[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 1st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 819 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
245/10:53:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
4
000/00:00:00
000 0
0 0
0 212
8
250/04:11:18
328 0
8 0
9 0
9
N/A 0
5 0
0 219
0
000/00:04:32
655 -0
1 0
0 213
3
Coasting Arc #1 (Orbit 3973)
---------------------------------------
Vector Time (GMT): 2015/243/08:06:25
568
Vector Time (MET): N/A
Weight (LBS) : 927021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4571503
45 A = 6776016
39 meter
Y = -1185162
13 meter E =
0007036
Z = 4854643
02 I = 51
97235
XDOT = -795
668390 Wp = 66
90594
YDOT = -7209
648941 meter/sec RA = 68
04043 deg
ZDOT = -2503
791926 TA = 47
59468
MA = 47
53517
Ha = 219
415 n
mi
Hp = 212
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14998370
88 X = -4581492
73
Y = -3888327
20 feet Y = -1236338
98 meter
Z = 15927306
48 Z = 4832411
63
XDOT = -2610
460597 XDOT = -702
826845
YDOT = -23653
703874 feet/sec YDOT = -7218
027811 meter/sec
ZDOT = -8214
540438 ZDOT = -2507
430754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1218172
25 X = -371298
90
Y = 15544299
50 feet Y = 4737902
49 meter
Z = 15831617
70 Z = 4825477
07
XDOT = -21722
637395 XDOT = -6621
059878
YDOT = 6697
347385 feet/sec YDOT = 2041
351483 meter/sec
ZDOT = -8228
912363 ZDOT = -2508
172488
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 15243
38161185
00016717 00000-0 10270-3 0 9005
2 25544 51
6444 68
5781 0000859 163
5486 196
5696 15
55301747 39749
Satellite: ISS
Catalog Number: 25544
Epoch time: 15243
38161185 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 68
5781 deg
Eccentricity:
0000859
Arg of perigee: 163
5486 deg
Mean anomaly: 196
5696 deg
Mean motion: 15
55301747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3974
Checksum: 338
Coasting Arc #2 (Orbit 3988)
---------------------------------------
Vector Time (GMT): 2015/244/08:06:25
568
Vector Time (MET): N/A
Weight (LBS) : 927021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4787717
65 A = 6780457
07 meter
Y = 3137214
64 meter E =
0005695
Z = -3640727
84 I = 51
97437
XDOT = -717
108725 Wp = 105
56772
YDOT = 6219
092995 meter/sec RA = 63
06286 deg
ZDOT = 4420
211385 TA = 211
48699
MA = 211
52109
Ha = 219
282 n
mi
Hp = 212
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15707735
07 X = 4769965
93
Y = 10292698
94 feet Y = 3190654
38 meter
Z = -11944645
15 Z = -3617513
63
XDOT = -2352
718915 XDOT = -808
070457
YDOT = 20403
848410 feet/sec YDOT = 6210
565713 meter/sec
ZDOT = 14502
005857 ZDOT = 4416
506194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7109141
28 X = 2166866
26
Y = -17449963
84 feet Y = -5318748
98 meter
Z = -11845083
90 Z = -3610381
57
XDOT = 19225
894299 XDOT = 5860
052582
YDOT = -1990
167548 feet/sec YDOT = -606
603069 meter/sec
ZDOT = 14484
868369 ZDOT = 4414
987879
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 15244
34543518
00016717 00000-0 10270-3 0 9017
2 25544 51
6446 63
7645 0000812 170
1330 189
9840 15
55278512 39894
Satellite: ISS
Catalog Number: 25544
Epoch time: 15244
34543518 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 63
7645 deg
Eccentricity:
0000812
Arg of perigee: 170
1330 deg
Mean anomaly: 189
9840 deg
Mean motion: 15
55278512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 315
Coasting Arc #3 (Orbit 4004)
---------------------------------------
Vector Time (GMT): 2015/245/08:06:25
568
Vector Time (MET): N/A
Weight (LBS) : 927021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4580371
44 A = 6784612
05 meter
Y = -4647180
76 meter E =
0014536
Z = 1832227
59 I = 51
97328
XDOT = 2372
503608 Wp = 116
86569
YDOT = -4586
984370 meter/sec RA = 58
10011 deg
ZDOT = -5675
079710 TA = 43
06259
MA = 42
94894
Ha = 219
337 n
mi
Hp = 212
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15027465
36 X = -4536965
38
Y = -15246656
04 feet Y = -4698158
61 meter
Z = 6011245
38 Z = 1810082
97
XDOT = 7783
804487 XDOT = 2451
187410
YDOT = -15049
161319 feet/sec YDOT = -4560
014093 meter/sec
ZDOT = -18619
027919 ZDOT = -5663
362997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11803873
49 X = -3597820
64
Y = 17890859
11 feet Y = 5453133
86 meter
Z = 5916590
02 Z = 1803376
64
XDOT = -15054
343047 XDOT = -4588
563761
YDOT = -3761
001220 feet/sec YDOT = -1146
353172 meter/sec
ZDOT = -18567
625781 ZDOT = -5659
412338
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 15245
37350150
00016717 00000-0 10270-3 0 9020
2 25544 51
6449 58
6305 0000901 166
3645 193
7533 15
55278067 40055
Satellite: ISS
Catalog Number: 25544
Epoch time: 15245
37350150 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 58
6305 deg
Eccentricity:
0000901
Arg of perigee: 166
3645 deg
Mean anomaly: 193
7533 deg
Mean motion: 15
55278067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4005
Checksum: 299
Coasting Arc #4 (Orbit 4006)
---------------------------------------
Vector Time (GMT): 2015/245/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3389513
31 A = 6774056
65 meter
Y = 2446505
93 meter E =
0002863
Z = 5328292
96 I = 51
93260
XDOT = -4259
286801 Wp = 117
06376
YDOT = -6378
300571 meter/sec RA = 57
54016 deg
ZDOT = 217
780804 TA = 330
86216
MA = 330
87813
Ha = 219
411 n
mi
Hp = 212
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11120450
49 X = -3442501
63
Y = 8026594
26 feet Y = 2408306
41 meter
Z = 17481276
10 Z = 5311698
44
XDOT = -13974
038062 XDOT = -4188
704436
YDOT = -20926
182976 feet/sec YDOT = -6425
536049 meter/sec
ZDOT = 714
503951 ZDOT = 197
262115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13804732
76 X = 4207682
55
Y = 183299
16 feet Y = 55869
58 meter
Z = 17409233
28 Z = 5306334
30
XDOT = -1117
039130 XDOT = -340
473527
YDOT = 24133
315299 feet/sec YDOT = 7355
834503 meter/sec
ZDOT = 627
188419 ZDOT = 191
167030
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 15245
50200832
00016717 00000-0 10270-3 0 9037
2 25544 51
6415 57
9859 0000934 173
0729 187
0437 15
55262569 40079
Satellite: ISS
Catalog Number: 25544
Epoch time: 15245
50200832 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 57
9859 deg
Eccentricity:
0000934
Arg of perigee: 173
0729 deg
Mean anomaly: 187
0437 deg
Mean motion: 15
55262569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4007
Checksum: 310
Coasting Arc #5 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2015/246/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4566249
87 A = 6775422
37 meter
Y = -474914
61 meter E =
0012852
Z = -4994819
48 I = 51
91929
XDOT = 3030
252902 Wp = 109
62224
YDOT = 6704
254072 meter/sec RA = 52
54688 deg
ZDOT = 2133
054107 TA = 181
09367
MA = 181
09648
Ha = 219
189 n
mi
Hp = 212
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14981134
74 X = 4595484
06
Y = -1558118
79 feet Y = -423688
75 meter
Z = -16387203
03 Z = -4972566
50
XDOT = 9941
774614 XDOT = 2944
697522
YDOT = 21995
584227 feet/sec YDOT = 6737
662162 meter/sec
ZDOT = 6998
209013 ZDOT = 2147
566120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13208929
28 X = -4026081
64
Y = -7451581
69 feet Y = -2271242
10 meter
Z = -16291122
53 Z = -4965534
15
XDOT = 4102
956206 XDOT = 1250
581051
YDOT = -22705
208328 feet/sec YDOT = -6920
547498 meter/sec
ZDOT = 7059
537852 ZDOT = 2151
747137
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 15246
46580595
00016717 00000-0 10270-3 0 9041
2 25544 51
6411 53
1713 0000979 175
3968 184
7194 15
55320028 40227
Satellite: ISS
Catalog Number: 25544
Epoch time: 15246
46580595 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 53
1713 deg
Eccentricity:
0000979
Arg of perigee: 175
3968 deg
Mean anomaly: 184
7194 deg
Mean motion: 15
55320028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 312
Coasting Arc #6 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2015/247/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5387263
12 A = 6779621
95 meter
Y = -1412894
27 meter E =
0011188
Z = 3856726
93 I = 51
91363
XDOT = -1337
936636 Wp = 86
58155
YDOT = -6303
155219 meter/sec RA = 47
56379 deg
ZDOT = -4166
990420 TA = 47
08997
MA = 46
99612
Ha = 219
208 n
mi
Hp = 212
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17674747
75 X = -5389797
91
Y = -4635479
89 feet Y = -1473152
10 meter
Z = 12653303
57 Z = 3830550
62
XDOT = -4389
555892 XDOT = -1247
112133
YDOT = -20679
643107 feet/sec YDOT = -6317
609364 meter/sec
ZDOT = -13671
228412 ZDOT = -4173
268811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12044901
06 X = 3671285
84
Y = 13843505
16 feet Y = 4219500
37 meter
Z = 12540661
72 Z = 3822393
69
XDOT = -7106
196511 XDOT = -2165
968697
YDOT = 18624
065877 feet/sec YDOT = 5676
615279 meter/sec
ZDOT = -13697
104861 ZDOT = -4174
877562
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 15247
49384482
00016717 00000-0 10270-3 0 9053
2 25544 51
6414 48
0372 0000926 188
6730 171
4408 15
55332314 40389
Satellite: ISS
Catalog Number: 25544
Epoch time: 15247
49384482 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 48
0372 deg
Eccentricity:
0000926
Arg of perigee: 188
6730 deg
Mean anomaly: 171
4408 deg
Mean motion: 15
55332314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 306
Coasting Arc #7 (Orbit 4052)
---------------------------------------
Vector Time (GMT): 2015/248/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5708811
23 A = 6783897
34 meter
Y = 2977601
15 meter E =
0005736
Z = -2132395
15 I = 51
90600
XDOT = -683
513455 Wp = 47
10417
YDOT = 5263
221181 meter/sec RA = 42
59352 deg
ZDOT = 5532
681662 TA = 289
35006
MA = 289
41208
Ha = 219
126 n
mi
Hp = 212
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18729695
65 X = 5685449
03
Y = 9769032
63 feet Y = 3041310
07 meter
Z = -6996047
07 Z = -2104719
86
XDOT = -2242
498211 XDOT = -769
192882
YDOT = 17267
786027 feet/sec YDOT = 5255
098959 meter/sec
ZDOT = 18151
842723 ZDOT = 5529
152870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10308992
02 X = -3142180
77
Y = -18482650
23 feet Y = -5633511
79 meter
Z = -6877244
81 Z = -2096184
22
XDOT = 10118
365036 XDOT = 3084
077663
YDOT = -12375
403914 feet/sec YDOT = -3772
023113 meter/sec
ZDOT = 18135
606754 ZDOT = 5527
732939
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 15248
45762071
00016717 00000-0 10270-3 0 9065
2 25544 51
6414 43
2230 0000975 181
3159 178
7991 15
55354528 40533
Satellite: ISS
Catalog Number: 25544
Epoch time: 15248
45762071 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 43
2230 deg
Eccentricity:
0000975
Arg of perigee: 181
3159 deg
Mean anomaly: 178
7991 deg
Mean motion: 15
55354528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4053
Checksum: 312
Coasting Arc #8 (Orbit 4068)
---------------------------------------
Vector Time (GMT): 2015/249/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5384776
77 A = 6785585
31 meter
Y = -4118607
07 meter E =
0012497
Z = 33599
34 I = 51
88816
XDOT = 2847
591099 Wp = 136
71357
YDOT = -3782
992849 meter/sec RA = 37
63373 deg
ZDOT = -6035
738735 TA = 42
92552
MA = 42
82806
Ha = 218
930 n
mi
Hp = 212
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17666590
46 X = -5338484
51
Y = -13512490
39 feet Y = -4178564
35 meter
Z = 110234
06 Z = 7553
98
XDOT = 9342
490481 XDOT = 2919
000991
YDOT = -12411
393860 feet/sec YDOT = -3750
750294 meter/sec
ZDOT = -19802
292439 ZDOT = -6021
732100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7685668
13 X = 2342591
65
Y = 20871954
15 feet Y = 6361771
63 meter
Z = -1311
23 Z = -399
66
XDOT = -13121
562288 XDOT = -3999
452185
YDOT = 4853
311156 feet/sec YDOT = 1479
289240 meter/sec
ZDOT = -19741
142486 ZDOT = -6017
100230
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 15249
48563352
00016717 00000-0 10270-3 0 9071
2 25544 51
6413 38
0883 0000679 192
2260 167
8877 15
55417613 40697
Satellite: ISS
Catalog Number: 25544
Epoch time: 15249
48563352 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 38
0883 deg
Eccentricity:
0000679
Arg of perigee: 192
2260 deg
Mean anomaly: 167
8877 deg
Mean motion: 15
55417613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4069
Checksum: 332
Coasting Arc #9 (Orbit 4079)
---------------------------------------
Vector Time (GMT): 2015/250/04:13:34
655
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2194052
55 A = 6774135
93 meter
Y = -3574816
28 meter E =
0014073
Z = -5331495
55 I = 51
83352
XDOT = 6416
751019 Wp = 91
11845
YDOT = 4180
324487 meter/sec RA = 34
04112 deg
ZDOT = -162
920089 TA = 177
33515
MA = 177
32765
Ha = 218
976 n
mi
Hp = 213
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7198335
14 X = 2259762
15
Y = -11728399
86 feet Y = -3549913
87 meter
Z = -17491783
29 Z = -5320677
53
XDOT = 21052
332738 XDOT = 6370
320110
YDOT = 13714
975351 feet/sec YDOT = 4251
821199 meter/sec
ZDOT = -534
514727 ZDOT = -131
862043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3937479
84 X = -1200143
86
Y = -13248476
43 feet Y = -4038135
62 meter
Z = -17444426
03 Z = -5317061
05
XDOT = 23259
531081 XDOT = 7089
505074
YDOT = -6387
075311 feet/sec YDOT = -1946
780555 meter/sec
ZDOT = -401
364038 ZDOT = -122
335759
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 15250
19238771
00016717 00000-0 10270-3 0 9086
2 25544 51
6452 34
5628 0001019 232
9039 127
2021 15
55236454 40809
Satellite: ISS
Catalog Number: 25544
Epoch time: 15250
19238771 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 34
5628 deg
Eccentricity:
0001019
Arg of perigee: 232
9039 deg
Mean anomaly: 127
2021 deg
Mean motion: 15
55236454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4080
Checksum: 289
Coasting Arc #10 (Orbit 4095)
---------------------------------------
Vector Time (GMT): 2015/251/04:13:34
655
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4021066
52 A = 6775600
41 meter
Y = 2238745
60 meter E =
0005327
Z = 4969928
86 I = 51
81159
XDOT = -5437
965728 Wp = 55
35634
YDOT = -4962
730057 meter/sec RA = 29
04286 deg
ZDOT = -2159
644632 TA = 55
65442
MA = 55
60403
Ha = 218
966 n
mi
Hp = 213
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13192475
47 X = -4069943
67
Y = 7344965
89 feet Y = 2193506
46 meter
Z = 16305540
86 Z = 4950276
62
XDOT = -17841
094909 XDOT = -5371
576481
YDOT = -16281
922758 feet/sec YDOT = -5023
169919 meter/sec
ZDOT = -7085
448268 ZDOT = -2185
899331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3057330
01 X = -931874
19
Y = 14879983
71 feet Y = 4535419
03 meter
Z = 16220339
51 Z = 4943959
48
XDOT = -22855
207871 XDOT = -6966
267359
YDOT = 3166
640902 feet/sec YDOT = 965
192147 meter/sec
ZDOT = -7197
722613 ZDOT = -2193
865853
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 15251
22048906
00016717 00000-0 10270-3 0 9091
2 25544 51
6449 29
4291 0001075 246
7041 113
3999 15
55276485 40967
Satellite: ISS
Catalog Number: 25544
Epoch time: 15251
22048906 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 29
4291 deg
Eccentricity:
0001075
Arg of perigee: 246
7041 deg
Mean anomaly: 113
3999 deg
Mean motion: 15
55276485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4096
Checksum: 322
Coasting Arc #11 (Orbit 4110)
---------------------------------------
Vector Time (GMT): 2015/252/04:13:34
655
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5506063
74 A = 6779810
05 meter
Y = -872762
95 meter E =
0005314
Z = -3864212
53 I = 51
79774
XDOT = 3741
542837 Wp = 109
92503
YDOT = 5245
865405 meter/sec RA = 24
05218 deg
ZDOT = 4149
317765 TA = 203
61110
MA = 203
63550
Ha = 218
869 n
mi
Hp = 213
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18064513
58 X = 5534184
64
Y = -2863395
50 feet Y = -811033
61 meter
Z = -12677862
62 Z = -3837397
08
XDOT = 12275
403009 XDOT = 3662
448625
YDOT = 17210
844505 feet/sec YDOT = 5287
263911 meter/sec
ZDOT = 13613
247260 ZDOT = 4167
300682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9344195
27 X = 2848110
72
Y = -15815662
19 feet Y = -4820613
84 meter
Z = -12562035
24 Z = -3828908
34
XDOT = 19879
385266 XDOT = 6059
236629
YDOT = 879
157406 feet/sec YDOT = 267
967177 meter/sec
ZDOT = 13689
784082 ZDOT = 4172
646188
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 15252
18432339
00016717 00000-0 10270-3 0 9106
2 25544 51
6455 24
6157 0001061 252
6582 107
4455 15
55264001 41113
Satellite: ISS
Catalog Number: 25544
Epoch time: 15252
18432339 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 24
6157 deg
Eccentricity:
0001061
Arg of perigee: 252
6582 deg
Mean anomaly: 107
4455 deg
Mean motion: 15
55264001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4111
Checksum: 273
Coasting Arc #12 (Orbit 4126)
---------------------------------------
Vector Time (GMT): 2015/253/04:13:34
655
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6417271
44 A = 6784186
00 meter
Y = -439313
75 meter E =
0013181
Z = 2136142
53 I = 51
78286
XDOT = -1494
498850 Wp = 112
61774
YDOT = -5115
423497 meter/sec RA = 19
07505 deg
ZDOT = -5519
548696 TA = 43
73225
MA = 43
62791
Ha = 218
938 n
mi
Hp = 213
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21054040
16 X = -6422258
44
Y = -1441318
07 feet Y = -511103
57 meter
Z = 7008341
64 Z = 2104956
98
XDOT = -4903
211450 XDOT = -1410
374286
YDOT = -16782
885488 feet/sec YDOT = -5131
666153 meter/sec
ZDOT = -18108
755563 ZDOT = -5526
603752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14278129
28 X = -4351973
81
Y = 15599711
07 feet Y = 4754791
93 meter
Z = 6873928
72 Z = 2095173
47
XDOT = -14971
308599 XDOT = -4563
254861
YDOT = -5677
807540 feet/sec YDOT = -1730
595738 meter/sec
ZDOT = -18138
183604 ZDOT = -5528
518363
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 15253
21240063
00016717 00000-0 10270-3 0 9113
2 25544 51
6455 19
4818 0000977 251
6787 108
4261 15
55258167 41279
Satellite: ISS
Catalog Number: 25544
Epoch time: 15253
21240063 = yrday
fracday
Element set: 911
Inclination: 51
6455 deg
RA of node: 19
4818 deg
Eccentricity:
0000977
Arg of perigee: 251
6787 deg
Mean anomaly: 108
4261 deg
Mean motion: 15
55258167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4127
Checksum: 306
Coasting Arc #13 (Orbit 4141)
---------------------------------------
Vector Time (GMT): 2015/254/04:13:34
655
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6593662
93 A = 6785871
27 meter
Y = 1576425
57 meter E =
0011185
Z = -99116
70 I = 51
75917
XDOT = -1024
041052 Wp = 40
81048
YDOT = 4637
343110 meter/sec RA = 14
10615 deg
ZDOT = 6023
633465 TA = 318
12304
MA = 318
20855
Ha = 218
739 n
mi
Hp = 213
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21632752
40 X = 6576026
37
Y = 5171999
90 feet Y = 1650061
63 meter
Z = -325186
03 Z = -67129
33
XDOT = -3359
714739 XDOT = -1105
081085
YDOT = 15214
380283 feet/sec YDOT = 4625
439185 meter/sec
ZDOT = 19762
576986 ZDOT = 6018
461553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17291795
18 X = 5270539
17
Y = -13992496
26 feet Y = -4264912
86 meter
Z = -187545
62 Z = -57163
91
XDOT = 8913
590345 XDOT = 2716
862337
YDOT = 10780
604218 feet/sec YDOT = 3285
928166 meter/sec
ZDOT = 19739
367271 ZDOT = 6016
559144
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 15254
17620841
00016717 00000-0 10270-3 0 9126
2 25544 51
6459 14
6682 0001125 266
1685 93
9340 15
55317921 41420
Satellite: ISS
Catalog Number: 25544
Epoch time: 15254
17620841 = yrday
fracday
Element set: 912
Inclination: 51
6459 deg
RA of node: 14
6682 deg
Eccentricity:
0001125
Arg of perigee: 266
1685 deg
Mean anomaly: 93
9340 deg
Mean motion: 15
55317921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4142
Checksum: 300
Coasting Arc #14 (Orbit 4157)
---------------------------------------
Vector Time (GMT): 2015/255/04:13:34
655
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5962559
90 A = 6784202
29 meter
Y = -2547541
82 meter E =
0005975
Z = -1987574
72 I = 51
72232
XDOT = 3522
859203 Wp = 148
58565
YDOT = -3897
501911 meter/sec RA = 9
13658 deg
ZDOT = -5585
261641 TA = 53
33587
MA = 53
28097
Ha = 218
681 n
mi
Hp = 213
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19562204
39 X = -5923974
71
Y = -8358076
85 feet Y = -2614003
61 meter
Z = -6520914
44 Z = -2016445
39
XDOT = 11557
937017 XDOT = 3593
311073
YDOT = -12787
079761 feet/sec YDOT = -3857
713779 meter/sec
ZDOT = -18324
349217 ZDOT = -5567
976800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18346978
10 X = -5592158
92
Y = 10690795
46 feet Y = 3258554
46 meter
Z = -6644915
48 Z = -2025370
24
XDOT = -2529
738267 XDOT = -771
064224
YDOT = -15659
104138 feet/sec YDOT = -4772
894941 meter/sec
ZDOT = -18249
052194 ZDOT = -5562
311109
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 15255
20425854
00016717 00000-0 10270-3 0 9139
2 25544 51
6458 9
5345 0001242 268
0037 92
0975 15
55292716 41585
Satellite: ISS
Catalog Number: 25544
Epoch time: 15255
20425854 = yrday
fracday
Element set: 913
Inclination: 51
6458 deg
RA of node: 9
5345 deg
Eccentricity:
0001242
Arg of perigee: 268
0037 deg
Mean anomaly: 92
0975 deg
Mean motion: 15
55292716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4158
Checksum: 308
Coasting Arc #15 (Orbit 4173)
---------------------------------------
Vector Time (GMT): 2015/256/04:13:34
655
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4590223
55 A = 6779837
92 meter
Y = 3295727
99 meter E =
0010430
Z = 3738046
47 I = 51
67620
XDOT = -5630
818989 Wp = 95
03030
YDOT = 2979
927382 meter/sec RA = 4
15297 deg
ZDOT = 4276
022799 TA = 309
65826
MA = 309
75023
Ha = 218
648 n
mi
Hp = 213
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15059788
55 X = 4534870
83
Y = 10812755
88 feet Y = 3346749
92 meter
Z = 12263931
99 Z = 3760209
87
XDOT = -18473
815582 XDOT = -5684
493977
YDOT = 9776
664638 feet/sec YDOT = 2916
660329 meter/sec
ZDOT = 14028
946190 ZDOT = 4248
538739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17514070
19 X = 5338288
59
Y = -5884977
83 feet Y = -1793741
24 meter
Z = 12358856
35 Z = 3766979
42
XDOT = -3286
143127 XDOT = -1001
616425
YDOT = 19508
179907 feet/sec YDOT = 5946
093236 meter/sec
ZDOT = 13909
856735 ZDOT = 4239
724333
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 15256
23229526
00016717 00000-0 10270-3 0 9142
2 25544 51
6456 4
3997 0001156 286
7997 73
3030 15
55320281 41746
Satellite: ISS
Catalog Number: 25544
Epoch time: 15256
23229526 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 4
3997 deg
Eccentricity:
0001156
Arg of perigee: 286
7997 deg
Mean anomaly: 73
3030 deg
Mean motion: 15
55320281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4174
Checksum: 312
Coasting Arc #16 (Orbit 4188)
---------------------------------------
Vector Time (GMT): 2015/257/04:13:34
655
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2624509
14 A = 6775394
93 meter
Y = -3858938
35 meter E =
0011248
Z = -4922378
16 I = 51
62908
XDOT = 7064
092017 Wp = 69
48888
YDOT = -1904
829061 meter/sec RA = 359
15189 deg
ZDOT = -2273
478329 TA = 178
27276
MA = 178
26887
Ha = 218
600 n
mi
Hp = 213
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8610594
30 X = -2557251
46
Y = -12660558
89 feet Y = -3887911
98 meter
Z = -16149534
65 Z = -4934963
58
XDOT = 23176
154913 XDOT = 7095
910949
YDOT = -6249
439178 feet/sec YDOT = -1825
656144 meter/sec
ZDOT = -7458
918403 ZDOT = -2239
084846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15253324
07 X = -4649213
18
Y = -192266
22 feet Y = -58602
74 meter
Z = -16203045
82 Z = -4938688
36
XDOT = 8035
811281 XDOT = 2449
315279
YDOT = -21550
133554 feet/sec YDOT = -6568
480707 meter/sec
ZDOT = -7310
258747 ZDOT = -2228
166866
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 15257
19606543
00016717 00000-0 10270-3 0 9157
2 25544 51
6448 359
5862 0001311 288
0711 72
0300 15
55366761 41890
Satellite: ISS
Catalog Number: 25544
Epoch time: 15257
19606543 = yrday
fracday
Element set: 915
Inclination: 51
6448 deg
RA of node: 359
5862 deg
Eccentricity:
0001311
Arg of perigee: 288
0711 deg
Mean anomaly: 72
0300 deg
Mean motion: 15
55366761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4189
Checksum: 311
Coasting Arc #17 (Orbit 4204)
---------------------------------------
Vector Time (GMT): 2015/258/04:13:34
655
Vector Time (MET): N/A
Weight (LBS) : 941209
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 334561
60 A = 6773720
87 meter
Y = 4195060
71 meter E =
0001455
Z = 5306737
21 I = 51
59187
XDOT = -7637
976312 Wp = 59
15898
YDOT = 716
886149 meter/sec RA = 354
13810 deg
ZDOT = -84
428463 TA = 31
65007
MA = 31
64132
Ha = 218
617 n
mi
Hp = 213
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1097643
04 X = 261848
35
Y = 13763322
54 feet Y = 4198396
19 meter
Z = 17410555
14 Z = 5308185
23
XDOT = -25058
977402 XDOT = -7645
014912
YDOT = 2351
988678 feet/sec YDOT = 631
433899 meter/sec
ZDOT = -276
996269 ZDOT = -121
549535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12007064
83 X = 3659753
36
Y = 6802593
83 feet Y = 2073430
60 meter
Z = 17415981
43 Z = 5308391
14
XDOT = -11423
833836 XDOT = -3481
984553
YDOT = 21289
405768 feet/sec YDOT = 6489
010878 meter/sec
ZDOT = -437
170829 ZDOT = -133
249669
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 15258
22407569
00016717 00000-0 10270-3 0 9160
2 25544 51
6450 354
4522 0001249 292
1542 67
9479 15
55375793 42052
Satellite: ISS
Catalog Number: 25544
Epoch time: 15258
22407569 = yrday
fracday
Element set: 916
Inclination: 51
6450 deg
RA of node: 354
4522 deg
Eccentricity:
0001249
Arg of perigee: 292
1542 deg
Mean anomaly: 67
9479 deg
Mean motion: 15
55375793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4205
Checksum: 326
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