[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 8th 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) : 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 553)
---------------------------------------
Vector Time (GMT): 2015/280/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4883872
89 A = 6780853
58 meter
Y = 1651915
74 meter E =
0013960
Z = 4401420
51 I = 51
30900
XDOT = 674
536093 Wp = 45
51674
YDOT = 6882
569176 meter/sec RA = 241
82296 deg
ZDOT = -3315
464434 TA = 78
19411
MA = 78
03756
Ha = 222
356 n
mi
Hp = 213
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16023205
03 X = 4843657
25
Y = 5419671
05 feet Y = 1706306
07 meter
Z = 14440356
01 Z = 4425047
64
XDOT = 2213
044925 XDOT = 613
628748
YDOT = 22580
607533 feet/sec YDOT = 6889
771350 meter/sec
ZDOT = -10877
507985 ZDOT = -3312
336384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12587966
95 X = -3836812
33
Y = 11167598
38 feet Y = 3403883
99 meter
Z = 14541927
31 Z = 4432379
44
XDOT = -19941
297859 XDOT = -6078
107587
YDOT = -8260
986426 feet/sec YDOT = -2517
948663 meter/sec
ZDOT = -10865
173977 ZDOT = -3311
705028
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
66804426
00016717 00000-0 10270-3 0 9009
2 25544 51
6421 242
6118 0006711 10
9032 349
2265 15
54177395 5547
Satellite: ISS
Catalog Number: 25544
Epoch time: 15280
66804426 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 242
6118 deg
Eccentricity:
0006711
Arg of perigee: 10
9032 deg
Mean anomaly: 349
2265 deg
Mean motion: 15
54177395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 554
Checksum: 290
Coasting Arc #2 (Orbit 568)
---------------------------------------
Vector Time (GMT): 2015/281/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5106677
84 A = 6784539
00 meter
Y = -3072621
60 meter E =
0009409
Z = -3239616
04 I = 51
33812
XDOT = 609
850914 Wp = 41
90539
YDOT = -5994
834264 meter/sec RA = 236
81339 deg
ZDOT = 4739
346454 TA = 280
38787
MA = 280
49390
Ha = 222
377 n
mi
Hp = 213
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16754192
40 X = -5056202
57
Y = -10080779
52 feet Y = -3129446
02 meter
Z = -10628661
55 Z = -3264300
43
XDOT = 2000
823210 XDOT = 653
819186
YDOT = -19668
091417 feet/sec YDOT = -5987
768069 meter/sec
ZDOT = 15549
036922 ZDOT = 4742
416559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16846457
79 X = 5134800
34
Y = -9811192
69 feet Y = -2990451
53 meter
Z = -10734564
86 Z = -3271895
37
XDOT = 15632
977687 XDOT = 4764
931599
YDOT = 9867
647156 feet/sec YDOT = 3007
658853 meter/sec
ZDOT = 15563
262049 ZDOT = 4743
682272
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 15281
63253501
00016717 00000-0 10270-3 0 9010
2 25544 51
6427 237
8026 0006699 14
2371 345
8969 15
54213020 5690
Satellite: ISS
Catalog Number: 25544
Epoch time: 15281
63253501 = yrday
fracday
Element set: 901
Inclination: 51
6427 deg
RA of node: 237
8026 deg
Eccentricity:
0006699
Arg of perigee: 14
2371 deg
Mean anomaly: 345
8969 deg
Mean motion: 15
54213020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 569
Checksum: 304
Coasting Arc #3 (Orbit 584)
---------------------------------------
Vector Time (GMT): 2015/282/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5034137
85 A = 6787833
49 meter
Y = 4226395
83 meter E =
0014666
Z = 1681929
33 I = 51
36751
XDOT = -2055
788319 Wp = 89
00686
YDOT = 4724
936886 meter/sec RA = 231
81563 deg
ZDOT = -5676
582458 TA = 72
49098
MA = 72
33075
Ha = 222
522 n
mi
Hp = 213
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16516200
31 X = 4978332
87
Y = 13866128
06 feet Y = 4282379
08 meter
Z = 5518140
84 Z = 1706248
27
XDOT = -6744
712334 XDOT = -2080
895989
YDOT = 15501
761437 feet/sec YDOT = 4701
806553 meter/sec
ZDOT = -18623
958194 ZDOT = -5686
630778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19932296
42 X = -6075363
95
Y = 8160739
02 feet Y = 2487393
25 meter
Z = 5622291
01 Z = 1713674
30
XDOT = -10058
367242 XDOT = -3065
790335
YDOT = -11610
024724 feet/sec YDOT = -3538
735536 meter/sec
ZDOT = -18668
050159 ZDOT = -5690
021689
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
66131003
00016717 00000-0 10270-3 0 9027
2 25544 51
6429 232
6728 0006660 18
2853 341
8538 15
54215330 5853
Satellite: ISS
Catalog Number: 25544
Epoch time: 15282
66131003 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 232
6728 deg
Eccentricity:
0006660
Arg of perigee: 18
2853 deg
Mean anomaly: 341
8538 deg
Mean motion: 15
54215330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 585
Checksum: 294
Coasting Arc #4 (Orbit 599)
---------------------------------------
Vector Time (GMT): 2015/283/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4625365
53 A = 6788994
17 meter
Y = -4955777
02 meter E =
0018458
Z = 22168
71 I = 51
39258
XDOT = 3519
688714 Wp = 37
05966
YDOT = -3246
605552 meter/sec RA = 226
82548 deg
ZDOT = 5996
500679 TA = 323
18012
MA = 323
30674
Ha = 222
533 n
mi
Hp = 213
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15175083
75 X = -4569712
74
Y = -16259110
96 feet Y = -5007189
73 meter
Z = 72731
98 Z = -164
80
XDOT = 11547
535150 XDOT = 3526
602373
YDOT = -10651
593020 feet/sec YDOT = -3207
206578 meter/sec
ZDOT = 19673
558657 ZDOT = 6013
616077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21340906
44 X = 6504708
28
Y = -6261975
77 feet Y = -1908650
21 meter
Z = -22751
84 Z = -6934
76
XDOT = 3932
954994 XDOT = 1198
764682
YDOT = 13430
586501 feet/sec YDOT = 4093
642765 meter/sec
ZDOT = 19747
875273 ZDOT = 6019
152383
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 15283
62577071
00016717 00000-0 10270-3 0 9034
2 25544 51
6435 227
8637 0006756 20
9063 339
2365 15
54245117 6007
Satellite: ISS
Catalog Number: 25544
Epoch time: 15283
62577071 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 227
8637 deg
Eccentricity:
0006756
Arg of perigee: 20
9063 deg
Mean anomaly: 339
2365 deg
Mean motion: 15
54245117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 600
Checksum: 305
Coasting Arc #5 (Orbit 615)
---------------------------------------
Vector Time (GMT): 2015/284/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3820724
34 A = 6787656
58 meter
Y = 5323575
50 meter E =
0007373
Z = -1776785
94 I = 51
41131
XDOT = -4911
486944 Wp = 89
66684
YDOT = 1647
963885 meter/sec RA = 221
83713 deg
ZDOT = -5644
151476 TA = 109
89411
MA = 109
81465
Ha = 222
578 n
mi
Hp = 213
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12535184
83 X = 3769541
94
Y = 17465798
90 feet Y = 5366014
94 meter
Z = -5829350
21 Z = -1758350
40
XDOT = -16113
802310 XDOT = -4902
132263
YDOT = 5406
705658 feet/sec YDOT = 1593
091915 meter/sec
ZDOT = -18517
557336 ZDOT = -5667
988380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21188716
62 X = -6458320
83
Y = 3759496
03 feet Y = 1145894
39 meter
Z = -5750720
93 Z = -1752819
74
XDOT = 2336
305764 XDOT = 712
105997
YDOT = -15212
217069 feet/sec YDOT = -4636
683763 meter/sec
ZDOT = -18620
597667 ZDOT = -5675
558169
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
65451345
00016717 00000-0 10270-3 0 9044
2 25544 51
6441 222
7339 0006570 24
5539 335
5925 15
54253664 6163
Satellite: ISS
Catalog Number: 25544
Epoch time: 15284
65451345 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 222
7339 deg
Eccentricity:
0006570
Arg of perigee: 24
5539 deg
Mean anomaly: 335
5925 deg
Mean motion: 15
54253664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 616
Checksum: 311
Coasting Arc #6 (Orbit 631)
---------------------------------------
Vector Time (GMT): 2015/285/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2658627
31 A = 6784276
22 meter
Y = -5283423
73 meter E =
0017122
Z = 3302526
39 I = 51
42478
XDOT = 6077
253195 Wp = 68
28739
YDOT = -119
124669 meter/sec RA = 216
84316 deg
ZDOT = 4688
442545 TA = 330
29139
MA = 330
38851
Ha = 222
678 n
mi
Hp = 212
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8722530
53 X = -2615391
91
Y = -17334067
36 feet Y = -5312912
07 meter
Z = 10835060
32 Z = 3289716
79
XDOT = 19938
494734 XDOT = 6055
358485
YDOT = -390
828965 feet/sec YDOT = -51
286605 meter/sec
ZDOT = 15382
029347 ZDOT = 4717
912026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19420982
14 X = 5919515
36
Y = -743969
76 feet Y = -226761
98 meter
Z = 10780673
64 Z = 3285949
32
XDOT = -7991
142206 XDOT = -2435
700145
YDOT = 16771
053288 feet/sec YDOT = 5111
817042 meter/sec
ZDOT = 15509
117010 ZDOT = 4727
178865
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
68323952
00016717 00000-0 10270-3 0 9051
2 25544 51
6443 217
6041 0006781 28
5012 331
6511 15
54289588 6322
Satellite: ISS
Catalog Number: 25544
Epoch time: 15285
68323952 = yrday
fracday
Element set: 905
Inclination: 51
6443 deg
RA of node: 217
6041 deg
Eccentricity:
0006781
Arg of perigee: 28
5012 deg
Mean anomaly: 331
6511 deg
Mean motion: 15
54289588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 632
Checksum: 307
Coasting Arc #7 (Orbit 646)
---------------------------------------
Vector Time (GMT): 2015/286/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1170013
71 A = 6780195
96 meter
Y = 4949222
51 meter E =
0015276
Z = -4499725
45 I = 51
43782
XDOT = -6848
253581 Wp = 53
90484
YDOT = -1271
019182 meter/sec RA = 211
84037 deg
ZDOT = -3177
419887 TA = 184
03042
MA = 184
04274
Ha = 222
591 n
mi
Hp = 212
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3838627
65 X = 1136441
78
Y = 16237606
66 feet Y = 4962118
10 meter
Z = -14762878
77 Z = -4494123
79
XDOT = -22468
023561 XDOT = -6818
096713
YDOT = -4170
010439 feet/sec YDOT = -1347
432649 meter/sec
ZDOT = -10424
605928 ZDOT = -3210
614658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16446978
15 X = -5013038
94
Y = -2929361
01 feet Y = -892869
23 meter
Z = -14739514
10 Z = -4492603
90
XDOT = 12614
628247 XDOT = 3844
938690
YDOT = -17632
468002 feet/sec YDOT = -5374
376247 meter/sec
ZDOT = -10567
545017 ZDOT = -3220
987721
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
64765352
00016717 00000-0 10270-3 0 9063
2 25544 51
6445 212
7951 0006677 30
4867 329
6673 15
54335313 6474
Satellite: ISS
Catalog Number: 25544
Epoch time: 15286
64765352 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 212
7951 deg
Eccentricity:
0006677
Arg of perigee: 30
4867 deg
Mean anomaly: 329
6673 deg
Mean motion: 15
54335313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 647
Checksum: 331
Coasting Arc #8 (Orbit 662)
---------------------------------------
Vector Time (GMT): 2015/287/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 530332
83 A = 6777300
78 meter
Y = -4344960
42 meter E =
0007991
Z = 5167139
59 I = 51
45599
XDOT = 7155
875199 Wp = 68
62494
YDOT = 2441
186281 meter/sec RA = 206
82901 deg
ZDOT = 1319
516945 TA = 8
68395
MA = 8
67013
Ha = 222
602 n
mi
Hp = 212
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1739937
12 X = 553779
22
Y = -14255119
49 feet Y = -4338898
22 meter
Z = 16952557
69 Z = 5169773
33
XDOT = 23477
280835 XDOT = 7121
635548
YDOT = 8009
141343 feet/sec YDOT = 2521
016698 meter/sec
ZDOT = 4329
123834 ZDOT = 1354
196151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12516204
52 X = 3814939
14
Y = 7012252
63 feet Y = 2137334
60 meter
Z = 16964609
12 Z = 5170812
86
XDOT = -15936
539771 XDOT = -4857
457322
YDOT = 17620
584512 feet/sec YDOT = 5370
754159 meter/sec
ZDOT = 4478
290512 ZDOT = 1364
982948
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
67634715
00016717 00000-0 10270-3 0 9076
2 25544 51
6445 207
6652 0006680 35
1232 325
0361 15
54353272 6633
Satellite: ISS
Catalog Number: 25544
Epoch time: 15287
67634715 = yrday
fracday
Element set: 907
Inclination: 51
6445 deg
RA of node: 207
6652 deg
Eccentricity:
0006680
Arg of perigee: 35
1232 deg
Mean anomaly: 325
0361 deg
Mean motion: 15
54353272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 663
Checksum: 303
Coasting Arc #9 (Orbit 677)
---------------------------------------
Vector Time (GMT): 2015/288/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2291057
16 A = 6776726
10 meter
Y = 3606233
38 meter E =
0019053
Z = -5276022
91 I = 51
48260
XDOT = -6852
514120 Wp = 78
35263
YDOT = -3341
063693 meter/sec RA = 201
81406 deg
ZDOT = 697
874520 TA = 198
30377
MA = 198
37243
Ha = 222
592 n
mi
Hp = 212
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7516591
75 X = -2305583
11
Y = 11831474
34 feet Y = 3580531
55 meter
Z = -17309786
46 Z = -5287188
31
XDOT = -22482
001707 XDOT = -6818
034328
YDOT = -10961
495055 feet/sec YDOT = -3417
500171 meter/sec
ZDOT = 2289
614567 ZDOT = 664
669620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8244601
73 X = -2512954
61
Y = -11261440
41 feet Y = -3432487
04 meter
Z = -17358517
97 Z = -5290876
28
XDOT = 17694
145731 XDOT = 5393
175619
YDOT = -16233
575247 feet/sec YDOT = -4947
993735 meter/sec
ZDOT = 2146
935238 ZDOT = 654
385861
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
64073122
00016717 00000-0 10270-3 0 9084
2 25544 51
6438 202
8554 0006640 37
4166 322
7448 15
54393945 6787
Satellite: ISS
Catalog Number: 25544
Epoch time: 15288
64073122 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 202
8554 deg
Eccentricity:
0006640
Arg of perigee: 37
4166 deg
Mean anomaly: 322
7448 deg
Mean motion: 15
54393945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 678
Checksum: 325
Coasting Arc #10 (Orbit 693)
---------------------------------------
Vector Time (GMT): 2015/289/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3973756
18 A = 6778725
39 meter
Y = -2744808
93 meter E =
0013830
Z = 4750951
92 I = 51
51975
XDOT = 5972
322504 Wp = 51
89204
YDOT = 4014
306669 meter/sec RA = 196
80389 deg
ZDOT = -2662
457428 TA = 64
49192
MA = 64
34896
Ha = 222
451 n
mi
Hp = 212
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13037257
80 X = 3981075
07
Y = -9005278
65 feet Y = -2700330
47 meter
Z = 15587112
61 Z = 4770274
10
XDOT = 19594
233937 XDOT = 5939
923192
YDOT = 13170
297470 feet/sec YDOT = 4080
911752 meter/sec
ZDOT = -8735
096550 ZDOT = -2633
523388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3833961
74 X = 1168591
54
Y = 15288785
38 feet Y = 4660021
78 meter
Z = 15670896
36 Z = 4776489
21
XDOT = -18164
120139 XDOT = -5536
423818
YDOT = 13426
802261 feet/sec YDOT = 4092
489329 meter/sec
ZDOT = -8610
931146 ZDOT = -2624
611813
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
66939087
00016717 00000-0 10270-3 0 9099
2 25544 51
6437 197
7254 0006589 40
2192 319
9447 15
54441624 6941
Satellite: ISS
Catalog Number: 25544
Epoch time: 15289
66939087 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 197
7254 deg
Eccentricity:
0006589
Arg of perigee: 40
2192 deg
Mean anomaly: 319
9447 deg
Mean motion: 15
54441624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 694
Checksum: 354
Coasting Arc #11 (Orbit 708)
---------------------------------------
Vector Time (GMT): 2015/290/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5359219
40 A = 6782506
83 meter
Y = 1887815
92 meter E =
0010828
Z = -3709569
53 I = 51
56177
XDOT = -4530
998968 Wp = 71
73397
YDOT = -4435
391580 meter/sec RA = 191
80401 deg
ZDOT = 4302
398155 TA = 244
00495
MA = 244
11652
Ha = 222
549 n
mi
Hp = 212
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17582740
80 X = -5361911
01
Y = 6193621
77 feet Y = 1827870
30 meter
Z = -12170503
69 Z = -3735610
79
XDOT = -14865
482178 XDOT = -4501
964474
YDOT = -14551
809645 feet/sec YDOT = -4485
897574 meter/sec
ZDOT = 14115
479511 ZDOT = 4280
457783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 94268
78 X = 28733
12
Y = -18567452
40 feet Y = -5659359
49 meter
Z = -12283147
39 Z = -3743903
32
XDOT = 17397
976095 XDOT = 5302
903114
YDOT = -9158
151427 feet/sec YDOT = -2791
404555 meter/sec
ZDOT = 14021
537128 ZDOT = 4273
764517
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
63374608
00016717 00000-0 10270-3 0 9102
2 25544 51
6424 192
9152 0006535 43
9971 316
1701 15
54430679 7094
Satellite: ISS
Catalog Number: 25544
Epoch time: 15290
63374608 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 192
9152 deg
Eccentricity:
0006535
Arg of perigee: 43
9971 deg
Mean anomaly: 316
1701 deg
Mean motion: 15
54430679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 709
Checksum: 310
Coasting Arc #12 (Orbit 724)
---------------------------------------
Vector Time (GMT): 2015/291/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6344035
64 A = 6786218
88 meter
Y = -984182
94 meter E =
0018009
Z = 2183676
57 I = 51
60590
XDOT = 2625
141377 Wp = 90
20698
YDOT = 4684
357813 meter/sec RA = 186
81831 deg
ZDOT = -5476
331224 TA = 65
53355
MA = 65
34582
Ha = 222
570 n
mi
Hp = 212
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20813765
22 X = 6343961
82
Y = -3228946
65 feet Y = -913240
04 meter
Z = 7164293
20 Z = 2214495
12
XDOT = 8612
668559 XDOT = 2599
167110
YDOT = 15368
627996 feet/sec YDOT = 4713
568331 meter/sec
ZDOT = -17966
965959 ZDOT = -5463
641915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3632009
08 X = -1107036
37
Y = 20700777
66 feet Y = 6309597
03 meter
Z = 7297419
44 Z = 2224253
44
XDOT = -15849
405406 XDOT = -4830
898768
YDOT = 3578
136521 feet/sec YDOT = 1090
616012 meter/sec
ZDOT = -17912
965620 ZDOT = -5459
871921
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
66237417
00016717 00000-0 10270-3 0 9113
2 25544 51
6424 187
7848 0006627 47
2754 312
8956 15
54478126 7258
Satellite: ISS
Catalog Number: 25544
Epoch time: 15291
66237417 = yrday
fracday
Element set: 911
Inclination: 51
6424 deg
RA of node: 187
7848 deg
Eccentricity:
0006627
Arg of perigee: 47
2754 deg
Mean anomaly: 312
8956 deg
Mean motion: 15
54478126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 725
Checksum: 335
Coasting Arc #13 (Orbit 739)
---------------------------------------
Vector Time (GMT): 2015/292/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6764646
85 A = 6788253
08 meter
Y = 135216
66 meter E =
0017514
Z = -445555
00 I = 51
64281
XDOT = -479
706192 Wp = 45
53022
YDOT = -4762
268713 meter/sec RA = 181
84213 deg
ZDOT = 5995
122500 TA = 309
66295
MA = 309
81732
Ha = 222
590 n
mi
Hp = 212
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22193723
28 X = -6763491
74
Y = 443624
22 feet Y = 59576
36 meter
Z = -1461794
63 Z = -478414
06
XDOT = -1573
839212 XDOT = -455
540212
YDOT = -15624
241183 feet/sec YDOT = -4767
497654 meter/sec
ZDOT = 19669
037074 ZDOT = 5992
851103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6359876
37 X = 1938490
32
Y = -21257361
35 feet Y = -6479243
74 meter
Z = -1603608
42 Z = -488779
85
XDOT = 13843
923755 XDOT = 4219
627960
YDOT = 2694
254426 feet/sec YDOT = 821
208749 meter/sec
ZDOT = 19659
996756 ZDOT = 5992
367011
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
62669876
00016717 00000-0 10270-3 0 9129
2 25544 51
6410 182
9739 0006504 50
9428 309
2302 15
54463935 7406
Satellite: ISS
Catalog Number: 25544
Epoch time: 15292
62669876 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 182
9739 deg
Eccentricity:
0006504
Arg of perigee: 50
9428 deg
Mean anomaly: 309
2302 deg
Mean motion: 15
54463935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 740
Checksum: 319
Coasting Arc #14 (Orbit 755)
---------------------------------------
Vector Time (GMT): 2015/293/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6596109
74 A = 6787483
14 meter
Y = 755504
80 meter E =
0011065
Z = -1409632
07 I = 51
67191
XDOT = -1767
527760 Wp = 107
20746
YDOT = 4687
919555 meter/sec RA = 176
87134 deg
ZDOT = -5799
090112 TA = 88
14462
MA = 88
01789
Ha = 222
637 n
mi
Hp = 212
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21640779
99 X = 6594018
82
Y = 2478690
28 feet Y = 829255
07 meter
Z = -4624777
12 Z = -1377594
15
XDOT = -5798
975591 XDOT = -1791
647674
YDOT = 15380
313501 feet/sec YDOT = 4668
018685 meter/sec
ZDOT = -19025
886195 ZDOT = -5807
735397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8641392
50 X = -2633896
43
Y = 20026290
48 feet Y = 6104013
34 meter
Z = -4486630
41 Z = -1367524
95
XDOT = -11618
200624 XDOT = -3541
227550
YDOT = -9253
393667 feet/sec YDOT = -2820
434390 meter/sec
ZDOT = -19063
945924 ZDOT = -5810
690718
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
65529587
00016717 00000-0 10270-3 0 9138
2 25544 51
6406 177
8431 0006450 55
1906 304
9853 15
54488524 7562
Satellite: ISS
Catalog Number: 25544
Epoch time: 15293
65529587 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 177
8431 deg
Eccentricity:
0006450
Arg of perigee: 55
1906 deg
Mean anomaly: 304
9853 deg
Mean motion: 15
54488524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 756
Checksum: 334
Coasting Arc #15 (Orbit 771)
---------------------------------------
Vector Time (GMT): 2015/294/15:01:05
188
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5831366
73 A = 6784276
74 meter
Y = -1604734
47 meter E =
0019043
Z = 3051856
09 I = 51
69284
XDOT = 3821
770992 Wp = 75
92266
YDOT = -4476
122906 meter/sec RA = 171
89527 deg
ZDOT = 4927
634788 TA = 319
11362
MA = 319
25631
Ha = 222
602 n
mi
Hp = 211
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19131780
60 X = -5827813
74
Y = -5264876
88 feet Y = -1669924
58 meter
Z = 10012651
22 Z = 3023536
87
XDOT = 12538
618739 XDOT = 3847
603165
YDOT = -14685
442604 feet/sec YDOT = -4433
240554 meter/sec
ZDOT = 16166
780799 ZDOT = 4946
263484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10300654
47 X = 3139639
48
Y = -17031389
85 feet Y = -5191167
63 meter
Z = 9890673
35 Z = 3014677
24
XDOT = 9492
940097 XDOT = 2893
448141
YDOT = 15217
954033 feet/sec YDOT = 4638
432389 meter/sec
ZDOT = 16247
902268 ZDOT = 4952
360611
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
68387568
00016717 00000-0 10270-3 0 9144
2 25544 51
6401 172
7111 0006309 59
0675 301
1097 15
54540116 7728
Satellite: ISS
Catalog Number: 25544
Epoch time: 15294
68387568 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 172
7111 deg
Eccentricity:
0006309
Arg of perigee: 59
0675 deg
Mean anomaly: 301
1097 deg
Mean motion: 15
54540116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 772
Checksum: 306
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