[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 10th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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 335)
---------------------------------------
Vector Time (GMT): 2015/009/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1976468
38 A = 6780258
66 meter
Y = -3705704
30 meter E =
0005267
Z = 5325441
33 I = 51
77384
XDOT = 6869
703110 Wp = 212
27172
YDOT = -3395
225825 meter/sec RA = 154
77644 deg
ZDOT = 182
774078 TA = 235
96387
MA = 236
01389
Ha = 222
015 n
mi
Hp = 218
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6484476
31 X = -1960752
14
Y = -12157822
52 feet Y = -3727718
70 meter
Z = 17471920
37 Z = 5315878
23
XDOT = 22538
396030 XDOT = 6906
270913
YDOT = -11139
192339 feet/sec YDOT = -3318
199882 meter/sec
ZDOT = 599
652488 ZDOT = 216
234137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5807307
86 X = 1770067
43
Y = -12551555
59 feet Y = -3825714
15 meter
Z = 17431658
28 Z = 5313169
44
XDOT = 21480
949218 XDOT = 6547
393322
YDOT = 10990
430109 feet/sec YDOT = 3349
883097 meter/sec
ZDOT = 743
257929 ZDOT = 226
545017
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 15009
60077405
00016717 00000-0 10270-3 0 9001
2 25544 51
6448 155
6265 0006586 232
6261 127
4292 15
53135470 3360
Satellite: ISS
Catalog Number: 25544
Epoch time: 15009
60077405 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 155
6265 deg
Eccentricity:
0006586
Arg of perigee: 232
6261 deg
Mean anomaly: 127
4292 deg
Mean motion: 15
53135470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 336
Checksum: 295
Coasting Arc #2 (Orbit 350)
---------------------------------------
Vector Time (GMT): 2015/010/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 705952
04 A = 6780730
13 meter
Y = 4315022
15 meter E =
0010366
Z = -5191158
03 I = 51
80418
XDOT = -6990
191548 Wp = 126
54180
YDOT = 2810
800631 meter/sec RA = 149
79825 deg
ZDOT = 1381
702272 TA = 156
75074
MA = 156
70382
Ha = 221
721 n
mi
Hp = 218
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2316115
62 X = 682864
45
Y = 14156896
81 feet Y = 4322787
54 meter
Z = -17031358
35 Z = -5187784
70
XDOT = -22933
699304 XDOT = -7027
814786
YDOT = 9221
786847 feet/sec YDOT = 2732
421386 meter/sec
ZDOT = 4533
143937 ZDOT = 1347
654237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9722152
97 X = -2963312
23
Y = 10570161
84 feet Y = 3221785
33 meter
Z = -17017658
67 Z = -5186982
36
XDOT = -20562
702285 XDOT = -6267
511657
YDOT = -11828
225147 feet/sec YDOT = -3605
243025 meter/sec
ZDOT = 4387
107391 ZDOT = 1337
190333
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 15010
56592275
00016717 00000-0 10270-3 0 9016
2 25544 51
6450 150
8235 0006470 235
7944 124
2596 15
53173219 3513
Satellite: ISS
Catalog Number: 25544
Epoch time: 15010
56592275 = yrday
fracday
Element set: 901
Inclination: 51
6450 deg
RA of node: 150
8235 deg
Eccentricity:
0006470
Arg of perigee: 235
7944 deg
Mean anomaly: 124
2596 deg
Mean motion: 15
53173219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 351
Checksum: 293
Coasting Arc #3 (Orbit 366)
---------------------------------------
Vector Time (GMT): 2015/011/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 504897
22 A = 6782798
89 meter
Y = -4868816
44 meter E =
0001664
Z = 4694077
67 I = 51
83815
XDOT = 6811
442766 Wp = 78
14270
YDOT = -2051
622150 meter/sec RA = 144
82362 deg
ZDOT = -2859
447197 TA = 40
17996
MA = 40
16766
Ha = 221
576 n
mi
Hp = 218
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1656486
94 X = 536502
02
Y = -15973807
20 feet Y = -4862993
67 meter
Z = 15400517
28 Z = 4696607
07
XDOT = 22347
253169 XDOT = 6847
768277
YDOT = -6731
043800 feet/sec YDOT = -1975
249042 meter/sec
ZDOT = -9381
388442 ZDOT = -2826
270532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13445914
35 X = 4098314
69
Y = -8761016
27 feet Y = -2670357
76 meter
Z = 15412150
38 Z = 4697623
43
XDOT = 18615
393919 XDOT = 5673
972066
YDOT = 12309
657627 feet/sec YDOT = 3751
983645 meter/sec
ZDOT = -9239
190112 ZDOT = -2816
105146
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 15011
59539590
00016717 00000-0 10270-3 0 9022
2 25544 51
6454 145
6988 0006362 239
9030 120
1492 15
53158112 3678
Satellite: ISS
Catalog Number: 25544
Epoch time: 15011
59539590 = yrday
fracday
Element set: 902
Inclination: 51
6454 deg
RA of node: 145
6988 deg
Eccentricity:
0006362
Arg of perigee: 239
9030 deg
Mean anomaly: 120
1492 deg
Mean motion: 15
53158112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 367
Checksum: 304
Coasting Arc #4 (Orbit 381)
---------------------------------------
Vector Time (GMT): 2015/012/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1613964
40 A = 6785647
50 meter
Y = 5336495
50 meter E =
0004416
Z = -3871908
38 I = 51
87346
XDOT = -6347
667328 Wp = 176
53978
YDOT = 1093
550026 meter/sec RA = 139
85653 deg
ZDOT = 4149
106668 TA = 136
98101
MA = 136
94648
Ha = 221
227 n
mi
Hp = 218
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5295158
80 X = -1654710
19
Y = 17508187
32 feet Y = 5318219
30 meter
Z = -12703111
49 Z = -3879847
61
XDOT = -20825
680210 XDOT = -6379
578612
YDOT = 3587
762552 feet/sec YDOT = 1022
387830 meter/sec
ZDOT = 13612
554684 ZDOT = 4118
193556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16807408
13 X = -5122898
00
Y = 7155398
50 feet Y = 2180965
46 meter
Z = -12737962
00 Z = -3882530
82
XDOT = -15584
503447 XDOT = -4750
156651
YDOT = -12585
790748 feet/sec YDOT = -3836
149020 meter/sec
ZDOT = 13480
183015 ZDOT = 4108
759783
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 15012
56050626
00016717 00000-0 10270-3 0 9039
2 25544 51
6455 140
8948 0006464 245
2886 114
7587 15
53201018 3829
Satellite: ISS
Catalog Number: 25544
Epoch time: 15012
56050626 = yrday
fracday
Element set: 903
Inclination: 51
6455 deg
RA of node: 140
8948 deg
Eccentricity:
0006464
Arg of perigee: 245
2886 deg
Mean anomaly: 114
7587 deg
Mean motion: 15
53201018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 382
Checksum: 302
Coasting Arc #5 (Orbit 397)
---------------------------------------
Vector Time (GMT): 2015/013/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2561215
19 A = 6788693
87 meter
Y = -5640264
69 meter E =
0008761
Z = 2764251
37 I = 51
90706
XDOT = 5670
932691 Wp = 123
31718
YDOT = 41
768115 meter/sec RA = 134
89810 deg
ZDOT = -5162
082096 TA = 25
49866
MA = 25
45546
Ha = 221
033 n
mi
Hp = 218
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8402936
98 X = 2610667
93
Y = -18504805
41 feet Y = -5611347
04 meter
Z = 9069066
18 Z = 2776813
28
XDOT = 18605
422213 XDOT = 5695
119562
YDOT = 137
034497 feet/sec YDOT = 105
319468 meter/sec
ZDOT = -16935
964882 ZDOT = -5134
475115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19477180
02 X = 5936644
47
Y = -5716803
21 feet Y = -1742481
62 meter
Z = 9123746
72 Z = 2780918
00
XDOT = 11665
967038 XDOT = 3555
786753
YDOT = 12868
514052 feet/sec YDOT = 3922
323083 meter/sec
ZDOT = -16817
912080 ZDOT = -5126
099602
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 15013
58993983
00016717 00000-0 10270-3 0 9045
2 25544 51
6453 135
7705 0006306 248
2950 111
7531 15
53220521 3984
Satellite: ISS
Catalog Number: 25544
Epoch time: 15013
58993983 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 135
7705 deg
Eccentricity:
0006306
Arg of perigee: 248
2950 deg
Mean anomaly: 111
7531 deg
Mean motion: 15
53220521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 398
Checksum: 303
Coasting Arc #6 (Orbit 412)
---------------------------------------
Vector Time (GMT): 2015/014/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3317407
06 A = 6790983
87 meter
Y = 5739307
09 meter E =
0005067
Z = -1458108
33 I = 51
93697
XDOT = -4828
208028 Wp = 349
15810
YDOT = -1316
091905 meter/sec RA = 129
94656 deg
ZDOT = 5806
131386 TA = 355
00820
MA = 355
01325
Ha = 220
649 n
mi
Hp = 218
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10883881
44 X = -3374255
85
Y = 18829747
66 feet Y = 5701891
86 meter
Z = -4783819
98 Z = -1474361
59
XDOT = -15840
577520 XDOT = -4841
336317
YDOT = -4317
886827 feet/sec YDOT = -1370
157600 meter/sec
ZDOT = 19048
987486 ZDOT = 5782
644996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21284923
71 X = -6487644
75
Y = 4392132
00 feet Y = 1338721
83 meter
Z = -4854318
17 Z = -1479596
18
XDOT = -7053
776235 XDOT = -2149
990996
YDOT = -13246
511828 feet/sec YDOT = -4037
536805 meter/sec
ZDOT = 18948
766023 ZDOT = 5775
583884
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 15014
55501360
00016717 00000-0 10270-3 0 9058
2 25544 51
6458 130
9656 0006291 254
9339 105
1117 15
53239746 4133
Satellite: ISS
Catalog Number: 25544
Epoch time: 15014
55501360 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 130
9656 deg
Eccentricity:
0006291
Arg of perigee: 254
9339 deg
Mean anomaly: 105
1117 deg
Mean motion: 15
53239746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 413
Checksum: 295
Coasting Arc #7 (Orbit 428)
---------------------------------------
Vector Time (GMT): 2015/015/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3874249
68 A = 6791779
53 meter
Y = -5570161
95 meter E =
0010205
Z = 27397
46 I = 51
95886
XDOT = 3894
481037 Wp = 164
95130
YDOT = 2676
622400 meter/sec RA = 125
00104 deg
ZDOT = -6039
317398 TA = 14
75494
MA = 14
72518
Ha = 220
498 n
mi
Hp = 218
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12710792
91 X = 3936115
51
Y = -18274809
56 feet Y = -5526491
66 meter
Z = 89886
67 Z = 46367
84
XDOT = 12777
168758 XDOT = 3893
597671
YDOT = 8781
569554 feet/sec YDOT = 2720
168304 meter/sec
ZDOT = -19814
033457 ZDOT = -6020
400836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22054859
70 X = 6722321
24
Y = -3015722
54 feet Y = -919192
23 meter
Z = 171993
69 Z = 52423
68
XDOT = 2051
795756 XDOT = 625
387346
YDOT = 13831
709390 feet/sec YDOT = 4215
905022 meter/sec
ZDOT = -19733
586787 ZDOT = -6014
797253
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 15015
58440745
00016717 00000-0 10270-3 0 9062
2 25544 51
6452 125
8412 0006241 257
4078 102
6377 15
53285954 4292
Satellite: ISS
Catalog Number: 25544
Epoch time: 15015
58440745 = yrday
fracday
Element set: 906
Inclination: 51
6452 deg
RA of node: 125
8412 deg
Eccentricity:
0006241
Arg of perigee: 257
4078 deg
Mean anomaly: 102
6377 deg
Mean motion: 15
53285954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 429
Checksum: 308
Coasting Arc #8 (Orbit 444)
---------------------------------------
Vector Time (GMT): 2015/016/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4230295
33 A = 6790867
99 meter
Y = 5116385
43 meter E =
0008453
Z = 1405336
14 I = 51
97426
XDOT = -2932
639096 Wp = 44
32787
YDOT = -4029
297801 meter/sec RA = 120
05570 deg
ZDOT = 5826
470121 TA = 330
91455
MA = 330
96161
Ha = 220
155 n
mi
Hp = 218
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13878921
69 X = -4294020
12
Y = 16786041
43 feet Y = 5068723
14 meter
Z = 4610682
86 Z = 1384631
74
XDOT = -9621
519343 XDOT = -2915
667296
YDOT = -13219
480976 feet/sec YDOT = -4061
997890 meter/sec
ZDOT = 19115
715620 ZDOT = 5812
264986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21747644
86 X = -6628682
15
Y = 1500855
04 feet Y = 457460
62 meter
Z = 4521219
74 Z = 1378067
78
XDOT = 2965
670796 XDOT = 903
936459
YDOT = -14583
949031 feet/sec YDOT = -4445
187665 meter/sec
ZDOT = 19055
656204 ZDOT = 5808
164011
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 15016
61378026
00016717 00000-0 10270-3 0 9070
2 25544 51
6460 120
7157 0006171 262
9961 97
0489 15
53323267 4454
Satellite: ISS
Catalog Number: 25544
Epoch time: 15016
61378026 = yrday
fracday
Element set: 907
Inclination: 51
6460 deg
RA of node: 120
7157 deg
Eccentricity:
0006171
Arg of perigee: 262
9961 deg
Mean anomaly: 97
0489 deg
Mean motion: 15
53323267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 445
Checksum: 308
Coasting Arc #9 (Orbit 459)
---------------------------------------
Vector Time (GMT): 2015/017/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4417418
89 A = 6788456
88 meter
Y = -4353851
39 meter E =
0003658
Z = -2753165
73 I = 51
98069
XDOT = 1989
441527 Wp = 215
21629
YDOT = 5292
144484 meter/sec RA = 115
10859 deg
ZDOT = -5176
446365 TA = 355
78075
MA = 355
78383
Ha = 220
063 n
mi
Hp = 218
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14492844
12 X = 4479150
12
Y = -14284289
34 feet Y = -4304107
61 meter
Z = -9032695
96 Z = -2731557
25
XDOT = 6527
039130 XDOT = 1955
260731
YDOT = 17362
678752 feet/sec YDOT = 5314
200926 meter/sec
ZDOT = -16983
091748 ZDOT = -5166
864793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20387359
05 X = 6214067
04
Y = 338090
72 feet Y = 103050
05 meter
Z = -8939481
78 Z = -2724754
05
XDOT = -7685
731357 XDOT = -2342
610917
YDOT = 15424
088678 feet/sec YDOT = 4701
262229 meter/sec
ZDOT = -16943
035972 ZDOT = -5164
237364
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 15017
57879963
00016717 00000-0 10270-3 0 9083
2 25544 51
6452 115
9114 0006166 266
7713 93
2734 15
53346672 4608
Satellite: ISS
Catalog Number: 25544
Epoch time: 15017
57879963 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 115
9114 deg
Eccentricity:
0006166
Arg of perigee: 266
7713 deg
Mean anomaly: 93
2734 deg
Mean motion: 15
53346672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 460
Checksum: 325
Coasting Arc #10 (Orbit 475)
---------------------------------------
Vector Time (GMT): 2015/018/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4458284
61 A = 6785117
33 meter
Y = 3313687
94 meter E =
0005214
Z = 3893213
35 I = 51
98343
XDOT = -1109
887243 Wp = 106
95596
YDOT = -6359
327183 meter/sec RA = 110
15480 deg
ZDOT = 4135
686616 TA = 299
80482
MA = 299
85665
Ha = 219
995 n
mi
Hp = 218
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14626918
03 X = -4513919
26
Y = 10871679
59 feet Y = 3263521
17 meter
Z = 12773009
68 Z = 3871421
20
XDOT = -3641
362345 XDOT = -1058
782650
YDOT = -20863
934329 feet/sec YDOT = -6371
453194 meter/sec
ZDOT = 13568
525643 ZDOT = 4130
418768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18113707
53 X = -5521058
06
Y = -2534157
51 feet Y = -772411
21 meter
Z = 12679178
57 Z = 3864613
63
XDOT = 11760
927785 XDOT = 3584
730789
YDOT = -16184
653636 feet/sec YDOT = -4933
082428 meter/sec
ZDOT = 13547
119987 ZDOT = 4129
162172
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 15018
60813300
00016717 00000-0 10270-3 0 9092
2 25544 51
6461 110
7858 0006182 271
5331 88
5113 15
53401099 4764
Satellite: ISS
Catalog Number: 25544
Epoch time: 15018
60813300 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 110
7858 deg
Eccentricity:
0006182
Arg of perigee: 271
5331 deg
Mean anomaly: 88
5113 deg
Mean motion: 15
53401099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 476
Checksum: 290
Coasting Arc #11 (Orbit 490)
---------------------------------------
Vector Time (GMT): 2015/019/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4399824
15 A = 6782013
28 meter
Y = -2030330
23 meter E =
0005971
Z = -4750516
49 I = 51
98240
XDOT = 303
475082 Wp = 45
18657
YDOT = 7138
186880 meter/sec RA = 105
19468 deg
ZDOT = -2767
760636 TA = 197
51149
MA = 197
53209
Ha = 220
004 n
mi
Hp = 218
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14435118
60 X = 4445276
62
Y = -6661188
41 feet Y = -1980874
12 meter
Z = -15585684
02 Z = -4729033
06
XDOT = 995
653157 XDOT = 237
076169
YDOT = 23419
248293 feet/sec YDOT = 7141
209435 meter/sec
ZDOT = -9080
579514 ZDOT = -2766
447305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15132683
40 X = 4612441
90
Y = 5158911
52 feet Y = 1572436
23 meter
Z = -15493390
57 Z = -4722385
45
XDOT = -14965
567726 XDOT = -4561
505043
YDOT = 16621
113306 feet/sec YDOT = 5066
115336 meter/sec
ZDOT = -9076
240211 ZDOT = -2766
438016
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 15019
57311721
00016717 00000-0 10270-3 0 9101
2 25544 51
6454 105
9813 0006108 276
1667 83
8789 15
53398471 4917
Satellite: ISS
Catalog Number: 25544
Epoch time: 15019
57311721 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 105
9813 deg
Eccentricity:
0006108
Arg of perigee: 276
1667 deg
Mean anomaly: 83
8789 deg
Mean motion: 15
53398471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 491
Checksum: 322
Coasting Arc #12 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2015/020/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4266554
59 A = 6779768
75 meter
Y = 578065
88 meter E =
0002898
Z = 5239637
06 I = 51
98336
XDOT = 426
359430 Wp = 248
01861
YDOT = -7561
933457 meter/sec RA = 100
22824 deg
ZDOT = 1180
918294 TA = 190
70170
MA = 190
70787
Ha = 220
248 n
mi
Hp = 217
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13997882
50 X = -4298153
23
Y = 1896541
59 feet Y = 530177
61 meter
Z = 17190410
29 Z = 5218834
66
XDOT = 1398
817027 XDOT = 505
150716
YDOT = -24809
492969 feet/sec YDOT = -7556
725126 meter/sec
ZDOT = 3874
403853 ZDOT = 1183
180509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11687301
50 X = -3562289
50
Y = -8124093
58 feet Y = -2476223
72 meter
Z = 17101282
93 Z = 5212471
04
XDOT = 17171
740761 XDOT = 5233
946584
YDOT = -16520
617676 feet/sec YDOT = -5035
484268 meter/sec
ZDOT = 3885
448134 ZDOT = 1184
284591
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 15020
60241239
00016717 00000-0 10270-3 0 9114
2 25544 51
6459 100
8558 0006106 280
9660 79
0806 15
53456870 5079
Satellite: ISS
Catalog Number: 25544
Epoch time: 15020
60241239 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 100
8558 deg
Eccentricity:
0006106
Arg of perigee: 280
9660 deg
Mean anomaly: 79
0806 deg
Mean motion: 15
53456870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 297
Coasting Arc #13 (Orbit 521)
---------------------------------------
Vector Time (GMT): 2015/021/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4094288
94 A = 6779404
04 meter
Y = 948929
17 meter E =
0008921
Z = -5327069
73 I = 51
98622
XDOT = -1094
770252 Wp = 85
79491
YDOT = 7565
456064 meter/sec RA = 95
25859 deg
ZDOT = 507
606280 TA = 189
02122
MA = 189
03726
Ha = 220
423 n
mi
Hp = 218
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13432706
49 X = 4109249
82
Y = 3113284
67 feet Y = 994797
89 meter
Z = -17477262
90 Z = -5307144
57
XDOT = -3591
765917 XDOT = -1181
753298
YDOT = 24821
050079 feet/sec YDOT = 7552
727274 meter/sec
ZDOT = 1665
374936 ZDOT = 502
077052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8084873
04 X = 2464269
30
Y = 11301879
21 feet Y = 3444812
78 meter
Z = -17392159
66 Z = -5301130
27
XDOT = -18315
658876 XDOT = -5582
612825
YDOT = 15619
572799 feet/sec YDOT = 4760
845789 meter/sec
ZDOT = 1640
341810 ZDOT = 499
976184
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 15021
56736056
00016717 00000-0 10270-3 0 9127
2 25544 51
6454 96
0503 0006048 285
9559 74
0926 15
53452049 5226
Satellite: ISS
Catalog Number: 25544
Epoch time: 15021
56736056 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 96
0503 deg
Eccentricity:
0006048
Arg of perigee: 285
9559 deg
Mean anomaly: 74
0926 deg
Mean motion: 15
53452049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 522
Checksum: 307
Coasting Arc #14 (Orbit 537)
---------------------------------------
Vector Time (GMT): 2015/022/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3883694
82 A = 6780647
19 meter
Y = -2461650
98 meter E =
0005515
Z = 4985543
03 I = 51
99293
XDOT = 1733
471775 Wp = 356
27315
YDOT = -7143
961209 meter/sec RA = 90
29046 deg
ZDOT = -2171
807187 TA = 114
83007
MA = 114
77271
Ha = 220
524 n
mi
Hp = 217
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12741780
92 X = -3880096
80
Y = -8076282
75 feet Y = -2505060
82 meter
Z = 16356768
47 Z = 4966685
97
XDOT = 5687
243357 XDOT = 1823
777990
YDOT = -23438
192942 feet/sec YDOT = -7124
071490 meter/sec
ZDOT = -7125
351663 ZDOT = -2163
167088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4524260
46 X = -1378994
59
Y = -14482041
87 feet Y = -4414126
36 meter
Z = 16276508
52 Z = 4961079
80
XDOT = 18524
160984 XDOT = 5646
164268
YDOT = -13771
613732 feet/sec YDOT = -4197
587866 meter/sec
ZDOT = -7087
074012 ZDOT = -2160
140159
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 15022
59661732
00016717 00000-0 10270-3 0 9130
2 25544 51
6452 90
9246 0006048 290
5197 69
5306 15
53527937 5388
Satellite: ISS
Catalog Number: 25544
Epoch time: 15022
59661732 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 90
9246 deg
Eccentricity:
0006048
Arg of perigee: 290
5197 deg
Mean anomaly: 69
5306 deg
Mean motion: 15
53527937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 538
Checksum: 322
Coasting Arc #15 (Orbit 552)
---------------------------------------
Vector Time (GMT): 2015/023/13:15:03
575
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3644722
45 A = 6783469
49 meter
Y = 3832160
92 meter E =
0002309
Z = -4250171
69 I = 52
00185
XDOT = -2357
212914 Wp = 95
05739
YDOT = 6304
796403 meter/sec RA = 85
32661 deg
ZDOT = 3664
798399 TA = 212
29434
MA = 212
30847
Ha = 220
788 n
mi
Hp = 217
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11957750
83 X = 3622244
80
Y = 12572706
43 feet Y = 3872792
78 meter
Z = -13944132
85 Z = -4232521
37
XDOT = -7733
638169 XDOT = -2445
341317
YDOT = 20685
027569 feet/sec YDOT = 6277
943859 meter/sec
ZDOT = 12023
616794 ZDOT = 3653
133511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1295185
91 X = 394772
67
Y = 17362745
04 feet Y = 5292164
69 meter
Z = -13869288
77 Z = -4227359
22
XDOT = -17919
995153 XDOT = -5462
014523
YDOT = 10896
391688 feet/sec YDOT = 3321
220187 meter/sec
ZDOT = 11972
538559 ZDOT = 3649
229753
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 15023
56153008
00016717 00000-0 10270-3 0 9141
2 25544 51
6453 86
1183 0005854 295
8245 64
2303 15
53540022 5538
Satellite: ISS
Catalog Number: 25544
Epoch time: 15023
56153008 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 86
1183 deg
Eccentricity:
0005854
Arg of perigee: 295
8245 deg
Mean anomaly: 64
2303 deg
Mean motion: 15
53540022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 553
Checksum: 283
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