[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 29th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
271/15:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 215
3
274/22:54:34
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
8
Coasting Arc #1 (Orbit 412)
---------------------------------------
Vector Time (GMT): 2015/271/12:53:56
156
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2187097
57 A = 6789527
97 meter
Y = -6413704
05 meter E =
0015656
Z = 214767
79 I = 51
31325
XDOT = 4479
055226 Wp = 25
56773
YDOT = 1732
770780 meter/sec RA = 287
37528 deg
ZDOT = 5984
389833 TA = 336
75812
MA = 336
82884
Ha = 221
473 n
mi
Hp = 215
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7175516
96 X = 2257611
34
Y = -21042336
14 feet Y = -6388852
19 meter
Z = 704618
72 Z = 225564
65
XDOT = 14695
063078 XDOT = 4430
275842
YDOT = 5684
943503 feet/sec YDOT = 1782
586710 meter/sec
ZDOT = 19633
824913 ZDOT = 6006
029683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 313321
14 X = 95500
28
Y = 22228367
42 feet Y = 6775206
39 meter
Z = 752298
42 Z = 229300
56
XDOT = -14012
102626 XDOT = -4270
888881
YDOT = -485
666721 feet/sec YDOT = -148
031217 meter/sec
ZDOT = 19726
758535 ZDOT = 6012
716001
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 15271
60132248
00016717 00000-0 10270-3 0 9009
2 25544 51
6411 287
8062 0006189 336
6895 23
3976 15
54054620 4137
Satellite: ISS
Catalog Number: 25544
Epoch time: 15271
60132248 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 287
8062 deg
Eccentricity:
0006189
Arg of perigee: 336
6895 deg
Mean anomaly: 23
3976 deg
Mean motion: 15
54054620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 413
Checksum: 300
Coasting Arc #2 (Orbit 413)
---------------------------------------
Vector Time (GMT): 2015/271/15:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 894988
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3749683
00 A = 6786558
68 meter
Y = 4990540
45 meter E =
0003621
Z = -2669268
84 I = 51
30102
XDOT = -2838
046921 Wp = 25
27619
YDOT = -4895
153865 meter/sec RA = 286
88610 deg
ZDOT = -5164
730237 TA = 184
97457
MA = 184
97817
Ha = 221
685 n
mi
Hp = 215
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12302109
57 X = -3792243
30
Y = 16373164
22 feet Y = 4948370
65 meter
Z = -8757443
70 Z = -2687588
40
XDOT = -9311
177563 XDOT = -2758
008594
YDOT = -16060
216092 feet/sec YDOT = -4926
444047 meter/sec
ZDOT = -16944
653007 ZDOT = -5178
321905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6806914
37 X = -2074747
50
Y = -19279097
56 feet Y = -5876268
94 meter
Z = -8837281
30 Z = -2693603
34
XDOT = 17061
596676 XDOT = 5200
374667
YDOT = 1770
580612 feet/sec YDOT = 539
672971 meter/sec
ZDOT = -17002
337550 ZDOT = -5182
312485
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 15271
66563141
00016717 00000-0 10270-3 0 9016
2 25544 51
6400 287
4844 0006525 337
6551 22
4317 15
54023604 4141
Satellite: ISS
Catalog Number: 25544
Epoch time: 15271
66563141 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 287
4844 deg
Eccentricity:
0006525
Arg of perigee: 337
6551 deg
Mean anomaly: 22
4317 deg
Mean motion: 15
54023604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 414
Checksum: 281
Coasting Arc #3 (Orbit 429)
---------------------------------------
Vector Time (GMT): 2015/272/15:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 894988
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4030486
17 A = 6782756
95 meter
Y = -3742638
22 meter E =
0009359
Z = 3958657
48 I = 51
28069
XDOT = 1929
513856 Wp = 64
68075
YDOT = 6277
770711 meter/sec RA = 281
88018 deg
ZDOT = 3967
248967 TA = 343
79826
MA = 343
82816
Ha = 221
529 n
mi
Hp = 215
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13223379
81 X = 4052807
75
Y = -12278996
79 feet Y = -3697441
32 meter
Z = 12987721
38 Z = 3978291
81
XDOT = 6330
426038 XDOT = 1839
899203
YDOT = 20596
360600 feet/sec YDOT = 6298
847286 meter/sec
ZDOT = 13015
908684 ZDOT = 3976
403775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3210676
62 X = 978614
23
Y = 17694655
49 feet Y = 5393330
99 meter
Z = 13072993
74 Z = 3984648
49
XDOT = -19410
253192 XDOT = -5916
245173
YDOT = -6130
883727 feet/sec YDOT = -1868
693360 meter/sec
ZDOT = 13054
232441 ZDOT = 3978
930048
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 15272
69453018
00016717 00000-0 10270-3 0 9022
2 25544 51
6403 282
3558 0006452 339
7391 20
3504 15
54069821 4308
Satellite: ISS
Catalog Number: 25544
Epoch time: 15272
69453018 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 282
3558 deg
Eccentricity:
0006452
Arg of perigee: 339
7391 deg
Mean anomaly: 20
3504 deg
Mean motion: 15
54069821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 430
Checksum: 294
Coasting Arc #4 (Orbit 444)
---------------------------------------
Vector Time (GMT): 2015/273/15:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 894988
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4195073
25 A = 6779421
95 meter
Y = 2192159
22 meter E =
0013820
Z = -4865589
31 I = 51
26407
XDOT = -1033
401271 Wp = 44
48248
YDOT = -7213
773914 meter/sec RA = 276
86250 deg
ZDOT = -2353
521508 TA = 202
28447
MA = 202
34458
Ha = 221
858 n
mi
Hp = 214
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13763363
67 X = -4195639
13
Y = 7192123
42 feet Y = 2145243
42 meter
Z = -15963219
51 Z = -4885970
11
XDOT = -3390
424119 XDOT = -941
225584
YDOT = -23667
237250 feet/sec YDOT = -7224
814976 meter/sec
ZDOT = -7721
527258 ZDOT = -2358
316926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1083990
22 X = 330400
22
Y = -15399928
11 feet Y = -4693898
09 meter
Z = -16051429
07 Z = -4892475
58
XDOT = 20754
999730 XDOT = 6326
123918
YDOT = 9548
385126 feet/sec YDOT = 2910
347786 meter/sec
ZDOT = -7740
906465 ZDOT = -2359
428291
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 15273
65911319
00016717 00000-0 10270-3 0 9033
2 25544 51
6406 277
5466 0006573 344
6377 15
4575 15
54054712 4450
Satellite: ISS
Catalog Number: 25544
Epoch time: 15273
65911319 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 277
5466 deg
Eccentricity:
0006573
Arg of perigee: 344
6377 deg
Mean anomaly: 15
4575 deg
Mean motion: 15
54054712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 445
Checksum: 317
Coasting Arc #5 (Orbit 460)
---------------------------------------
Vector Time (GMT): 2015/274/15:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 894988
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4242309
94 A = 6777531
53 meter
Y = -422640
47 meter E =
0005610
Z = 5267309
28 I = 51
25592
XDOT = 152
802785 Wp = 11
66270
YDOT = 7652
522008 meter/sec RA = 271
83833 deg
ZDOT = 496
267925 TA = 73
60963
MA = 73
54797
Ha = 221
792 n
mi
Hp = 214
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13918339
69 X = 4221133
70
Y = -1386615
71 feet Y = -375318
06 meter
Z = 17281198
42 Z = 5287866
51
XDOT = 501
321474 XDOT = 64
808347
YDOT = 25106
699502 feet/sec YDOT = 7653
738791 meter/sec
ZDOT = 1628
175606 ZDOT = 496
795753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5880709
08 X = -1792440
13
Y = 12569331
44 feet Y = 3831132
22 meter
Z = 17369855
19 Z = 5294331
86
XDOT = -20900
286498 XDOT = -6370
407325
YDOT = -12005
779014 feet/sec YDOT = -3659
361444 meter/sec
ZDOT = 1629
095640 ZDOT = 496
548351
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 15274
68798656
00016717 00000-0 10270-3 0 9045
2 25544 51
6413 272
4182 0006635 347
7466 12
3524 15
54092165 4611
Satellite: ISS
Catalog Number: 25544
Epoch time: 15274
68798656 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 272
4182 deg
Eccentricity:
0006635
Arg of perigee: 347
7466 deg
Mean anomaly: 12
3524 deg
Mean motion: 15
54092165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 461
Checksum: 320
Coasting Arc #6 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2015/274/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3382321
27 A = 6781941
36 meter
Y = -4110456
31 meter E =
0009121
Z = 4192504
42 I = 51
26919
XDOT = 2893
737232 Wp = 65
58340
YDOT = 6101
000674 meter/sec RA = 270
27530 deg
ZDOT = 3644
505934 TA = 346
89801
MA = 346
92169
Ha = 221
836 n
mi
Hp = 214
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11096854
56 X = 3407668
09
Y = -13485749
06 feet Y = -4072490
86 meter
Z = 13754935
75 Z = 4208997
26
XDOT = 9493
888556 XDOT = 2807
595383
YDOT = 20016
406412 feet/sec YDOT = 6132
879036 meter/sec
ZDOT = 11957
040465 ZDOT = 3658
353563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12538194
28 X = 3821641
62
Y = -12075556
25 feet Y = -3680629
54 meter
Z = 13826731
06 Z = 4214387
63
XDOT = 6082
596300 XDOT = 1853
975352
YDOT = 20083
324631 feet/sec YDOT = 6121
397348 meter/sec
ZDOT = 12015
633419 ZDOT = 3662
365066
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 15275
00950581
00016717 00000-0 10270-3 0 9050
2 25544 51
6403 270
8134 0006660 347
6800 12
4188 15
54074415 4668
Satellite: ISS
Catalog Number: 25544
Epoch time: 15275
00950581 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 270
8134 deg
Eccentricity:
0006660
Arg of perigee: 347
6800 deg
Mean anomaly: 12
4188 deg
Mean motion: 15
54074415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 292
Coasting Arc #7 (Orbit 480)
---------------------------------------
Vector Time (GMT): 2015/275/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3817754
37 A = 6778703
33 meter
Y = 2542517
08 meter E =
0015120
Z = -5004114
63 I = 51
25872
XDOT = -2156
699637 Wp = 50
15625
YDOT = -7084
348175 meter/sec RA = 265
25540 deg
ZDOT = -1948
479225 TA = 200
77256
MA = 200
83407
Ha = 221
999 n
mi
Hp = 214
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12525440
85 X = -3821593
25
Y = 8341591
47 feet Y = 2499802
57 meter
Z = -16417698
91 Z = -5022670
29
XDOT = -7075
786212 XDOT = -2067
855344
YDOT = -23242
612122 feet/sec YDOT = -7107
969211 meter/sec
ZDOT = -6392
648376 ZDOT = -1958
739811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13207294
39 X = -4025583
33
Y = 7027765
85 feet Y = 2142063
03 meter
Z = -16498107
05 Z = -5028623
03
XDOT = -4111
285978 XDOT = -1253
119966
YDOT = -22877
113394 feet/sec YDOT = -6972
944163 meter/sec
ZDOT = -6435
621646 ZDOT = -1961
577478
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 15275
97405847
00016717 00000-0 10270-3 0 9067
2 25544 51
6396 266
0046 0006506 352
5999 7
5056 15
54106058 4816
Satellite: ISS
Catalog Number: 25544
Epoch time: 15275
97405847 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 266
0046 deg
Eccentricity:
0006506
Arg of perigee: 352
5999 deg
Mean anomaly: 7
5056 deg
Mean motion: 15
54106058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 481
Checksum: 327
Coasting Arc #8 (Orbit 496)
---------------------------------------
Vector Time (GMT): 2015/276/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4171299
40 A = 6777478
39 meter
Y = -764092
41 meter E =
0006680
Z = 5285027
79 I = 51
25803
XDOT = 1336
247949 Wp = 17
73531
YDOT = 7553
115658 meter/sec RA = 260
22867 deg
ZDOT = 43
591508 TA = 71
88359
MA = 71
81084
Ha = 222
024 n
mi
Hp = 214
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13685365
49 X = 4153860
72
Y = -2506864
85 feet Y = -717543
28 meter
Z = 17339330
01 Z = 5305249
04
XDOT = 4384
015581 XDOT = 1251
476108
YDOT = 24780
563181 feet/sec YDOT = 7567
584479 meter/sec
ZDOT = 143
016757 ZDOT = 49
876299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13738196
56 X = 4187402
31
Y = -1342108
93 feet Y = -409074
80 meter
Z = 17426607
92 Z = 5311630
10
XDOT = 2162
377576 XDOT = 659
092685
YDOT = 24061
697397 feet/sec YDOT = 7334
005366 meter/sec
ZDOT = 168
787766 ZDOT = 51
446511
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 15277
00290213
00016717 00000-0 10270-3 0 9073
2 25544 51
6396 260
8748 0006476 356
8082 3
3029 15
54083161 4973
Satellite: ISS
Catalog Number: 25544
Epoch time: 15277
00290213 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 260
8748 deg
Eccentricity:
0006476
Arg of perigee: 356
8082 deg
Mean anomaly: 3
3029 deg
Mean motion: 15
54083161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 497
Checksum: 310
Coasting Arc #9 (Orbit 511)
---------------------------------------
Vector Time (GMT): 2015/277/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4440332
65 A = 6778438
53 meter
Y = -1006797
51 meter E =
0013197
Z = -5031870
40 I = 51
26795
XDOT = -417
078921 Wp = 75
94251
YDOT = -7418
927393 meter/sec RA = 255
20209 deg
ZDOT = 1859
720249 TA = 212
15091
MA = 212
23145
Ha = 222
076 n
mi
Hp = 214
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14568020
52 X = -4404301
28
Y = -3303141
44 feet Y = -1056251
20 meter
Z = -16508761
15 Z = -5053353
21
XDOT = -1368
369165 XDOT = -343
121559
YDOT = -24340
312970 feet/sec YDOT = -7423
177768 meter/sec
ZDOT = 6101
444388 ZDOT = 1857
874409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14204644
49 X = -4329575
64
Y = -4278574
45 feet Y = -1304109
49 meter
Z = -16601175
73 Z = -5060038
36
XDOT = -64
114557 XDOT = -19
542117
YDOT = -23343
337346 feet/sec YDOT = -7115
049223 meter/sec
ZDOT = 6094
766694 ZDOT = 1857
684888
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 15277
96742799
00016717 00000-0 10270-3 0 9080
2 25544 51
6394 256
0655 0006369
8367 359
2795 15
54146801 5120
Satellite: ISS
Catalog Number: 25544
Epoch time: 15277
96742799 = yrday
fracday
Element set: 908
Inclination: 51
6394 deg
RA of node: 256
0655 deg
Eccentricity:
0006369
Arg of perigee:
8367 deg
Mean anomaly: 359
2795 deg
Mean motion: 15
54146801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 512
Checksum: 344
Coasting Arc #10 (Orbit 527)
---------------------------------------
Vector Time (GMT): 2015/278/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4568775
30 A = 6781598
70 meter
Y = 2694725
48 meter E =
0013570
Z = 4222737
35 I = 51
28718
XDOT = -635
830119 Wp = 47
73209
YDOT = 6742
105022 meter/sec RA = 250
18224 deg
ZDOT = -3598
103205 TA = 79
30864
MA = 79
15587
Ha = 222
134 n
mi
Hp = 214
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14989420
28 X = 4517790
09
Y = 8840962
85 feet Y = 2745531
86 meter
Z = 13854125
17 Z = 4244807
58
XDOT = -2086
056822 XDOT = -693
696400
YDOT = 22119
767132 feet/sec YDOT = 6734
670862 meter/sec
ZDOT = -11804
800540 ZDOT = -3601
333144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14433170
93 X = 4399230
50
Y = 9586287
16 feet Y = 2921900
33 meter
Z = 13948792
22 Z = 4251591
87
XDOT = -2430
374139 XDOT = -740
778038
YDOT = 20935
842075 feet/sec YDOT = 6381
244664 meter/sec
ZDOT = -11819
870367 ZDOT = -3602
696488
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 15278
99624220
00016717 00000-0 10270-3 0 9093
2 25544 51
6389 250
9359 0006349 4
0222 356
0980 15
54151054 5286
Satellite: ISS
Catalog Number: 25544
Epoch time: 15278
99624220 = yrday
fracday
Element set: 909
Inclination: 51
6389 deg
RA of node: 250
9359 deg
Eccentricity:
0006349
Arg of perigee: 4
0222 deg
Mean anomaly: 356
0980 deg
Mean motion: 15
54151054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 528
Checksum: 313
Coasting Arc #11 (Orbit 542)
---------------------------------------
Vector Time (GMT): 2015/279/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4524404
82 A = 6785281
41 meter
Y = -4072342
75 meter E =
0009318
Z = -2992442
61 I = 51
31216
XDOT = 1773
173782 Wp = 34
36659
YDOT = -5588
963130 meter/sec RA = 245
17293 deg
ZDOT = 4940
036809 TA = 291
21772
MA = 291
31723
Ha = 222
164 n
mi
Hp = 213
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14843847
84 X = -4463994
41
Y = -13360704
56 feet Y = -4122600
17 meter
Z = -9817725
08 Z = -3014274
20
XDOT = 5817
499286 XDOT = 1811
542199
YDOT = -18336
493209 feet/sec YDOT = -5568
919276 meter/sec
ZDOT = 16207
469846 ZDOT = 4948
744362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14324756
70 X = -4366185
84
Y = -13849424
57 feet Y = -4221304
61 meter
Z = -9911143
00 Z = -3020916
39
XDOT = 5315
172534 XDOT = 1620
064589
YDOT = -17088
676702 feet/sec YDOT = -5208
628659 meter/sec
ZDOT = 16245
944048 ZDOT = 4951
763746
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 15279
96074220
00016717 00000-0 10270-3 0 9102
2 25544 51
6395 246
1266 0006278 8
9047 351
2216 15
54187914 5436
Satellite: ISS
Catalog Number: 25544
Epoch time: 15279
96074220 = yrday
fracday
Element set: 910
Inclination: 51
6395 deg
RA of node: 246
1266 deg
Eccentricity:
0006278
Arg of perigee: 8
9047 deg
Mean anomaly: 351
2216 deg
Mean motion: 15
54187914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 543
Checksum: 312
Coasting Arc #12 (Orbit 558)
---------------------------------------
Vector Time (GMT): 2015/280/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4224791
61 A = 6788171
86 meter
Y = 5122785
80 meter E =
0013355
Z = 1396430
76 I = 51
33578
XDOT = -2997
082027 Wp = 92
36878
YDOT = 4058
060398 meter/sec RA = 240
17447 deg
ZDOT = -5772
113187 TA = 72
34937
MA = 72
20358
Ha = 222
258 n
mi
Hp = 213
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13860864
86 X = 4160410
01
Y = 16807040
02 feet Y = 5169670
39 meter
Z = 4581465
74 Z = 1416797
07
XDOT = -9832
946283 XDOT = -3014
198607
YDOT = 13313
846451 feet/sec YDOT = 4024
448661 meter/sec
ZDOT = -18937
379222 ZDOT = -5786
714547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13555255
12 X = 4131641
76
Y = 17030884
92 feet Y = 5191013
72 meter
Z = 4668406
04 Z = 1422930
16
XDOT = -8685
766764 XDOT = -2647
421710
YDOT = 12163
455320 feet/sec YDOT = 3707
421181 meter/sec
ZDOT = -19000
996504 ZDOT = -5791
503734
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 15280
98952611
00016717 00000-0 10270-3 0 9116
2 25544 51
6389 240
9964 0006374 11
4307 348
6989 15
54231488 5591
Satellite: ISS
Catalog Number: 25544
Epoch time: 15280
98952611 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 240
9964 deg
Eccentricity:
0006374
Arg of perigee: 11
4307 deg
Mean anomaly: 348
6989 deg
Mean motion: 15
54231488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 559
Checksum: 341
Coasting Arc #13 (Orbit 574)
---------------------------------------
Vector Time (GMT): 2015/281/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3656200
97 A = 6788962
58 meter
Y = -5699541
38 meter E =
0018228
Z = 315896
47 I = 51
35641
XDOT = 4192
971861 Wp = 38
41734
YDOT = -2348
637694 meter/sec RA = 235
18263 deg
ZDOT = 5982
613624 TA = 325
00320
MA = 325
12287
Ha = 222
281 n
mi
Hp = 213
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11995409
99 X = -3593730
09
Y = -18699282
73 feet Y = -5740078
09 meter
Z = 1036405
74 Z = 298287
72
XDOT = 13756
469360 XDOT = 4189
861789
YDOT = -7705
504246 feet/sec YDOT = -2301
765732 meter/sec
ZDOT = 19627
997453 ZDOT = 6002
975139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12018349
28 X = -3663192
86
Y = -18688555
26 feet Y = -5696271
64 meter
Z = 961433
86 Z = 293045
04
XDOT = 12261
185563 XDOT = 3737
209360
YDOT = -6839
421538 feet/sec YDOT = -2084
655685 meter/sec
ZDOT = 19716
161287 ZDOT = 6009
485960
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 15282
01829660
00016717 00000-0 10270-3 0 9120
2 25544 51
6402 235
8666 0006203 17
3306 342
8057 15
54244513 5757
Satellite: ISS
Catalog Number: 25544
Epoch time: 15282
01829660 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 235
8666 deg
Eccentricity:
0006203
Arg of perigee: 17
3306 deg
Mean anomaly: 342
8057 deg
Mean motion: 15
54244513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 575
Checksum: 291
Coasting Arc #14 (Orbit 589)
---------------------------------------
Vector Time (GMT): 2015/282/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2757169
97 A = 6787155
94 meter
Y = 5858312
80 meter E =
0006587
Z = -2043012
57 I = 51
36956
XDOT = -5278
004576 Wp = 82
75350
YDOT = 562
645950 meter/sec RA = 230
19068 deg
ZDOT = -5524
151185 TA = 119
90257
MA = 119
83712
Ha = 222
387 n
mi
Hp = 213
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9045833
22 X = 2701380
25
Y = 19220186
35 feet Y = 5888833
07 meter
Z = -6702797
14 Z = -2029754
97
XDOT = -17316
287980 XDOT = -5257
069446
YDOT = 1845
951279 feet/sec YDOT = 503
740120 meter/sec
ZDOT = -18123
855594 ZDOT = -5549
740158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9434608
12 X = 2875668
55
Y = 19052062
27 feet Y = 5807068
58 meter
Z = -6646596
45 Z = -2025882
60
XDOT = -15774
690354 XDOT = -4808
125620
YDOT = 1467
138632 feet/sec YDOT = 447
183855 meter/sec
ZDOT = -18234
265900 ZDOT = -5557
804246
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 15282
98275387
00016717 00000-0 10270-3 0 9138
2 25544 51
6401 231
0571 0006343 20
5426 339
5981 15
54275760 5907
Satellite: ISS
Catalog Number: 25544
Epoch time: 15282
98275387 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 231
0571 deg
Eccentricity:
0006343
Arg of perigee: 20
5426 deg
Mean anomaly: 339
5981 deg
Mean motion: 15
54275760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 590
Checksum: 309
Coasting Arc #15 (Orbit 605)
---------------------------------------
Vector Time (GMT): 2015/283/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1575891
60 A = 6783596
15 meter
Y = -5571992
18 meter E =
0015605
Z = 3515850
15 I = 51
38005
XDOT = 6135
459967 Wp = 70
73658
YDOT = 1098
561356 meter/sec RA = 225
19252 deg
ZDOT = 4479
876074 TA = 330
88964
MA = 330
97654
Ha = 222
342 n
mi
Hp = 213
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5170248
02 X = -1530545
99
Y = -18280814
23 feet Y = -5589360
80 meter
Z = 11534941
45 Z = 3508305
61
XDOT = 20129
461833 XDOT = 6100
957753
YDOT = 3604
203923 feet/sec YDOT = 1166
979831 meter/sec
ZDOT = 14697
756147 ZDOT = 4509
597350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5885529
08 X = -1793909
26
Y = -18083384
65 feet Y = -5511815
64 meter
Z = 11503314
96 Z = 3506210
40
XDOT = 18831
241050 XDOT = 5739
762272
YDOT = 3325
563207 feet/sec YDOT = 1013
631665 meter/sec
ZDOT = 14825
719382 ZDOT = 4518
879268
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 15284
01149273
00016717 00000-0 10270-3 0 9149
2 25544 51
6412 225
9273 0006140 24
2652 335
8788 15
54304455 6063
Satellite: ISS
Catalog Number: 25544
Epoch time: 15284
01149273 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 225
9273 deg
Eccentricity:
0006140
Arg of perigee: 24
2652 deg
Mean anomaly: 335
8788 deg
Mean motion: 15
54304455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 606
Checksum: 296
Coasting Arc #16 (Orbit 620)
---------------------------------------
Vector Time (GMT): 2015/284/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 134915
97 A = 6779739
03 meter
Y = 4959655
78 meter E =
0015534
Z = -4635791
69 I = 51
39087
XDOT = -6609
633856 Wp = 54
75827
YDOT = -2541
466725 meter/sec RA = 220
18559 deg
ZDOT = -2909
515250 TA = 186
13163
MA = 186
15067
Ha = 222
446 n
mi
Hp = 213
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 442637
69 X = 101965
16
Y = 16271836
53 feet Y = 4960979
61 meter
Z = -15209290
33 Z = -4635217
01
XDOT = -21685
150447 XDOT = -6566
589750
YDOT = -8338
145422 feet/sec YDOT = -2615
139739 meter/sec
ZDOT = -9545
653708 ZDOT = -2941
519168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1392728
46 X = 424503
63
Y = 16219741
63 feet Y = 4943777
25 meter
Z = -15207609
72 Z = -4635279
44
XDOT = -20848
718938 XDOT = -6354
689532
YDOT = -7294
521464 feet/sec YDOT = -2223
370142 meter/sec
ZDOT = -9683
235884 ZDOT = -2951
450297
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 15284
97592230
00016717 00000-0 10270-3 0 9150
2 25544 51
6418 221
1187 0006241 27
7271 332
4214 15
54303325 6217
Satellite: ISS
Catalog Number: 25544
Epoch time: 15284
97592230 = yrday
fracday
Element set: 915
Inclination: 51
6418 deg
RA of node: 221
1187 deg
Eccentricity:
0006241
Arg of perigee: 27
7271 deg
Mean anomaly: 332
4214 deg
Mean motion: 15
54303325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 621
Checksum: 281
Coasting Arc #17 (Orbit 636)
---------------------------------------
Vector Time (GMT): 2015/285/22:54:34
000
Vector Time (MET): N/A
Weight (LBS) : 910421
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1455496
09 A = 6777053
05 meter
Y = -4066854
25 meter E =
0007101
Z = 5216177
38 I = 51
40806
XDOT = 6651
546327 Wp = 62
63993
YDOT = 3688
893626 meter/sec RA = 215
16952 deg
ZDOT = 1022
208423 TA = 17
56039
MA = 17
53585
Ha = 222
330 n
mi
Hp = 212
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4775249
62 X = 1475525
74
Y = -13342697
66 feet Y = -4050465
25 meter
Z = 17113442
85 Z = 5223297
22
XDOT = 21822
658554 XDOT = 6604
836258
YDOT = 12102
669377 feet/sec YDOT = 3763
014568 meter/sec
ZDOT = 3353
702175 ZDOT = 1054
407015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3725448
12 X = 1135516
59
Y = -13633692
77 feet Y = -4155549
56 meter
Z = 17144794
36 Z = 5225733
32
XDOT = 21596
511401 XDOT = 6582
616675
YDOT = 10283
765100 feet/sec YDOT = 3134
491603 meter/sec
ZDOT = 3491
951201 ZDOT = 1064
346726
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
00463013
00016717 00000-0 10270-3 0 9163
2 25544 51
6425 215
9883 0006196 30
7550 329
3965 15
54355771 6379
Satellite: ISS
Catalog Number: 25544
Epoch time: 15286
00463013 = yrday
fracday
Element set: 916
Inclination: 51
6425 deg
RA of node: 215
9883 deg
Eccentricity:
0006196
Arg of perigee: 30
7550 deg
Mean anomaly: 329
3965 deg
Mean motion: 15
54355771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 637
Checksum: 316
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