[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 14th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 905 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 629)
---------------------------------------
Vector Time (GMT): 2015/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1057467
65 A = 6781070
39 meter
Y = -5129399
72 meter E =
0012738
Z = 4294872
69 I = 51
40946
XDOT = 6645
787279 Wp = 76
95324
YDOT = 1570
032877 meter/sec RA = 217
47526 deg
ZDOT = 3505
451849 TA = 337
26690
MA = 337
32326
Ha = 222
589 n
mi
Hp = 213
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3469382
05 X = -1020894
11
Y = -16828739
23 feet Y = -5141019
94 meter
Z = 14090789
66 Z = 4289825
16
XDOT = 21803
764038 XDOT = 6610
708380
YDOT = 5151
026498 feet/sec YDOT = 1644
154790 meter/sec
ZDOT = 11500
826276 ZDOT = 3537
650942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9075418
38 X = 2766187
52
Y = 14610598
51 feet Y = 4453310
43 meter
Z = 14069847
96 Z = 4288489
66
XDOT = -21120
402336 XDOT = -6437
498632
YDOT = 1891
543956 feet/sec YDOT = 576
542598 meter/sec
ZDOT = 11639
411689 ZDOT = 3547
692683
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 15285
55469807
00016717 00000-0 10270-3 0 9002
2 25544 51
6430 218
2489 0006601 27
2414 332
9084 15
54279615 6301
Satellite: ISS
Catalog Number: 25544
Epoch time: 15285
55469807 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 218
2489 deg
Eccentricity:
0006601
Arg of perigee: 27
2414 deg
Mean anomaly: 332
9084 deg
Mean motion: 15
54279615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 630
Checksum: 307
Coasting Arc #2 (Orbit 644)
---------------------------------------
Vector Time (GMT): 2015/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -534672
38 A = 6777921
03 meter
Y = 4467333
56 meter E =
0018579
Z = -5085744
35 I = 51
42530
XDOT = -6921
702586 Wp = 62
01705
YDOT = -2783
560600 meter/sec RA = 212
46379 deg
ZDOT = -1713
663888 TA = 191
32223
MA = 191
36409
Ha = 222
689 n
mi
Hp = 212
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1754174
47 X = -559882
30
Y = 14656606
17 feet Y = 4461212
90 meter
Z = -16685512
95 Z = -5088403
53
XDOT = -22708
997985 XDOT = -6881
737183
YDOT = -9132
416667 feet/sec YDOT = -2860
740400 meter/sec
ZDOT = -5622
256850 ZDOT = -1747
191440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3686177
65 X = -1123546
95
Y = -14279309
99 feet Y = -4352333
69 meter
Z = -16697693
72 Z = -5089457
05
XDOT = 23397
579091 XDOT = 7131
582107
YDOT = 717
275144 feet/sec YDOT = 218
625464 meter/sec
ZDOT = -5766
387762 ZDOT = -1757
594990
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 15286
51914155
00016717 00000-0 10270-3 0 9011
2 25544 51
6434 213
4397 0006736 30
7330 329
4216 15
54288462 6459
Satellite: ISS
Catalog Number: 25544
Epoch time: 15286
51914155 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 213
4397 deg
Eccentricity:
0006736
Arg of perigee: 30
7330 deg
Mean anomaly: 329
4216 deg
Mean motion: 15
54288462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 645
Checksum: 304
Coasting Arc #3 (Orbit 660)
---------------------------------------
Vector Time (GMT): 2015/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2217522
79 A = 6776773
70 meter
Y = -3599524
68 meter E =
0008552
Z = 5291230
11 I = 51
44932
XDOT = 6703
942806 Wp = 45
57963
YDOT = 3724
471490 meter/sec RA = 207
44881 deg
ZDOT = -269
750619 TA = 47
03242
MA = 46
96074
Ha = 222
550 n
mi
Hp = 212
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7275337
23 X = 2231905
34
Y = -11809464
16 feet Y = -3574645
86 meter
Z = 17359678
85 Z = 5302037
99
XDOT = 21994
563012 XDOT = 6663
106980
YDOT = 12219
394651 feet/sec YDOT = 3799
211043 meter/sec
ZDOT = -885
008593 ZDOT = -237
283040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2249093
98 X = -685523
85
Y = 13627000
61 feet Y = 4153509
79 meter
Z = 17406862
32 Z = 5305611
63
XDOT = -23974
763005 XDOT = -7307
507764
YDOT = -2978
886334 feet/sec YDOT = -907
964555 meter/sec
ZDOT = -745
586079 ZDOT = -227
254637
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 15287
54786785
00016717 00000-0 10270-3 0 9022
2 25544 51
6434 208
3106 0006646 33
2589 326
8980 15
54329620 6613
Satellite: ISS
Catalog Number: 25544
Epoch time: 15287
54786785 = yrday
fracday
Element set: 902
Inclination: 51
6434 deg
RA of node: 208
3106 deg
Eccentricity:
0006646
Arg of perigee: 33
2589 deg
Mean anomaly: 326
8980 deg
Mean motion: 15
54329620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 661
Checksum: 329
Coasting Arc #4 (Orbit 675)
---------------------------------------
Vector Time (GMT): 2015/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3816317
03 A = 6778386
62 meter
Y = 2674278
78 meter E =
0016139
Z = -4935714
53 I = 51
48363
XDOT = -5902
179648 Wp = 83
51353
YDOT = -4345
947384 meter/sec RA = 202
43584 deg
ZDOT = 2216
894867 TA = 208
15889
MA = 208
24626
Ha = 222
734 n
mi
Hp = 212
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12520725
18 X = -3821961
41
Y = 8773880
50 feet Y = 2631570
17 meter
Z = -16193289
15 Z = -4954267
86
XDOT = -19364
106456 XDOT = -5863
912640
YDOT = -14258
357559 feet/sec YDOT = -4411
735271 meter/sec
ZDOT = 7273
277122 ZDOT = 2188
315920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8033754
63 X = 2448688
41
Y = -12907226
18 feet Y = -3934122
54 meter
Z = -16273734
98 Z = -4960234
42
XDOT = 22483
311286 XDOT = 6852
913280
YDOT = 5011
407830 feet/sec YDOT = 1527
477107 meter/sec
ZDOT = 7150
711353 ZDOT = 2179
536820
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 15288
51229033
00016717 00000-0 10270-3 0 9039
2 25544 51
6437 203
5013 0006738 37
3564 322
8056 15
54312432 6769
Satellite: ISS
Catalog Number: 25544
Epoch time: 15288
51229033 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 203
5013 deg
Eccentricity:
0006738
Arg of perigee: 37
3564 deg
Mean anomaly: 322
8056 deg
Mean motion: 15
54312432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 676
Checksum: 292
Coasting Arc #5 (Orbit 691)
---------------------------------------
Vector Time (GMT): 2015/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5210955
57 A = 6781883
63 meter
Y = -1688220
90 meter E =
0016678
Z = 3991047
38 I = 51
52476
XDOT = 4572
264914 Wp = 64
70637
YDOT = 4726
527239 meter/sec RA = 197
43271 deg
ZDOT = -3950
584933 TA = 66
51241
MA = 66
33721
Ha = 222
716 n
mi
Hp = 212
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17096310
91 X = 5210058
90
Y = -5538782
47 feet Y = -1629953
25 meter
Z = 13093987
46 Z = 4016359
74
XDOT = 15000
869140 XDOT = 4538
262823
YDOT = 15506
979129 feet/sec YDOT = 4777
466883 meter/sec
ZDOT = -12961
236656 ZDOT = -3928
456213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13321331
64 X = -4060341
88
Y = 11942603
47 feet Y = 3640105
54 meter
Z = 13203439
38 Z = 4024408
32
XDOT = -19193
595662 XDOT = -5850
207958
YDOT = -7112
870622 feet/sec YDOT = -2168
002966 meter/sec
ZDOT = -12866
540804 ZDOT = -3921
721637
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 15289
54099533
00016717 00000-0 10270-3 0 9044
2 25544 51
6432 198
3718 0006742 41
4683 318
6980 15
54325607 6925
Satellite: ISS
Catalog Number: 25544
Epoch time: 15289
54099533 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 198
3718 deg
Eccentricity:
0006742
Arg of perigee: 41
4683 deg
Mean anomaly: 318
6980 deg
Mean motion: 15
54325607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 692
Checksum: 333
Coasting Arc #6 (Orbit 706)
---------------------------------------
Vector Time (GMT): 2015/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6203185
07 A = 6785617
88 meter
Y = 773101
16 meter E =
0011591
Z = -2635774
70 I = 51
56868
XDOT = -2813
370314 Wp = 49
47051
YDOT = -4860
633107 meter/sec RA = 192
44208 deg
ZDOT = 5217
934500 TA = 280
79573
MA = 280
92618
Ha = 222
717 n
mi
Hp = 212
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20351657
06 X = -6198565
15
Y = 2536421
14 feet Y = 703758
71 meter
Z = -8647554
80 Z = -2665898
06
XDOT = -9230
217566 XDOT = -2784
155760
YDOT = -15946
959014 feet/sec YDOT = -4891
930371 meter/sec
ZDOT = 17119
207676 ZDOT = 5204
338683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17354707
82 X = 5289714
94
Y = -10824552
49 feet Y = -3299323
60 meter
Z = -8777628
44 Z = -2675421
15
XDOT = 14382
912998 XDOT = 4383
911882
YDOT = 9283
569317 feet/sec YDOT = 2829
631928 meter/sec
ZDOT = 17061
332515 ZDOT = 5200
294151
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 15290
50539480
00016717 00000-0 10270-3 0 9053
2 25544 51
6436 193
5623 0006707 44
5579 315
6112 15
54358950 7078
Satellite: ISS
Catalog Number: 25544
Epoch time: 15290
50539480 = yrday
fracday
Element set: 905
Inclination: 51
6436 deg
RA of node: 193
5623 deg
Eccentricity:
0006707
Arg of perigee: 44
5579 deg
Mean anomaly: 315
6112 deg
Mean motion: 15
54358950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 707
Checksum: 315
Coasting Arc #7 (Orbit 722)
---------------------------------------
Vector Time (GMT): 2015/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6719386
67 A = 6788311
60 meter
Y = 141750
63 meter E =
0016464
Z = 924156
78 I = 51
60850
XDOT = 723
823421 Wp = 101
91810
YDOT = 4822
924138 meter/sec RA = 187
46343 deg
ZDOT = -5916
643675 TA = 68
07295
MA = 67
89802
Ha = 222
842 n
mi
Hp = 212
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22045231
85 X = 6712812
88
Y = 465061
11 feet Y = 216854
53 meter
Z = 3032010
44 Z = 956782
91
XDOT = 2374
748757 XDOT = 698
579907
YDOT = 15823
241922 feet/sec YDOT = 4830
876921 meter/sec
ZDOT = -19411
560612 ZDOT = -5913
189008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20029671
37 X = -6105043
83
Y = 9173195
64 feet Y = 2795990
03 meter
Z = 3172753
22 Z = 967055
18
XDOT = -8470
676784 XDOT = -2581
862284
YDOT = -11693
527885 feet/sec YDOT = -3564
187299 meter/sec
ZDOT = -19397
426177 ZDOT = -5912
335499
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 15291
53407731
00016717 00000-0 10270-3 0 9061
2 25544 51
6434 188
4321 0006656 48
7733 311
3993 15
54342485 7239
Satellite: ISS
Catalog Number: 25544
Epoch time: 15291
53407731 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 188
4321 deg
Eccentricity:
0006656
Arg of perigee: 48
7733 deg
Mean anomaly: 311
3993 deg
Mean motion: 15
54342485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 723
Checksum: 314
Coasting Arc #8 (Orbit 738)
---------------------------------------
Vector Time (GMT): 2015/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6657151
02 A = 6788347
86 meter
Y = -958218
97 meter E =
0020076
Z = 844076
18 I = 51
64064
XDOT = 1432
277670 Wp = 53
05659
YDOT = -4643
014420 meter/sec RA = 182
49053 deg
ZDOT = 5939
667872 TA = 316
08079
MA = 316
24019
Ha = 222
843 n
mi
Hp = 212
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21841046
66 X = -6650041
48
Y = -3143763
02 feet Y = -1032623
82 meter
Z = 2769278
80 Z = 811753
83
XDOT = 4699
073722 XDOT = 1455
237387
YDOT = -15232
986942 feet/sec YDOT = -4626
869046 meter/sec
ZDOT = 19487
099317 ZDOT = 5946
681733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20927402
03 X = 6378672
14
Y = -7050576
89 feet Y = -2149015
84 meter
Z = 2629958
22 Z = 801611
27
XDOT = 2270
940749 XDOT = 692
182740
YDOT = 14131
506311 feet/sec YDOT = 4307
283124 meter/sec
ZDOT = 19518
106817 ZDOT = 5949
118958
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 15292
56274727
00016717 00000-0 10270-3 0 9073
2 25544 51
6436 183
3018 0006731 50
7941 309
3809 15
54374920 7395
Satellite: ISS
Catalog Number: 25544
Epoch time: 15292
56274727 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 183
3018 deg
Eccentricity:
0006731
Arg of perigee: 50
7941 deg
Mean anomaly: 309
3809 deg
Mean motion: 15
54374920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 739
Checksum: 322
Coasting Arc #9 (Orbit 753)
---------------------------------------
Vector Time (GMT): 2015/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6024995
66 A = 6785878
26 meter
Y = 1777260
09 meter E =
0009338
Z = -2575571
11 I = 51
66451
XDOT = -3515
812218 Wp = 87
60997
YDOT = 4317
074350 meter/sec RA = 177
51659 deg
ZDOT = -5261
629739 TA = 121
31354
MA = 121
22209
Ha = 222
827 n
mi
Hp = 212
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19767046
14 X = 6017185
44
Y = 5830905
80 feet Y = 1844591
74 meter
Z = -8450036
47 Z = -2546321
54
XDOT = -11534
816988 XDOT = -3538
266121
YDOT = 14163
629758 feet/sec YDOT = 4277
632363 meter/sec
ZDOT = -17262
564759 ZDOT = -5278
763892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20252886
28 X = -6173079
74
Y = 4082748
18 feet Y = 1244421
64 meter
Z = -8324088
92 Z = -2537182
30
XDOT = 3802
031806 XDOT = 1158
859294
YDOT = -16378
047149 feet/sec YDOT = -4992
028771 meter/sec
ZDOT = -17337
199832 ZDOT = -5284
378509
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 15293
52711495
00016717 00000-0 10270-3 0 9089
2 25544 51
6439 178
4922 0006519 54
4224 305
7535 15
54375455 7543
Satellite: ISS
Catalog Number: 25544
Epoch time: 15293
52711495 = yrday
fracday
Element set: 908
Inclination: 51
6439 deg
RA of node: 178
4922 deg
Eccentricity:
0006519
Arg of perigee: 54
4224 deg
Mean anomaly: 305
7535 deg
Mean motion: 15
54375455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 754
Checksum: 326
Coasting Arc #10 (Orbit 769)
---------------------------------------
Vector Time (GMT): 2015/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4874527
41 A = 6781949
14 meter
Y = -2523418
36 meter E =
0016672
Z = 3967675
52 I = 51
68340
XDOT = 5277
359896 Wp = 84
52701
YDOT = -3881
208925 meter/sec RA = 172
53480 deg
ZDOT = 4002
233237 TA = 323
77444
MA = 323
88723
Ha = 222
984 n
mi
Hp = 212
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15992544
00 X = -4865221
35
Y = -8278931
63 feet Y = -2577876
23 meter
Z = 13017308
15 Z = 3944018
52
XDOT = 17314
172887 XDOT = 5300
926716
YDOT = -12733
625082 feet/sec YDOT = -3822
061958 meter/sec
ZDOT = 13130
686472 ZDOT = 4027
927433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18075039
69 X = 5509272
10
Y = -482334
38 feet Y = -147015
52 meter
Z = 12915602
11 Z = 3936675
52
XDOT = -9008
785631 XDOT = -2745
877860
YDOT = 18135
967663 feet/sec YDOT = 5527
842944 meter/sec
ZDOT = 13242
208062 ZDOT = 4036
225017
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 15294
55576373
00016717 00000-0 10270-3 0 9098
2 25544 51
6439 173
3617 0006747 57
6241 302
5564 15
54401328 7709
Satellite: ISS
Catalog Number: 25544
Epoch time: 15294
55576373 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 173
3617 deg
Eccentricity:
0006747
Arg of perigee: 57
6241 deg
Mean anomaly: 302
5564 deg
Mean motion: 15
54401328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 770
Checksum: 321
Coasting Arc #11 (Orbit 784)
---------------------------------------
Vector Time (GMT): 2015/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3320949
17 A = 6778173
95 meter
Y = 3263896
04 meter E =
0018617
Z = -4942987
06 I = 51
70254
XDOT = -6549
485126 Wp = 69
06138
YDOT = 3263
102993 meter/sec RA = 167
54367 deg
ZDOT = -2245
968960 TA = 178
98508
MA = 178
98129
Ha = 222
777 n
mi
Hp = 212
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10895502
52 X = 3308216
12
Y = 10708320
33 feet Y = 3300961
47 meter
Z = -16217149
16 Z = -4926885
56
XDOT = -21487
812092 XDOT = -6574
576964
YDOT = 10705
718480 feet/sec YDOT = 3189
721843 meter/sec
ZDOT = -7368
664566 ZDOT = -2277
846667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14862806
09 X = -4530183
30
Y = -3835337
62 feet Y = -1169010
91 meter
Z = -16148164
20 Z = -4921960
45
XDOT = 13019
379419 XDOT = 3968
306847
YDOT = -18851
553839 feet/sec YDOT = -5745
953610 meter/sec
ZDOT = -7506
792784 ZDOT = -2288
070441
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 15295
52011011
00016717 00000-0 10270-3 0 9101
2 25544 51
6438 168
5518 0006584 59
8997 300
2808 15
54444878 7854
Satellite: ISS
Catalog Number: 25544
Epoch time: 15295
52011011 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 168
5518 deg
Eccentricity:
0006584
Arg of perigee: 59
8997 deg
Mean anomaly: 300
2808 deg
Mean motion: 15
54444878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 785
Checksum: 329
Coasting Arc #12 (Orbit 800)
---------------------------------------
Vector Time (GMT): 2015/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1511600
28 A = 6776415
37 meter
Y = -3917438
24 meter E =
0008688
Z = 5311380
12 I = 51
72803
XDOT = 7260
375044 Wp = 74
97869
YDOT = -2480
206532 meter/sec RA = 162
54687 deg
ZDOT = 238
863307 TA = 12
76068
MA = 12
73870
Ha = 222
847 n
mi
Hp = 211
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4959318
49 X = -1493483
21
Y = -12852487
68 feet Y = -3934240
12 meter
Z = 17425787
78 Z = 5304081
36
XDOT = 23820
128096 XDOT = 7286
409384
YDOT = -8137
160538 feet/sec YDOT = -2398
870638 meter/sec
ZDOT = 783
672267 ZDOT = 274
196732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10927567
25 X = 3330722
50
Y = 8452512
63 feet Y = 2576325
85 meter
Z = 17394903
38 Z = 5301966
55
XDOT = -15691
235900 XDOT = -4782
688702
YDOT = 18371
114136 feet/sec YDOT = 5599
515589 meter/sec
ZDOT = 936
608915 ZDOT = 285
478397
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 15296
54873708
00016717 00000-0 10270-3 0 9114
2 25544 51
6440 163
4216 0006587 64
1628 296
0203 15
54454964 8016
Satellite: ISS
Catalog Number: 25544
Epoch time: 15296
54873708 = yrday
fracday
Element set: 911
Inclination: 51
6440 deg
RA of node: 163
4216 deg
Eccentricity:
0006587
Arg of perigee: 64
1628 deg
Mean anomaly: 296
0203 deg
Mean motion: 15
54454964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 801
Checksum: 314
Coasting Arc #13 (Orbit 815)
---------------------------------------
Vector Time (GMT): 2015/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -343855
57 A = 6777359
41 meter
Y = 4481363
70 meter E =
0018924
Z = -5089137
84 I = 51
76060
XDOT = -7292
093117 Wp = 91
80177
YDOT = 1478
432469 meter/sec RA = 157
55007 deg
ZDOT = 1799
773911 TA = 195
58692
MA = 195
64526
Ha = 222
755 n
mi
Hp = 211
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1128135
08 X = -369220
19
Y = 14702636
80 feet Y = 4477376
09 meter
Z = -16696646
45 Z = -5090870
35
XDOT = -23924
190015 XDOT = -7316
826109
YDOT = 4850
500225 feet/sec YDOT = 1396
749380 meter/sec
ZDOT = 5904
770049 ZDOT = 1764
289536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6863022
43 X = -2091849
24
Y = -13040909
46 feet Y = -3974869
20 meter
Z = -16704844
33 Z = -5091636
55
XDOT = 16877
611195 XDOT = 5144
295892
YDOT = -16227
507474 feet/sec YDOT = -4946
144278 meter/sec
ZDOT = 5751
327353 ZDOT = 1753
004577
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 15297
51306444
00016717 00000-0 10270-3 0 9121
2 25544 51
6430 158
6110 0006515 66
7674 293
4164 15
54476835 8168
Satellite: ISS
Catalog Number: 25544
Epoch time: 15297
51306444 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 158
6110 deg
Eccentricity:
0006515
Arg of perigee: 66
7674 deg
Mean anomaly: 293
4164 deg
Mean motion: 15
54476835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 816
Checksum: 313
Coasting Arc #14 (Orbit 831)
---------------------------------------
Vector Time (GMT): 2015/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2117203
08 A = 6780529
95 meter
Y = -4849364
12 meter E =
0016440
Z = 4229656
22 I = 51
80082
XDOT = 6742
733325 Wp = 72
33527
YDOT = -259
280586 meter/sec RA = 152
56252 deg
ZDOT = -3655
873754 TA = 55
05510
MA = 54
90079
Ha = 222
635 n
mi
Hp = 211
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6946204
34 X = 2150725
99
Y = -15909987
26 feet Y = -4825500
25 meter
Z = 13876824
85 Z = 4240023
35
XDOT = 22121
828494 XDOT = 6762
890754
YDOT = -850
658090 feet/sec YDOT = -183
766590 meter/sec
ZDOT = -11994
336463 ZDOT = -3623
069211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2828891
73 X = 862246
20
Y = 17091187
72 feet Y = 5209394
02 meter
Z = 13922370
16 Z = 4243538
43
XDOT = -16969
770924 XDOT = -5172
386178
YDOT = 12507
965557 feet/sec YDOT = 3812
427902 meter/sec
ZDOT = -11852
647702 ZDOT = -3612
687019
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 15298
54166869
00016717 00000-0 10270-3 0 9131
2 25544 51
6430 153
4805 0006440 69
2884 290
8959 15
54523424 8328
Satellite: ISS
Catalog Number: 25544
Epoch time: 15298
54166869 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 153
4805 deg
Eccentricity:
0006440
Arg of perigee: 69
2884 deg
Mean anomaly: 290
8959 deg
Mean motion: 15
54523424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 832
Checksum: 333
Coasting Arc #15 (Orbit 846)
---------------------------------------
Vector Time (GMT): 2015/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3578031
00 A = 6784609
96 meter
Y = 4979192
20 meter E =
0010962
Z = -2908670
73 I = 51
84036
XDOT = -5649
582093 Wp = 70
84030
YDOT = -1117
974607 meter/sec RA = 147
58707 deg
ZDOT = 5054
930605 TA = 256
12856
MA = 256
25054
Ha = 222
704 n
mi
Hp = 211
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11738946
86 X = -3619314
03
Y = 16335932
40 feet Y = 4938949
18 meter
Z = -9542882
98 Z = -2926153
31
XDOT = -18535
374320 XDOT = -5661
216303
YDOT = -3667
895692 feet/sec YDOT = -1181
216511 meter/sec
ZDOT = 16584
417997 ZDOT = 5027
457210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 651177
42 X = 198478
88
Y = -20069364
80 feet Y = -6117142
39 meter
Z = -9619186
08 Z = -2931927
92
XDOT = 16078
972751 XDOT = 4900
870894
YDOT = -7340
691348 feet/sec YDOT = -2237
442723 meter/sec
ZDOT = 16465
962634 ZDOT = 5018
825411
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 15299
50597729
00016717 00000-0 10270-3 0 9142
2 25544 51
6413 148
6697 0006412 73
5706 286
6152 15
54496419 8471
Satellite: ISS
Catalog Number: 25544
Epoch time: 15299
50597729 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 148
6697 deg
Eccentricity:
0006412
Arg of perigee: 73
5706 deg
Mean anomaly: 286
6152 deg
Mean motion: 15
54496419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 847
Checksum: 347
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