[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 19th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 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
057/09:19:29
255 0
0 2
7 2
7
N/A 2
6 -0
1 222
5
000/00:05:58
511 0
6 0
2 211
2
062/07:21:41
075 -0
6 1
4 1
4
N/A -1
3 -0
1 222
5
000/00:03:22
149 -0
0 0
1 211
2
Coasting Arc #1 (Orbit 958)
---------------------------------------
Vector Time (GMT): 2015/049/15:13:13
985
Vector Time (MET): N/A
Weight (LBS) : 905927
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5277826
91 A = 6786567
27 meter
Y = 4167936
59 meter E =
0008032
Z = -908972
13 I = 51
41393
XDOT = -2368
112334 Wp = 103
00708
YDOT = -4276
093903 meter/sec RA = 315
51057 deg
ZDOT = -5903
056314 TA = 86
85949
MA = 86
76759
Ha = 221
126 n
mi
Hp = 212
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17315705
07 X = -5319626
17
Y = 13674332
63 feet Y = 4108682
69 meter
Z = -2982192
02 Z = -934712
05
XDOT = -7769
397420 XDOT = -2291
445930
YDOT = -14029
179472 feet/sec YDOT = -4302
147574 meter/sec
ZDOT = -19366
982657 ZDOT = -5914
373233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12938628
12 X = -3943693
85
Y = 17853269
85 feet Y = 5441676
65 meter
Z = -3093079
75 Z = -942770
71
XDOT = -9864
012327 XDOT = -3006
550957
YDOT = -10487
079415 feet/sec YDOT = -3196
461806 meter/sec
ZDOT = -19414
585200 ZDOT = -5917
565569
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
66454424
00016717 00000-0 10270-3 0 9001
2 25544 51
6465 315
9764 0006070 15
3571 344
7765 15
54947032 9598
Satellite: ISS
Catalog Number: 25544
Epoch time: 15049
66454424 = yrday
fracday
Element set: 900
Inclination: 51
6465 deg
RA of node: 315
9764 deg
Eccentricity:
0006070
Arg of perigee: 15
3571 deg
Mean anomaly: 344
7765 deg
Mean motion: 15
54947032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 959
Checksum: 323
Coasting Arc #2 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2015/050/15:13:13
985
Vector Time (MET): N/A
Weight (LBS) : 905927
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5430384
16 A = 6783407
30 meter
Y = -2962785
91 meter E =
0017166
Z = 2758665
27 I = 51
38125
XDOT = 503
638546 Wp = 61
10514
YDOT = 5701
629349 meter/sec RA = 310
51417 deg
ZDOT = 5116
102452 TA = 330
31314
MA = 330
41045
Ha = 220
980 n
mi
Hp = 212
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17816220
99 X = 5449710
87
Y = -9720426
20 feet Y = -2901951
43 meter
Z = 9050739
07 Z = 2785091
71
XDOT = 1652
357436 XDOT = 414
992602
YDOT = 18706
133035 feet/sec YDOT = 5706
766314 meter/sec
ZDOT = 16785
113031 ZDOT = 5118
333000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14210129
00 X = 4331247
32
Y = -14419003
37 feet Y = -4394912
23 meter
Z = 9164325
89 Z = 2793286
53
XDOT = 5812
803564 XDOT = 1771
742526
YDOT = 16435
100961 feet/sec YDOT = 5009
418773 meter/sec
ZDOT = 16793
591518 ZDOT = 5118
686695
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
69280202
00016717 00000-0 10270-3 0 9018
2 25544 51
6455 310
8429 0006140 17
8970 342
2398 15
55026643 9757
Satellite: ISS
Catalog Number: 25544
Epoch time: 15050
69280202 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 310
8429 deg
Eccentricity:
0006140
Arg of perigee: 17
8970 deg
Mean anomaly: 342
2398 deg
Mean motion: 15
55026643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 299
Coasting Arc #3 (Orbit 989)
---------------------------------------
Vector Time (GMT): 2015/051/15:13:13
985
Vector Time (MET): N/A
Weight (LBS) : 905927
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5121701
77 A = 6778864
08 meter
Y = 1319544
12 meter E =
0013269
Z = -4254611
12 I = 51
34498
XDOT = 1247
589689 Wp = 49
43773
YDOT = -6660
933626 meter/sec RA = 305
50407 deg
ZDOT = -3566
583547 TA = 183
94531
MA = 183
95578
Ha = 221
118 n
mi
Hp = 211
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16803483
48 X = -5115409
63
Y = 4329212
99 feet Y = 1262304
54 meter
Z = -13958697
90 Z = -4279475
78
XDOT = 4093
142025 XDOT = 1339
305909
YDOT = -21853
456779 feet/sec YDOT = -6646
469909 meter/sec
ZDOT = -11701
389589 ZDOT = -3560
299485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14605856
69 X = -4451865
12
Y = 9207655
77 feet Y = 2806493
48 meter
Z = -14065291
14 Z = -4287100
74
XDOT = -2007
264355 XDOT = -611
814175
YDOT = -21021
321434 feet/sec YDOT = -6407
298773 meter/sec
ZDOT = -11673
283073 ZDOT = -3558
016681
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
65677033
00016717 00000-0 10270-3 0 9028
2 25544 51
6439 306
0307 0006117 21
9378 338
2036 15
55052665 9907
Satellite: ISS
Catalog Number: 25544
Epoch time: 15051
65677033 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 306
0307 deg
Eccentricity:
0006117
Arg of perigee: 21
9378 deg
Mean anomaly: 338
2036 deg
Mean motion: 15
55052665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 990
Checksum: 299
Coasting Arc #4 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2015/052/15:13:13
985
Vector Time (MET): N/A
Weight (LBS) : 905927
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4394185
25 A = 6775372
40 meter
Y = 608299
18 meter E =
0007108
Z = 5114916
65 I = 51
31551
XDOT = -2726
245611 Wp = 66
27343
YDOT = 7014
546075 meter/sec RA = 300
47802 deg
ZDOT = 1509
027991 TA = 9
14534
MA = 9
13240
Ha = 221
063 n
mi
Hp = 211
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14416618
27 X = 4362210
51
Y = 1995732
22 feet Y = 657259
70 meter
Z = 16781222
61 Z = 5136184
71
XDOT = -8944
375365 XDOT = -2811
811493
YDOT = 23013
602607 feet/sec YDOT = 6983
581186 meter/sec
ZDOT = 4950
879236 ZDOT = 1495
575874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14195063
50 X = 4326655
35
Y = -2695282
13 feet Y = -821521
99 meter
Z = 16872074
22 Z = 5142608
22
XDOT = -1321
250671 XDOT = -402
717204
YDOT = 23641
624198 feet/sec YDOT = 7205
967056 meter/sec
ZDOT = 4892
062031 ZDOT = 1491
100507
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
68497770
00016717 00000-0 10270-3 0 9031
2 25544 51
6437 300
8968 0006149 26
2218 333
9245 15
55057209 10068
Satellite: ISS
Catalog Number: 25544
Epoch time: 15052
68497770 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 300
8968 deg
Eccentricity:
0006149
Arg of perigee: 26
2218 deg
Mean anomaly: 333
9245 deg
Mean motion: 15
55057209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 313
Coasting Arc #5 (Orbit 1020)
---------------------------------------
Vector Time (GMT): 2015/053/15:13:13
985
Vector Time (MET): N/A
Weight (LBS) : 905927
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3419047
95 A = 6774633
34 meter
Y = -2605936
88 meter E =
0017844
Z = -5250648
61 I = 51
29717
XDOT = 3827
538161 Wp = 77
94490
YDOT = -6586
171371 meter/sec RA = 295
44295 deg
ZDOT = 782
318623 TA = 199
54299
MA = 199
61147
Ha = 221
081 n
mi
Hp = 211
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11217348
91 X = -3364148
22
Y = -8549661
69 feet Y = -2643864
57 meter
Z = -17226537
43 Z = -5267123
85
XDOT = 12557
539898 XDOT = 3897
101642
YDOT = -21608
173789 feet/sec YDOT = -6542
980298 meter/sec
ZDOT = 2566
662150 ZDOT = 801
081603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13339020
26 X = -4065733
38
Y = -4310445
65 feet Y = -1313823
84 meter
Z = -17296526
24 Z = -5271981
20
XDOT = 4216
460900 XDOT = 1285
177282
YDOT = -23596
639473 feet/sec YDOT = -7192
255711 meter/sec
ZDOT = 2648
104396 ZDOT = 807
142220
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
64889500
00016717 00000-0 10270-3 0 9045
2 25544 51
6424 296
0831 0006038 29
8366 330
3130 15
55138165 10211
Satellite: ISS
Catalog Number: 25544
Epoch time: 15053
64889500 = yrday
fracday
Element set: 904
Inclination: 51
6424 deg
RA of node: 296
0831 deg
Eccentricity:
0006038
Arg of perigee: 29
8366 deg
Mean anomaly: 330
3130 deg
Mean motion: 15
55138165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1021
Checksum: 290
Coasting Arc #6 (Orbit 1036)
---------------------------------------
Vector Time (GMT): 2015/054/15:13:13
985
Vector Time (MET): N/A
Weight (LBS) : 905927
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2256535
82 A = 6777347
96 meter
Y = 4453947
83 meter E =
0013849
Z = 4577677
47 I = 51
29402
XDOT = -4562
801209 Wp = 51
96108
YDOT = 5397
228518 meter/sec RA = 290
41122 deg
ZDOT = -2987
568568 TA = 68
04290
MA = 67
89577
Ha = 221
023 n
mi
Hp = 211
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7403332
73 X = 2184326
57
Y = 14612689
72 feet Y = 4478778
61 meter
Z = 15018626
88 Z = 4588463
34
XDOT = -14969
820238 XDOT = -4608
302815
YDOT = 17707
442643 feet/sec YDOT = 5345
949576 meter/sec
ZDOT = -9801
734148 ZDOT = -3009
844644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11995647
37 X = 3656273
32
Y = 11094186
66 feet Y = 3381508
09 meter
Z = 15063952
22 Z = 4591492
64
XDOT = -6889
548071 XDOT = -2099
934252
YDOT = 20953
809396 feet/sec YDOT = 6386
721104 meter/sec
ZDOT = -9897
977930 ZDOT = -3016
903673
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
67704836
00016717 00000-0 10270-3 0 9058
2 25544 51
6426 290
9494 0005948 32
5189 327
6329 15
55167976 10372
Satellite: ISS
Catalog Number: 25544
Epoch time: 15054
67704836 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 290
9494 deg
Eccentricity:
0005948
Arg of perigee: 32
5189 deg
Mean anomaly: 327
6329 deg
Mean motion: 15
55167976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1037
Checksum: 344
Coasting Arc #7 (Orbit 1051)
---------------------------------------
Vector Time (GMT): 2015/055/15:13:13
985
Vector Time (MET): N/A
Weight (LBS) : 905927
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1083933
15 A = 6781692
19 meter
Y = -5856450
33 meter E =
0009773
Z = -3244298
88 I = 51
29832
XDOT = 4899
686817 Wp = 56
74927
YDOT = -3518
789908 meter/sec RA = 285
39036 deg
ZDOT = 4730
556624 TA = 265
44756
MA = 265
55920
Ha = 221
052 n
mi
Hp = 211
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3556211
12 X = -1002604
93
Y = -19214075
89 feet Y = -5868117
13 meter
Z = -10644025
19 Z = -3249366
31
XDOT = 16075
087982 XDOT = 4915
691537
YDOT = -11544
586313 feet/sec YDOT = -3463
908509 meter/sec
ZDOT = 15520
198897 ZDOT = 4754
397317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10332613
85 X = -3149380
70
Y = -16571813
24 feet Y = -5051088
68 meter
Z = -10664648
10 Z = -3250584
74
XDOT = 9381
268762 XDOT = 2859
410719
YDOT = -15870
283073 feet/sec YDOT = -4837
262281 meter/sec
ZDOT = 15622
791791 ZDOT = 4761
826938
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
64091838
00016717 00000-0 10270-3 0 9068
2 25544 51
6421 286
1355 0005946 37
4172 322
7395 15
55211826 10524
Satellite: ISS
Catalog Number: 25544
Epoch time: 15055
64091838 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 286
1355 deg
Eccentricity:
0005946
Arg of perigee: 37
4172 deg
Mean anomaly: 322
7395 deg
Mean motion: 15
55211826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1052
Checksum: 306
Coasting Arc #8 (Orbit 1067)
---------------------------------------
Vector Time (GMT): 2015/056/15:13:13
985
Vector Time (MET): N/A
Weight (LBS) : 905927
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -108066
31 A = 6785151
57 meter
Y = 6641948
31 meter E =
0015871
Z = 1361837
08 I = 51
30335
XDOT = -4913
364324 Wp = 97
76835
YDOT = 1116
995986 meter/sec RA = 280
38425 deg
ZDOT = -5781
814996 TA = 67
32040
MA = 67
15267
Ha = 220
985 n
mi
Hp = 211
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -354548
25 X = -188945
33
Y = 21791168
98 feet Y = 6640287
72 meter
Z = 4467969
42 Z = 1361115
16
XDOT = -16119
961692 XDOT = -4897
404070
YDOT = 3664
684992 feet/sec YDOT = 1062
140331 meter/sec
ZDOT = -18969
209305 ZDOT = -5805
644233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8034673
94 X = 2448968
62
Y = 20259883
87 feet Y = 6175212
60 meter
Z = 4463700
36 Z = 1360535
87
XDOT = -11879
307483 XDOT = -3620
812921
YDOT = 8953
371346 feet/sec YDOT = 2728
987586 meter/sec
ZDOT = -19071
323692 ZDOT = -5812
939461
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
66901812
00016717 00000-0 10270-3 0 9074
2 25544 51
6422 281
0014 0006025 38
4338 321
7243 15
55296671 10684
Satellite: ISS
Catalog Number: 25544
Epoch time: 15056
66901812 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 281
0014 deg
Eccentricity:
0006025
Arg of perigee: 38
4338 deg
Mean anomaly: 321
7243 deg
Mean motion: 15
55296671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1068
Checksum: 292
Coasting Arc #9 (Orbit 1079)
---------------------------------------
Vector Time (GMT): 2015/057/09:22:28
511
Vector Time (MET): N/A
Weight (LBS) : 905666
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4271176
55 A = 6775540
32 meter
Y = -339985
06 meter E =
0009606
Z = 5240671
05 I = 51
26633
XDOT = -291
267386 Wp = 67
02654
YDOT = 7636
261856 meter/sec RA = 276
61142 deg
ZDOT = 735
394762 TA = 15
93492
MA = 15
90472
Ha = 222
464 n
mi
Hp = 211
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14013046
43 X = 4249204
00
Y = -1115436
56 feet Y = -292344
45 meter
Z = 17193802
66 Z = 5261365
99
XDOT = -955
601661 XDOT = -380
208449
YDOT = 25053
352546 feet/sec YDOT = 7632
507470 meter/sec
ZDOT = 2412
712475 ZDOT = 733
763269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7032144
40 X = 2143397
61
Y = 12045951
55 feet Y = 3671606
03 meter
Z = 17282375
86 Z = 5267668
16
XDOT = -22118
704911 XDOT = -6741
781257
YDOT = 9475
036220 feet/sec YDOT = 2887
991040 meter/sec
ZDOT = 2404
385040 ZDOT = 732
856560
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
44009871
00016717 00000-0 10270-3 0 9086
2 25544 51
6459 277
1555 0008002 49
8561 310
3292 15
54806737 10802
Satellite: ISS
Catalog Number: 25544
Epoch time: 15057
44009871 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 277
1555 deg
Eccentricity:
0008002
Arg of perigee: 49
8561 deg
Mean anomaly: 310
3292 deg
Mean motion: 15
54806737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 312
Coasting Arc #10 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2015/058/09:22:28
511
Vector Time (MET): N/A
Weight (LBS) : 905666
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4077405
49 A = 6776003
23 meter
Y = -1741127
17 meter E =
0020063
Z = -5141040
21 I = 51
26568
XDOT = 1356
266780 Wp = 83
51060
YDOT = -7396
095599 meter/sec RA = 271
57807 deg
ZDOT = 1436
255754 TA = 200
36621
MA = 200
44633
Ha = 222
599 n
mi
Hp = 210
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13377314
60 X = -4032659
89
Y = -5712359
47 feet Y = -1786473
57 meter
Z = -16866929
81 Z = -5160738
34
XDOT = 4449
694161 XDOT = 1431
894181
YDOT = -24265
405509 feet/sec YDOT = -7380
505976 meter/sec
ZDOT = 4712
125176 ZDOT = 1443
028371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -853016
92 X = -259999
56
Y = -14422794
22 feet Y = -4396067
68 meter
Z = -16950878
65 Z = -5166627
81
XDOT = 22614
151420 XDOT = 6892
793353
YDOT = -6884
003129 feet/sec YDOT = -2098
244154 meter/sec
ZDOT = 4742
387265 ZDOT = 1445
479639
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
40421258
00016717 00000-0 10270-3 0 9091
2 25544 51
6463 272
3446 0008043 52
6002 307
5882 15
54830332 10957
Satellite: ISS
Catalog Number: 25544
Epoch time: 15058
40421258 = yrday
fracday
Element set: 909
Inclination: 51
6463 deg
RA of node: 272
3446 deg
Eccentricity:
0008043
Arg of perigee: 52
6002 deg
Mean anomaly: 307
5882 deg
Mean motion: 15
54830332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 292
Coasting Arc #11 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2015/059/09:22:28
511
Vector Time (MET): N/A
Weight (LBS) : 905666
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3687210
77 A = 6779119
21 meter
Y = 3699275
39 meter E =
0017531
Z = 4312573
05 I = 51
27648
XDOT = -2386
207361 Wp = 64
18577
YDOT = 6425
162221 meter/sec RA = 266
55022 deg
ZDOT = -3452
757349 TA = 61
11843
MA = 60
94264
Ha = 222
482 n
mi
Hp = 210
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12097148
19 X = 3624622
07
Y = 12136730
27 feet Y = 3740158
58 meter
Z = 14148861
71 Z = 4330332
16
XDOT = -7828
764309 XDOT = -2441
105794
YDOT = 21079
928545 feet/sec YDOT = 6398
170859 meter/sec
ZDOT = -11327
944058 ZDOT = -3464
482732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5175059
54 X = -1577358
15
Y = 16270304
56 feet Y = 4959188
83 meter
Z = 14224185
46 Z = 4335531
73
XDOT = -21084
107652 XDOT = -6426
436012
YDOT = 3294
754155 feet/sec YDOT = 1004
241066 meter/sec
ZDOT = -11379
210126 ZDOT = -3468
383246
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
43257343
00016717 00000-0 10270-3 0 9109
2 25544 51
6459 267
2126 0008063 55
3144 304
8768 15
54892736 11117
Satellite: ISS
Catalog Number: 25544
Epoch time: 15059
43257343 = yrday
fracday
Element set: 910
Inclination: 51
6459 deg
RA of node: 267
2126 deg
Eccentricity:
0008063
Arg of perigee: 55
3144 deg
Mean anomaly: 304
8768 deg
Mean motion: 15
54892736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 310
Coasting Arc #12 (Orbit 1125)
---------------------------------------
Vector Time (GMT): 2015/060/09:22:28
511
Vector Time (MET): N/A
Weight (LBS) : 905666
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3158289
30 A = 6783374
99 meter
Y = -5237208
27 meter E =
0012502
Z = -2936234
04 I = 51
29350
XDOT = 3323
439194 Wp = 61
59017
YDOT = -4784
488210 meter/sec RA = 261
53475 deg
ZDOT = 4981
114756 TA = 264
72481
MA = 264
86748
Ha = 222
510 n
mi
Hp = 210
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10361841
53 X = -3085228
03
Y = -17182441
82 feet Y = -5272118
08 meter
Z = -9633313
77 Z = -2951398
15
XDOT = 10903
671896 XDOT = 3352
497557
YDOT = -15697
139796 feet/sec YDOT = -4747
160409 meter/sec
ZDOT = 16342
240013 ZDOT = 4997
330077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10140248
28 X = 3090747
68
Y = -17278391
32 feet Y = -5266453
67 meter
Z = -9697286
18 Z = -2955732
83
XDOT = 17692
159829 XDOT = 5392
570316
YDOT = 1212
138616 feet/sec YDOT = 369
459850 meter/sec
ZDOT = 16412
420920 ZDOT = 5002
505896
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
39663785
00016717 00000-0 10270-3 0 9118
2 25544 51
6458 262
4012 0007982 58
2637 301
9293 15
54899973 11262
Satellite: ISS
Catalog Number: 25544
Epoch time: 15060
39663785 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 262
4012 deg
Eccentricity:
0007982
Arg of perigee: 58
2637 deg
Mean anomaly: 301
9293 deg
Mean motion: 15
54899973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1126
Checksum: 334
Coasting Arc #13 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2015/061/09:22:28
511
Vector Time (MET): N/A
Weight (LBS) : 905666
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2393060
71 A = 6786543
56 meter
Y = 6251131
78 meter E =
0018938
Z = 1088002
64 I = 51
30934
XDOT = -4191
134786 Wp = 101
71823
YDOT = 2638
187121 meter/sec RA = 256
53212 deg
ZDOT = -5856
427354 TA = 66
41998
MA = 66
22120
Ha = 222
565 n
mi
Hp = 210
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7851249
04 X = 2317696
22
Y = 20508962
54 feet Y = 6277471
28 meter
Z = 3569562
47 Z = 1099443
70
XDOT = -13750
442211 XDOT = -4191
876380
YDOT = 8655
469557 feet/sec YDOT = 2591
314342 meter/sec
ZDOT = -19214
000504 ZDOT = -5876
788734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13954866
20 X = -4253443
22
Y = 16946302
83 feet Y = 5165233
10 meter
Z = 3617452
39 Z = 1102599
49
XDOT = -13025
214533 XDOT = -3970
085390
YDOT = -6548
432089 feet/sec YDOT = -1995
962101 meter/sec
ZDOT = -19301
548587 ZDOT = -5883
112009
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
42494742
00016717 00000-0 10270-3 0 9129
2 25544 51
6454 257
2688 0007969 63
1263 297
0704 15
54910526 11422
Satellite: ISS
Catalog Number: 25544
Epoch time: 15061
42494742 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 257
2688 deg
Eccentricity:
0007969
Arg of perigee: 63
1263 deg
Mean anomaly: 297
0704 deg
Mean motion: 15
54910526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 315
Coasting Arc #14 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2015/062/07:23:22
149
Vector Time (MET): N/A
Weight (LBS) : 905518
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3890140
25 A = 6775676
82 meter
Y = 1740715
67 meter E =
0021312
Z = -5285919
00 I = 51
27839
XDOT = -2667
070685 Wp = 79
19758
YDOT = -7163
216363 meter/sec RA = 251
94419 deg
ZDOT = -393
555193 TA = 187
00858
MA = 187
03843
Ha = 222
485 n
mi
Hp = 211
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12762927
32 X = -3883639
72
Y = 5711009
41 feet Y = 1697249
28 meter
Z = -17342253
93 Z = -5304800
58
XDOT = -8750
231905 XDOT = -2584
859980
YDOT = -23501
366021 feet/sec YDOT = -7192
581669 meter/sec
ZDOT = -1291
191577 ZDOT = -406
310487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5877882
22 X = -1791578
50
Y = -12575377
66 feet Y = -3832975
11 meter
Z = -17423320
32 Z = -5310628
03
XDOT = 22465
673008 XDOT = 6847
537133
YDOT = -8626
220155 feet/sec YDOT = -2629
271903 meter/sec
ZDOT = -1344
567319 ZDOT = -409
824119
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
32469489
00016717 00000-0 10270-3 0 9130
2 25544 51
6451 252
7770 0006945 62
4391 297
7467 15
54726406 11568
Satellite: ISS
Catalog Number: 25544
Epoch time: 15062
32469489 = yrday
fracday
Element set: 913
Inclination: 51
6451 deg
RA of node: 252
7770 deg
Eccentricity:
0006945
Arg of perigee: 62
4391 deg
Mean anomaly: 297
7467 deg
Mean motion: 15
54726406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 332
Coasting Arc #15 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2015/063/07:23:22
149
Vector Time (MET): N/A
Weight (LBS) : 905518
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4503682
48 A = 6776421
24 meter
Y = 245333
65 meter E =
0012079
Z = 5049764
06 I = 51
29205
XDOT = 1582
324171 Wp = 60
62598
YDOT = 7302
667485 meter/sec RA = 246
91277 deg
ZDOT = -1756
991470 TA = 46
48146
MA = 46
38115
Ha = 222
220 n
mi
Hp = 211
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14775861
15 X = 4476074
98
Y = 804900
41 feet Y = 295543
09 meter
Z = 16567467
37 Z = 5071574
57
XDOT = 5191
352266 XDOT = 1509
081063
YDOT = 23958
882825 feet/sec YDOT = 7319
952300 meter/sec
ZDOT = -5764
407710 ZDOT = -1749
483887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -357833
01 X = -109067
50
Y = 14688317
70 feet Y = 4476999
24 meter
Z = 16660738
02 Z = 5078192
95
XDOT = -22716
409189 XDOT = -6923
961521
YDOT = 5983
328614 feet/sec YDOT = 1823
718562 meter/sec
ZDOT = -5733
487574 ZDOT = -1747
567012
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 15063
35312710
00016717 00000-0 10270-3 0 9149
2 25544 51
6449 247
6452 0006829 64
6934 295
4926 15
54793596 11720
Satellite: ISS
Catalog Number: 25544
Epoch time: 15063
35312710 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 247
6452 deg
Eccentricity:
0006829
Arg of perigee: 64
6934 deg
Mean anomaly: 295
4926 deg
Mean motion: 15
54793596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1172
Checksum: 333
Coasting Arc #16 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2015/064/07:23:22
149
Vector Time (MET): N/A
Weight (LBS) : 905518
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4916805
90 A = 6779866
34 meter
Y = -2093819
51 meter E =
0013828
Z = -4184357
78 I = 51
31717
XDOT = -255
350121 Wp = 90
69023
YDOT = -6716
926185 meter/sec RA = 241
88916 deg
ZDOT = 3671
530134 TA = 217
14735
MA = 217
24312
Ha = 222
344 n
mi
Hp = 211
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16131252
95 X = -4872701
17
Y = -6869486
59 feet Y = -2148556
46 meter
Z = -13728207
95 Z = -4208134
85
XDOT = -837
762865 XDOT = -198
055518
YDOT = -22037
159400 feet/sec YDOT = -6719
460780 meter/sec
ZDOT = 12045
702541 ZDOT = 3670
429870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6096982
90 X = 1858360
39
Y = -16353590
04 feet Y = -4984574
24 meter
Z = -13829597
02 Z = -4215261
17
XDOT = 20774
820234 XDOT = 6332
165207
YDOT = -2409
603987 feet/sec YDOT = -734
447295 meter/sec
ZDOT = 12042
084301 ZDOT = 3670
427295
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 15064
31725886
00016717 00000-0 10270-3 0 9159
2 25544 51
6452 242
8339 0006835 67
6320 292
5557 15
54794772 11875
Satellite: ISS
Catalog Number: 25544
Epoch time: 15064
31725886 = yrday
fracday
Element set: 915
Inclination: 51
6452 deg
RA of node: 242
8339 deg
Eccentricity:
0006835
Arg of perigee: 67
6320 deg
Mean anomaly: 292
5557 deg
Mean motion: 15
54794772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 338
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