[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 6th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
256/03:27:36
190 1
3 1
4 1
4
N/A 0
6 0
0 228
0
000/00:03:12
381 -0
3 0
0 220
1
Coasting Arc #1 (Orbit 700)
---------------------------------------
Vector Time (GMT): 2013/247/11:19:33
929
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2473060
13 A = 6791719
80 meter
Y = 4402113
18 meter E =
0009701
Z = 4533998
38 I = 51
98197
XDOT = -4124
216589 Wp = 90
24461
YDOT = -5616
869434 meter/sec RA = 74
73764 deg
ZDOT = 3198
005871 TA = 327
75800
MA = 327
81727
Ha = 227
893 n
mi
Hp = 219
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8113714
33 X = -2544126
41
Y = 14442628
56 feet Y = 4374060
98 meter
Z = 14875322
77 Z = 4521811
53
XDOT = -13530
894320 XDOT = -4076
635881
YDOT = -18428
049324 feet/sec YDOT = -5662
722668 meter/sec
ZDOT = 10492
145247 ZDOT = 3178
087183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13897995
89 X = 4236109
15
Y = -9099722
15 feet Y = -2773595
31 meter
Z = 14823558
08 Z = 4518220
50
XDOT = 3012
389699 XDOT = 918
176380
YDOT = 21589
562930 feet/sec YDOT = 6580
498781 meter/sec
ZDOT = 10409
324829 ZDOT = 3172
762208
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 13247
52599030
00016717 00000-0 10270-3 0 9007
2 25544 51
6464 75
1920 0003619 24
5395 335
5927 15
50344329 7017
Satellite: ISS
Catalog Number: 25544
Epoch time: 13247
52599030 = yrday
fracday
Element set: 900
Inclination: 51
6464 deg
RA of node: 75
1920 deg
Eccentricity:
0003619
Arg of perigee: 24
5395 deg
Mean anomaly: 335
5927 deg
Mean motion: 15
50344329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 701
Checksum: 298
Coasting Arc #2 (Orbit 715)
---------------------------------------
Vector Time (GMT): 2013/248/11:19:33
929
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2441382
10 A = 6790712
67 meter
Y = -4180975
97 meter E =
0013902
Z = -4775050
78 I = 51
96890
XDOT = 4359
097102 Wp = 61
24255
YDOT = 5663
923027 meter/sec RA = 69
80092 deg
ZDOT = -2730
066787 TA = 181
81730
MA = 181
82236
Ha = 227
788 n
mi
Hp = 219
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8009783
80 X = 2511148
96
Y = -13717112
75 feet Y = -4153285
36 meter
Z = -15666177
10 Z = -4763020
91
XDOT = 14301
499680 XDOT = 4308
699718
YDOT = 18582
424629 feet/sec YDOT = 5712
387108 meter/sec
ZDOT = -8956
912031 ZDOT = -2709
013940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13330302
17 X = -4063076
10
Y = 8730215
01 feet Y = 2660969
53 meter
Z = -15615098
90 Z = -4759482
14
XDOT = -4042
270366 XDOT = -1232
084007
YDOT = -22038
988536 feet/sec YDOT = -6717
483706 meter/sec
ZDOT = -8869
345030 ZDOT = -2703
376365
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 13248
49285784
00016717 00000-0 10270-3 0 9013
2 25544 51
6454 70
3988 0003548 29
5771 330
5580 15
50381040 7168
Satellite: ISS
Catalog Number: 25544
Epoch time: 13248
49285784 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 70
3988 deg
Eccentricity:
0003548
Arg of perigee: 29
5771 deg
Mean anomaly: 330
5580 deg
Mean motion: 15
50381040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 716
Checksum: 315
Coasting Arc #3 (Orbit 731)
---------------------------------------
Vector Time (GMT): 2013/249/11:19:33
929
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2434985
67 A = 6789992
39 meter
Y = 3942328
67 meter E =
0007414
Z = 4956892
40 I = 51
95489
XDOT = -4618
101216 Wp = 92
75216
YDOT = -5690
115092 meter/sec RA = 64
86257 deg
ZDOT = 2253
669142 TA = 335
31399
MA = 335
34946
Ha = 227
990 n
mi
Hp = 219
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7988798
13 X = -2502967
82
Y = 12934149
17 feet Y = 3914719
62 meter
Z = 16262770
33 Z = 4944897
89
XDOT = -15151
250708 XDOT = -4565
077544
YDOT = -18668
356600 feet/sec YDOT = -5741
460880 meter/sec
ZDOT = 7393
927632 ZDOT = 2231
364420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12829027
66 X = 3910287
63
Y = -8257245
23 feet Y = -2516808
35 meter
Z = 16211870
95 Z = 4941378
27
XDOT = 5195
241295 XDOT = 1583
509547
YDOT = 22427
331985 feet/sec YDOT = 6835
850789 meter/sec
ZDOT = 7301
119495 ZDOT = 2225
381222
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 13249
52417919
00016717 00000-0 10270-3 0 9026
2 25544 51
6455 65
2857 0003615 32
5870 327
5504 15
50355174 7325
Satellite: ISS
Catalog Number: 25544
Epoch time: 13249
52417919 = yrday
fracday
Element set: 902
Inclination: 51
6455 deg
RA of node: 65
2857 deg
Eccentricity:
0003615
Arg of perigee: 32
5870 deg
Mean anomaly: 327
5504 deg
Mean motion: 15
50355174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 732
Checksum: 305
Coasting Arc #4 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2013/250/11:19:33
929
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2484783
87 A = 6789207
10 meter
Y = -3715986
13 meter E =
0016256
Z = -5124471
68 I = 51
93862
XDOT = 4851
555967 Wp = 68
96976
YDOT = 5651
538526 meter/sec RA = 59
92319 deg
ZDOT = -1744
528351 TA = 184
18719
MA = 184
20081
Ha = 227
874 n
mi
Hp = 219
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8152178
04 X = 2551045
45
Y = -12191555
55 feet Y = -3687829
84 meter
Z = -16812571
12 Z = -5112239
42
XDOT = 15917
178369 XDOT = 4796
473091
YDOT = 18541
793064 feet/sec YDOT = 5705
483506 meter/sec
ZDOT = -5723
518213 ZDOT = -1721
094427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12532497
59 X = -3819905
26
Y = 7731101
70 feet Y = 2356439
80 meter
Z = -16760702
61 Z = -5108662
15
XDOT = -6375
506802 XDOT = -1943
254473
YDOT = -22540
502796 feet/sec YDOT = -6870
345252 meter/sec
ZDOT = -5625
976840 ZDOT = -1714
797741
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 13250
49103539
00016717 00000-0 10270-3 0 9035
2 25544 51
6454 60
4926 0003571 38
4782 321
6623 15
50401559 7478
Satellite: ISS
Catalog Number: 25544
Epoch time: 13250
49103539 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 60
4926 deg
Eccentricity:
0003571
Arg of perigee: 38
4782 deg
Mean anomaly: 321
6623 deg
Mean motion: 15
50401559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 297
Coasting Arc #5 (Orbit 762)
---------------------------------------
Vector Time (GMT): 2013/251/11:19:33
929
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2563837
39 A = 6788787
10 meter
Y = 3480918
85 meter E =
0005754
Z = 5229235
28 I = 51
92079
XDOT = -5094
851534 Wp = 84
83883
YDOT = -5596
373811 meter/sec RA = 54
98192 deg
ZDOT = 1226
705093 TA = 353
42961
MA = 353
43715
Ha = 228
090 n
mi
Hp = 219
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8411540
00 X = -2627973
53
Y = 11420337
45 feet Y = 3451890
39 meter
Z = 17156283
72 Z = 5216624
17
XDOT = -16715
392172 XDOT = -5037
852015
YDOT = -18360
806466 feet/sec YDOT = -5653
028834 meter/sec
ZDOT = 4024
623010 ZDOT = 1202
093774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12333625
55 X = 3759289
07
Y = -7133737
45 feet Y = -2174363
17 meter
Z = 17102855
16 Z = 5212950
25
XDOT = 7616
588990 XDOT = 2321
536324
YDOT = 22576
788214 feet/sec YDOT = 6881
405047 meter/sec
ZDOT = 3922
145200 ZDOT = 1195
469857
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 13251
52234461
00016717 00000-0 10270-3 0 9040
2 25544 51
6455 55
3795 0003641 41
5018 318
6409 15
50367793 7638
Satellite: ISS
Catalog Number: 25544
Epoch time: 13251
52234461 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 55
3795 deg
Eccentricity:
0003641
Arg of perigee: 41
5018 deg
Mean anomaly: 318
6409 deg
Mean motion: 15
50367793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 763
Checksum: 302
Coasting Arc #6 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2013/252/11:19:33
929
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2692176
25 A = 6788315
54 meter
Y = -3276566
69 meter E =
0017616
Z = -5315931
42 I = 51
90205
XDOT = 5295
882034 Wp = 77
38438
YDOT = 5476
193593 meter/sec RA = 50
04017 deg
ZDOT = -691
516940 TA = 186
00864
MA = 186
02979
Ha = 227
949 n
mi
Hp = 219
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8832599
26 X = 2754438
96
Y = -10749890
71 feet Y = -3246113
46 meter
Z = -17440719
89 Z = -5302701
44
XDOT = 17374
941058 XDOT = 5237
611656
YDOT = 17966
514414 feet/sec YDOT = 5535
089632 meter/sec
ZDOT = -2268
756366 ZDOT = -665
931960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12346505
03 X = -3763214
73
Y = 6564221
56 feet Y = 2000774
73 meter
Z = -17384719
70 Z = -5298862
56
XDOT = -8810
330732 XDOT = -2685
388807
YDOT = -22313
270994 feet/sec YDOT = -6801
084999 meter/sec
ZDOT = -2162
187931 ZDOT = -659
034881
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 13252
48918909
00016717 00000-0 10270-3 0 9053
2 25544 51
6463 50
5870 0003614 47
1958 312
9496 15
50422467 7782
Satellite: ISS
Catalog Number: 25544
Epoch time: 13252
48918909 = yrday
fracday
Element set: 905
Inclination: 51
6463 deg
RA of node: 50
5870 deg
Eccentricity:
0003614
Arg of perigee: 47
1958 deg
Mean anomaly: 312
9496 deg
Mean motion: 15
50422467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 329
Coasting Arc #7 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2013/253/11:19:33
929
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2849756
77 A = 6788271
24 meter
Y = 3071865
47 meter E =
0005672
Z = 5336139
54 I = 51
88084
XDOT = -5492
370220 Wp = 67
53593
YDOT = -5347
284720 meter/sec RA = 45
09577 deg
ZDOT = 147
077529 TA = 21
07853
MA = 21
05516
Ha = 228
177 n
mi
Hp = 219
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9349595
71 X = -2909816
94
Y = 10078298
77 feet Y = 3039662
30 meter
Z = 17507019
48 Z = 5322149
45
XDOT = -18019
587336 XDOT = -5432
881971
YDOT = -17543
585041 feet/sec YDOT = -5408
371262 meter/sec
ZDOT = 482
537824 ZDOT = 120
540849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12470304
81 X = 3800948
91
Y = -5962098
46 feet Y = -1817247
61 meter
Z = 17447855
38 Z = 5318106
32
XDOT = 9995
926820 XDOT = 3046
758495
YDOT = 21976
849785 feet/sec YDOT = 6698
543815 meter/sec
ZDOT = 371
968457 ZDOT = 113
375986
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 13253
52048584
00016717 00000-0 10270-3 0 9063
2 25544 51
6461 45
4739 0003694 50
3662 309
7814 15
50383761 7942
Satellite: ISS
Catalog Number: 25544
Epoch time: 13253
52048584 = yrday
fracday
Element set: 906
Inclination: 51
6461 deg
RA of node: 45
4739 deg
Eccentricity:
0003694
Arg of perigee: 50
3662 deg
Mean anomaly: 309
7814 deg
Mean motion: 15
50383761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 794
Checksum: 319
Coasting Arc #8 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2013/254/11:19:33
929
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3044247
16 A = 6788172
23 meter
Y = -2914389
99 meter E =
0017763
Z = -5336699
91 I = 51
85981
XDOT = 5632
718835 Wp = 85
65056
YDOT = 5160
250448 meter/sec RA = 40
15155 deg
ZDOT = 397
527617 TA = 188
12362
MA = 188
15242
Ha = 228
003 n
mi
Hp = 219
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9987687
53 X = 3102534
63
Y = -9561646
94 feet Y = -2880021
72 meter
Z = -17508857
99 Z = -5321769
40
XDOT = 18480
048672 XDOT = 5572
666054
YDOT = 16929
955537 feet/sec YDOT = 5222
903337 meter/sec
ZDOT = 1304
224464 ZDOT = 424
744802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12785322
81 X = -3896966
39
Y = 5469903
51 feet Y = 1667226
59 meter
Z = -17445766
79 Z = -5317469
72
XDOT = -11058
118197 XDOT = -3370
514426
YDOT = -21351
399977 feet/sec YDOT = -6507
906713 meter/sec
ZDOT = 1417
667696 ZDOT = 432
105114
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 13254
48731807
00016717 00000-0 10270-3 0 9077
2 25544 51
6473 40
6821 0003658 54
9913 305
1581 15
50442884 8093
Satellite: ISS
Catalog Number: 25544
Epoch time: 13254
48731807 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 40
6821 deg
Eccentricity:
0003658
Arg of perigee: 54
9913 deg
Mean anomaly: 305
1581 deg
Mean motion: 15
50442884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 314
Coasting Arc #9 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2013/255/11:19:33
929
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3264193
98 A = 6788531
81 meter
Y = 2763123
21 meter E =
0007326
Z = 5267224
24 I = 51
83606
XDOT = -5754
994058 Wp = 57
76900
YDOT = -4975
533721 meter/sec RA = 35
20384 deg
ZDOT = -951
591645 TA = 41
34142
MA = 41
28599
Ha = 228
232 n
mi
Hp = 219
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10709297
84 X = -3320436
03
Y = 9065364
86 feet Y = 2726306
73 meter
Z = 17280919
43 Z = 5251230
30
XDOT = -18881
214100 XDOT = -5694
306239
YDOT = -16323
929531 feet/sec YDOT = -5039
550443 meter/sec
ZDOT = -3122
019832 ZDOT = -979
401278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13205043
77 X = 4024897
34
Y = -4982597
08 feet Y = -1518695
59 meter
Z = 17213384
96 Z = 5246639
74
XDOT = 12043
465316 XDOT = 3670
848228
YDOT = 20677
422870 feet/sec YDOT = 6302
478491 meter/sec
ZDOT = -3237
970043 ZDOT = -986
933269
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 13255
51860179
00016717 00000-0 10270-3 0 9088
2 25544 51
6468 35
5688 0003742 58
3783 301
7732 15
50404176 8258
Satellite: ISS
Catalog Number: 25544
Epoch time: 13255
51860179 = yrday
fracday
Element set: 908
Inclination: 51
6468 deg
RA of node: 35
5688 deg
Eccentricity:
0003742
Arg of perigee: 58
3783 deg
Mean anomaly: 301
7732 deg
Mean motion: 15
50404176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 825
Checksum: 320
Coasting Arc #10 (Orbit 834)
---------------------------------------
Vector Time (GMT): 2013/256/03:29:12
381
Vector Time (MET): N/A
Weight (LBS) : 957326
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1181756
59 A = 6789139
36 meter
Y = -4139816
24 meter E =
0016707
Z = -5264173
03 I = 51
82258
XDOT = 6830
155757 Wp = 75
78865
YDOT = 3281
813900 meter/sec RA = 31
89681 deg
ZDOT = -1046
351216 TA = 184
18360
MA = 184
19758
Ha = 228
030 n
mi
Hp = 220
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3877154
17 X = 1253533
01
Y = -13582074
29 feet Y = -4126200
03 meter
Z = -17270908
88 Z = -5258257
62
XDOT = 22408
647497 XDOT = 6798
033049
YDOT = 10767
105972 feet/sec YDOT = 3358
013378 meter/sec
ZDOT = -3432
910814 ZDOT = -1013
249144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6520602
25 X = -1987479
56
Y = -12564445
42 feet Y = -3829642
96 meter
Z = -17245457
89 Z = -5256415
56
XDOT = 22728
013320 XDOT = 6927
498460
YDOT = -7267
877491 feet/sec YDOT = -2215
249059 meter/sec
ZDOT = -3294
497765 ZDOT = -1004
162919
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 13256
16314921
00016717 00000-0 10270-3 0 9090
2 25544 51
6503 32
3788 0002897 44
5983 315
5400 15
50205100 8355
Satellite: ISS
Catalog Number: 25544
Epoch time: 13256
16314921 = yrday
fracday
Element set: 909
Inclination: 51
6503 deg
RA of node: 32
3788 deg
Eccentricity:
0002897
Arg of perigee: 44
5983 deg
Mean anomaly: 315
5400 deg
Mean motion: 15
50205100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 835
Checksum: 289
Coasting Arc #11 (Orbit 850)
---------------------------------------
Vector Time (GMT): 2013/257/03:29:12
381
Vector Time (MET): N/A
Weight (LBS) : 957326
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1297799
03 A = 6788829
71 meter
Y = 4025383
81 meter E =
0004711
Z = 5306314
35 I = 51
79494
XDOT = -7011
890773 Wp = 79
22712
YDOT = -3041
588227 meter/sec RA = 26
94995 deg
ZDOT = 592
826568 TA = 5
12767
MA = 5
12285
Ha = 228
047 n
mi
Hp = 220
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4257870
84 X = -1368491
82
Y = 13206639
78 feet Y = 4010476
03 meter
Z = 17409167
82 Z = 5299837
85
XDOT = -23004
890986 XDOT = -6980
237703
YDOT = -9978
964000 feet/sec YDOT = -3119
822626 meter/sec
ZDOT = 1944
969054 ZDOT = 558
840652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6200470
08 X = 1889903
28
Y = 12452542
37 feet Y = 3795534
92 meter
Z = 17381377
45 Z = 5297843
85
XDOT = -22461
375269 XDOT = -6846
227182
YDOT = 8669
657613 feet/sec YDOT = 2642
511641 meter/sec
ZDOT = 1802
812863 ZDOT = 549
497361
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 13257
19459557
00016717 00000-0 10270-3 0 9101
2 25544 51
6501 27
2676 0002806 46
5236 313
6148 15
50225201 8515
Satellite: ISS
Catalog Number: 25544
Epoch time: 13257
19459557 = yrday
fracday
Element set: 910
Inclination: 51
6501 deg
RA of node: 27
2676 deg
Eccentricity:
0002806
Arg of perigee: 46
5236 deg
Mean anomaly: 313
6148 deg
Mean motion: 15
50225201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 851
Checksum: 290
Coasting Arc #12 (Orbit 865)
---------------------------------------
Vector Time (GMT): 2013/258/03:29:12
381
Vector Time (MET): N/A
Weight (LBS) : 957326
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1436673
08 A = 6788746
71 meter
Y = -3957375
56 meter E =
0017158
Z = -5340373
95 I = 51
76728
XDOT = 7129
659068 Wp = 82
55894
YDOT = 2768
667696 meter/sec RA = 22
00085 deg
ZDOT = -131
836165 TA = 186
17326
MA = 186
19443
Ha = 228
038 n
mi
Hp = 220
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4713494
36 X = 1506760
43
Y = -12983515
61 feet Y = -3940918
28 meter
Z = -17520911
90 Z = -5333224
24
XDOT = 23391
269909 XDOT = 7098
809746
YDOT = 9083
555433 feet/sec YDOT = 2848
223573 meter/sec
ZDOT = -432
533350 ZDOT = -97
276333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5935512
46 X = -1809144
20
Y = -12515187
79 feet Y = -3814629
24 meter
Z = -17490306
65 Z = -5331045
47
XDOT = 21918
240852 XDOT = 6680
679812
YDOT = -9984
390901 feet/sec YDOT = -3043
242346 meter/sec
ZDOT = -287
929672 ZDOT = -87
760964
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 13258
16157169
00016717 00000-0 10270-3 0 9114
2 25544 51
6506 22
4757 0002909 48
7941 311
3460 15
50225821 8664
Satellite: ISS
Catalog Number: 25544
Epoch time: 13258
16157169 = yrday
fracday
Element set: 911
Inclination: 51
6506 deg
RA of node: 22
4757 deg
Eccentricity:
0002909
Arg of perigee: 48
7941 deg
Mean anomaly: 311
3460 deg
Mean motion: 15
50225821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 866
Checksum: 302
Coasting Arc #13 (Orbit 881)
---------------------------------------
Vector Time (GMT): 2013/259/03:29:12
381
Vector Time (MET): N/A
Weight (LBS) : 957326
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1595393
46 A = 6788707
83 meter
Y = 3898910
43 meter E =
0005359
Z = 5319587
73 I = 51
73869
XDOT = -7239
646160 Wp = 60
94192
YDOT = -2498
454928 meter/sec RA = 17
04981 deg
ZDOT = -337
234433 TA = 32
28616
MA = 32
25336
Ha = 228
061 n
mi
Hp = 219
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5234230
52 X = -1664714
25
Y = 12791700
90 feet Y = 3880682
65 meter
Z = 17452715
66 Z = 5311668
77
XDOT = -23752
119946 XDOT = -7209
531642
YDOT = -8197
030604 feet/sec YDOT = -2579
244903 meter/sec
ZDOT = -1106
412183 ZDOT = -372
330276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5653613
36 X = 1723221
35
Y = 12658629
19 feet Y = 3858350
18 meter
Z = 17418892
84 Z = 5309278
54
XDOT = -21320
535416 XDOT = -6498
499195
YDOT = 11259
466514 feet/sec YDOT = 3431
885394 meter/sec
ZDOT = -1253
302244 ZDOT = -382
006524
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 13259
19300463
00016717 00000-0 10270-3 0 9126
2 25544 51
6508 17
3643 0002845 50
8564 309
2840 15
50249408 8820
Satellite: ISS
Catalog Number: 25544
Epoch time: 13259
19300463 = yrday
fracday
Element set: 912
Inclination: 51
6508 deg
RA of node: 17
3643 deg
Eccentricity:
0002845
Arg of perigee: 50
8564 deg
Mean anomaly: 309
2840 deg
Mean motion: 15
50249408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 882
Checksum: 300
Coasting Arc #14 (Orbit 896)
---------------------------------------
Vector Time (GMT): 2013/260/03:29:12
381
Vector Time (MET): N/A
Weight (LBS) : 957326
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1760283
18 A = 6788922
42 meter
Y = -3893734
64 meter E =
0016693
Z = -5289802
46 I = 51
70981
XDOT = 7280
673529 Wp = 89
17252
YDOT = 2206
910437 meter/sec RA = 12
09663 deg
ZDOT = 800
737960 TA = 188
47731
MA = 188
50554
Ha = 228
037 n
mi
Hp = 219
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5775207
29 X = 1829389
18
Y = -12774719
94 feet Y = -3873664
26 meter
Z = -17354994
93 Z = -5281082
91
XDOT = 23886
724178 XDOT = 7251
564517
YDOT = 7240
519807 feet/sec YDOT = 2288
164891 meter/sec
ZDOT = 2627
093044 ZDOT = 836
035574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5494407
76 X = -1674695
48
Y = -12947859
19 feet Y = -3946507
48 meter
Z = -17317816
37 Z = -5278470
43
XDOT = 20472
001319 XDOT = 6239
866002
YDOT = -12388
005705 feet/sec YDOT = -3775
864139 meter/sec
ZDOT = 2774
867521 ZDOT = 845
779621
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 13260
15996814
00016717 00000-0 10270-3 0 9136
2 25544 51
6510 12
5723 0002901 52
7850 307
3565 15
50245327 8976
Satellite: ISS
Catalog Number: 25544
Epoch time: 13260
15996814 = yrday
fracday
Element set: 913
Inclination: 51
6510 deg
RA of node: 12
5723 deg
Eccentricity:
0002901
Arg of perigee: 52
7850 deg
Mean anomaly: 307
3565 deg
Mean motion: 15
50245327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 897
Checksum: 296
Coasting Arc #15 (Orbit 912)
---------------------------------------
Vector Time (GMT): 2013/261/03:29:12
381
Vector Time (MET): N/A
Weight (LBS) : 957326
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1940917
44 A = 6789170
43 meter
Y = 3900524
14 meter E =
0007146
Z = 5202609
58 I = 51
68103
XDOT = -7308
753829 Wp = 54
66768
YDOT = -1930
509700 meter/sec RA = 7
14194 deg
ZDOT = -1274
025083 TA = 47
59181
MA = 47
53137
Ha = 228
062 n
mi
Hp = 219
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6367839
38 X = -2009662
47
Y = 12796995
21 feet Y = 3878435
88 meter
Z = 17068929
06 Z = 5193013
32
XDOT = -23978
851145 XDOT = -7280
434399
YDOT = -6333
693240 feet/sec YDOT = -2012
082656 meter/sec
ZDOT = -4179
872321 ZDOT = -1309
461146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5343103
78 X = 1628578
03
Y = 13310023
67 feet Y = 4056895
22 meter
Z = 17028074
34 Z = 5190157
06
XDOT = -19595
655616 XDOT = -5972
755832
YDOT = 13425
885083 feet/sec YDOT = 4092
209773 meter/sec
ZDOT = -4328
260421 ZDOT = -1319
253776
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 13261
19138767
00016717 00000-0 10270-3 0 9147
2 25544 51
6513 7
4612 0002858 54
9358 305
2061 15
50272560 9133
Satellite: ISS
Catalog Number: 25544
Epoch time: 13261
19138767 = yrday
fracday
Element set: 914
Inclination: 51
6513 deg
RA of node: 7
4612 deg
Eccentricity:
0002858
Arg of perigee: 54
9358 deg
Mean anomaly: 305
2061 deg
Mean motion: 15
50272560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 913
Checksum: 294
Coasting Arc #16 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2013/262/03:29:12
381
Vector Time (MET): N/A
Weight (LBS) : 957326
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2109573
97 A = 6789672
13 meter
Y = -3962908
72 meter E =
0015359
Z = -5107199
97 I = 51
65147
XDOT = 7268
710039 Wp = 95
09162
YDOT = 1645
789507 meter/sec RA = 2
18486 deg
ZDOT = 1728
521516 TA = 191
63426
MA = 191
66979
Ha = 228
037 n
mi
Hp = 219
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6921174
43 X = 2178540
70
Y = -13001669
03 feet Y = -3938933
23 meter
Z = -16755905
40 Z = -5096783
77
XDOT = 23847
473880 XDOT = 7241
369538
YDOT = 5399
571874 feet/sec YDOT = 1726
920217 meter/sec
ZDOT = 5671
002349 ZDOT = 1763
765613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5370613
79 X = -1636963
08
Y = -13768994
07 feet Y = -4196789
39 meter
Z = -16711604
62 Z = -5093697
09
XDOT = 18518
288892 XDOT = 5644
374454
YDOT = -14272
597216 feet/sec YDOT = -4350
287632 meter/sec
ZDOT = 5818
617045 ZDOT = 1773
514475
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 13262
15833867
00016717 00000-0 10270-3 0 9158
2 25544 51
6509 2
6690 0002883 57
3380 302
8049 15
50263382 9288
Satellite: ISS
Catalog Number: 25544
Epoch time: 13262
15833867 = yrday
fracday
Element set: 915
Inclination: 51
6509 deg
RA of node: 2
6690 deg
Eccentricity:
0002883
Arg of perigee: 57
3380 deg
Mean anomaly: 302
8049 deg
Mean motion: 15
50263382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 310
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