[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 17th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21689 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 219 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
057/09:19:24
589 0
0 2
7 2
7
N/A 2
6 -0
2 222
4
000/00:05:49
177 0
6 0
2 211
1
062/07:21:38
442 -0
6 1
4 1
4
N/A -1
3 -0
1 222
4
000/00:03:16
884 -0
0 0
1 211
2
Coasting Arc #1 (Orbit 925)
---------------------------------------
Vector Time (GMT): 2015/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -276511
25 A = 6777412
65 meter
Y = 4783577
10 meter E =
0012330
Z = 4790564
50 I = 51
43485
XDOT = -6899
156030 Wp = 37
82875
YDOT = 2172
631032 meter/sec RA = 326
16499 deg
ZDOT = -2554
626492 TA = 77
44874
MA = 77
31085
Ha = 221
194 n
mi
Hp = 212
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -907189
13 X = -353252
02
Y = 15694150
58 feet Y = 4780056
10 meter
Z = 15717075
13 Z = 4789034
68
XDOT = -22635
026346 XDOT = -6910
529009
YDOT = 7128
054567 feet/sec YDOT = 2095
416468 meter/sec
ZDOT = -8381
320513 ZDOT = -2588
168210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9756877
92 X = -2973896
39
Y = 12335611
18 feet Y = 3759894
29 meter
Z = 15709609
65 Z = 4788289
02
XDOT = -21726
501857 XDOT = -6622
237766
YDOT = -6273
040190 feet/sec YDOT = -1912
022650 meter/sec
ZDOT = -8525
219737 ZDOT = -2598
486976
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 15047
54366566
00016717 00000-0 10270-3 0 9005
2 25544 51
6460 326
5598 0006214 10
6037 349
5246 15
54877732 9261
Satellite: ISS
Catalog Number: 25544
Epoch time: 15047
54366566 = yrday
fracday
Element set: 900
Inclination: 51
6460 deg
RA of node: 326
5598 deg
Eccentricity:
0006214
Arg of perigee: 10
6037 deg
Mean anomaly: 349
5246 deg
Mean motion: 15
54877732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 926
Checksum: 320
Coasting Arc #2 (Orbit 940)
---------------------------------------
Vector Time (GMT): 2015/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1995683
03 A = 6781380
07 meter
Y = -5351959
07 meter E =
0008618
Z = -3656530
81 I = 51
42343
XDOT = 6286
781467 Wp = 53
19789
YDOT = -614
884344 meter/sec RA = 321
15380 deg
ZDOT = 4343
394727 TA = 263
20016
MA = 263
29823
Ha = 221
185 n
mi
Hp = 212
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6547516
49 X = 2073143
18
Y = -17558920
83 feet Y = -5329209
18 meter
Z = -11996492
17 Z = -3646647
92
XDOT = 20625
923447 XDOT = 6272
091953
YDOT = -2017
337085 feet/sec YDOT = -544
663302 meter/sec
ZDOT = 14249
982701 ZDOT = 4373
898278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15250869
74 X = 4648465
10
Y = -10937713
42 feet Y = -3333815
05 meter
Z = -11953196
01 Z = -3643334
14
XDOT = 17407
632123 XDOT = 5305
846271
YDOT = 8600
204867 feet/sec YDOT = 2621
342443 meter/sec
ZDOT = 14380
582683 ZDOT = 4383
201602
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 15048
50772115
00016717 00000-0 10270-3 0 9014
2 25544 51
6466 321
7483 0006176 14
0789 346
0535 15
54924415 9417
Satellite: ISS
Catalog Number: 25544
Epoch time: 15048
50772115 = yrday
fracday
Element set: 901
Inclination: 51
6466 deg
RA of node: 321
7483 deg
Eccentricity:
0006176
Arg of perigee: 14
0789 deg
Mean anomaly: 346
0535 deg
Mean motion: 15
54924415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 941
Checksum: 305
Coasting Arc #3 (Orbit 956)
---------------------------------------
Vector Time (GMT): 2015/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3451962
56 A = 6785348
45 meter
Y = 5495252
68 meter E =
0014771
Z = 1970130
51 I = 51
41269
XDOT = -5136
555366 Wp = 87
73849
YDOT = -1219
565142 meter/sec RA = 316
15465 deg
ZDOT = -5561
574966 TA = 70
44477
MA = 70
28534
Ha = 221
211 n
mi
Hp = 212
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11325336
50 X = -3522725
13
Y = 18029044
24 feet Y = 5456255
11 meter
Z = 6463682
76 Z = 1953189
60
XDOT = -16852
215768 XDOT = -5095
520784
YDOT = -4001
197971 feet/sec YDOT = -1276
776525 meter/sec
ZDOT = -18246
637026 ZDOT = -5586
426936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19305147
43 X = -5884208
94
Y = 9031375
75 feet Y = 2752763
33 meter
Z = 6390180
95 Z = 1947727
15
XDOT = -11262
452614 XDOT = -3432
795557
YDOT = -11002
464802 feet/sec YDOT = -3353
551272 meter/sec
ZDOT = -18352
711665 ZDOT = -5593
906516
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 15049
53601873
00016717 00000-0 10270-3 0 9021
2 25544 51
6464 316
6162 0006105 17
8629 342
2737 15
54945316 9570
Satellite: ISS
Catalog Number: 25544
Epoch time: 15049
53601873 = yrday
fracday
Element set: 902
Inclination: 51
6464 deg
RA of node: 316
6162 deg
Eccentricity:
0006105
Arg of perigee: 17
8629 deg
Mean anomaly: 342
2737 deg
Mean motion: 15
54945316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 957
Checksum: 315
Coasting Arc #4 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2015/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4438137
93 A = 6786813
40 meter
Y = -5121602
68 meter E =
0017894
Z = -37355
18 I = 51
39608
XDOT = 3635
070738 Wp = 36
65728
YDOT = 3117
173012 meter/sec RA = 311
16280 deg
ZDOT = 5997
435780 TA = 322
93860
MA = 323
06205
Ha = 221
183 n
mi
Hp = 212
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14560819
96 X = 4495260
50
Y = -16803158
39 feet Y = -5071653
14 meter
Z = -122556
38 Z = -15656
75
XDOT = 11926
085100 XDOT = 3570
810985
YDOT = 10226
945577 feet/sec YDOT = 3157
464133 meter/sec
ZDOT = 19676
626574 ZDOT = 6014
937402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21220284
58 X = 6467942
74
Y = -6639075
50 feet Y = -2023590
21 meter
Z = -28788
73 Z = -8774
81
XDOT = 4177
534234 XDOT = 1273
312435
YDOT = 13357
698093 feet/sec YDOT = 4071
426379 meter/sec
ZDOT = 19750
905682 ZDOT = 6020
076052
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 15050
50001976
00016717 00000-0 10270-3 0 9039
2 25544 51
6465 311
8046 0006191 20
1318 340
0078 15
54995580 9725
Satellite: ISS
Catalog Number: 25544
Epoch time: 15050
50001976 = yrday
fracday
Element set: 903
Inclination: 51
6465 deg
RA of node: 311
8046 deg
Eccentricity:
0006191
Arg of perigee: 20
1318 deg
Mean anomaly: 340
0078 deg
Mean motion: 15
54995580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 972
Checksum: 288
Coasting Arc #5 (Orbit 987)
---------------------------------------
Vector Time (GMT): 2015/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4984677
20 A = 6785049
73 meter
Y = 4170273
64 meter E =
0006727
Z = -1955619
28 I = 51
37048
XDOT = -1924
785054 Wp = 87
06164
YDOT = -4902
812134 meter/sec RA = 306
16957 deg
ZDOT = -5565
223137 TA = 114
58299
MA = 114
51288
Ha = 221
145 n
mi
Hp = 212
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16353927
81 X = -5021440
22
Y = 13682000
13 feet Y = 4114325
93 meter
Z = -6416073
75 Z = -1979923
24
XDOT = -6314
911594 XDOT = -1842
784338
YDOT = -16085
341647 feet/sec YDOT = -4923
878556 meter/sec
ZDOT = -18258
606091 ZDOT = -5574
373394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21013451
59 X = -6404900
05
Y = 3424639
30 feet Y = 1043830
06 meter
Z = -6520796
18 Z = -1987538
67
XDOT = 3141
349461 XDOT = 957
483316
YDOT = -15463
476663 feet/sec YDOT = -4713
267687 meter/sec
ZDOT = -18296
837777 ZDOT = -5576
876155
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 15051
52825967
00016717 00000-0 10270-3 0 9047
2 25544 51
6465 306
6719 0005997 23
3167 336
8257 15
55022589 9884
Satellite: ISS
Catalog Number: 25544
Epoch time: 15051
52825967 = yrday
fracday
Element set: 904
Inclination: 51
6465 deg
RA of node: 306
6719 deg
Eccentricity:
0005997
Arg of perigee: 23
3167 deg
Mean anomaly: 336
8257 deg
Mean motion: 15
55022589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 988
Checksum: 345
Coasting Arc #6 (Orbit 1003)
---------------------------------------
Vector Time (GMT): 2015/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5033746
36 A = 6780840
02 meter
Y = -2696832
78 meter E =
0015276
Z = 3639435
69 I = 51
33863
XDOT = 238
511761 Wp = 72
53172
YDOT = 6324
327295 meter/sec RA = 301
16436 deg
ZDOT = 4345
879108 TA = 330
96208
MA = 331
04696
Ha = 221
081 n
mi
Hp = 211
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16514915
89 X = 5045850
10
Y = -8847876
56 feet Y = -2640473
99 meter
Z = 11940405
81 Z = 3663918
04
XDOT = 782
518901 XDOT = 146
663564
YDOT = 20749
105298 feet/sec YDOT = 6326
481498 meter/sec
ZDOT = 14258
133557 ZDOT = 4346
813829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18662227
20 X = 5688246
85
Y = 474556
75 feet Y = 144644
90 meter
Z = 12045610
37 Z = 3671502
04
XDOT = -9659
271270 XDOT = -2944
145883
YDOT = 16999
016570 feet/sec YDOT = 5181
300251 meter/sec
ZDOT = 14260
973403 ZDOT = 4346
744693
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 15052
55647029
00016717 00000-0 10270-3 0 9053
2 25544 51
6461 301
5386 0006197 27
3070 332
8408 15
55077264 10048
Satellite: ISS
Catalog Number: 25544
Epoch time: 15052
55647029 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 301
5386 deg
Eccentricity:
0006197
Arg of perigee: 27
3070 deg
Mean anomaly: 332
8408 deg
Mean motion: 15
55077264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1004
Checksum: 295
Coasting Arc #7 (Orbit 1018)
---------------------------------------
Vector Time (GMT): 2015/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4702262
06 A = 6776380
21 meter
Y = 803367
58 meter E =
0016741
Z = -4828560
03 I = 51
30857
XDOT = 1307
997106 Wp = 57
59429
YDOT = -7132
670035 meter/sec RA = 296
14327 deg
ZDOT = -2457
960781 TA = 188
10685
MA = 188
13393
Ha = 221
100 n
mi
Hp = 211
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15427368
95 X = -4687440
94
Y = 2635720
42 feet Y = 750866
11 meter
Z = -15841732
40 Z = -4851366
56
XDOT = 4291
329089 XDOT = 1399
598816
YDOT = -23401
148409 feet/sec YDOT = -7117
531279 meter/sec
ZDOT = -8064
175790 ZDOT = -2451
383507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14703615
61 X = -4481662
04
Y = -5064567
37 feet Y = -1543680
13 meter
Z = -15939418
61 Z = -4858334
79
XDOT = 14696
512078 XDOT = 4479
496881
YDOT = -17353
968886 feet/sec YDOT = -5289
489716 meter/sec
ZDOT = -8034
749329 ZDOT = -2448
991596
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 15053
52038960
00016717 00000-0 10270-3 0 9060
2 25544 51
6458 296
7261 0006128 28
9088 331
2404 15
55148379 10192
Satellite: ISS
Catalog Number: 25544
Epoch time: 15053
52038960 = yrday
fracday
Element set: 906
Inclination: 51
6458 deg
RA of node: 296
7261 deg
Eccentricity:
0006128
Arg of perigee: 28
9088 deg
Mean anomaly: 331
2404 deg
Mean motion: 15
55148379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1019
Checksum: 316
Coasting Arc #8 (Orbit 1034)
---------------------------------------
Vector Time (GMT): 2015/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4029641
41 A = 6774264
93 meter
Y = 1311955
24 meter E =
0007404
Z = 5279949
93 I = 51
28882
XDOT = -2610
233829 Wp = 50
07729
YDOT = 7214
864937 meter/sec RA = 291
10964 deg
ZDOT = 203
865592 TA = 37
99811
MA = 37
94589
Ha = 220
953 n
mi
Hp = 211
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13220608
30 X = 3989023
54
Y = 4304315
10 feet Y = 1356790
77 meter
Z = 17322670
38 Z = 5299426
17
XDOT = -8563
759283 XDOT = -2691
708448
YDOT = 23670
816721 feet/sec YDOT = 7185
220070 meter/sec
ZDOT = 668
850367 ZDOT = 190
987046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9593847
61 X = 2924204
75
Y = 9918931
20 feet Y = 3023290
23 meter
Z = 17405729
32 Z = 5305266
30
XDOT = -17887
401154 XDOT = -5452
079872
YDOT = 16252
089486 feet/sec YDOT = 4953
636875 meter/sec
ZDOT = 612
468708 ZDOT = 186
680462
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 15054
54854322
00016717 00000-0 10270-3 0 9072
2 25544 51
6459 291
5924 0006065 32
8134 327
3395 15
55189147 10359
Satellite: ISS
Catalog Number: 25544
Epoch time: 15054
54854322 = yrday
fracday
Element set: 907
Inclination: 51
6459 deg
RA of node: 291
5924 deg
Eccentricity:
0006065
Arg of perigee: 32
8134 deg
Mean anomaly: 327
3395 deg
Mean motion: 15
55189147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1035
Checksum: 315
Coasting Arc #9 (Orbit 1049)
---------------------------------------
Vector Time (GMT): 2015/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3167783
91 A = 6775615
09 meter
Y = -3373383
13 meter E =
0015661
Z = -4962182
65 I = 51
28258
XDOT = 3594
356377 Wp = 84
00914
YDOT = -6433
616948 meter/sec RA = 286
07348 deg
ZDOT = 2086
406723 TA = 206
38493
MA = 206
46477
Ha = 221
016 n
mi
Hp = 211
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10392991
82 X = -3105722
29
Y = -11067529
96 feet Y = -3408460
80 meter
Z = -16280126
80 Z = -4977419
94
XDOT = 11792
507800 XDOT = 3655
896569
YDOT = -21107
667151 feet/sec YDOT = -6393
078231 meter/sec
ZDOT = 6845
166415 ZDOT = 2104
017305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4196818
43 X = -1279190
26
Y = -14518432
89 feet Y = -4425218
35 meter
Z = -16344688
69 Z = -4981861
11
XDOT = 18941
883036 XDOT = 5773
485949
YDOT = -13240
945606 feet/sec YDOT = -4035
840221 meter/sec
ZDOT = 6921
637616 ZDOT = 2109
715145
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 15055
51241080
00016717 00000-0 10270-3 0 9082
2 25544 51
6453 286
7789 0006052 34
8980 325
2569 15
55230810 10506
Satellite: ISS
Catalog Number: 25544
Epoch time: 15055
51241080 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 286
7789 deg
Eccentricity:
0006052
Arg of perigee: 34
8980 deg
Mean anomaly: 325
2569 deg
Mean motion: 15
55230810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1050
Checksum: 302
Coasting Arc #10 (Orbit 1065)
---------------------------------------
Vector Time (GMT): 2015/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2139063
80 A = 6779571
03 meter
Y = 5148212
36 meter E =
0016228
Z = 3850279
80 I = 51
28891
XDOT = -4294
376578 Wp = 66
16171
YDOT = 4862
917935 meter/sec RA = 281
04677 deg
ZDOT = -4096
255547 TA = 67
09587
MA = 66
92465
Ha = 220
950 n
mi
Hp = 211
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7017925
84 X = 2062633
27
Y = 16890460
51 feet Y = 5171705
73 meter
Z = 12632151
59 Z = 3860484
81
XDOT = -14089
162000 XDOT = -4328
537836
YDOT = 15954
455167 feet/sec YDOT = 4814
704086 meter/sec
ZDOT = -13439
158618 ZDOT = -4117
199935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1106118
29 X = -337144
85
Y = 18227289
86 feet Y = 5555677
95 meter
Z = 12674880
67 Z = 3863303
63
XDOT = -18222
235384 XDOT = -5554
137345
YDOT = 8348
254279 feet/sec YDOT = 2544
547904 meter/sec
ZDOT = -13529
601641 ZDOT = -4123
822580
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 15056
54050717
00016717 00000-0 10270-3 0 9092
2 25544 51
6455 281
6451 0006108 37
2246 322
9330 15
55305296 10660
Satellite: ISS
Catalog Number: 25544
Epoch time: 15056
54050717 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 281
6451 deg
Eccentricity:
0006108
Arg of perigee: 37
2246 deg
Mean anomaly: 322
9330 deg
Mean motion: 15
55305296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1066
Checksum: 296
Coasting Arc #11 (Orbit 1079)
---------------------------------------
Vector Time (GMT): 2015/057/09:22:19
177
Vector Time (MET): N/A
Weight (LBS) : 890392
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4273516
51 A = 6775526
24 meter
Y = -406587
17 meter E =
0009576
Z = 5233956
53 I = 51
26594
XDOT = -243
373392 Wp = 68
19024
YDOT = 7632
119832 meter/sec RA = 276
61037 deg
ZDOT = 793
927615 TA = 14
20495
MA = 14
17804
Ha = 222
423 n
mi
Hp = 211
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14020723
45 X = 4252321
16
Y = -1333947
42 feet Y = -358916
05 meter
Z = 17171773
41 Z = 5254664
74
XDOT = -798
469134 XDOT = -332
556025
YDOT = 25039
763228 feet/sec YDOT = 7628
899681 meter/sec
ZDOT = 2604
749393 ZDOT = 792
528192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7224297
74 X = 2201965
95
Y = 11963172
52 feet Y = 3646374
98 meter
Z = 17260415
09 Z = 5260974
52
XDOT = -22051
795391 XDOT = -6721
387235
YDOT = 9580
033535 feet/sec YDOT = 2919
994221 meter/sec
ZDOT = 2597
415268 ZDOT = 791
692174
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 15057
44009077
00016717 00000-0 10270-3 0 9107
2 25544 51
6454 277
1534 0007940 50
2546 309
9306 15
54821837 10801
Satellite: ISS
Catalog Number: 25544
Epoch time: 15057
44009077 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 277
1534 deg
Eccentricity:
0007940
Arg of perigee: 50
2546 deg
Mean anomaly: 309
9306 deg
Mean motion: 15
54821837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 302
Coasting Arc #12 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2015/058/09:22:19
177
Vector Time (MET): N/A
Weight (LBS) : 890392
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4087772
94 A = 6775899
97 meter
Y = -1683914
66 meter E =
0020129
Z = -5151830
89 I = 51
26503
XDOT = 1316
003495 Wp = 83
54992
YDOT = -7412
957305 meter/sec RA = 271
57673 deg
ZDOT = 1385
685159 TA = 199
82861
MA = 199
90697
Ha = 222
550 n
mi
Hp = 210
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13411328
53 X = -4043613
91
Y = -5524654
41 feet Y = -1729380
28 meter
Z = -16902332
31 Z = -5171580
81
XDOT = 4317
596767 XDOT = 1392
068088
YDOT = -24320
726066 feet/sec YDOT = -7397
815491 meter/sec
ZDOT = 4546
211153 ZDOT = 1392
263252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1026124
55 X = -312762
76
Y = -14369406
11 feet Y = -4379794
98 meter
Z = -16986512
68 Z = -5177489
07
XDOT = 22613
466716 XDOT = 6892
584655
YDOT = -6997
213130 feet/sec YDOT = -2132
750562 meter/sec
ZDOT = 4575
644161 ZDOT = 1394
656340
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 15058
40419367
00016717 00000-0 10270-3 0 9112
2 25544 51
6457 272
3423 0007977 52
9558 307
2323 15
54849567 10956
Satellite: ISS
Catalog Number: 25544
Epoch time: 15058
40419367 = yrday
fracday
Element set: 911
Inclination: 51
6457 deg
RA of node: 272
3423 deg
Eccentricity:
0007977
Arg of perigee: 52
9558 deg
Mean anomaly: 307
2323 deg
Mean motion: 15
54849567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 332
Coasting Arc #13 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2015/059/09:22:19
177
Vector Time (MET): N/A
Weight (LBS) : 890392
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3702968
37 A = 6778968
94 meter
Y = 3656659
98 meter E =
0017383
Z = 4335116
12 I = 51
27571
XDOT = -2354
853138 Wp = 64
04671
YDOT = 6456
293948 meter/sec RA = 266
54841 deg
ZDOT = -3416
215354 TA = 60
82957
MA = 60
65575
Ha = 222
422 n
mi
Hp = 210
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12148846
36 X = 3640745
53
Y = 11996915
95 feet Y = 3697721
43 meter
Z = 14222821
90 Z = 4352952
67
XDOT = -7725
896122 XDOT = -2410
279527
YDOT = 21182
066760 feet/sec YDOT = 6429
650262 meter/sec
ZDOT = -11208
055622 ZDOT = -3427
789712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5038509
87 X = -1535737
81
Y = 16247334
83 feet Y = 4952187
66 meter
Z = 14298484
26 Z = 4358178
00
XDOT = -21130
917254 XDOT = -6440
703579
YDOT = 3407
470209 feet/sec YDOT = 1038
596920 meter/sec
ZDOT = -11258
681071 ZDOT = -3431
645990
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 15059
43254078
00016717 00000-0 10270-3 0 9123
2 25544 51
6454 267
2102 0007991 55
6225 304
5683 15
54915450 11110
Satellite: ISS
Catalog Number: 25544
Epoch time: 15059
43254078 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 267
2102 deg
Eccentricity:
0007991
Arg of perigee: 55
6225 deg
Mean anomaly: 304
5683 deg
Mean motion: 15
54915450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 297
Coasting Arc #14 (Orbit 1125)
---------------------------------------
Vector Time (GMT): 2015/060/09:22:19
177
Vector Time (MET): N/A
Weight (LBS) : 890392
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3175865
43 A = 6783235
90 meter
Y = -5211884
51 meter E =
0012405
Z = -2962225
66 I = 51
29279
XDOT = 3302
078638 Wp = 62
25817
YDOT = -4819
617794 meter/sec RA = 261
53247 deg
ZDOT = 4961
289880 TA = 263
71771
MA = 263
85903
Ha = 222
447 n
mi
Hp = 210
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10419506
00 X = -3102959
77
Y = -17099358
64 feet Y = -5246991
75 meter
Z = -9718588
12 Z = -2977475
53
XDOT = 10833
591332 XDOT = 3331
627716
YDOT = -15812
394336 feet/sec YDOT = -4782
526118 meter/sec
ZDOT = 16277
197768 ZDOT = 4977
402633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10051720
94 X = 3063764
54
Y = -17281848
26 feet Y = -5267507
35 meter
Z = -9782931
72 Z = -2981837
59
XDOT = 17758
396803 XDOT = 5412
759346
YDOT = 1115
137805 feet/sec YDOT = 339
894003 meter/sec
ZDOT = 16346
945921 ZDOT = 4982
549117
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 15060
39659041
00016717 00000-0 10270-3 0 9130
2 25544 51
6453 262
3987 0007909 58
5598 301
6328 15
54925235 11262
Satellite: ISS
Catalog Number: 25544
Epoch time: 15060
39659041 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 262
3987 deg
Eccentricity:
0007909
Arg of perigee: 58
5598 deg
Mean anomaly: 301
6328 deg
Mean motion: 15
54925235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1126
Checksum: 326
Coasting Arc #15 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2015/061/09:22:19
177
Vector Time (MET): N/A
Weight (LBS) : 890392
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2409051
93 A = 6786439
14 meter
Y = 6240930
42 meter E =
0018946
Z = 1109985
59 I = 51
30879
XDOT = -4179
572072 Wp = 101
79252
YDOT = 2668
436895 meter/sec RA = 256
52950 deg
ZDOT = -5851
160123 TA = 66
10202
MA = 65
90365
Ha = 222
496 n
mi
Hp = 210
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7903713
68 X = 2333693
54
Y = 20475493
50 feet Y = 6267448
77 meter
Z = 3641685
00 Z = 1121504
35
XDOT = -13712
506799 XDOT = -4180
678372
YDOT = 8754
714223 feet/sec YDOT = 2621
691379 meter/sec
ZDOT = -19196
719565 ZDOT = -5871
466225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13911614
51 X = -4240260
10
Y = 16965492
82 feet Y = 5171082
21 meter
Z = 3689909
03 Z = 1124684
27
XDOT = -13086
275106 XDOT = -3988
696652
YDOT = -6479
382320 feet/sec YDOT = -1974
915731 meter/sec
ZDOT = -19284
036269 ZDOT = -5877
774255
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 15061
42488206
00016717 00000-0 10270-3 0 9149
2 25544 51
6449 257
2660 0007897 63
4068 296
7894 15
54939325 11426
Satellite: ISS
Catalog Number: 25544
Epoch time: 15061
42488206 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 257
2660 deg
Eccentricity:
0007897
Arg of perigee: 63
4068 deg
Mean anomaly: 296
7894 deg
Mean motion: 15
54939325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 339
Coasting Arc #16 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2015/062/07:23:16
884
Vector Time (MET): N/A
Weight (LBS) : 890249
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3894989
15 A = 6775581
31 meter
Y = 1727521
16 meter E =
0021250
Z = -5286502
86 I = 51
27789
XDOT = -2658
264841 Wp = 79
39385
YDOT = -7167
271022 meter/sec RA = 251
94116 deg
ZDOT = -381
034797 TA = 186
93292
MA = 186
96236
Ha = 222
409 n
mi
Hp = 211
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12778835
81 X = -3888337
89
Y = 5667720
35 feet Y = 1684001
40 meter
Z = -17344169
48 Z = -5305407
63
XDOT = -8721
341341 XDOT = -2576
070269
YDOT = -23514
668706 feet/sec YDOT = -7196
537943 meter/sec
ZDOT = -1250
114165 ZDOT = -393
747354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5829974
21 X = -1776976
14
Y = -12594089
43 feet Y = -3838678
46 meter
Z = -17425332
86 Z = -5311241
46
XDOT = 22481
452396 XDOT = 6852
346690
YDOT = -8592
280912 feet/sec YDOT = -2618
927222 meter/sec
ZDOT = -1303
306405 ZDOT = -397
247792
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 15062
32461202
00016717 00000-0 10270-3 0 9157
2 25544 51
6446 252
7741 0006870 62
6610 297
5241 15
54758108 11565
Satellite: ISS
Catalog Number: 25544
Epoch time: 15062
32461202 = yrday
fracday
Element set: 915
Inclination: 51
6446 deg
RA of node: 252
7741 deg
Eccentricity:
0006870
Arg of perigee: 62
6610 deg
Mean anomaly: 297
5241 deg
Mean motion: 15
54758108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 296
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