[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 21st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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 1859)
---------------------------------------
Vector Time (GMT): 2015/107/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5338449
23 A = 6777448
10 meter
Y = -933204
30 meter E =
0006164
Z = -4076004
85 I = 51
81009
XDOT = 3898
525910 Wp = 158
28610
YDOT = 5338
069825 meter/sec RA = 26
35793 deg
ZDOT = 3880
132569 TA = 151
82766
MA = 151
79430
Ha = 217
588 n
mi
Hp = 213
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17514597
22 X = 5368287
76
Y = -3061693
89 feet Y = -873339
88 meter
Z = -13372719
32 Z = -4049998
76
XDOT = 12790
439338 XDOT = 3819
696102
YDOT = 17513
352445 feet/sec YDOT = 5381
225349 meter/sec
ZDOT = 12730
093729 ZDOT = 3898
879059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10788865
42 X = 3288446
18
Y = -14237637
07 feet Y = -4339631
78 meter
Z = -13261024
88 Z = -4041960
38
XDOT = 20199
779356 XDOT = 6156
892748
YDOT = 3364
556091 feet/sec YDOT = 1025
516697 meter/sec
ZDOT = 12809
452926 ZDOT = 3904
321252
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 15107
56011412
00016717 00000-0 10270-3 0 9001
2 25544 51
6478 26
9199 0005741 232
3396 127
7237 15
55831869 18609
Satellite: ISS
Catalog Number: 25544
Epoch time: 15107
56011412 = yrday
fracday
Element set: 900
Inclination: 51
6478 deg
RA of node: 26
9199 deg
Eccentricity:
0005741
Arg of perigee: 232
3396 deg
Mean anomaly: 127
7237 deg
Mean motion: 15
55831869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1860
Checksum: 314
Coasting Arc #2 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2015/108/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6361368
77 A = 6782217
83 meter
Y = -582389
96 meter E =
0011459
Z = 2257196
20 I = 51
79743
XDOT = -1466
169837 Wp = 132
39829
YDOT = -5189
030865 meter/sec RA = 21
37688 deg
ZDOT = -5460
798390 TA = 22
51657
MA = 22
46632
Ha = 217
539 n
mi
Hp = 213
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20870632
44 X = -6365348
36
Y = -1910728
21 feet Y = -653548
98 meter
Z = 7405499
35 Z = 2226283
76
XDOT = -4810
268494 XDOT = -1381
508913
YDOT = -17024
379477 feet/sec YDOT = -5204
953681 meter/sec
ZDOT = -17916
005216 ZDOT = -5467
714757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16382798
95 X = -4993477
12
Y = 13144656
31 feet Y = 4006491
24 meter
Z = 7273067
47 Z = 2216830
97
XDOT = -14240
670681 XDOT = -4340
556423
YDOT = -7801
193704 feet/sec YDOT = -2377
803841 meter/sec
ZDOT = -17944
655735 ZDOT = -5469
531068
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 15108
58780479
00016717 00000-0 10270-3 0 9011
2 25544 51
6478 21
7842 0005806 235
0205 125
0404 15
55858500 18763
Satellite: ISS
Catalog Number: 25544
Epoch time: 15108
58780479 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 21
7842 deg
Eccentricity:
0005806
Arg of perigee: 235
0205 deg
Mean anomaly: 125
0404 deg
Mean motion: 15
55858500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1876
Checksum: 308
Coasting Arc #3 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2015/109/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6507775
06 A = 6784051
09 meter
Y = 1902735
95 meter E =
0006633
Z = -16317
96 I = 51
77509
XDOT = -1320
434268 Wp = 32
23849
YDOT = 4558
134215 meter/sec RA = 16
40641 deg
ZDOT = 6025
053596 TA = 327
58598
MA = 327
62671
Ha = 217
081 n
mi
Hp = 213
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21350968
06 X = 6486093
81
Y = 6242572
03 feet Y = 1975388
92 meter
Z = -53536
61 Z = 15243
35
XDOT = -4332
133425 XDOT = -1400
574284
YDOT = 14954
508580 feet/sec YDOT = 4542
920606 meter/sec
ZDOT = 19767
236208 ZDOT = 6018
444073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19521801
25 X = 5950245
02
Y = -10664382
63 feet Y = -3250503
82 meter
Z = 81411
17 Z = 24814
12
XDOT = 6632
868807 XDOT = 2021
698412
YDOT = 12311
200903 feet/sec YDOT = 3752
454035 meter/sec
ZDOT = 19738
008192 ZDOT = 6016
144897
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 15109
61545573
00016717 00000-0 10270-3 0 9021
2 25544 51
6482 16
6474 0005904 240
7579 119
2985 15
55945702 18926
Satellite: ISS
Catalog Number: 25544
Epoch time: 15109
61545573 = yrday
fracday
Element set: 902
Inclination: 51
6482 deg
RA of node: 16
6474 deg
Eccentricity:
0005904
Arg of perigee: 240
7579 deg
Mean anomaly: 119
2985 deg
Mean motion: 15
55945702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 331
Coasting Arc #4 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2015/110/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5663319
74 A = 6781769
30 meter
Y = -2960855
41 meter E =
0007033
Z = -2256058
41 I = 51
73700
XDOT = 4039
952096 Wp = 191
05055
YDOT = -3573
128313 meter/sec RA = 11
43437 deg
ZDOT = -5455
925030 TA = 14
03502
MA = 14
01549
Ha = 216
848 n
mi
Hp = 213
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18580445
33 X = -5618830
54
Y = -9714092
56 feet Y = -3023937
71 meter
Z = -7401766
44 Z = -2283462
02
XDOT = 13254
436011 XDOT = 4106
110738
YDOT = -11722
861919 feet/sec YDOT = -3527
581285 meter/sec
ZDOT = -17900
016502 ZDOT = -5436
138491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19870365
97 X = -6056487
55
Y = 6559025
20 feet Y = 1999190
88 meter
Z = -7518672
34 Z = -2291691
33
XDOT = 1352
025217 XDOT = 412
097286
YDOT = -16310
448347 feet/sec YDOT = -4971
424656 meter/sec
ZDOT = -17814
483073 ZDOT = -5429
854441
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 15110
57884637
00016717 00000-0 10270-3 0 9036
2 25544 51
6481 11
8322 0006131 244
0290 116
0233 15
55962619 19078
Satellite: ISS
Catalog Number: 25544
Epoch time: 15110
57884637 = yrday
fracday
Element set: 903
Inclination: 51
6481 deg
RA of node: 11
8322 deg
Eccentricity:
0006131
Arg of perigee: 244
0290 deg
Mean anomaly: 116
0233 deg
Mean motion: 15
55962619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 288
Coasting Arc #5 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2015/111/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3930631
68 A = 6776597
15 meter
Y = 3700332
30 meter E =
0006550
Z = 4095554
41 I = 51
68880
XDOT = -6213
965591 Wp = 134
33001
YDOT = 2347
150846 meter/sec RA = 6
44448 deg
ZDOT = 3834
822265 TA = 276
04963
MA = 276
12426
Ha = 216
534 n
mi
Hp = 213
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12895773
23 X = 3869066
56
Y = 12140197
85 feet Y = 3743943
09 meter
Z = 13436858
29 Z = 4114499
32
XDOT = -20387
026218 XDOT = -6258
378585
YDOT = 7700
626134 feet/sec YDOT = 2277
414009 meter/sec
ZDOT = 12581
437878 ZDOT = 3804
527590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17617797
99 X = 5369904
83
Y = -1062569
64 feet Y = -323871
23 meter
Z = 13517347
06 Z = 4120087
38
XDOT = -8432
506034 XDOT = -2570
227839
YDOT = 18923
874361 feet/sec YDOT = 5767
996905 meter/sec
ZDOT = 12451
095409 ZDOT = 3795
093881
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 15111
60642723
00016717 00000-0 10270-3 0 9040
2 25544 51
6478 6
6948 0005934 249
0783 110
9736 15
56028953 19236
Satellite: ISS
Catalog Number: 25544
Epoch time: 15111
60642723 = yrday
fracday
Element set: 904
Inclination: 51
6478 deg
RA of node: 6
6948 deg
Eccentricity:
0005934
Arg of perigee: 249
0783 deg
Mean anomaly: 110
9736 deg
Mean motion: 15
56028953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 320
Coasting Arc #6 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2015/112/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1532672
39 A = 6772209
43 meter
Y = -4121211
50 meter E =
0007792
Z = -5157542
52 I = 51
64258
XDOT = 7465
705594 Wp = 83
51412
YDOT = -961
856473 meter/sec RA = 1
43345 deg
ZDOT = -1451
028043 TA = 172
52355
MA = 172
51192
Ha = 216
203 n
mi
Hp = 213
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5028452
73 X = -1461420
38
Y = -13521035
09 feet Y = -4137952
54 meter
Z = -16921071
27 Z = -5164814
91
XDOT = 24493
784756 XDOT = 7482
955074
YDOT = -3155
697089 feet/sec YDOT = -878
273653 meter/sec
ZDOT = -4760
590692 ZDOT = -1414
718704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13332703
30 X = -4063807
97
Y = -5414276
47 feet Y = -1650271
47 meter
Z = -16951430
99 Z = -5166796
17
XDOT = 13704
053624 XDOT = 4176
995544
YDOT = -19339
962461 feet/sec YDOT = -5894
820558 meter/sec
ZDOT = -4604
739502 ZDOT = -1403
524600
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 15112
56974901
00016717 00000-0 10270-3 0 9053
2 25544 51
6471 1
8782 0006144 253
4608 106
5871 15
56119742 19385
Satellite: ISS
Catalog Number: 25544
Epoch time: 15112
56974901 = yrday
fracday
Element set: 905
Inclination: 51
6471 deg
RA of node: 1
8782 deg
Eccentricity:
0006144
Arg of perigee: 253
4608 deg
Mean anomaly: 106
5871 deg
Mean motion: 15
56119742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 312
Coasting Arc #7 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2015/113/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1123661
20 A = 6771939
78 meter
Y = 4196374
25 meter E =
0002805
Z = 5197355
63 I = 51
61056
XDOT = -7554
352757 Wp = 289
33036
YDOT = -501
222096 meter/sec RA = 356
41143 deg
ZDOT = -1228
183178 TA = 172
46009
MA = 172
45587
Ha = 215
952 n
mi
Hp = 213
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3686552
49 X = -1195749
60
Y = 13767632
06 feet Y = 4183405
74 meter
Z = 17051691
69 Z = 5191721
88
XDOT = -24784
621907 XDOT = -7542
220401
YDOT = -1644
429448 feet/sec YDOT = -585
631986 meter/sec
ZDOT = -4029
472368 ZDOT = -1264
851644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7878738
24 X = 2401439
42
Y = 11912820
79 feet Y = 3631027
78 meter
Z = 17026706
54 Z = 5189740
15
XDOT = -16650
330208 XDOT = -5075
020647
YDOT = 16997
457269 feet/sec YDOT = 5180
824975 meter/sec
ZDOT = -4186
568866 ZDOT = -1276
066190
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 15113
59725819
00016717 00000-0 10270-3 0 9060
2 25544 51
6473 356
7408 0006256 256
9593 103
0862 15
56172900 19544
Satellite: ISS
Catalog Number: 25544
Epoch time: 15113
59725819 = yrday
fracday
Element set: 906
Inclination: 51
6473 deg
RA of node: 356
7408 deg
Eccentricity:
0006256
Arg of perigee: 256
9593 deg
Mean anomaly: 103
0862 deg
Mean motion: 15
56172900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 328
Coasting Arc #8 (Orbit 1968)
---------------------------------------
Vector Time (GMT): 2015/114/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3607142
32 A = 6775860
27 meter
Y = -3912242
33 meter E =
0003800
Z = -4198059
53 I = 51
59136
XDOT = 6429
805073 Wp = 162
91644
YDOT = 1977
222290 meter/sec RA = 351
39327 deg
ZDOT = 3679
432676 TA = 144
85929
MA = 144
83422
Ha = 215
665 n
mi
Hp = 213
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11834456
44 X = 3671014
60
Y = -12835440
72 feet Y = -3871547
86 meter
Z = -13773161
18 Z = -4180381
38
XDOT = 21095
161000 XDOT = 6389
343990
YDOT = 6486
949769 feet/sec YDOT = 2048
898416 meter/sec
ZDOT = 12071
629513 ZDOT = 3710
569327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2131799
24 X = -649772
41
Y = -17388542
60 feet Y = -5300027
78 meter
Z = -13696601
21 Z = -4174724
05
XDOT = 17238
743907 XDOT = 5254
369143
YDOT = -11733
879026 feet/sec YDOT = -3576
486327 meter/sec
ZDOT = 12204
714568 ZDOT = 3719
997000
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 15114
56051567
00016717 00000-0 10270-3 0 9071
2 25544 51
6463 351
9231 0006351 260
8410 99
2026 15
56216787 19698
Satellite: ISS
Catalog Number: 25544
Epoch time: 15114
56051567 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 351
9231 deg
Eccentricity:
0006351
Arg of perigee: 260
8410 deg
Mean anomaly: 99
2026 deg
Mean motion: 15
56216787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1969
Checksum: 313
Coasting Arc #9 (Orbit 1984)
---------------------------------------
Vector Time (GMT): 2015/115/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5483208
47 A = 6780816
02 meter
Y = 3228300
71 meter E =
0008277
Z = 2329419
18 I = 51
57777
XDOT = -4282
740169 Wp = 123
76393
YDOT = -3370
757473 meter/sec RA = 346
39339 deg
ZDOT = -5400
359997 TA = 30
20890
MA = 30
16120
Ha = 215
393 n
mi
Hp = 213
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17989529
10 X = -5530216
08
Y = 10591537
78 feet Y = 3166721
13 meter
Z = 7642451
39 Z = 2302668
39
XDOT = -14050
984806 XDOT = -4218
496182
YDOT = -11058
915593 feet/sec YDOT = -3418
290834 meter/sec
ZDOT = -17717
716526 ZDOT = -5421
008682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3170860
09 X = -966478
16
Y = 20676041
88 feet Y = 6302057
56 meter
Z = 7527139
65 Z = 2294272
17
XDOT = -15869
035087 XDOT = -4836
881895
YDOT = 4059
740291 feet/sec YDOT = 1237
408841 meter/sec
ZDOT = -17805
563066 ZDOT = -5427
135622
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 15115
58795479
00016717 00000-0 10270-3 0 9082
2 25544 51
6466 346
7855 0006377 265
9461 94
0964 15
56289987 19859
Satellite: ISS
Catalog Number: 25544
Epoch time: 15115
58795479 = yrday
fracday
Element set: 908
Inclination: 51
6466 deg
RA of node: 346
7855 deg
Eccentricity:
0006377
Arg of perigee: 265
9461 deg
Mean anomaly: 94
0964 deg
Mean motion: 15
56289987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1985
Checksum: 385
Coasting Arc #10 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2015/116/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6430094
49 A = 6782989
88 meter
Y = -2141314
31 meter E =
0008660
Z = 26289
38 I = 51
55344
XDOT = 1483
515851 Wp = 15
35763
YDOT = 4534
044091 meter/sec RA = 341
40505 deg
ZDOT = 6008
721374 TA = 344
92615
MA = 344
95194
Ha = 215
221 n
mi
Hp = 213
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21096110
52 X = 6453433
57
Y = -7025309
43 feet Y = -2069278
30 meter
Z = 86251
26 Z = 57582
48
XDOT = 4867
177990 XDOT = 1403
516564
YDOT = 14875
472740 feet/sec YDOT = 4550
186696 meter/sec
ZDOT = 19713
652802 ZDOT = 6015
733533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7508431
88 X = 2288570
04
Y = -20928043
00 feet Y = -6378867
51 meter
Z = 220811
93 Z = 67303
48
XDOT = 13101
949544 XDOT = 3993
474221
YDOT = 4914
959873 feet/sec YDOT = 1498
079769 meter/sec
ZDOT = 19742
815087 ZDOT = 6017
610038
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 15116
61535894
00016717 00000-0 10270-3 0 9091
2 25544 51
6453 341
6461 0006481 268
8575 91
1836 15
56311767 20014
Satellite: ISS
Catalog Number: 25544
Epoch time: 15116
61535894 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 341
6461 deg
Eccentricity:
0006481
Arg of perigee: 268
8575 deg
Mean anomaly: 91
1836 deg
Mean motion: 15
56311767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 319
Coasting Arc #11 (Orbit 2015)
---------------------------------------
Vector Time (GMT): 2015/117/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6303285
85 A = 6780321
98 meter
Y = 671237
62 meter E =
0004231
Z = -2398409
56 I = 51
51470
XDOT = 1475
000514 Wp = 215
77623
YDOT = -5289
662401 meter/sec RA = 336
41555 deg
ZDOT = -5355
452879 TA = 351
10141
MA = 351
10891
Ha = 215
114 n
mi
Hp = 213
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20680071
68 X = -6298672
67
Y = 2202223
17 feet Y = 600775
83 meter
Z = -7868797
76 Z = -2429018
71
XDOT = 4839
240531 XDOT = 1560
056095
YDOT = -17354
535437 feet/sec YDOT = -5272
692696 meter/sec
ZDOT = -17570
383461 ZDOT = -5348
080692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10709920
99 X = -3264383
92
Y = 17768754
96 feet Y = 5415916
51 meter
Z = -8000129
33 Z = -2438439
42
XDOT = -9543
247537 XDOT = -2908
781849
YDOT = -13650
267212 feet/sec YDOT = -4160
601446 meter/sec
ZDOT = -17537
743845 ZDOT = -5345
504324
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 15117
57851747
00016717 00000-0 10270-3 0 9107
2 25544 51
6447 336
8292 0006549 272
4631 87
5773 15
56359687 20162
Satellite: ISS
Catalog Number: 25544
Epoch time: 15117
57851747 = yrday
fracday
Element set: 910
Inclination: 51
6447 deg
RA of node: 336
8292 deg
Eccentricity:
0006549
Arg of perigee: 272
4631 deg
Mean anomaly: 87
5773 deg
Mean motion: 15
56359687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2016
Checksum: 343
Coasting Arc #12 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2015/118/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5155311
60 A = 6774867
58 meter
Y = 1058389
88 meter E =
0003537
Z = 4265283
48 I = 51
46778
XDOT = -4066
081599 Wp = 127
96331
YDOT = 5444
669937 meter/sec RA = 331
40536 deg
ZDOT = 3559
350225 TA = 285
63668
MA = 285
67571
Ha = 215
052 n
mi
Hp = 213
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16913751
96 X = 5122373
96
Y = 3472407
73 feet Y = 1115856
04 meter
Z = 13993712
19 Z = 4290247
11
XDOT = -13340
162728 XDOT = -4143
953124
YDOT = 17863
090346 feet/sec YDOT = 5398
765165 meter/sec
ZDOT = 11677
658220 ZDOT = 3539
408359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12736721
03 X = 3882152
57
Y = -11528591
96 feet Y = -3513914
83 meter
Z = 14100500
21 Z = 4297832
46
XDOT = 5658
281823 XDOT = 1724
644300
YDOT = 20444
737323 feet/sec YDOT = 6231
555936 meter/sec
ZDOT = 11591
120357 ZDOT = 3532
973485
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 15118
60585253
00016717 00000-0 10270-3 0 9119
2 25544 51
6442 331
6893 0006630 276
7525 83
2875 15
56403721 20320
Satellite: ISS
Catalog Number: 25544
Epoch time: 15118
60585253 = yrday
fracday
Element set: 911
Inclination: 51
6442 deg
RA of node: 331
6893 deg
Eccentricity:
0006630
Arg of perigee: 276
7525 deg
Mean anomaly: 83
2875 deg
Mean motion: 15
56403721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 303
Coasting Arc #13 (Orbit 2046)
---------------------------------------
Vector Time (GMT): 2015/119/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3234459
05 A = 6770832
57 meter
Y = -2854357
69 meter E =
0008403
Z = -5225965
40 I = 51
42640
XDOT = 5862
892490 Wp = 69
40116
YDOT = -4840
799325 meter/sec RA = 326
37348 deg
ZDOT = -983
065124 TA = 191
14931
MA = 191
16794
Ha = 215
231 n
mi
Hp = 213
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10611742
29 X = -3176914
49
Y = -9364690
57 feet Y = -2890206
10 meter
Z = -17145555
79 Z = -5241537
99
XDOT = 19235
211581 XDOT = 5921
363129
YDOT = -15881
887548 feet/sec YDOT = -4774
909761 meter/sec
ZDOT = -3225
279279 ZDOT = -954
441697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13707603
22 X = -4178077
46
Y = 3183426
10 feet Y = 970308
28 meter
Z = -17211740
16 Z = -5246138
40
XDOT = -1646
922173 XDOT = -501
981878
YDOT = -23889
760215 feet/sec YDOT = -7281
598913 meter/sec
ZDOT = -3101
661441 ZDOT = -945
386407
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 15119
56894604
00016717 00000-0 10270-3 0 9129
2 25544 51
6432 326
8710 0006521 279
5190 80
5226 15
56472077 20477
Satellite: ISS
Catalog Number: 25544
Epoch time: 15119
56894604 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 326
8710 deg
Eccentricity:
0006521
Arg of perigee: 279
5190 deg
Mean anomaly: 80
5226 deg
Mean motion: 15
56472077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2047
Checksum: 310
Coasting Arc #14 (Orbit 2062)
---------------------------------------
Vector Time (GMT): 2015/120/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 903914
47 A = 6771607
91 meter
Y = 4431663
46 meter E =
0004995
Z = 5042552
90 I = 51
40323
XDOT = -6614
085299 Wp = 337
84435
YDOT = 3428
467291 meter/sec RA = 321
33277 deg
ZDOT = -1823
546025 TA = 129
88823
MA = 129
84430
Ha = 215
428 n
mi
Hp = 213
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2965598
64 X = 829796
19
Y = 14539578
28 feet Y = 4441357
51 meter
Z = 16543808
72 Z = 5046763
70
XDOT = -21699
754919 XDOT = -6643
073433
YDOT = 11248
252268 feet/sec YDOT = 3354
342070 meter/sec
ZDOT = -5982
762550 ZDOT = -1855
747036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13633114
19 X = 4155373
21
Y = 5810628
63 feet Y = 1771079
61 meter
Z = 16560993
66 Z = 5047790
87
XDOT = -2454
692379 XDOT = -748
190237
YDOT = 23242
995980 feet/sec YDOT = 7084
465175 meter/sec
ZDOT = -6121
427078 ZDOT = -1865
810973
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 15120
59621173
00016717 00000-0 10270-3 0 9134
2 25544 51
6432 321
7315 0006627 283
1206 76
9208 15
56500126 20632
Satellite: ISS
Catalog Number: 25544
Epoch time: 15120
59621173 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 321
7315 deg
Eccentricity:
0006627
Arg of perigee: 283
1206 deg
Mean anomaly: 76
9208 deg
Mean motion: 15
56500126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2063
Checksum: 280
Coasting Arc #15 (Orbit 2077)
---------------------------------------
Vector Time (GMT): 2015/121/13:13:50
043
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1399401
62 A = 6776293
27 meter
Y = -5471498
92 meter E =
0000879
Z = -3743589
25 I = 51
39504
XDOT = 6258
978537 Wp = 317
91713
YDOT = -1299
504826 meter/sec RA = 316
30128 deg
ZDOT = 4239
059042 TA = 357
09094
MA = 357
09145
Ha = 215
511 n
mi
Hp = 213
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4591212
66 X = 1478666
48
Y = -17951111
94 feet Y = -5455406
90 meter
Z = -12282116
96 Z = -3736598
28
XDOT = 20534
706485 XDOT = 6252
452609
YDOT = -4263
467277 feet/sec YDOT = -1229
549094 meter/sec
ZDOT = 13907
674023 ZDOT = 4269
448686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12458471
78 X = -3797342
20
Y = -13742965
09 feet Y = -4188855
76 meter
Z = -12251099
63 Z = -3734135
17
XDOT = 6636
308358 XDOT = 2022
746788
YDOT = -18530
105599 feet/sec YDOT = -5647
976187 meter/sec
ZDOT = 14038
154558 ZDOT = 4278
829509
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 15121
55924038
00016717 00000-0 10270-3 0 9148
2 25544 51
6428 316
9120 0006565 286
5726 73
4706 15
56575503 20784
Satellite: ISS
Catalog Number: 25544
Epoch time: 15121
55924038 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 316
9120 deg
Eccentricity:
0006565
Arg of perigee: 286
5726 deg
Mean anomaly: 73
4706 deg
Mean motion: 15
56575503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2078
Checksum: 316
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