[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 28th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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 874)
---------------------------------------
Vector Time (GMT): 2015/301/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4996566
61 A = 6787825
76 meter
Y = 4585027
47 meter E =
0017481
Z = -32454
60 I = 51
90175
XDOT = -3212
709615 Wp = 57
71738
YDOT = -3475
163106 meter/sec RA = 137
67439 deg
ZDOT = 6036
022730 TA = 301
93418
MA = 302
10407
Ha = 222
479 n
mi
Hp = 211
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16392935
06 X = -5047308
49
Y = 15042741
05 feet Y = 4528868
85 meter
Z = -106478
33 Z = -56851
12
XDOT = -10540
385877 XDOT = -3202
932272
YDOT = -11401
453761 feet/sec YDOT = -3511
034753 meter/sec
ZDOT = 19803
224179 ZDOT = 6020
439511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4816322
19 X = 1468015
00
Y = -21720532
98 feet Y = -6620418
45 meter
Z = -212611
11 Z = -64803
87
XDOT = 13689
834973 XDOT = 4172
661700
YDOT = 2880
607340 feet/sec YDOT = 878
009117 meter/sec
ZDOT = 19736
498036 ZDOT = 6015
684601
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 15301
49813815
00016717 00000-0 10270-3 0 9006
2 25544 51
6395 138
7341 0006315 81
3644 278
8224 15
54645042 8758
Satellite: ISS
Catalog Number: 25544
Epoch time: 15301
49813815 = yrday
fracday
Element set: 900
Inclination: 51
6395 deg
RA of node: 138
7341 deg
Eccentricity:
0006315
Arg of perigee: 81
3644 deg
Mean anomaly: 278
8224 deg
Mean motion: 15
54645042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 875
Checksum: 308
Coasting Arc #2 (Orbit 890)
---------------------------------------
Vector Time (GMT): 2015/302/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5387836
46 A = 6786295
46 meter
Y = -3678054
49 meter E =
0011985
Z = -1867385
64 I = 51
91959
XDOT = 1443
299385 Wp = 115
49449
YDOT = 4968
483257 meter/sec RA = 132
71897 deg
ZDOT = -5655
058915 TA = 84
96939
MA = 84
83260
Ha = 222
478 n
mi
Hp = 211
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17676628
80 X = 5437636
21
Y = -12067107
92 feet Y = -3617525
77 meter
Z = -6126593
32 Z = -1841090
83
XDOT = 4735
234203 XDOT = 1415
104193
YDOT = 16300
798087 feet/sec YDOT = 4984
465357 meter/sec
ZDOT = -18553
342896 ZDOT = -5648
116106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7259737
77 X = -2212768
07
Y = 20168311
55 feet Y = 6147301
36 meter
Z = -6012392
33 Z = -1832577
18
XDOT = -12025
724958 XDOT = -3665
440967
YDOT = -9817
878915 feet/sec YDOT = -2992
489493 meter/sec
ZDOT = -18524
191210 ZDOT = -5646
173481
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 15302
52661421
00016717 00000-0 10270-3 0 9016
2 25544 51
6392 133
6021 0006329 84
9533 275
2342 15
54680154 8918
Satellite: ISS
Catalog Number: 25544
Epoch time: 15302
52661421 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 133
6021 deg
Eccentricity:
0006329
Arg of perigee: 84
9533 deg
Mean anomaly: 275
2342 deg
Mean motion: 15
54680154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 891
Checksum: 288
Coasting Arc #3 (Orbit 906)
---------------------------------------
Vector Time (GMT): 2015/303/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5298285
15 A = 6782556
91 meter
Y = 2387847
38 meter E =
0018546
Z = 3481266
51 I = 51
92805
XDOT = 241
409264 Wp = 90
56584
YDOT = -6160
379309 meter/sec RA = 127
75566 deg
ZDOT = 4571
761157 TA = 310
18483
MA = 310
34704
Ha = 222
435 n
mi
Hp = 211
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17382825
29 X = -5341503
92
Y = 7834144
95 feet Y = 2328356
87 meter
Z = 11421478
06 Z = 3455422
88
XDOT = 792
025144 XDOT = 288
069784
YDOT = -20211
218205 feet/sec YDOT = -6157
418739 meter/sec
ZDOT = 14999
216395 ZDOT = 4573
047345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9246755
94 X = 2818411
21
Y = -16750552
08 feet Y = -5105568
27 meter
Z = 11309425
83 Z = 3447112
99
XDOT = 10363
869365 XDOT = 3158
907382
YDOT = 15899
861308 feet/sec YDOT = 4846
277727 meter/sec
ZDOT = 15005
824345 ZDOT = 4573
775260
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 15303
55507230
00016717 00000-0 10270-3 0 9028
2 25544 51
6389 128
4692 0006207 89
6430 270
5434 15
54722864 9076
Satellite: ISS
Catalog Number: 25544
Epoch time: 15303
55507230 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 128
4692 deg
Eccentricity:
0006207
Arg of perigee: 89
6430 deg
Mean anomaly: 270
5434 deg
Mean motion: 15
54722864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 907
Checksum: 308
Coasting Arc #4 (Orbit 921)
---------------------------------------
Vector Time (GMT): 2015/304/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4843279
47 A = 6778325
14 meter
Y = -717490
28 meter E =
0016737
Z = -4703232
48 I = 51
93282
XDOT = -1759
260011 Wp = 79
03721
YDOT = 6877
952202 meter/sec RA = 122
78175 deg
ZDOT = -2866
435868 TA = 162
59650
MA = 162
53906
Ha = 222
414 n
mi
Hp = 211
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15890024
50 X = 4873789
62
Y = -2353970
72 feet Y = -663159
00 meter
Z = -15430552
74 Z = -4679630
21
XDOT = -5771
850429 XDOT = -1822
115866
YDOT = 22565
459981 feet/sec YDOT = 6857
927511 meter/sec
ZDOT = -9404
317153 ZDOT = -2875
134934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11166815
56 X = -3403645
38
Y = 11682324
01 feet Y = 3560772
36 meter
Z = -15328455
59 Z = -4672113
26
XDOT = -8506
721657 XDOT = -2592
848761
YDOT = -20497
669557 feet/sec YDOT = -6247
689681 meter/sec
ZDOT = -9443
088353 ZDOT = -2878
253330
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 15304
51923801
00016717 00000-0 10270-3 0 9032
2 25544 51
6388 123
6576 0006454 92
6502 267
5390 15
54737889 9228
Satellite: ISS
Catalog Number: 25544
Epoch time: 15304
51923801 = yrday
fracday
Element set: 903
Inclination: 51
6388 deg
RA of node: 123
6576 deg
Eccentricity:
0006454
Arg of perigee: 92
6502 deg
Mean anomaly: 267
5390 deg
Mean motion: 15
54737889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 922
Checksum: 324
Coasting Arc #5 (Orbit 937)
---------------------------------------
Vector Time (GMT): 2015/305/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4082407
06 A = 6775869
50 meter
Y = -1124332
33 meter E =
0009544
Z = 5282126
16 I = 51
94093
XDOT = 2986
971818 Wp = 104
02462
YDOT = -7025
187466 meter/sec RA = 117
79797 deg
ZDOT = 809
717652 TA = 338
25657
MA = 338
29706
Ha = 222
587 n
mi
Hp = 211
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13393723
96 X = -4095190
07
Y = -3688754
38 feet Y = -1170055
88 meter
Z = 17329810
24 Z = 5262263
29
XDOT = 9799
776305 XDOT = 3061
373812
YDOT = -23048
515309 feet/sec YDOT = -6991
369157 meter/sec
ZDOT = 2656
553978 ZDOT = 824
408848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12825211
65 X = 3909124
51
Y = -5610104
93 feet Y = -1709959
98 meter
Z = 17244179
95 Z = 5256026
05
XDOT = 6450
123653 XDOT = 1965
997690
YDOT = 23145
319459 feet/sec YDOT = 7054
693371 meter/sec
ZDOT = 2721
257806 ZDOT = 829
439379
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 15305
54766471
00016717 00000-0 10270-3 0 9045
2 25544 51
6388 118
5250 0006450 96
0295 264
1593 15
54712576 9384
Satellite: ISS
Catalog Number: 25544
Epoch time: 15305
54766471 = yrday
fracday
Element set: 904
Inclination: 51
6388 deg
RA of node: 118
5250 deg
Eccentricity:
0006450
Arg of perigee: 96
0295 deg
Mean anomaly: 264
1593 deg
Mean motion: 15
54712576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 938
Checksum: 323
Coasting Arc #6 (Orbit 952)
---------------------------------------
Vector Time (GMT): 2015/306/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3157477
76 A = 6776066
84 meter
Y = 3002804
37 meter E =
0020414
Z = -5207306
09 I = 51
95684
XDOT = -3878
716820 Wp = 100
48784
YDOT = 6454
535560 meter/sec RA = 112
81183 deg
ZDOT = 1371
086702 TA = 182
65397
MA = 182
66482
Ha = 222
330 n
mi
Hp = 211
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10359179
02 X = 3148960
47
Y = 9851720
38 feet Y = 3038065
60 meter
Z = -17084337
57 Z = -5191988
26
XDOT = -12725
448886 XDOT = -3957
265047
YDOT = 21176
297769 feet/sec YDOT = 6410
722041 meter/sec
ZDOT = 4498
315950 ZDOT = 1352
053430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14348954
97 X = -4373561
47
Y = -846089
29 feet Y = -257888
01 meter
Z = -17018672
07 Z = -5187291
25
XDOT = -3853
953296 XDOT = -1174
684965
YDOT = -23381
810542 feet/sec YDOT = -7126
775853 meter/sec
ZDOT = 4414
932509 ZDOT = 1345
671429
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 15306
51179638
00016717 00000-0 10270-3 0 9057
2 25544 51
6394 113
7134 0006479 100
4051 259
7833 15
54779539 9536
Satellite: ISS
Catalog Number: 25544
Epoch time: 15306
51179638 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 113
7134 deg
Eccentricity:
0006479
Arg of perigee: 100
4051 deg
Mean anomaly: 259
7833 deg
Mean motion: 15
54779539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 953
Checksum: 327
Coasting Arc #7 (Orbit 968)
---------------------------------------
Vector Time (GMT): 2015/307/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2118617
82 A = 6779184
04 meter
Y = -4679329
49 meter E =
0015140
Z = 4412083
45 I = 51
97848
XDOT = 4472
038546 Wp = 83
91849
YDOT = -5235
899950 meter/sec RA = 107
83191 deg
ZDOT = -3394
119790 TA = 40
27837
MA = 40
16631
Ha = 222
358 n
mi
Hp = 211
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6950845
87 X = -2087567
46
Y = -15352130
88 feet Y = -4702847
48 meter
Z = 14475339
39 Z = 4401867
10
XDOT = 14672
042474 XDOT = 4546
742843
YDOT = -17178
149442 feet/sec YDOT = -5185
473110 meter/sec
ZDOT = -11135
563616 ZDOT = -3372
213567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15370652
94 X = 4684975
02
Y = 6999823
63 feet Y = 2133546
24 meter
Z = 14432017
48 Z = 4398878
93
XDOT = 602
527732 XDOT = 183
650453
YDOT = 21516
935120 feet/sec YDOT = 6558
361825 meter/sec
ZDOT = -11039
964840 ZDOT = -3364
981283
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 15307
54018750
00016717 00000-0 10270-3 0 9069
2 25544 51
6389 108
5808 0006412 103
9438 256
2428 15
54786755 9691
Satellite: ISS
Catalog Number: 25544
Epoch time: 15307
54018750 = yrday
fracday
Element set: 906
Inclination: 51
6389 deg
RA of node: 108
5808 deg
Eccentricity:
0006412
Arg of perigee: 103
9438 deg
Mean anomaly: 256
2428 deg
Mean motion: 15
54786755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 969
Checksum: 334
Coasting Arc #8 (Orbit 983)
---------------------------------------
Vector Time (GMT): 2015/308/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1096952
58 A = 6783302
08 meter
Y = 5955468
67 meter E =
0010523
Z = -3066294
13 I = 52
00274
XDOT = -4746
062212 Wp = 93
25462
YDOT = 3415
263356 meter/sec RA = 102
86486 deg
ZDOT = 4949
394220 TA = 231
76841
MA = 231
86318
Ha = 222
227 n
mi
Hp = 211
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3598925
79 X = 1045170
64
Y = 19538939
22 feet Y = 5967445
83 meter
Z = -10060020
13 Z = -3061091
38
XDOT = -15571
070250 XDOT = -4807
942382
YDOT = 11204
932269 feet/sec YDOT = 3361
844026 meter/sec
ZDOT = 16238
170014 ZDOT = 4926
188005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15765040
04 X = -4805184
20
Y = -12108528
36 feet Y = -3690679
44 meter
Z = -10038599
06 Z = -3059764
99
XDOT = 3314
733964 XDOT = 1010
330912
YDOT = -17656
108967 feet/sec YDOT = -5381
582013 meter/sec
ZDOT = 16137
265193 ZDOT = 4918
638431
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 15308
50428756
00016717 00000-0 10270-3 0 9078
2 25544 51
6401 103
7692 0006500 107
3954 252
7910 15
54835316 9845
Satellite: ISS
Catalog Number: 25544
Epoch time: 15308
50428756 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 103
7692 deg
Eccentricity:
0006500
Arg of perigee: 107
3954 deg
Mean anomaly: 252
7910 deg
Mean motion: 15
54835316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 984
Checksum: 307
Coasting Arc #9 (Orbit 999)
---------------------------------------
Vector Time (GMT): 2015/309/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -62358
33 A = 6786509
21 meter
Y = -6660374
31 meter E =
0020009
Z = 1253127
05 I = 52
01917
XDOT = 4794
727318 Wp = 117
78790
YDOT = -1162
503655 meter/sec RA = 97
91023 deg
ZDOT = -5877
857765 TA = 48
64563
MA = 48
47369
Ha = 222
104 n
mi
Hp = 211
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -204587
70 X = 6036
93
Y = -21851621
75 feet Y = -6660689
15 meter
Z = 4111309
20 Z = 1252990
65
XDOT = 15730
732670 XDOT = 4835
923193
YDOT = -3813
988370 feet/sec YDOT = -1108
655868 meter/sec
ZDOT = -19284
310254 ZDOT = -5854
465453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15027130
03 X = 4580269
23
Y = 15865546
34 feet Y = 4835818
52 meter
Z = 4111921
10 Z = 1253313
55
XDOT = -7873
329341 XDOT = -2399
790783
YDOT = 12481
906950 feet/sec YDOT = 3804
485238 meter/sec
ZDOT = -19182
998150 ZDOT = -5846
977836
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 15309
53264256
00016717 00000-0 10270-3 0 9086
2 25544 51
6393 98
6362 0006328 110
2368 249
9466 15
54871584 10002
Satellite: ISS
Catalog Number: 25544
Epoch time: 15309
53264256 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 98
6362 deg
Eccentricity:
0006328
Arg of perigee: 110
2368 deg
Mean anomaly: 249
9466 deg
Mean motion: 15
54871584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1000
Checksum: 322
Coasting Arc #10 (Orbit 1015)
---------------------------------------
Vector Time (GMT): 2015/310/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -878988
81 A = 6786884
23 meter
Y = 6689976
26 meter E =
0017220
Z = 681658
80 I = 52
02562
XDOT = -4622
155132 Wp = 71
72815
YDOT = -1230
219188 meter/sec RA = 92
96234 deg
ZDOT = 5995
081525 TA = 295
59746
MA = 295
77532
Ha = 222
076 n
mi
Hp = 211
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2883821
56 X = -957043
73
Y = 21948741
00 feet Y = 6679710
44 meter
Z = 2236413
38 Z = 677198
75
XDOT = -15164
550958 XDOT = -4637
177333
YDOT = -4036
152193 feet/sec YDOT = -1281
990784 meter/sec
ZDOT = 19668
902641 ZDOT = 5972
591215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13108103
80 X = -3995350
04
Y = -17841875
65 feet Y = -5438203
70 meter
Z = 2215917
74 Z = 675411
73
XDOT = 12523
569323 XDOT = 3817
183930
YDOT = -6721
360454 feet/sec YDOT = -2048
670666 meter/sec
ZDOT = 19571
920580 ZDOT = 5965
521393
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 15310
56098014
00016717 00000-0 10270-3 0 9099
2 25544 51
6407 93
5039 0006489 114
5984 245
5846 15
54904124 10160
Satellite: ISS
Catalog Number: 25544
Epoch time: 15310
56098014 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 93
5039 deg
Eccentricity:
0006489
Arg of perigee: 114
5984 deg
Mean anomaly: 245
5846 deg
Mean motion: 15
54904124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1016
Checksum: 313
Coasting Arc #11 (Orbit 1030)
---------------------------------------
Vector Time (GMT): 2015/311/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1815146
72 A = 6784200
41 meter
Y = -6001364
75 meter E =
0011467
Z = -2590149
89 I = 52
01746
XDOT = 4255
865086 Wp = 121
82048
YDOT = 3560
038850 meter/sec RA = 88
01071 deg
ZDOT = -5289
124360 TA = 87
15356
MA = 87
02233
Ha = 222
013 n
mi
Hp = 211
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5955205
78 X = 1894702
76
Y = -19689516
90 feet Y = -5980621
93 meter
Z = -8497867
09 Z = -2581138
47
XDOT = 13962
811961 XDOT = 4241
432642
YDOT = 11679
917486 feet/sec YDOT = 3607
549706 meter/sec
ZDOT = -17352
770210 ZDOT = -5268
485077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9613936
78 X = 2930327
93
Y = 18204200
53 feet Y = 5548640
32 meter
Z = -8457812
92 Z = -2577941
38
XDOT = -16887
281362 XDOT = -5147
243359
YDOT = 932
572773 feet/sec YDOT = 284
248181 meter/sec
ZDOT = -17264
218985 ZDOT = -5262
133947
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 15311
52502993
00016717 00000-0 10270-3 0 9104
2 25544 51
6406 88
6916 0006389 116
7410 243
4398 15
54921271 10313
Satellite: ISS
Catalog Number: 25544
Epoch time: 15311
52502993 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 88
6916 deg
Eccentricity:
0006389
Arg of perigee: 116
7410 deg
Mean anomaly: 243
4398 deg
Mean motion: 15
54921271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1031
Checksum: 301
Coasting Arc #12 (Orbit 1046)
---------------------------------------
Vector Time (GMT): 2015/312/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2650071
96 A = 6779817
94 meter
Y = 4700160
16 meter E =
0016735
Z = 4095498
62 I = 52
00224
XDOT = -3716
284172 Wp = 109
52061
YDOT = -5485
278324 meter/sec RA = 83
04785 deg
ZDOT = 3872
161897 TA = 300
58339
MA = 300
74838
Ha = 221
915 n
mi
Hp = 211
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8694461
82 X = -2722328
19
Y = 15420472
98 feet Y = 4670121
54 meter
Z = 13436675
27 Z = 4082449
01
XDOT = -12192
533374 XDOT = -3673
480182
YDOT = -17996
319959 feet/sec YDOT = -5526
596706 meter/sec
ZDOT = 12703
943232 ZDOT = 3854
212799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4933817
74 X = -1503827
65
Y = -17046351
17 feet Y = -5195727
84 meter
Z = 13379396
47 Z = 4078040
04
XDOT = 20214
338220 XDOT = 6161
330289
YDOT = 4107
531750 feet/sec YDOT = 1251
975677 meter/sec
ZDOT = 12627
385681 ZDOT = 3848
827155
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 15312
55333043
00016717 00000-0 10270-3 0 9117
2 25544 51
6416 83
5590 0006322 121
2018 238
9755 15
54970030 10478
Satellite: ISS
Catalog Number: 25544
Epoch time: 15312
55333043 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 83
5590 deg
Eccentricity:
0006322
Arg of perigee: 121
2018 deg
Mean anomaly: 238
9755 deg
Mean motion: 15
54970030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1047
Checksum: 279
Coasting Arc #13 (Orbit 1061)
---------------------------------------
Vector Time (GMT): 2015/313/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3449450
52 A = 6776052
36 meter
Y = -2889635
76 meter E =
0017944
Z = -5081550
91 I = 51
98544
XDOT = 2943
222748 Wp = 90
77357
YDOT = 6813
195767 meter/sec RA = 78
07158 deg
ZDOT = -1882
387336 TA = 161
07721
MA = 161
01044
Ha = 221
822 n
mi
Hp = 211
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11317094
89 X = 3506191
65
Y = -9480432
28 feet Y = -2850744
72 meter
Z = -16671754
95 Z = -5064655
76
XDOT = 9656
242612 XDOT = 2875
961343
YDOT = 22353
004485 feet/sec YDOT = 6845
732654 meter/sec
ZDOT = -6175
811469 ZDOT = -1868
253081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -912363
76 X = -278088
47
Y = 14817910
65 feet Y = 4516499
17 meter
Z = -16598185
51 Z = -5059126
94
XDOT = -21848
222600 XDOT = -6659
338248
YDOT = -8174
029820 feet/sec YDOT = -2491
444289 meter/sec
ZDOT = -6116
005925 ZDOT = -1864
158606
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 15313
51734685
00016717 00000-0 10270-3 0 9122
2 25544 51
6422 78
7477 0006263 123
1639 237
0116 15
54971252 10624
Satellite: ISS
Catalog Number: 25544
Epoch time: 15313
51734685 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 78
7477 deg
Eccentricity:
0006263
Arg of perigee: 123
1639 deg
Mean anomaly: 237
0116 deg
Mean motion: 15
54971252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1062
Checksum: 300
Coasting Arc #14 (Orbit 1077)
---------------------------------------
Vector Time (GMT): 2015/314/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4098335
64 A = 6774815
21 meter
Y = 831449
49 meter E =
0008045
Z = 5323543
21 I = 51
97501
XDOT = -1963
135073 Wp = 111
01897
YDOT = -7412
509504 meter/sec RA = 73
08578 deg
ZDOT = -355
990375 TA = 342
34207
MA = 342
37002
Ha = 221
842 n
mi
Hp = 211
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13445983
06 X = -4133188
98
Y = 2727852
66 feet Y = 785424
50 meter
Z = 17465692
94 Z = 5303549
07
XDOT = -6440
731867 XDOT = -1878
371362
YDOT = -24319
256902 feet/sec YDOT = -7433
988646 meter/sec
ZDOT = -1167
947424 ZDOT = -365
321021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7091382
34 X = 2161453
34
Y = -11872856
36 feet Y = -3618846
62 meter
Z = 17379115
31 Z = 5297154
35
XDOT = 21464
944954 XDOT = 6542
515222
YDOT = 11065
439454 feet/sec YDOT = 3372
745945 meter/sec
ZDOT = -1206
859336 ZDOT = -367
850725
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 15314
54561198
00016717 00000-0 10270-3 0 9134
2 25544 51
6430 73
6144 0006194 126
1304 234
0423 15
55011204 10781
Satellite: ISS
Catalog Number: 25544
Epoch time: 15314
54561198 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 73
6144 deg
Eccentricity:
0006194
Arg of perigee: 126
1304 deg
Mean anomaly: 234
0423 deg
Mean motion: 15
55011204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1078
Checksum: 269
Coasting Arc #15 (Orbit 1092)
---------------------------------------
Vector Time (GMT): 2015/315/11:57:08
112
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4587934
89 A = 6776882
46 meter
Y = 1259352
13 meter E =
0017416
Z = -4842636
36 I = 51
97244
XDOT = 729
551422 Wp = 115
43418
YDOT = 7178
968608 meter/sec RA = 68
10210 deg
ZDOT = 2557
997633 TA = 179
66416
MA = 179
66299
Ha = 221
619 n
mi
Hp = 211
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15052279
82 X = 4597035
87
Y = 4131732
71 feet Y = 1310708
25 meter
Z = -15887914
56 Z = -4820326
36
XDOT = 2393
541411 XDOT = 636
794085
YDOT = 23553
046613 feet/sec YDOT = 7186
608337 meter/sec
ZDOT = 8392
380687 ZDOT = 2561
316331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13096171
83 X = -3991713
17
Y = 8670624
03 feet Y = 2642806
21 meter
Z = -15791729
93 Z = -4813319
28
XDOT = -18620
087890 XDOT = -5675
402789
YDOT = -12814
692416 feet/sec YDOT = -3905
918249 meter/sec
ZDOT = 8405
334316 ZDOT = 2561
945899
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 15315
50959388
00016717 00000-0 10270-3 0 9144
2 25544 51
6435 68
8034 0006225 129
4318 230
7387 15
55039746 10936
Satellite: ISS
Catalog Number: 25544
Epoch time: 15315
50959388 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 68
8034 deg
Eccentricity:
0006225
Arg of perigee: 129
4318 deg
Mean anomaly: 230
7387 deg
Mean motion: 15
55039746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1093
Checksum: 324
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