[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 19th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 32291 73 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
077/23:47:09
199 -1
9 1
9 1
9
N/A 0
1 -0
2 222
0
000/00:04:18
398 0
4 0
1 210
9
Coasting Arc #1 (Orbit 1392)
---------------------------------------
Vector Time (GMT): 2015/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4676988
64 A = 6779028
12 meter
Y = -2834682
34 meter E =
0019348
Z = 3994140
67 I = 51
66357
XDOT = 5543
676117 Wp = 107
52117
YDOT = -3534
036212 meter/sec RA = 175
94252 deg
ZDOT = 3961
786219 TA = 301
23486
MA = 301
42429
Ha = 222
148 n
mi
Hp = 209
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15344450
91 X = -4664344
76
Y = -9300138
91 feet Y = -2886912
19 meter
Z = 13104136
07 Z = 3971452
17
XDOT = 18187
913771 XDOT = 5563
537882
YDOT = -11594
606995 feet/sec YDOT = -3471
931566 meter/sec
ZDOT = 12997
986283 ZDOT = 3988
764762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14538833
21 X = -4431436
36
Y = -10634550
78 feet Y = -3241411
08 meter
Z = 13007374
76 Z = 3964647
83
XDOT = 18289
211988 XDOT = 5574
551814
YDOT = -8876
657254 feet/sec YDOT = -2705
605131 meter/sec
ZDOT = 13114
085640 ZDOT = 3997
173303
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 15077
55563791
00016717 00000-0 10270-3 0 9008
2 25544 51
6461 176
7617 0008529 115
7184 244
4850 15
55374311 13939
Satellite: ISS
Catalog Number: 25544
Epoch time: 15077
55563791 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 176
7617 deg
Eccentricity:
0008529
Arg of perigee: 115
7184 deg
Mean anomaly: 244
4850 deg
Mean motion: 15
55374311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1393
Checksum: 321
Coasting Arc #2 (Orbit 1399)
---------------------------------------
Vector Time (GMT): 2015/077/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1719899
62 A = 6775934
08 meter
Y = 4210074
95 meter E =
0019801
Z = -5041081
64 I = 51
66499
XDOT = -7373
144118 Wp = 108
55598
YDOT = -693
844334 meter/sec RA = 173
44490 deg
ZDOT = 1936
170014 TA = 180
25559
MA = 180
25660
Ha = 222
003 n
mi
Hp = 210
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5642715
30 X = -1742362
41
Y = 13812581
87 feet Y = 4190715
53 meter
Z = -16538981
75 Z = -5049491
71
XDOT = -24190
105374 XDOT = -7374
242493
YDOT = -2276
392172 feet/sec YDOT = -776
301486 meter/sec
ZDOT = 6352
263825 ZDOT = 1900
350528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7245846
23 X = 2208533
93
Y = -12996589
03 feet Y = -3961360
34 meter
Z = -16575643
50 Z = -5052256
14
XDOT = 22797
375722 XDOT = 6948
640120
YDOT = 4804
342991 feet/sec YDOT = 1464
363744 meter/sec
ZDOT = 6198
924262 ZDOT = 1889
432115
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 15078
00539522
00016717 00000-0 10270-3 0 9015
2 25544 51
6455 174
5178 0006868 115
7050 244
4813 15
55024975 14002
Satellite: ISS
Catalog Number: 25544
Epoch time: 15078
00539522 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 174
5178 deg
Eccentricity:
0006868
Arg of perigee: 115
7050 deg
Mean anomaly: 244
4813 deg
Mean motion: 15
55024975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1400
Checksum: 301
Coasting Arc #3 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2015/078/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3703467
87 A = 6779579
48 meter
Y = -3996052
71 meter E =
0016561
Z = 4019533
08 I = 51
70902
XDOT = 6317
309596 Wp = 94
07199
YDOT = 1881
444979 meter/sec RA = 168
44733 deg
ZDOT = -3937
303583 TA = 36
78043
MA = 36
66691
Ha = 221
818 n
mi
Hp = 210
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12150485
15 X = 3728352
16
Y = -13110409
17 feet Y = -3954498
31 meter
Z = 13187444
50 Z = 4037584
81
XDOT = 20726
081353 XDOT = 6314
927153
YDOT = 6172
719747 feet/sec YDOT = 1952
075281 meter/sec
ZDOT = -12917
662675 ZDOT = -3906
621609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13433510
70 X = -4094534
06
Y = 11704538
21 feet Y = 3567543
25 meter
Z = 13265383
01 Z = 4043288
74
XDOT = -19150
292699 XDOT = -5837
009215
YDOT = -7440
169207 feet/sec YDOT = -2267
763574 meter/sec
ZDOT = -12786
499600 ZDOT = -3897
325078
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 15079
03360897
00016717 00000-0 10270-3 0 9027
2 25544 51
6453 169
3854 0006886 118
7550 241
4296 15
55089922 14163
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
03360897 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 169
3854 deg
Eccentricity:
0006886
Arg of perigee: 118
7550 deg
Mean anomaly: 241
4296 deg
Mean motion: 15
55089922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1416
Checksum: 334
Coasting Arc #4 (Orbit 1430)
---------------------------------------
Vector Time (GMT): 2015/079/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5241945
72 A = 6783690
25 meter
Y = 3557651
89 meter E =
0009833
Z = -2434215
04 I = 51
75491
XDOT = -4550
134893 Wp = 90
40053
YDOT = -3052
582901 meter/sec RA = 163
46477 deg
ZDOT = 5355
679922 TA = 242
42576
MA = 242
52567
Ha = 221
674 n
mi
Hp = 210
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17197984
66 X = -5269514
14
Y = 11672086
27 feet Y = 3498878
48 meter
Z = -7986269
82 Z = -2459746
92
XDOT = -14928
264086 XDOT = -4541
677878
YDOT = -10015
035763 feet/sec YDOT = -3103
417301 meter/sec
ZDOT = 17571
128352 ZDOT = 5333
597327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18155356
69 X = 5533752
72
Y = -10031120
41 feet Y = -3057485
50 meter
Z = -8096198
27 Z = -2467721
23
XDOT = 13314
609330 XDOT = 4058
292924
YDOT = 10041
000628 feet/sec YDOT = 3060
496991 meter/sec
ZDOT = 17476
977130 ZDOT = 5326
982629
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 15079
99751542
00016717 00000-0 10270-3 0 9034
2 25544 51
6458 164
5729 0006808 121
7335 238
4482 15
55178007 14318
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
99751542 = yrday
fracday
Element set: 903
Inclination: 51
6458 deg
RA of node: 164
5729 deg
Eccentricity:
0006808
Arg of perigee: 121
7335 deg
Mean anomaly: 238
4482 deg
Mean motion: 15
55178007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1431
Checksum: 326
Coasting Arc #5 (Orbit 1446)
---------------------------------------
Vector Time (GMT): 2015/080/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6166433
07 A = 6786108
96 meter
Y = -2780257
07 meter E =
0019699
Z = 414599
98 I = 51
79305
XDOT = 2300
577734 Wp = 128
88799
YDOT = 4179
331038 meter/sec RA = 158
49614 deg
ZDOT = -6011
454440 TA = 46
64664
MA = 46
48267
Ha = 221
620 n
mi
Hp = 210
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20231079
63 X = 6195050
28
Y = -9121578
32 feet Y = -2711139
92 meter
Z = 1360236
14 Z = 444625
33
XDOT = 7547
827212 XDOT = 2282
873965
YDOT = 13711
716003 feet/sec YDOT = 4204
957680 meter/sec
ZDOT = -19722
619554 ZDOT = -6000
322298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20853644
08 X = -6356190
71
Y = 7566868
23 feet Y = 2306381
44 meter
Z = 1489312
12 Z = 453942
33
XDOT = -6062
749531 XDOT = -1847
926057
YDOT = -12730
047895 feet/sec YDOT = -3880
118599 meter/sec
ZDOT = -19675
555893 ZDOT = -5997
109436
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 15081
02563770
00016717 00000-0 10270-3 0 9046
2 25544 51
6456 159
4393 0006815 125
5002 234
6788 15
55208640 14478
Satellite: ISS
Catalog Number: 25544
Epoch time: 15081
02563770 = yrday
fracday
Element set: 904
Inclination: 51
6456 deg
RA of node: 159
4393 deg
Eccentricity:
0006815
Arg of perigee: 125
5002 deg
Mean anomaly: 234
6788 deg
Mean motion: 15
55208640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1447
Checksum: 308
Coasting Arc #6 (Orbit 1462)
---------------------------------------
Vector Time (GMT): 2015/081/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6349449
26 A = 6784866
87 meter
Y = 1724174
72 meter E =
0017870
Z = 1636013
75 I = 51
81844
XDOT = 108
240665 Wp = 82
93763
YDOT = -5092
306604 meter/sec RA = 153
53129 deg
ZDOT = 5735
337434 TA = 294
94015
MA = 295
12572
Ha = 221
419 n
mi
Hp = 210
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20831526
46 X = -6376204
67
Y = 5656741
22 feet Y = 1653021
66 meter
Z = 5367499
20 Z = 1605103
99
XDOT = 355
120292 XDOT = 137
315737
YDOT = -16707
042663 feet/sec YDOT = -5090
932838 meter/sec
ZDOT = 18816
723865 ZDOT = 5735
934562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21160014
54 X = 6449572
43
Y = -4428557
65 feet Y = -1349824
37 meter
Z = 5234780
34 Z = 1595561
05
XDOT = -1534
269253 XDOT = -467
645268
YDOT = 15120
070782 feet/sec YDOT = 4608
597574 meter/sec
ZDOT = 18820
063867 ZDOT = 5736
355467
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 15082
05371215
00016717 00000-0 10270-3 0 9052
2 25544 51
6453 154
3053 0006642 127
2119 232
9641 15
55294052 14637
Satellite: ISS
Catalog Number: 25544
Epoch time: 15082
05371215 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 154
3053 deg
Eccentricity:
0006642
Arg of perigee: 127
2119 deg
Mean anomaly: 232
9641 deg
Mean motion: 15
55294052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1463
Checksum: 283
Coasting Arc #7 (Orbit 1477)
---------------------------------------
Vector Time (GMT): 2015/082/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5797756
03 A = 6780636
46 meter
Y = -314382
56 meter E =
0010685
Z = -3506380
13 I = 51
83296
XDOT = -2431
569223 Wp = 112
98163
YDOT = 5673
025602 meter/sec RA = 148
55920 deg
ZDOT = -4544
274821 TA = 108
12889
MA = 108
01250
Ha = 221
250 n
mi
Hp = 210
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19021509
29 X = 5817873
39
Y = -1031438
84 feet Y = -249436
19 meter
Z = -11503871
83 Z = -3478166
73
XDOT = -7977
589314 XDOT = -2472
751124
YDOT = 18612
288721 feet/sec YDOT = 5645
603421 meter/sec
ZDOT = -14909
038126 ZDOT = -4556
187651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19120420
97 X = -5827904
31
Y = 244097
71 feet Y = 74400
98 meter
Z = -11382911
18 Z = -3469511
33
XDOT = 8661
505581 XDOT = 2640
026901
YDOT = -16875
756321 feet/sec YDOT = -5143
730527 meter/sec
ZDOT = -14960
970940 ZDOT = -4560
103943
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 15083
01748878
00016717 00000-0 10270-3 0 9063
2 25544 51
6454 149
4918 0006513 131
7259 228
4453 15
55361025 14787
Satellite: ISS
Catalog Number: 25544
Epoch time: 15083
01748878 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 149
4918 deg
Eccentricity:
0006513
Arg of perigee: 131
7259 deg
Mean anomaly: 228
4453 deg
Mean motion: 15
55361025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1478
Checksum: 324
Coasting Arc #8 (Orbit 1493)
---------------------------------------
Vector Time (GMT): 2015/083/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4620276
31 A = 6775906
93 meter
Y = -1263771
31 meter E =
0014044
Z = 4786164
12 I = 51
84426
XDOT = 4323
684327 Wp = 125
60053
YDOT = -5766
527090 meter/sec RA = 143
57304 deg
ZDOT = 2637
789553 TA = 298
41129
MA = 298
55277
Ha = 221
200 n
mi
Hp = 210
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15158386
84 X = -4629050
60
Y = -4146231
32 feet Y = -1315486
84 meter
Z = 15702638
19 Z = 4763698
46
XDOT = 14185
316034 XDOT = 4375
032216
YDOT = -18919
052134 feet/sec YDOT = -5717
889464 meter/sec
ZDOT = 8654
165200 ZDOT = 2658
918531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15153585
25 X = 4618812
78
Y = 4510580
74 feet Y = 1374825
01 meter
Z = 15606546
30 Z = 4756875
31
XDOT = -14252
094164 XDOT = -4344
038301
YDOT = 17467
985310 feet/sec YDOT = 5324
241923 meter/sec
ZDOT = 8745
628071 ZDOT = 2665
667436
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 15084
04547360
00016717 00000-0 10270-3 0 9071
2 25544 51
6453 144
3572 0006577 133
5894 226
5806 15
55434819 14942
Satellite: ISS
Catalog Number: 25544
Epoch time: 15084
04547360 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 144
3572 deg
Eccentricity:
0006577
Arg of perigee: 133
5894 deg
Mean anomaly: 226
5806 deg
Mean motion: 15
55434819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1494
Checksum: 327
Coasting Arc #9 (Orbit 1508)
---------------------------------------
Vector Time (GMT): 2015/084/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2983308
38 A = 6773311
40 meter
Y = 2951870
62 meter E =
0019632
Z = -5332759
69 I = 51
86119
XDOT = -5603
584080 Wp = 102
46454
YDOT = 5211
591681 meter/sec RA = 138
57465 deg
ZDOT = -254
931460 TA = 165
13819
MA = 165
08041
Ha = 220
824 n
mi
Hp = 210
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9787757
17 X = 2975982
72
Y = 9684614
88 feet Y = 2985190
47 meter
Z = -17495930
74 Z = -5318285
41
XDOT = -18384
462204 XDOT = -5660
206499
YDOT = 17098
397902 feet/sec YDOT = 5148
612127 meter/sec
ZDOT = -836
389306 ZDOT = -282
290608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9831985
28 X = -2996789
11
Y = -9750639
98 feet Y = -2971995
07 meter
Z = -17434352
11 Z = -5313990
52
XDOT = 17784
426916 XDOT = 5420
693324
YDOT = -16255
085289 feet/sec YDOT = -4954
549996 meter/sec
ZDOT = -954
488905 ZDOT = -290
928218
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 15085
00916587
00016717 00000-0 10270-3 0 9080
2 25544 51
6450 139
5426 0006412 137
2313 222
9341 15
55529070 15093
Satellite: ISS
Catalog Number: 25544
Epoch time: 15085
00916587 = yrday
fracday
Element set: 908
Inclination: 51
6450 deg
RA of node: 139
5426 deg
Eccentricity:
0006412
Arg of perigee: 137
2313 deg
Mean anomaly: 222
9341 deg
Mean motion: 15
55529070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1509
Checksum: 297
Coasting Arc #10 (Orbit 1524)
---------------------------------------
Vector Time (GMT): 2015/085/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1134535
51 A = 6774531
79 meter
Y = -4457575
84 meter E =
0009349
Z = 4965187
03 I = 51
88971
XDOT = 6175
292897 Wp = 99
67517
YDOT = -4005
685703 meter/sec RA = 133
57691 deg
ZDOT = -2183
173439 TA = 11
52147
MA = 11
50009
Ha = 220
658 n
mi
Hp = 210
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3722229
38 X = -1108724
50
Y = -14624592
65 feet Y = -4470118
19 meter
Z = 16289983
71 Z = 4959738
79
XDOT = 20260
147301 XDOT = 6230
231483
YDOT = -13142
013460 feet/sec YDOT = -3936
322562 meter/sec
ZDOT = -7162
642518 ZDOT = -2153
041323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3976676
66 X = 1212091
04
Y = 14582766
10 feet Y = 4444827
11 meter
Z = 16267336
80 Z = 4958284
26
XDOT = -19104
621105 XDOT = -5823
088513
YDOT = 13062
173776 feet/sec YDOT = 3981
350567 meter/sec
ZDOT = -7032
827656 ZDOT = -2143
605869
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 15086
03705975
00016717 00000-0 10270-3 0 9092
2 25544 51
6453 134
4077 0006315 141
2033 218
9575 15
55616274 15253
Satellite: ISS
Catalog Number: 25544
Epoch time: 15086
03705975 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 134
4077 deg
Eccentricity:
0006315
Arg of perigee: 141
2033 deg
Mean anomaly: 218
9575 deg
Mean motion: 15
55616274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1525
Checksum: 309
Coasting Arc #11 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2015/086/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -683328
74 A = 6778851
04 meter
Y = 5597928
36 meter E =
0011496
Z = -3775323
25 I = 51
92497
XDOT = -5988
305307 Wp = 124
67349
YDOT = 2144
848251 meter/sec RA = 128
59019 deg
ZDOT = 4267
038008 TA = 190
36145
MA = 190
38516
Ha = 220
480 n
mi
Hp = 210
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2241892
20 X = -727536
29
Y = 18365906
70 feet Y = 5590039
39 meter
Z = -12386231
12 Z = -3778750
63
XDOT = -19646
670956 XDOT = -6032
572031
YDOT = 7036
903711 feet/sec YDOT = 2077
636013 meter/sec
ZDOT = 13999
468530 ZDOT = 4237
840384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1656463
85 X = 504890
18
Y = -18417443
44 feet Y = -5613636
76 meter
Z = -12401823
90 Z = -3780075
92
XDOT = 18190
648604 XDOT = 5544
509695
YDOT = -7699
994072 feet/sec YDOT = -2346
958193 meter/sec
ZDOT = 13873
941108 ZDOT = 4228
777250
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 15087
00067007
00016717 00000-0 10270-3 0 9109
2 25544 51
6446 129
5927 0006306 144
5683 215
5890 15
55650392 15400
Satellite: ISS
Catalog Number: 25544
Epoch time: 15087
00067007 = yrday
fracday
Element set: 910
Inclination: 51
6446 deg
RA of node: 129
5927 deg
Eccentricity:
0006306
Arg of perigee: 144
5683 deg
Mean anomaly: 215
5890 deg
Mean motion: 15
55650392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1540
Checksum: 303
Coasting Arc #12 (Orbit 1555)
---------------------------------------
Vector Time (GMT): 2015/087/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2281736
48 A = 6783180
90 meter
Y = -6092083
34 meter E =
0019548
Z = 1882930
89 I = 51
95928
XDOT = 5189
880392 Wp = 123
75289
YDOT = 186
245305 meter/sec RA = 123
62226 deg
ZDOT = -5655
161304 TA = 35
57484
MA = 35
44468
Ha = 220
347 n
mi
Hp = 210
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7486012
07 X = 2340543
49
Y = -19987150
06 feet Y = -6066238
46 meter
Z = 6177594
77 Z = 1894158
55
XDOT = 17027
166640 XDOT = 5214
882530
YDOT = 611
041027 feet/sec YDOT = 244
421123 meter/sec
ZDOT = -18553
678818 ZDOT = -5629
889313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6544955
46 X = -1994902
43
Y = 20299771
53 feet Y = 6187370
36 meter
Z = 6226721
06 Z = 1897904
58
XDOT = -15674
334415 XDOT = -4777
537130
YDOT = 635
559230 feet/sec YDOT = 193
718453 meter/sec
ZDOT = -18445
347026 ZDOT = -5622
141773
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 15088
02847577
00016717 00000-0 10270-3 0 9111
2 25544 51
6449 124
4573 0006340 147
1534 213
0014 15
55720306 15567
Satellite: ISS
Catalog Number: 25544
Epoch time: 15088
02847577 = yrday
fracday
Element set: 911
Inclination: 51
6449 deg
RA of node: 124
4573 deg
Eccentricity:
0006340
Arg of perigee: 147
1534 deg
Mean anomaly: 213
0014 deg
Mean motion: 15
55720306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1556
Checksum: 292
Coasting Arc #13 (Orbit 1571)
---------------------------------------
Vector Time (GMT): 2015/088/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3468135
24 A = 6784453
02 meter
Y = 5819332
50 meter E =
0012790
Z = 321792
32 I = 51
97984
XDOT = -3910
125413 Wp = 77
41601
YDOT = -2674
684850 meter/sec RA = 118
66519 deg
ZDOT = 6029
158910 TA = 286
03692
MA = 286
17774
Ha = 220
147 n
mi
Hp = 210
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11378396
45 X = -3534513
77
Y = 19092298
23 feet Y = 5780178
44 meter
Z = 1055749
09 Z = 304782
97
XDOT = -12828
495448 XDOT = -3909
213067
YDOT = -8775
212763 feet/sec YDOT = -2718
404600 meter/sec
ZDOT = 19780
705085 ZDOT = 6010
166935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10180808
43 X = 3103110
41
Y = -19760704
58 feet Y = -6023062
76 meter
Z = 981864
34 Z = 299272
25
XDOT = 12031
148001 XDOT = 3667
093911
YDOT = 7212
144479 feet/sec YDOT = 2198
261637 meter/sec
ZDOT = 19699
699905 ZDOT = 6004
468531
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 15089
05623387
00016717 00000-0 10270-3 0 9127
2 25544 51
6437 119
3204 0006334 151
8784 208
2712 15
55793795 15721
Satellite: ISS
Catalog Number: 25544
Epoch time: 15089
05623387 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 119
3204 deg
Eccentricity:
0006334
Arg of perigee: 151
8784 deg
Mean anomaly: 208
2712 deg
Mean motion: 15
55793795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1572
Checksum: 322
Coasting Arc #14 (Orbit 1586)
---------------------------------------
Vector Time (GMT): 2015/089/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213527
37 A = 6781685
52 meter
Y = -4664893
34 meter E =
0011346
Z = -2535833
94 I = 51
98449
XDOT = 2346
959268 Wp = 144
30488
YDOT = 5001
112222 meter/sec RA = 113
70777 deg
ZDOT = -5321
205556 TA = 64
04489
MA = 63
92803
Ha = 220
066 n
mi
Hp = 210
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13823908
68 X = 4277696
22
Y = -15304768
18 feet Y = -4617416
47 meter
Z = -8319665
15 Z = -2515209
07
XDOT = 7699
997597 XDOT = 2316
709511
YDOT = 16407
848496 feet/sec YDOT = 5027
187613 meter/sec
ZDOT = -17458
023477 ZDOT = -5309
878678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12622599
35 X = -3847368
28
Y = 16354902
06 feet Y = 4984974
15 meter
Z = -8230453
97 Z = -2508642
37
XDOT = -7890
920652 XDOT = -2405
152615
YDOT = -14816
823027 feet/sec YDOT = -4516
167659 meter/sec
ZDOT = -17410
268693 ZDOT = -5306
649898
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 15090
01971592
00016717 00000-0 10270-3 0 9130
2 25544 51
6428 114
5051 0006328 155
6787 204
4666 15
55838047 15878
Satellite: ISS
Catalog Number: 25544
Epoch time: 15090
01971592 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 114
5051 deg
Eccentricity:
0006328
Arg of perigee: 155
6787 deg
Mean anomaly: 204
4666 deg
Mean motion: 15
55838047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1587
Checksum: 322
Coasting Arc #15 (Orbit 1602)
---------------------------------------
Vector Time (GMT): 2015/090/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4464211
05 A = 6776569
98 meter
Y = 2795946
26 meter E =
0014749
Z = 4258594
24 I = 51
97930
XDOT = -723
047140 Wp = 125
94465
YDOT = -6718
017583 meter/sec RA = 108
73473 deg
ZDOT = 3635
497388 TA = 287
00050
MA = 287
16207
Ha = 219
904 n
mi
Hp = 210
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14646361
73 X = -4515830
80
Y = 9173052
05 feet Y = 2745736
52 meter
Z = 13971765
87 Z = 4236782
26
XDOT = -2372
201902 XDOT = -665
530771
YDOT = -22040
740102 feet/sec YDOT = -6725
781060 meter/sec
ZDOT = 11927
484870 ZDOT = 3632
125632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13783635
19 X = 4201252
00
Y = -10549414
26 feet Y = -3215461
47 meter
Z = 13877762
69 Z = 4229942
07
XDOT = 3787
747309 XDOT = 1154
505380
YDOT = 20696
803434 feet/sec YDOT = 6308
385687 meter/sec
ZDOT = 11914
133933 ZDOT = 3631
428023
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 15091
04738449
00016717 00000-0 10270-3 0 9147
2 25544 51
6423 109
3673 0006276 158
8815 201
2599 15
55902927 16032
Satellite: ISS
Catalog Number: 25544
Epoch time: 15091
04738449 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 109
3673 deg
Eccentricity:
0006276
Arg of perigee: 158
8815 deg
Mean anomaly: 201
2599 deg
Mean motion: 15
55902927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1603
Checksum: 323
Coasting Arc #16 (Orbit 1617)
---------------------------------------
Vector Time (GMT): 2015/091/23:49:18
398
Vector Time (MET): N/A
Weight (LBS) : 889206
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4300938
80 A = 6772446
32 meter
Y = -364240
13 meter E =
0016365
Z = -5231732
36 I = 51
97435
XDOT = -849
064218 Wp = 103
62800
YDOT = 7513
545136 meter/sec RA = 103
74410 deg
ZDOT = -1228
070989 TA = 154
66979
MA = 154
58947
Ha = 219
709 n
mi
Hp = 210
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14110691
62 X = 4330105
97
Y = -1195013
55 feet Y = -315981
91 meter
Z = -17164476
25 Z = -5210768
34
XDOT = -2785
643759 XDOT = -927
053847
YDOT = 24650
738635 feet/sec YDOT = 7503
614098 meter/sec
ZDOT = -4029
104293 ZDOT = -1232
386118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13992108
75 X = -4264794
75
Y = 2800175
99 feet Y = 853493
64 meter
Z = -17074508
12 Z = -5204310
07
XDOT = 152
991765 XDOT = 46
631890
YDOT = -23784
043936 feet/sec YDOT = -7249
376592 meter/sec
ZDOT = -4048
861847 ZDOT = -1234
093091
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 15092
01077939
00016717 00000-0 10270-3 0 9156
2 25544 51
6410 104
5503 0006453 162
0390 198
0993 15
55988703 16182
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
01077939 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 104
5503 deg
Eccentricity:
0006453
Arg of perigee: 162
0390 deg
Mean anomaly: 198
0993 deg
Mean motion: 15
55988703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1618
Checksum: 312
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