[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 16th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 730 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 3244)
---------------------------------------
Vector Time (GMT): 2015/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1387728
74 A = 6783731
50 meter
Y = 6115225
55 meter E =
0012276
Z = 2571589
38 I = 51
34820
XDOT = -5527
548133 Wp = 109
06735
YDOT = 953
906526 meter/sec RA = 301
93196 deg
ZDOT = -5234
711449 TA = 41
86435
MA = 41
77054
Ha = 218
891 n
mi
Hp = 213
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4552915
82 X = -1468499
14
Y = 20063075
94 feet Y = 6099255
15 meter
Z = 8436973
02 Z = 2564652
67
XDOT = -18135
000437 XDOT = -5512
376276
YDOT = 3129
614587 feet/sec YDOT = 892
179278 meter/sec
ZDOT = -17174
250162 ZDOT = -5261
525816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20318016
63 X = 6192931
47
Y = -3310193
19 feet Y = -1008946
88 meter
Z = 8405914
19 Z = 2562122
64
XDOT = 9461
074807 XDOT = 2883
735601
YDOT = 14028
225485 feet/sec YDOT = 4275
803128 meter/sec
ZDOT = -17289
731417 ZDOT = -5269
910136
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 15196
53730546
00016717 00000-0 10270-3 0 9002
2 25544 51
6448 302
4500 0001876 243
9811 116
1149 15
55096438 32457
Satellite: ISS
Catalog Number: 25544
Epoch time: 15196
53730546 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 302
4500 deg
Eccentricity:
0001876
Arg of perigee: 243
9811 deg
Mean anomaly: 116
1149 deg
Mean motion: 15
55096438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3245
Checksum: 303
Coasting Arc #2 (Orbit 3259)
---------------------------------------
Vector Time (GMT): 2015/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2589361
74 A = 6786240
21 meter
Y = -6234429
58 meter E =
0009339
Z = -644265
76 I = 51
34150
XDOT = 4660
376141 Wp = 33
86481
YDOT = 1326
356853 meter/sec RA = 296
93322 deg
ZDOT = 5944
858889 TA = 319
14713
MA = 319
21709
Ha = 218
787 n
mi
Hp = 213
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8495281
28 X = 2662013
72
Y = -20454165
30 feet Y = -6205067
36 meter
Z = -2113732
79 Z = -631511
52
XDOT = 15289
947970 XDOT = 4616
320774
YDOT = 4351
564479 feet/sec YDOT = 1378
225319 meter/sec
ZDOT = 19504
130213 ZDOT = 5967
390801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22152330
58 X = -6752030
36
Y = 225560
82 feet Y = 68750
94 meter
Z = -2057649
30 Z = -627171
51
XDOT = -1948
171040 XDOT = -593
802533
YDOT = -14039
684620 feet/sec YDOT = -4279
295872 meter/sec
ZDOT = 19600
743502 ZDOT = 5974
306619
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 15197
50121224
00016717 00000-0 10270-3 0 9018
2 25544 51
6453 297
6378 0001804 257
0043 103
0909 15
55133339 32603
Satellite: ISS
Catalog Number: 25544
Epoch time: 15197
50121224 = yrday
fracday
Element set: 901
Inclination: 51
6453 deg
RA of node: 297
6378 deg
Eccentricity:
0001804
Arg of perigee: 257
0043 deg
Mean anomaly: 103
0909 deg
Mean motion: 15
55133339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3260
Checksum: 285
Coasting Arc #3 (Orbit 3275)
---------------------------------------
Vector Time (GMT): 2015/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3493071
65 A = 6785380
85 meter
Y = 5637200
35 meter E =
0007838
Z = -1416854
87 I = 51
32482
XDOT = -3518
496939 Wp = 154
35605
YDOT = -3625
606387 meter/sec RA = 291
93757 deg
ZDOT = -5769
625852 TA = 41
16680
MA = 41
10771
Ha = 218
658 n
mi
Hp = 213
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11460208
82 X = -3548966
15
Y = 18494751
81 feet Y = 5597826
13 meter
Z = -4648474
00 Z = -1433958
51
XDOT = -11543
625129 XDOT = -3449
666910
YDOT = -11895
034077 feet/sec YDOT = -3664
567203 meter/sec
ZDOT = -18929
218676 ZDOT = -5786
550810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21552371
99 X = 6569162
98
Y = 2861445
75 feet Y = 872168
66 meter
Z = -4723127
23 Z = -1439609
18
XDOT = -5972
139795 XDOT = -1820
308209
YDOT = 13719
279295 feet/sec YDOT = 4181
636329 meter/sec
ZDOT = -19001
274549 ZDOT = -5791
588482
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 15198
52935581
00016717 00000-0 10270-3 0 9021
2 25544 51
6446 292
5051 0001835 258
6719 101
4228 15
55183884 32761
Satellite: ISS
Catalog Number: 25544
Epoch time: 15198
52935581 = yrday
fracday
Element set: 902
Inclination: 51
6446 deg
RA of node: 292
5051 deg
Eccentricity:
0001835
Arg of perigee: 258
6719 deg
Mean anomaly: 101
4228 deg
Mean motion: 15
55183884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3276
Checksum: 326
Coasting Arc #4 (Orbit 3291)
---------------------------------------
Vector Time (GMT): 2015/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4046577
95 A = 6781547
68 meter
Y = -4359367
04 meter E =
0010899
Z = 3247458
32 I = 51
30163
XDOT = 2246
155645 Wp = 87
84154
YDOT = 5613
234983 meter/sec RA = 286
93203 deg
ZDOT = 4722
941340 TA = 310
03850
MA = 310
13406
Ha = 218
526 n
mi
Hp = 213
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13276174
37 X = 4079250
06
Y = -14302385
29 feet Y = -4313933
07 meter
Z = 10654390
81 Z = 3267194
50
XDOT = 7369
277049 XDOT = 2160
278334
YDOT = 18416
125272 feet/sec YDOT = 5637
872498 meter/sec
ZDOT = 15495
214371 ZDOT = 4733
644291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18557920
22 X = -5656454
08
Y = -5880891
89 feet Y = -1792495
85 meter
Z = 10740101
59 Z = 3273582
97
XDOT = 13155
168576 XDOT = 4009
695382
YDOT = -13052
995309 feet/sec YDOT = -3978
552970 meter/sec
ZDOT = 15540
139056 ZDOT = 4736
634384
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 15199
55747325
00016717 00000-0 10270-3 0 9033
2 25544 51
6446 287
3713 0001797 265
9231 94
1717 15
55240818 32925
Satellite: ISS
Catalog Number: 25544
Epoch time: 15199
55747325 = yrday
fracday
Element set: 903
Inclination: 51
6446 deg
RA of node: 287
3713 deg
Eccentricity:
0001797
Arg of perigee: 265
9231 deg
Mean anomaly: 94
1717 deg
Mean motion: 15
55240818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3292
Checksum: 332
Coasting Arc #5 (Orbit 3306)
---------------------------------------
Vector Time (GMT): 2015/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4304476
96 A = 6776961
56 meter
Y = 2493520
15 meter E =
0008720
Z = -4610951
85 I = 51
27704
XDOT = -923
675447 Wp = 65
51776
YDOT = -7018
140227 meter/sec RA = 281
91191 deg
ZDOT = -2933
843662 TA = 175
09604
MA = 175
08750
Ha = 218
554 n
mi
Hp = 213
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14122299
75 X = -4309642
32
Y = 8180840
38 feet Y = 2445356
00 meter
Z = -15127794
77 Z = -4631874
21
XDOT = -3030
431258 XDOT = -830
877014
YDOT = -23025
394447 feet/sec YDOT = -7027
950364 meter/sec
ZDOT = -9625
471332 ZDOT = -2938
105561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13519924
87 X = 4120873
10
Y = 8990693
79 feet Y = 2740363
47 meter
Z = -15218236
78 Z = -4638518
57
XDOT = -18710
520860 XDOT = -5702
966758
YDOT = 11819
508265 feet/sec YDOT = 3602
586119 meter/sec
ZDOT = -9642
443848 ZDOT = -2939
016885
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 15200
52131242
00016717 00000-0 10270-3 0 9049
2 25544 51
6437 282
5593 0001852 272
3879 87
7062 15
55245819 33074
Satellite: ISS
Catalog Number: 25544
Epoch time: 15200
52131242 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 282
5593 deg
Eccentricity:
0001852
Arg of perigee: 272
3879 deg
Mean anomaly: 87
7062 deg
Mean motion: 15
55245819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3307
Checksum: 307
Coasting Arc #6 (Orbit 3322)
---------------------------------------
Vector Time (GMT): 2015/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4273719
04 A = 6774030
49 meter
Y = -275515
89 meter E =
0001373
Z = 5247870
96 I = 51
26246
XDOT = -360
397717 Wp = 140
91662
YDOT = 7631
577488 meter/sec RA = 276
87674 deg
ZDOT = 693
012325 TA = 302
42622
MA = 302
43949
Ha = 218
297 n
mi
Hp = 213
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14021387
93 X = 4250990
51
Y = -903923
52 feet Y = -227851
64 meter
Z = 17217424
40 Z = 5268576
31
XDOT = -1182
407207 XDOT = -449
075406
YDOT = 25037
983885 feet/sec YDOT = 7627
051433 meter/sec
ZDOT = 2273
662483 ZDOT = 691
046507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7143043
91 X = -2177199
78
Y = -11971544
34 feet Y = -3648926
71 meter
Z = 17306506
01 Z = 5275023
03
XDOT = 21959
387328 XDOT = 6693
221257
YDOT = -9824
493426 feet/sec YDOT = -2994
505596 meter/sec
ZDOT = 2263
756098 ZDOT = 689
992859
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 15201
54938190
00016717 00000-0 10270-3 0 9050
2 25544 51
6438 277
4249 0001873 279
2707 80
8235 15
55321928 33235
Satellite: ISS
Catalog Number: 25544
Epoch time: 15201
54938190 = yrday
fracday
Element set: 905
Inclination: 51
6438 deg
RA of node: 277
4249 deg
Eccentricity:
0001873
Arg of perigee: 279
2707 deg
Mean anomaly: 80
8235 deg
Mean motion: 15
55321928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3323
Checksum: 319
Coasting Arc #7 (Orbit 3337)
---------------------------------------
Vector Time (GMT): 2015/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4012580
98 A = 6774794
34 meter
Y = -2024358
34 meter E =
0011628
Z = -5079906
68 I = 51
26103
XDOT = 1574
936948 Wp = 101
54744
YDOT = -7309
636323 meter/sec RA = 271
83809 deg
ZDOT = 1669
851476 TA = 184
67292
MA = 184
68379
Ha = 218
497 n
mi
Hp = 213
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13164635
76 X = -3964969
94
Y = -6641595
61 feet Y = -2068963
29 meter
Z = -16666360
51 Z = -5099283
19
XDOT = 5167
115972 XDOT = 1648
446602
YDOT = -23981
746466 feet/sec YDOT = -7291
613379 meter/sec
ZDOT = 5478
515340 ZDOT = 1677
680435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 289864
17 X = 88350
60
Y = 14647971
95 feet Y = 4464701
85 meter
Z = -16749295
39 Z = -5105185
24
XDOT = -22503
895382 XDOT = -6859
187312
YDOT = 6746
203551 feet/sec YDOT = 2056
242842 meter/sec
ZDOT = 5513
555927 ZDOT = 1680
531847
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 15202
51317728
00016717 00000-0 10270-3 0 9067
2 25544 51
6427 272
6121 0001808 289
7827 70
3132 15
55329433 33381
Satellite: ISS
Catalog Number: 25544
Epoch time: 15202
51317728 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 272
6121 deg
Eccentricity:
0001808
Arg of perigee: 289
7827 deg
Mean anomaly: 70
3132 deg
Mean motion: 15
55329433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3338
Checksum: 302
Coasting Arc #8 (Orbit 3353)
---------------------------------------
Vector Time (GMT): 2015/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3512775
44 A = 6778459
92 meter
Y = 4104801
66 meter E =
0009097
Z = 4088669
16 I = 51
27433
XDOT = -2703
328577 Wp = 68
91064
YDOT = 6098
173359 meter/sec RA = 266
80652 deg
ZDOT = -3789
620036 TA = 60
41888
MA = 60
32826
Ha = 218
326 n
mi
Hp = 213
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11524853
81 X = 3446752
47
Y = 13467197
04 feet Y = 4143714
54 meter
Z = 13414268
90 Z = 4105573
12
XDOT = -8869
188245 XDOT = -2752
910540
YDOT = 20007
130444 feet/sec YDOT = 6067
665846 meter/sec
ZDOT = -12433
136601 ZDOT = -3802
872398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6209914
24 X = 1892781
86
Y = -16543576
55 feet Y = -5042482
13 meter
Z = 13486189
28 Z = 4110590
49
XDOT = 20549
661850 XDOT = 6263
536932
YDOT = -2495
848953 feet/sec YDOT = -760
734761 meter/sec
ZDOT = -12491
258282 ZDOT = -3807
335524
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 15203
54120077
00016717 00000-0 10270-3 0 9071
2 25544 51
6431 267
4773 0001920 295
7839 64
3116 15
55398402 33541
Satellite: ISS
Catalog Number: 25544
Epoch time: 15203
54120077 = yrday
fracday
Element set: 907
Inclination: 51
6431 deg
RA of node: 267
4773 deg
Eccentricity:
0001920
Arg of perigee: 295
7839 deg
Mean anomaly: 64
3116 deg
Mean motion: 15
55398402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3354
Checksum: 306
Coasting Arc #9 (Orbit 3368)
---------------------------------------
Vector Time (GMT): 2015/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2806329
75 A = 6783040
12 meter
Y = -5663201
97 meter E =
0005152
Z = -2456861
73 I = 51
29149
XDOT = 3696
506402 Wp = 28
92087
YDOT = -4127
426876 meter/sec RA = 261
79060 deg
ZDOT = 5300
742294 TA = 303
41431
MA = 303
46358
Ha = 218
447 n
mi
Hp = 213
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9207118
59 X = -2730859
47
Y = -18580058
95 feet Y = -5694162
13 meter
Z = -8060569
97 Z = -2470311
10
XDOT = 12127
645676 XDOT = 3716
636735
YDOT = -13541
426758 feet/sec YDOT = -4085
977730 meter/sec
ZDOT = 17390
886790 ZDOT = 5318
747825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11492947
50 X = -3503050
40
Y = 17233197
46 feet Y = 5252678
59 meter
Z = -8117356
40 Z = -2474170
23
XDOT = -16481
801433 XDOT = -5023
653077
YDOT = -2777
337185 feet/sec YDOT = -846
532374 meter/sec
ZDOT = 17469
074401 ZDOT = 5324
573877
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 15204
50495340
00016717 00000-0 10270-3 0 9087
2 25544 51
6423 262
6638 0001822 301
5893 58
5082 15
55397362 33693
Satellite: ISS
Catalog Number: 25544
Epoch time: 15204
50495340 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 262
6638 deg
Eccentricity:
0001822
Arg of perigee: 301
5893 deg
Mean anomaly: 58
5082 deg
Mean motion: 15
55397362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3369
Checksum: 314
Coasting Arc #10 (Orbit 3384)
---------------------------------------
Vector Time (GMT): 2015/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1850963
27 A = 6785412
46 meter
Y = 6510820
31 meter E =
0011010
Z = 391832
58 I = 51
30594
XDOT = -4524
046097 Wp = 130
53289
YDOT = 1651
661211 meter/sec RA = 256
78765 deg
ZDOT = -5969
928083 TA = 45
22081
MA = 45
13130
Ha = 218
483 n
mi
Hp = 213
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6072714
13 X = 1776116
78
Y = 21360959
01 feet Y = 6531100
49 meter
Z = 1285539
97 Z = 400642
62
XDOT = -14842
670921 XDOT = -4513
179640
YDOT = 5418
835993 feet/sec YDOT = 1601
131357 meter/sec
ZDOT = -19586
378226 ZDOT = -5991
878426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15171195
41 X = 4624180
36
Y = -16214424
83 feet Y = -4942156
69 meter
Z = 1322231
83 Z = 403016
26
XDOT = 11050
355721 XDOT = 3368
148424
YDOT = 8707
493661 feet/sec YDOT = 2654
044068 meter/sec
ZDOT = -19681
072629 ZDOT = -5998
790937
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 15205
53293248
00016717 00000-0 10270-3 0 9095
2 25544 51
6429 257
5288 0001811 311
7857 48
3142 15
55453205 33855
Satellite: ISS
Catalog Number: 25544
Epoch time: 15205
53293248 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 257
5288 deg
Eccentricity:
0001811
Arg of perigee: 311
7857 deg
Mean anomaly: 48
3142 deg
Mean motion: 15
55453205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3385
Checksum: 314
Coasting Arc #11 (Orbit 3400)
---------------------------------------
Vector Time (GMT): 2015/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -694635
40 A = 6784287
30 meter
Y = -6518242
65 meter E =
0013662
Z = 1719850
06 I = 51
30948
XDOT = 5089
245228 Wp = 57
30374
YDOT = 958
388827 meter/sec RA = 251
78746 deg
ZDOT = 5662
219132 TA = 321
66988
MA = 321
76689
Ha = 218
601 n
mi
Hp = 213
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2278987
55 X = -630049
56
Y = -21385310
52 feet Y = -6525649
49 meter
Z = 5642552
68 Z = 1716632
20
XDOT = 16696
998781 XDOT = 5050
645269
YDOT = 3144
320300 feet/sec YDOT = 1015
083981 meter/sec
ZDOT = 18576
834423 ZDOT = 5686
847854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16899294
91 X = -5150905
09
Y = 13307206
68 feet Y = 4056036
60 meter
Z = 5629899
92 Z = 1715993
50
XDOT = -5157
782040 XDOT = -1572
091966
YDOT = -14489
717267 feet/sec YDOT = -4416
465823 meter/sec
ZDOT = 18682
575652 ZDOT = 5694
449059
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 15206
56089011
00016717 00000-0 10270-3 0 9102
2 25544 51
6422 252
3938 0001803 321
7224 38
3802 15
55435112 34011
Satellite: ISS
Catalog Number: 25544
Epoch time: 15206
56089011 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 252
3938 deg
Eccentricity:
0001803
Arg of perigee: 321
7224 deg
Mean anomaly: 38
3802 deg
Mean motion: 15
55435112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3401
Checksum: 267
Coasting Arc #12 (Orbit 3415)
---------------------------------------
Vector Time (GMT): 2015/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -669435
43 A = 6779847
98 meter
Y = 5719688
19 meter E =
0004721
Z = -3583819
00 I = 51
30707
XDOT = -5286
657430 Wp = 64
08084
YDOT = -3376
372170 meter/sec RA = 246
77788 deg
ZDOT = -4403
601129 TA = 158
52512
MA = 158
50531
Ha = 218
526 n
mi
Hp = 212
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2196310
48 X = -715935
88
Y = 18765381
21 feet Y = 5711942
37 meter
Z = -11757936
35 Z = -3587183
52
XDOT = -17344
676607 XDOT = -5227
118207
YDOT = -11077
336515 feet/sec YDOT = -3435
157840 meter/sec
ZDOT = -14447
510265 ZDOT = -4429
138130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16888615
62 X = 5147650
04
Y = -8448264
42 feet Y = -2575030
99 meter
Z = -11773439
16 Z = -3588544
26
XDOT = -501
959658 XDOT = -152
997304
YDOT = 19271
250691 feet/sec YDOT = 5873
877211 meter/sec
ZDOT = -14556
730752 ZDOT = -4436
891533
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 15207
52457665
00016717 00000-0 10270-3 0 9114
2 25544 51
6431 247
5797 0001752 323
5270 36
5764 15
55511001 34169
Satellite: ISS
Catalog Number: 25544
Epoch time: 15207
52457665 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 247
5797 deg
Eccentricity:
0001752
Arg of perigee: 323
5270 deg
Mean anomaly: 36
5764 deg
Mean motion: 15
55511001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3416
Checksum: 297
Coasting Arc #13 (Orbit 3431)
---------------------------------------
Vector Time (GMT): 2015/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2116721
52 A = 6775221
86 meter
Y = -4243690
38 meter E =
0005569
Z = 4835117
08 I = 51
30407
XDOT = 5028
476422 Wp = 111
64656
YDOT = 5267
596546 meter/sec RA = 241
75266 deg
ZDOT = 2417
632998 TA = 314
52125
MA = 314
56674
Ha = 218
462 n
mi
Hp = 212
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6944624
41 X = 2140531
20
Y = -13922868
70 feet Y = -4219887
07 meter
Z = 15863245
02 Z = 4845457
11
XDOT = 16497
626056 XDOT = 4957
455315
YDOT = 17282
140898 feet/sec YDOT = 5323
430972 meter/sec
ZDOT = 7931
866792 ZDOT = 2441
888059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15367702
74 X = -4684075
80
Y = 2114379
72 feet Y = 644462
94 meter
Z = 15908479
95 Z = 4848904
69
XDOT = 5280
819638 XDOT = 1609
593826
YDOT = -22179
818534 feet/sec YDOT = -6760
408689 meter/sec
ZDOT = 8035
249730 ZDOT = 2449
144118
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 15208
55248756
00016717 00000-0 10270-3 0 9128
2 25544 51
6418 242
4446 0001755 329
8633 30
2419 15
55541821 34323
Satellite: ISS
Catalog Number: 25544
Epoch time: 15208
55248756 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 242
4446 deg
Eccentricity:
0001755
Arg of perigee: 329
8633 deg
Mean anomaly: 30
2419 deg
Mean motion: 15
55541821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3432
Checksum: 305
Coasting Arc #14 (Orbit 3446)
---------------------------------------
Vector Time (GMT): 2015/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3539501
16 A = 6773203
30 meter
Y = 2333553
89 meter E =
0014104
Z = -5294468
18 I = 51
31421
XDOT = -4208
330387 Wp = 83
39840
YDOT = -6401
162111 meter/sec RA = 236
71593 deg
ZDOT = -6
368744 TA = 186
53138
MA = 186
54978
Ha = 218
534 n
mi
Hp = 212
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11612536
61 X = -3539614
24
Y = 7656016
69 feet Y = 2293972
68 meter
Z = -17370302
42 Z = -5311662
25
XDOT = -13806
858226 XDOT = -4136
407344
YDOT = -21001
188029 feet/sec YDOT = -6447
820276 meter/sec
ZDOT = -20
894828 ZDOT = -26
637588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12866885
39 X = 3921826
67
Y = 5031837
46 feet Y = 1533704
06 meter
Z = -17444680
46 Z = -5317138
60
XDOT = -8918
420517 XDOT = -2718
334574
YDOT = 22416
614597 feet/sec YDOT = 6832
584129 meter/sec
ZDOT = -106
948582 ZDOT = -32
597928
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 15209
51613343
00016717 00000-0 10270-3 0 9134
2 25544 51
6427 237
6304 0001843 331
2689 28
8363 15
55555896 34472
Satellite: ISS
Catalog Number: 25544
Epoch time: 15209
51613343 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 237
6304 deg
Eccentricity:
0001843
Arg of perigee: 331
2689 deg
Mean anomaly: 28
8363 deg
Mean motion: 15
55555896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3447
Checksum: 320
Coasting Arc #15 (Orbit 3462)
---------------------------------------
Vector Time (GMT): 2015/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4735977
61 A = 6774914
36 meter
Y = -247240
72 meter E =
0007465
Z = 4835670
05 I = 51
33724
XDOT = 2830
859378 Wp = 45
38007
YDOT = 6707
210316 meter/sec RA = 231
67965 deg
ZDOT = -2422
106464 TA = 68
50658
MA = 68
42701
Ha = 218
390 n
mi
Hp = 212
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15537984
28 X = 4714900
85
Y = -811157
21 feet Y = -194398
14 meter
Z = 15865059
22 Z = 4858624
91
XDOT = 9287
596384 XDOT = 2767
412831
YDOT = 22005
283188 feet/sec YDOT = 6738
512283 meter/sec
ZDOT = -7946
543517 ZDOT = -2408
508500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9724762
32 X = -2964107
55
Y = -12015457
97 feet Y = -3662311
59 meter
Z = 15963859
27 Z = 4865784
31
XDOT = 11443
317611 XDOT = 3487
923208
YDOT = -19775
722520 feet/sec YDOT = -6027
640224 meter/sec
ZDOT = -7889
221375 ZDOT = -2404
634675
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 15210
54399882
00016717 00000-0 10270-3 0 9149
2 25544 51
6410 232
4947 0001860 339
1680 20
9398 15
55624512 34638
Satellite: ISS
Catalog Number: 25544
Epoch time: 15210
54399882 = yrday
fracday
Element set: 914
Inclination: 51
6410 deg
RA of node: 232
4947 deg
Eccentricity:
0001860
Arg of perigee: 339
1680 deg
Mean anomaly: 20
9398 deg
Mean motion: 15
55624512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3463
Checksum: 311
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