[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 12th 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
226/10:19:30
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 212
6
232/11:08:01
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 212
4
Coasting Arc #1 (Orbit 3679)
---------------------------------------
Vector Time (GMT): 2015/224/10:43:27
413
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 802483
63 A = 6775545
00 meter
Y = -4445839
99 meter E =
0006941
Z = 5045998
00 I = 51
73254
XDOT = 7388
721769 Wp = 53
24209
YDOT = -826
427098 meter/sec RA = 162
00467 deg
ZDOT = -1897
325699 TA = 55
14791
MA = 55
08266
Ha = 219
778 n
mi
Hp = 212
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2632820
30 X = 827627
39
Y = -14586089
20 feet Y = -4436725
55 meter
Z = 16555111
56 Z = 5049957
26
XDOT = 24241
213154 XDOT = 7406
630237
YDOT = -2711
374992 feet/sec YDOT = -743
701409 meter/sec
ZDOT = -6224
821848 ZDOT = -1861
389988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13840630
78 X = -4218624
26
Y = 5247215
67 feet Y = 1599351
34 meter
Z = 16572903
39 Z = 5051420
95
XDOT = -14308
999505 XDOT = -4361
383049
YDOT = -18511
212890 feet/sec YDOT = -5642
217689 meter/sec
ZDOT = -6069
833078 ZDOT = -1850
085122
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 15224
49186909
00016717 00000-0 10270-3 0 9007
2 25544 51
6416 162
9116 0001435 42
2438 317
8826 15
55137582 36801
Satellite: ISS
Catalog Number: 25544
Epoch time: 15224
49186909 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 162
9116 deg
Eccentricity:
0001435
Arg of perigee: 42
2438 deg
Mean anomaly: 317
8826 deg
Mean motion: 15
55137582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3680
Checksum: 312
Coasting Arc #2 (Orbit 3694)
---------------------------------------
Vector Time (GMT): 2015/225/10:43:27
413
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2811857
10 A = 6779358
20 meter
Y = 4658856
19 meter E =
0007951
Z = -4051024
57 I = 51
77581
XDOT = -6563
844591 Wp = 99
41774
YDOT = -563
363262 meter/sec RA = 157
01031 deg
ZDOT = 3913
413447 TA = 211
10755
MA = 211
15465
Ha = 219
778 n
mi
Hp = 212
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9225252
96 X = -2844066
65
Y = 15284961
24 feet Y = 4627232
03 meter
Z = -13290763
02 Z = -4064761
99
XDOT = -21534
923199 XDOT = -6576
066568
YDOT = -1848
304664 feet/sec YDOT = -636
832791 meter/sec
ZDOT = 12839
282964 ZDOT = 3881
498587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17807039
96 X = 5427585
78
Y = -216788
58 feet Y = -66077
16 meter
Z = -13350732
00 Z = -4069303
11
XDOT = 9730
376304 XDOT = 2965
818697
YDOT = 18084
257632 feet/sec YDOT = 5512
081726 meter/sec
ZDOT = 12701
832193 ZDOT = 3871
518453
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 15225
45576362
00016717 00000-0 10270-3 0 9011
2 25544 51
6420 158
0991 0001442 42
2684 317
8580 15
55143282 36951
Satellite: ISS
Catalog Number: 25544
Epoch time: 15225
45576362 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 158
0991 deg
Eccentricity:
0001442
Arg of perigee: 42
2684 deg
Mean anomaly: 317
8580 deg
Mean motion: 15
55143282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3695
Checksum: 306
Coasting Arc #3 (Orbit 3710)
---------------------------------------
Vector Time (GMT): 2015/226/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4714205
68 A = 6777318
84 meter
Y = -1597971
16 meter E =
0009197
Z = 4593164
43 I = 51
79863
XDOT = 4739
403586 Wp = 106
64853
YDOT = -5211
813783 meter/sec RA = 152
15876 deg
ZDOT = 3043
492063 TA = 313
00222
MA = 313
07926
Ha = 219
779 n
mi
Hp = 212
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15466554
06 X = -4718297
79
Y = -5242687
54 feet Y = -1650711
27 meter
Z = 15069437
12 Z = 4570254
34
XDOT = 15549
224365 XDOT = 4782
547284
YDOT = -17099
126586 feet/sec YDOT = -5158
573352 meter/sec
ZDOT = 9985
210179 ZDOT = 3066
619581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2269891
75 X = 691863
01
Y = 16263644
98 feet Y = 4957158
99 meter
Z = 14970953
39 Z = 4563146
59
XDOT = -21031
639960 XDOT = -6410
443860
YDOT = -6371
866177 feet/sec YDOT = -1942
144811 meter/sec
ZDOT = 10085
748524 ZDOT = 3074
136150
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 15226
48390462
00016717 00000-0 10270-3 0 9021
2 25544 51
6428 152
9660 0001267 46
4582 313
6677 15
55214580 37113
Satellite: ISS
Catalog Number: 25544
Epoch time: 15226
48390462 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 152
9660 deg
Eccentricity:
0001267
Arg of perigee: 46
4582 deg
Mean anomaly: 313
6677 deg
Mean motion: 15
55214580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3711
Checksum: 308
Coasting Arc #4 (Orbit 3725)
---------------------------------------
Vector Time (GMT): 2015/227/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3037139
51 A = 6774509
39 meter
Y = 2984470
51 meter E =
0015655
Z = -5282656
91 I = 51
81699
XDOT = -6020
594248 Wp = 80
70484
YDOT = 4660
612370 meter/sec RA = 147
16232 deg
ZDOT = -827
983265 TA = 181
38751
MA = 181
39186
Ha = 219
732 n
mi
Hp = 212
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9964368
47 X = 3029201
36
Y = 9791569
91 feet Y = 3018389
19 meter
Z = -17331551
53 Z = -5267922
78
XDOT = -19752
605802 XDOT = -6068
240929
YDOT = 15290
722998 feet/sec YDOT = 4593
019686 meter/sec
ZDOT = -2716
480529 ZDOT = -857
345464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4021458
34 X = 1225740
50
Y = -13460012
19 feet Y = -4102611
72 meter
Z = -17268529
27 Z = -5263447
72
XDOT = 21701
895553 XDOT = 6614
737764
YDOT = 10133
941782 feet/sec YDOT = 3088
825455 meter/sec
ZDOT = -2843
813360 ZDOT = -866
794312
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 15227
44777794
00016717 00000-0 10270-3 0 9036
2 25544 51
6430 148
1528 0001402 47
6707 312
4565 15
55192757 37269
Satellite: ISS
Catalog Number: 25544
Epoch time: 15227
44777794 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 148
1528 deg
Eccentricity:
0001402
Arg of perigee: 47
6707 deg
Mean anomaly: 312
4565 deg
Mean motion: 15
55192757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3726
Checksum: 319
Coasting Arc #5 (Orbit 3741)
---------------------------------------
Vector Time (GMT): 2015/228/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1137353
03 A = 6774895
90 meter
Y = -4243548
49 meter E =
0006057
Z = 5153885
21 I = 51
84533
XDOT = 6596
456709 Wp = 54
11672
YDOT = -3615
042687 meter/sec RA = 142
16492 deg
ZDOT = -1516
107818 TA = 50
46238
MA = 50
40887
Ha = 219
753 n
mi
Hp = 212
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3731473
20 X = -1114851
31
Y = -13922403
17 feet Y = -4256141
02 meter
Z = 16909072
20 Z = 5148415
15
XDOT = 21641
918335 XDOT = 6643
755279
YDOT = -11860
376269 feet/sec YDOT = -3541
012393 meter/sec
ZDOT = -4974
107013 ZDOT = -1483
949011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10396745
10 X = -3168927
91
Y = 10021886
92 feet Y = 3054671
13 meter
Z = 16886189
59 Z = 5146910
59
XDOT = -20041
210187 XDOT = -6108
560865
YDOT = -12618
334029 feet/sec YDOT = -3846
068212 meter/sec
ZDOT = -4834
878196 ZDOT = -1473
670874
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 15228
47589580
00016717 00000-0 10270-3 0 9045
2 25544 51
6434 143
0200 0001419 50
2193 309
9085 15
55217567 37424
Satellite: ISS
Catalog Number: 25544
Epoch time: 15228
47589580 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 143
0200 deg
Eccentricity:
0001419
Arg of perigee: 50
2193 deg
Mean anomaly: 309
9085 deg
Mean motion: 15
55217567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3742
Checksum: 303
Coasting Arc #6 (Orbit 3756)
---------------------------------------
Vector Time (GMT): 2015/229/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -719475
10 A = 6778392
89 meter
Y = 5227714
57 meter E =
0009082
Z = -4263363
02 I = 51
88163
XDOT = -6422
807683 Wp = 103
05004
YDOT = 2071
331002 meter/sec RA = 137
17503 deg
ZDOT = 3628
249535 TA = 203
93472
MA = 203
97697
Ha = 219
681 n
mi
Hp = 212
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2360482
62 X = -757169
68
Y = 17151294
52 feet Y = 5219457
89 meter
Z = -13987411
49 Z = -4266949
93
XDOT = -21072
203683 XDOT = -6463
116866
YDOT = 6795
705386 feet/sec YDOT = 1999
281794 meter/sec
ZDOT = 11903
705824 ZDOT = 3596
951212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16043274
04 X = 4889989
93
Y = -6472643
22 feet Y = -1972861
65 meter
Z = -14003739
13 Z = -4268339
69
XDOT = 15861
307549 XDOT = 4834
526541
YDOT = 13884
838403 feet/sec YDOT = 4232
098745 meter/sec
ZDOT = 11768
429386 ZDOT = 3587
017277
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 15229
43974433
00016717 00000-0 10270-3 0 9058
2 25544 51
6433 138
2069 0001392 51
6178 308
5100 15
55233946 37578
Satellite: ISS
Catalog Number: 25544
Epoch time: 15229
43974433 = yrday
fracday
Element set: 905
Inclination: 51
6433 deg
RA of node: 138
2069 deg
Eccentricity:
0001392
Arg of perigee: 51
6178 deg
Mean anomaly: 308
5100 deg
Mean motion: 15
55233946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3757
Checksum: 310
Coasting Arc #7 (Orbit 3772)
---------------------------------------
Vector Time (GMT): 2015/230/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2371420
89 A = 6782944
85 meter
Y = -5751045
47 meter E =
0014522
Z = 2688441
63 I = 51
92014
XDOT = 5628
424111 Wp = 97
79613
YDOT = -126
395942 meter/sec RA = 132
20143 deg
ZDOT = -5213
009119 TA = 51
94020
MA = 51
80926
Ha = 219
652 n
mi
Hp = 212
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7780252
27 X = 2422494
93
Y = -18868259
43 feet Y = -5724240
93 meter
Z = 8820346
54 Z = 2700085
84
XDOT = 18465
958369 XDOT = 5654
741738
YDOT = -414
684848 feet/sec YDOT = -63
308408 meter/sec
ZDOT = -17103
048290 ZDOT = -5185
603716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20176835
43 X = -6149899
44
Y = 2921256
57 feet Y = 890399
00 meter
Z = 8871506
31 Z = 2704035
12
XDOT = -9573
266644 XDOT = -2917
931673
YDOT = -14321
738899 feet/sec YDOT = -4365
266016 meter/sec
ZDOT = -16984
868583 ZDOT = -5176
987944
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 15230
46783730
00016717 00000-0 10270-3 0 9062
2 25544 51
6436 133
0732 0001411 54
7119 305
4166 15
55258147 37738
Satellite: ISS
Catalog Number: 25544
Epoch time: 15230
46783730 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 133
0732 deg
Eccentricity:
0001411
Arg of perigee: 54
7119 deg
Mean anomaly: 305
4166 deg
Mean motion: 15
55258147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3773
Checksum: 294
Coasting Arc #8 (Orbit 3787)
---------------------------------------
Vector Time (GMT): 2015/231/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3611178
39 A = 6785793
46 meter
Y = 5692586
80 meter E =
0011768
Z = -728560
99 I = 51
94993
XDOT = -4357
942706 Wp = 41
93266
YDOT = -2006
844853 meter/sec RA = 127
24196 deg
ZDOT = 5984
214032 TA = 310
22510
MA = 310
32800
Ha = 219
645 n
mi
Hp = 212
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11847698
12 X = -3671026
83
Y = 18676465
89 feet Y = 5651869
55 meter
Z = -2390291
96 Z = -746248
99
XDOT = -14297
712291 XDOT = -4364
246615
YDOT = -6584
136656 feet/sec YDOT = -2055
613075 meter/sec
ZDOT = 19633
248135 ZDOT = 5963
028999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22106349
44 X = 6738015
31
Y = 335446
99 feet Y = 102244
24 meter
Z = -2467511
75 Z = -752097
58
XDOT = 1944
232393 XDOT = 592
602033
YDOT = 14125
045274 feet/sec YDOT = 4305
313799 meter/sec
ZDOT = 19542
239005 ZDOT = 5956
474449
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 15231
43166278
00016717 00000-0 10270-3 0 9073
2 25544 51
6432 128
2601 0001395 54
9192 305
2092 15
55262019 37884
Satellite: ISS
Catalog Number: 25544
Epoch time: 15231
43166278 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 128
2601 deg
Eccentricity:
0001395
Arg of perigee: 54
9192 deg
Mean anomaly: 305
2092 deg
Mean motion: 15
55262019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3788
Checksum: 301
Coasting Arc #9 (Orbit 3803)
---------------------------------------
Vector Time (GMT): 2015/232/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4416964
59 A = 6785190
56 meter
Y = -4955640
17 meter E =
0009001
Z = -1389432
28 I = 51
96738
XDOT = 2794
931375 Wp = 134
16549
YDOT = 4118
320407 meter/sec RA = 122
28789 deg
ZDOT = -5833
094245 TA = 60
91003
MA = 60
81992
Ha = 219
653 n
mi
Hp = 212
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14491353
65 X = 4478800
78
Y = -16258661
99 feet Y = -4905901
11 meter
Z = -4558504
84 Z = -1367825
15
XDOT = 9169
722359 XDOT = 2777
006414
YDOT = 13511
549892 feet/sec YDOT = 4149
474578 meter/sec
ZDOT = -19137
448310 ZDOT = -5819
560889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21512721
99 X = -6557077
66
Y = -3520574
81 feet Y = -1073071
20 meter
Z = -4464496
83 Z = -1360778
63
XDOT = 6152
261524 XDOT = 1875
209313
YDOT = -13523
461377 feet/sec YDOT = -4121
951028 meter/sec
ZDOT = -19079
787774 ZDOT = -5815
519313
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 15232
45973123
00016717 00000-0 10270-3 0 9082
2 25544 51
6440 123
1257 0001337 60
8005 299
3282 15
55281228 38045
Satellite: ISS
Catalog Number: 25544
Epoch time: 15232
45973123 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 123
1257 deg
Eccentricity:
0001337
Arg of perigee: 60
8005 deg
Mean anomaly: 299
3282 deg
Mean motion: 15
55281228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3804
Checksum: 291
Coasting Arc #10 (Orbit 3804)
---------------------------------------
Vector Time (GMT): 2015/232/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4719181
81 A = 6784093
27 meter
Y = 4367526
91 meter E =
0015332
Z = 2139816
26 I = 51
96429
XDOT = -2026
446629 Wp = 69
03963
YDOT = -4914
025847 meter/sec RA = 122
12647 deg
ZDOT = 5534
240286 TA = 314
59461
MA = 314
71962
Ha = 219
700 n
mi
Hp = 212
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15482879
94 X = -4778064
17
Y = 14329156
53 feet Y = 4314424
82 meter
Z = 7020394
55 Z = 2116748
24
XDOT = -6648
446947 XDOT = -1998
229303
YDOT = -16122
132043 feet/sec YDOT = -4936
528788 meter/sec
ZDOT = 18156
956319 ZDOT = 5524
465104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21106352
23 X = 6433216
16
Y = 981406
44 feet Y = 299132
68 meter
Z = 6920186
05 Z = 2109272
71
XDOT = -6647
421161 XDOT = -2026
133970
YDOT = 14600
262686 feet/sec YDOT = 4450
160067 meter/sec
ZDOT = 18115
635796 ZDOT = 5521
645791
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 15232
52398539
00016717 00000-0 10270-3 0 9093
2 25544 51
6441 122
8050 0001431 59
0016 301
1277 15
55282026 38054
Satellite: ISS
Catalog Number: 25544
Epoch time: 15232
52398539 = yrday
fracday
Element set: 909
Inclination: 51
6441 deg
RA of node: 122
8050 deg
Eccentricity:
0001431
Arg of perigee: 59
0016 deg
Mean anomaly: 301
1277 deg
Mean motion: 15
55282026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3805
Checksum: 281
Coasting Arc #11 (Orbit 3819)
---------------------------------------
Vector Time (GMT): 2015/233/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4829835
42 A = 6779589
90 meter
Y = -2763228
20 meter E =
0007547
Z = -3881033
21 I = 51
96642
XDOT = 348
615174 Wp = 72
65967
YDOT = 6431
961217 meter/sec RA = 117
16079 deg
ZDOT = -4150
050242 TA = 153
91750
MA = 153
87946
Ha = 219
577 n
mi
Hp = 212
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15845916
72 X = 4879228
06
Y = -9065709
31 feet Y = -2708941
84 meter
Z = -12733048
59 Z = -3857450
80
XDOT = 1143
750572 XDOT = 296
824821
YDOT = 21102
234963 feet/sec YDOT = 6435
569864 meter/sec
ZDOT = -13615
650400 ZDOT = -4148
482878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17724674
72 X = -5402480
86
Y = -4659121
58 feet Y = -1420100
26 meter
Z = -12630882
01 Z = -3849892
84
XDOT = 13538
988012 XDOT = 4126
683546
YDOT = -14649
493524 feet/sec YDOT = -4465
165626 meter/sec
ZDOT = -13609
989676 ZDOT = -4148
324853
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 15233
48778648
00016717 00000-0 10270-3 0 9104
2 25544 51
6447 117
9918 0001319 59
3015 300
8268 15
55317061 38206
Satellite: ISS
Catalog Number: 25544
Epoch time: 15233
48778648 = yrday
fracday
Element set: 910
Inclination: 51
6447 deg
RA of node: 117
9918 deg
Eccentricity:
0001319
Arg of perigee: 59
3015 deg
Mean anomaly: 300
8268 deg
Mean motion: 15
55317061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3820
Checksum: 314
Coasting Arc #12 (Orbit 3835)
---------------------------------------
Vector Time (GMT): 2015/234/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4517701
26 A = 6775364
30 meter
Y = 741890
65 meter E =
0007046
Z = 4989911
31 I = 51
96609
XDOT = 1165
962783 Wp = 113
59839
YDOT = -7278
897028 meter/sec RA = 112
18053 deg
ZDOT = 2132
715482 TA = 315
71221
MA = 315
76857
Ha = 219
713 n
mi
Hp = 212
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14821854
53 X = -4549900
51
Y = 2434024
43 feet Y = 691190
91 meter
Z = 16371100
11 Z = 4967887
05
XDOT = 3825
337214 XDOT = 1236
910622
YDOT = -23880
895760 feet/sec YDOT = -7265
461686 meter/sec
ZDOT = 6997
098037 ZDOT = 2138
552099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12519122
10 X = 3815828
42
Y = 8484603
00 feet Y = 2586106
99 meter
Z = 16275990
27 Z = 4960921
84
XDOT = -18534
507904 XDOT = -5649
318009
YDOT = 13842
233270 feet/sec YDOT = 4219
112701 meter/sec
ZDOT = 7023
525371 ZDOT = 2140
770533
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 15234
51583048
00016717 00000-0 10270-3 0 9118
2 25544 51
6447 112
8574 0001347 64
2150 295
9142 15
55331141 38361
Satellite: ISS
Catalog Number: 25544
Epoch time: 15234
51583048 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 112
8574 deg
Eccentricity:
0001347
Arg of perigee: 64
2150 deg
Mean anomaly: 295
9142 deg
Mean motion: 15
55331141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3836
Checksum: 293
Coasting Arc #13 (Orbit 3850)
---------------------------------------
Vector Time (GMT): 2015/235/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3911413
67 A = 6773775
65 meter
Y = 1487706
50 meter E =
0015987
Z = -5340250
75 I = 51
97262
XDOT = -2438
370232 Wp = 89
56887
YDOT = 7256
414347 meter/sec RA = 107
19068 deg
ZDOT = 236
284451 TA = 182
67145
MA = 182
68000
Ha = 219
480 n
mi
Hp = 212
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12832722
00 X = 3920427
86
Y = 4880926
82 feet Y = 1531496
74 meter
Z = -17520507
70 Z = -5321228
11
XDOT = -7999
902337 XDOT = -2520
479761
YDOT = 23807
133686 feet/sec YDOT = 7228
687794 meter/sec
ZDOT = 775
211452 ZDOT = 224
239745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6266758
37 X = -1910107
95
Y = -12332437
61 feet Y = -3758926
98 meter
Z = -17438724
52 Z = -5315323
23
XDOT = 21066
865187 XDOT = 6421
180509
YDOT = -11722
737760 feet/sec YDOT = -3573
090469 meter/sec
ZDOT = 721
997855 ZDOT = 220
064946
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 15235
47961016
00016717 00000-0 10270-3 0 9120
2 25544 51
6450 108
0438 0001279 61
9233 298
2050 15
55364674 38519
Satellite: ISS
Catalog Number: 25544
Epoch time: 15235
47961016 = yrday
fracday
Element set: 912
Inclination: 51
6450 deg
RA of node: 108
0438 deg
Eccentricity:
0001279
Arg of perigee: 61
9233 deg
Mean anomaly: 298
2050 deg
Mean motion: 15
55364674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3851
Checksum: 303
Coasting Arc #14 (Orbit 3866)
---------------------------------------
Vector Time (GMT): 2015/236/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3075091
52 A = 6775786
22 meter
Y = -3623121
52 meter E =
0008506
Z = 4825249
09 I = 51
98859
XDOT = 3436
188139 Wp = 60
46788
YDOT = -6358
854362 meter/sec RA = 102
20291 deg
ZDOT = -2577
317979 TA = 54
80402
MA = 54
72439
Ha = 219
474 n
mi
Hp = 212
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10088882
94 X = -3057787
42
Y = -11886881
63 feet Y = -3657412
37 meter
Z = 15830869
72 Z = 4810353
11
XDOT = 11273
583132 XDOT = 3519
558546
YDOT = -20862
383076 feet/sec YDOT = -6319
962547 meter/sec
ZDOT = -8455
767646 ZDOT = -2560
423152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -222851
15 X = -67925
03
Y = 15653876
23 feet Y = 4771301
48 meter
Z = 15767258
68 Z = 4805860
45
XDOT = -21155
537671 XDOT = -6448
207882
YDOT = 8166
140783 feet/sec YDOT = 2489
039711 meter/sec
ZDOT = -8381
776069 ZDOT = -2554
765346
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 15236
50762966
00016717 00000-0 10270-3 0 9139
2 25544 51
6453 102
9096 0001206 58
4916 301
6355 15
55408392 38674
Satellite: ISS
Catalog Number: 25544
Epoch time: 15236
50762966 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 102
9096 deg
Eccentricity:
0001206
Arg of perigee: 58
4916 deg
Mean anomaly: 301
6355 deg
Mean motion: 15
55408392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3867
Checksum: 317
Coasting Arc #15 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2015/237/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2127365
32 A = 6780329
59 meter
Y = 5363576
88 meter E =
0006201
Z = -3566091
78 I = 52
00919
XDOT = -4130
900984 Wp = 89
67478
YDOT = 4627
031537 meter/sec RA = 97
22710 deg
ZDOT = 4501
749681 TA = 228
48326
MA = 228
53648
Ha = 219
424 n
mi
Hp = 212
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6979545
01 X = 2084552
94
Y = 17597037
00 feet Y = 5387127
03 meter
Z = -11699776
17 Z = -3555861
65
XDOT = -13552
824751 XDOT = -4204
202123
YDOT = 15180
549663 feet/sec YDOT = 4580
427322 meter/sec
ZDOT = 14769
519952 ZDOT = 4481
504662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6044064
26 X = 1842230
79
Y = -17967955
99 feet Y = -5476632
99 meter
Z = -11656601
86 Z = -3552932
25
XDOT = 18923
747521 XDOT = 5767
958244
YDOT = -3144
409153 feet/sec YDOT = -958
415910 meter/sec
ZDOT = 14681
370021 ZDOT = 4474
881582
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 15237
47138897
00016717 00000-0 10270-3 0 9147
2 25544 51
6451 98
0960 0001161 60
1456 299
9813 15
55381812 38828
Satellite: ISS
Catalog Number: 25544
Epoch time: 15237
47138897 = yrday
fracday
Element set: 914
Inclination: 51
6451 deg
RA of node: 98
0960 deg
Eccentricity:
0001161
Arg of perigee: 60
1456 deg
Mean anomaly: 299
9813 deg
Mean motion: 15
55381812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3882
Checksum: 329
Coasting Arc #16 (Orbit 3897)
---------------------------------------
Vector Time (GMT): 2015/238/11:08:01
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1072686
77 A = 6784463
09 meter
Y = -6472600
44 meter E =
0014835
Z = 1701286
06 I = 52
02608
XDOT = 4566
941881 Wp = 112
25500
YDOT = -2272
276290 meter/sec RA = 92
26757 deg
ZDOT = -5731
142869 TA = 49
17773
MA = 49
04918
Ha = 219
473 n
mi
Hp = 212
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3519313
54 X = -1008492
95
Y = -21235565
74 feet Y = -6484236
95 meter
Z = 5581647
17 Z = 1696231
33
XDOT = 14983
405123 XDOT = 4619
850945
YDOT = -7454
974705 feet/sec YDOT = -2220
910070 meter/sec
ZDOT = -18802
962169 ZDOT = -5708
829301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10748410
31 X = -3276115
46
Y = 18655737
65 feet Y = 5686268
84 meter
Z = 5561001
16 Z = 1694993
15
XDOT = -15039
777026 XDOT = -4584
124038
YDOT = -3055
367789 feet/sec YDOT = -931
276102 meter/sec
ZDOT = -18706
298974 ZDOT = -5701
679927
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 15238
49938727
00016717 00000-0 10270-3 0 9151
2 25544 51
6451 92
9618 0001245 69
3135 290
8152 15
55384792 38982
Satellite: ISS
Catalog Number: 25544
Epoch time: 15238
49938727 = yrday
fracday
Element set: 915
Inclination: 51
6451 deg
RA of node: 92
9618 deg
Eccentricity:
0001245
Arg of perigee: 69
3135 deg
Mean anomaly: 290
8152 deg
Mean motion: 15
55384792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3898
Checksum: 347
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