423
45 X = 2194169
68
Y = 11722797
15 feet Y = 3597725
48 meter
Z = -17481939
77 Z = -5317801
25
XDOT = -21785
977593 XDOT = -6681
546282
YDOT = 12501
675639 feet/sec YDOT = 3736
023593 meter/sec
ZDOT = -632
303470 ZDOT = -225
083592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13489100
61 X = 4111477
86
Y = -3089781
72 feet Y = -941765
47 meter
Z = -17436621
40 Z = -5314682
20
XDOT = 4412
661997 XDOT = 1344
979377
YDOT = 23698
615891 feet/sec YDOT = 7223
338124 meter/sec
ZDOT = -771
971483 ZDOT = -235
296908
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 15154
51648365
00016717 00000-0 10270-3 0 9056
2 25544 51
6397 152
2948 0004601 14
9327 345
1961 15
55262489 25914
Satellite: ISS
Catalog Number: 25544
Epoch time: 15154
51648365 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 152
2948 deg
Eccentricity:
0004601
Arg of perigee: 14
9327 deg
Mean anomaly: 345
1961 deg
Mean motion: 15
55262489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2591
Checksum: 324
Coasting Arc #7 (Orbit 2606)
---------------------------------------
Vector Time (GMT): 2015/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -148606
50 A = 6775438
19 meter
Y = -4599062
74 meter E =
0010242
Z = 4970067
33 I = 51
82137
XDOT = 6901
634829 Wp = 40
55676
YDOT = -2565
645687 meter/sec RA = 146
28571 deg
ZDOT = -2157
675979 TA = 70
45991
MA = 70
34933
Ha = 220
202 n
mi
Hp = 212
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -487554
14 X = -121310
52
Y = -15088788
52 feet Y = -4600572
58 meter
Z = 16305995
19 Z = 4969411
13
XDOT = 22643
158889 XDOT = 6940
292794
YDOT = -8417
472728 feet/sec YDOT = -2488
250666 meter/sec
ZDOT = -7078
989434 ZDOT = -2124
055389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14515243
04 X = -4424246
08
Y = -4157239
60 feet Y = -1267126
63 meter
Z = 16303981
29 Z = 4969453
50
XDOT = -1202
966046 XDOT = -366
664051
YDOT = -23123
908402 feet/sec YDOT = -7048
167281 meter/sec
ZDOT = -6934
087932 ZDOT = -2113
510002
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 15155
54454955
00016717 00000-0 10270-3 0 9061
2 25544 51
6393 147
1598 0004675 17
7047 342
4269 15
55295236 26070
Satellite: ISS
Catalog Number: 25544
Epoch time: 15155
54454955 = yrday
fracday
Element set: 906
Inclination: 51
6393 deg
RA of node: 147
1598 deg
Eccentricity:
0004675
Arg of perigee: 17
7047 deg
Mean anomaly: 342
4269 deg
Mean motion: 15
55295236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2607
Checksum: 335
Coasting Arc #8 (Orbit 2621)
---------------------------------------
Vector Time (GMT): 2015/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1752213
80 A = 6779605
90 meter
Y = 5291416
43 meter E =
0008381
Z = -3863854
73 I = 51
86142
XDOT = -6371
799556 Wp = 71
19454
YDOT = 920
098245 meter/sec RA = 141
29791 deg
ZDOT = 4159
576416 TA = 242
39203
MA = 242
47716
Ha = 220
319 n
mi
Hp = 212
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5748732
96 X = -1792484
26
Y = 17360290
11 feet Y = 5271597
34 meter
Z = -12676688
74 Z = -3872463
82
XDOT = -20904
854185 XDOT = -6401
820459
YDOT = 3018
695031 feet/sec YDOT = 848
676241 meter/sec
ZDOT = 13646
904252 ZDOT = 4128
550565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14899242
43 X = 4541289
09
Y = 10558275
76 feet Y = 3218162
45 meter
Z = -12714614
77 Z = -3875414
58
XDOT = -2567
230797 XDOT = -782
491947
YDOT = 19856
651863 feet/sec YDOT = 6052
307488 meter/sec
ZDOT = 13513
419545 ZDOT = 4118
890277
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 15156
50835461
00016717 00000-0 10270-3 0 9074
2 25544 51
6396 142
3468 0004780 21
6509 338
4845 15
55280754 26221
Satellite: ISS
Catalog Number: 25544
Epoch time: 15156
50835461 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 142
3468 deg
Eccentricity:
0004780
Arg of perigee: 21
6509 deg
Mean anomaly: 338
4845 deg
Mean motion: 15
55280754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2622
Checksum: 319
Coasting Arc #9 (Orbit 2637)
---------------------------------------
Vector Time (GMT): 2015/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3356672
35 A = 6783893
38 meter
Y = -5497534
16 meter E =
0015039
Z = 2114950
69 I = 51
90058
XDOT = 5204
792152 Wp = 91
37616
YDOT = 1034
439488 meter/sec RA = 136
32603 deg
ZDOT = -5538
157416 TA = 65
26941
MA = 65
11296
Ha = 220
294 n
mi
Hp = 211
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11012704
55 X = 3407623
98
Y = -18036529
38 feet Y = -5459713
00 meter
Z = 6938814
60 Z = 2131379
88
XDOT = 17076
089736 XDOT = 5219
740247
YDOT = 3393
830340 feet/sec YDOT = 1092
727084 meter/sec
ZDOT = -18169
807796 ZDOT = -5512
837131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14244755
01 X = -4341801
33
Y = -15578335
15 feet Y = -4748276
55 meter
Z = 7010394
47 Z = 2136768
24
XDOT = 6932
566883 XDOT = 2113
046386
YDOT = -14515
847445 feet/sec YDOT = -4424
430301 meter/sec
ZDOT = -18061
171472 ZDOT = -5505
045065
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 15157
53640479
00016717 00000-0 10270-3 0 9082
2 25544 51
6398 137
2118 0004854 23
7453 336
3923 15
55333448 26381
Satellite: ISS
Catalog Number: 25544
Epoch time: 15157
53640479 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 137
2118 deg
Eccentricity:
0004854
Arg of perigee: 23
7453 deg
Mean anomaly: 336
3923 deg
Mean motion: 15
55333448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2638
Checksum: 327
Coasting Arc #10 (Orbit 2652)
---------------------------------------
Vector Time (GMT): 2015/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4436771
36 A = 6785764
38 meter
Y = 5122757
29 meter E =
0016517
Z = -71339
86 I = 51
92926
XDOT = -3613
189700 Wp = 40
75451
YDOT = -3056
327935 meter/sec RA = 131
36796 deg
ZDOT = 6040
698389 TA = 318
47938
MA = 318
60473
Ha = 220
322 n
mi
Hp = 211
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14556336
47 X = -4493378
96
Y = 16806946
50 feet Y = 5072825
91 meter
Z = -234054
66 Z = -93029
80
XDOT = -11854
296916 XDOT = -3608
087965
YDOT = -10027
322620 feet/sec YDOT = -3096
705043 meter/sec
ZDOT = 19818
564267 ZDOT = 6023
158340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12380599
65 X = 3773606
77
Y = 18466949
02 feet Y = 5628726
06 meter
Z = -328191
77 Z = -100032
85
XDOT = -11479
951084 XDOT = -3499
089090
YDOT = 8014
114072 feet/sec YDOT = 2442
701969 meter/sec
ZDOT = 19743
716453 ZDOT = 6017
884775
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 15158
50019526
00016717 00000-0 10270-3 0 9094
2 25544 51
6398 132
3990 0004708 29
6662 330
4758 15
55354855 26533
Satellite: ISS
Catalog Number: 25544
Epoch time: 15158
50019526 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 132
3990 deg
Eccentricity:
0004708
Arg of perigee: 29
6662 deg
Mean anomaly: 330
4758 deg
Mean motion: 15
55354855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2653
Checksum: 331
Coasting Arc #11 (Orbit 2668)
---------------------------------------
Vector Time (GMT): 2015/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5004875
39 A = 6784090
33 meter
Y = -4106563
51 meter E =
0006923
Z = -2031439
00 I = 51
94463
XDOT = 1790
561263 Wp = 98
22883
YDOT = 4935
541275 meter/sec RA = 126
41080 deg
ZDOT = -5582
986900 TA = 104
11849
MA = 104
04154
Ha = 220
431 n
mi
Hp = 211
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16420194
85 X = 5060291
95
Y = -13472977
38 feet Y = -4050285
70 meter
Z = -6664826
11 Z = -2006992
03
XDOT = 5874
544827 XDOT = 1762
357812
YDOT = 16192
720719 feet/sec YDOT = 4955
407250 meter/sec
ZDOT = -18316
886156 ZDOT = -5574
356821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8995473
97 X = -2741820
46
Y = -19277570
29 feet Y = -5875803
42 meter
Z = -6559005
84 Z = -1999184
98
XDOT = 15762
835316 XDOT = 4804
512204
YDOT = -1155
074367 feet/sec YDOT = -352
066667 meter/sec
ZDOT = -18280
669697 ZDOT = -5571
948124
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 15159
52822980
00016717 00000-0 10270-3 0 9105
2 25544 51
6406 127
2639 0004901 30
9710 329
1732 15
55346055 26697
Satellite: ISS
Catalog Number: 25544
Epoch time: 15159
52822980 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 127
2639 deg
Eccentricity:
0004901
Arg of perigee: 30
9710 deg
Mean anomaly: 329
1732 deg
Mean motion: 15
55346055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2669
Checksum: 306
Coasting Arc #12 (Orbit 2684)
---------------------------------------
Vector Time (GMT): 2015/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5015911
52 A = 6779705
27 meter
Y = 2533405
99 meter E =
0014415
Z = 3778601
58 I = 51
94854
XDOT = -5
836320 Wp = 79
73579
YDOT = -6385
051044 meter/sec RA = 121
44522 deg
ZDOT = 4261
929933 TA = 325
38637
MA = 325
48012
Ha = 220
462 n
mi
Hp = 211
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16456402
61 X = -5062222
93
Y = 8311699
43 feet Y = 2477055
59 meter
Z = 12396986
80 Z = 3754122
89
XDOT = -19
148032 XDOT = 44
860389
YDOT = -20948
330196 feet/sec YDOT = -6384
833134 meter/sec
ZDOT = 13982
709755 ZDOT = 4262
024290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4286661
86 X = 1306574
53
Y = 18003646
49 feet Y = 5487511
45 meter
Z = 12291300
14 Z = 3746388
28
XDOT = -19097
381007 XDOT = -5820
881731
YDOT = -5025
559487 feet/sec YDOT = -1531
790532 meter/sec
ZDOT = 13984
262126 ZDOT = 4262
403096
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 15160
55625449
00016717 00000-0 10270-3 0 9112
2 25544 51
6407 122
1301 0004695 34
2187 325
9268 15
55386384 26858
Satellite: ISS
Catalog Number: 25544
Epoch time: 15160
55625449 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 122
1301 deg
Eccentricity:
0004695
Arg of perigee: 34
2187 deg
Mean anomaly: 325
9268 deg
Mean motion: 15
55386384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2685
Checksum: 314
Coasting Arc #13 (Orbit 2699)
---------------------------------------
Vector Time (GMT): 2015/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4600481
06 A = 6775451
17 meter
Y = -528015
42 meter E =
0016424
Z = -4961245
42 I = 51
94997
XDOT = -1597
911536 Wp = 63
65526
YDOT = 7145
835032 meter/sec RA = 116
46363 deg
ZDOT = -2240
875340 TA = 184
52205
MA = 184
53691
Ha = 220
477 n
mi
Hp = 211
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15093441
79 X = 4630143
53
Y = -1732334
06 feet Y = -476403
66 meter
Z = -16277051
89 Z = -4938825
04
XDOT = -5242
491915 XDOT = -1666
813821
YDOT = 23444
340656 feet/sec YDOT = 7127
581031 meter/sec
ZDOT = -7351
953216 ZDOT = -2248
804618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1546595
44 X = 471402
29
Y = -15216854
99 feet Y = -4638097
40 meter
Z = -16180567
09 Z = -4931836
85
XDOT = 20686
878835 XDOT = 6305
360669
YDOT = 9962
510937 feet/sec YDOT = 3036
573334 meter/sec
ZDOT = -7387
336841 ZDOT = -2251
660269
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 15161
52002234
00016717 00000-0 10270-3 0 9122
2 25544 51
6408 117
3157 0004872 37
3075 322
8416 15
55362110 27001
Satellite: ISS
Catalog Number: 25544
Epoch time: 15161
52002234 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 117
3157 deg
Eccentricity:
0004872
Arg of perigee: 37
3075 deg
Mean anomaly: 322
8416 deg
Mean motion: 15
55362110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2700
Checksum: 267
Coasting Arc #14 (Orbit 2715)
---------------------------------------
Vector Time (GMT): 2015/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3827395
67 A = 6773686
46 meter
Y = -1664178
84 meter E =
0006809
Z = 5330508
83 I = 51
95810
XDOT = 2903
191807 Wp = 54
48190
YDOT = -7103
834190 meter/sec RA = 111
47346 deg
ZDOT = -129
297398 TA = 36
76709
MA = 36
72041
Ha = 220
608 n
mi
Hp = 211
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12557072
42 X = -3834395
81
Y = -5459904
32 feet Y = -1707018
82 meter
Z = 17488546
04 Z = 5311898
80
XDOT = 9524
907504 XDOT = 2983
040891
YDOT = -23306
542619 feet/sec YDOT = -7070
922328 meter/sec
ZDOT = -424
204061 ZDOT = -115
000713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7840026
89 X = -2389640
20
Y = 11349281
61 feet Y = 3459261
04 meter
Z = 17408838
30 Z = 5306213
91
XDOT = -20153
803909 XDOT = -6142
879431
YDOT = -13347
659776 feet/sec YDOT = -4068
366700 meter/sec
ZDOT = -361
436397 ZDOT = -110
165814
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 15162
54803130
00016717 00000-0 10270-3 0 9130
2 25544 51
6412 112
1816 0004877 39
9481 320
2031 15
55386343 27161
Satellite: ISS
Catalog Number: 25544
Epoch time: 15162
54803130 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 112
1816 deg
Eccentricity:
0004877
Arg of perigee: 39
9481 deg
Mean anomaly: 320
2031 deg
Mean motion: 15
55386343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2716
Checksum: 285
Coasting Arc #15 (Orbit 2730)
---------------------------------------
Vector Time (GMT): 2015/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2866766
13 A = 6775683
29 meter
Y = 3747697
71 meter E =
0014560
Z = -4875281
10 I = 51
97568
XDOT = -3838
507624 Wp = 90
06919
YDOT = 6148
802792 meter/sec RA = 106
48362 deg
ZDOT = 2475
901616 TA = 204
12203
MA = 204
19029
Ha = 220
544 n
mi
Hp = 211
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9405400
68 X = 2848327
95
Y = 12295596
16 feet Y = 3779653
11 meter
Z = -15995016
73 Z = -4861399
20
XDOT = -12593
528949 XDOT = -3919
006851
YDOT = 20173
237507 feet/sec YDOT = 6105
427765 meter/sec
ZDOT = 8123
036798 ZDOT = 2457
059721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13800985
12 X = 4206540
26
Y = -7145612
12 feet Y = -2177982
58 meter
Z = -15936023
47 Z = -4857299
95
XDOT = 17055
342177 XDOT = 5198
468296
YDOT = 15054
570917 feet/sec YDOT = 4588
633216 meter/sec
ZDOT = 8040
883781 ZDOT = 2450
861377
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 15163
51178205
00016717 00000-0 10270-3 0 9147
2 25544 51
6413 107
3674 0004887 43
1334 317
0201 15
55385007 27311
Satellite: ISS
Catalog Number: 25544
Epoch time: 15163
51178205 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 107
3674 deg
Eccentricity:
0004887
Arg of perigee: 43
1334 deg
Mean anomaly: 317
0201 deg
Mean motion: 15
55385007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2731
Checksum: 282
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