[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 10th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
162/10:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 211
9
Coasting Arc #1 (Orbit 2700)
---------------------------------------
Vector Time (GMT): 2015/161/13:05:17
188
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -10005
41 A = 6781375
63 meter
Y = -5896202
85 meter E =
0015230
Z = 3341076
23 I = 51
97052
XDOT = 5427
725282 Wp = 76
07318
YDOT = -2689
039369 meter/sec RA = 116
20996 deg
ZDOT = -4707
762017 TA = 65
18016
MA = 65
02184
Ha = 220
459 n
mi
Hp = 211
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -32826
14 X = 39698
30
Y = -19344497
54 feet Y = -5896037
05 meter
Z = 10961536
20 Z = 3341147
97
XDOT = 17807
497643 XDOT = 5480
260030
YDOT = -8822
307641 feet/sec YDOT = -2628
048946 meter/sec
ZDOT = -15445
413440 ZDOT = -4681
267607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19287826
47 X = -5878929
51
Y = 1469771
09 feet Y = 447986
23 meter
Z = 10962913
00 Z = 3341495
88
XDOT = -9960
305834 XDOT = -3035
901218
YDOT = -15830
285207 feet/sec YDOT = -4825
070931 meter/sec
ZDOT = -15331
021647 ZDOT = -4672
895398
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 15161
58446913
00016717 00000-0 10270-3 0 9001
2 25544 51
6419 117
0087 0004550 29
1673 330
9734 15
55234900 27017
Satellite: ISS
Catalog Number: 25544
Epoch time: 15161
58446913 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 117
0087 deg
Eccentricity:
0004550
Arg of perigee: 29
1673 deg
Mean anomaly: 330
9734 deg
Mean motion: 15
55234900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2701
Checksum: 292
Coasting Arc #2 (Orbit 2714)
---------------------------------------
Vector Time (GMT): 2015/162/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4610909
90 A = 6776938
21 meter
Y = 1735958
85 meter E =
0009941
Z = 4644632
24 I = 51
96583
XDOT = 333
850950 Wp = 89
05141
YDOT = -7070
689889 meter/sec RA = 111
85579 deg
ZDOT = 2968
838108 TA = 331
51188
MA = 331
56618
Ha = 220
538 n
mi
Hp = 211
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15127657
14 X = -4652541
18
Y = 5695403
06 feet Y = 1684163
52 meter
Z = 15238294
74 Z = 4622132
15
XDOT = 1095
311517 XDOT = 398
470658
YDOT = -23197
801473 feet/sec YDOT = -7066
595458 meter/sec
ZDOT = 9740
282506 ZDOT = 2970
616341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4447731
97 X = -1355668
70
Y = 15634889
66 feet Y = 4765514
37 meter
Z = 15141240
34 Z = 4615050
06
XDOT = -16918
930958 XDOT = -5156
890156
YDOT = -14271
363760 feet/sec YDOT = -4349
911674 meter/sec
ZDOT = 9749
220889 ZDOT = 2971
562527
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 15162
48405175
00016717 00000-0 10270-3 0 9017
2 25544 51
6399 112
5160 0004383 32
5451 327
5971 15
55273307 27156
Satellite: ISS
Catalog Number: 25544
Epoch time: 15162
48405175 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 112
5160 deg
Eccentricity:
0004383
Arg of perigee: 32
5451 deg
Mean anomaly: 327
5971 deg
Mean motion: 15
55273307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2715
Checksum: 297
Coasting Arc #3 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2015/163/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4205385
98 A = 6774203
80 meter
Y = 438982
13 meter E =
0017944
Z = -5307969
11 I = 51
96795
XDOT = -1675
464840 Wp = 73
95126
YDOT = 7437
903161 meter/sec RA = 106
86855 deg
ZDOT = -709
463734 TA = 189
27681
MA = 189
31000
Ha = 220
487 n
mi
Hp = 211
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13797198
09 X = 4225949
02
Y = 1440230
07 feet Y = 486124
96 meter
Z = -17414596
81 Z = -5287489
95
XDOT = -5496
931890 XDOT = -1755
066382
YDOT = 24402
569427 feet/sec YDOT = 7418
722003 meter/sec
ZDOT = -2327
636924 ZDOT = -717
795583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9230869
18 X = 2813568
93
Y = -10501630
51 feet Y = -3200896
98 meter
Z = -17326624
91 Z = -5281155
27
XDOT = 15946
489990 XDOT = 4860
490149
YDOT = 17934
043871 feet/sec YDOT = 5466
296572 meter/sec
ZDOT = -2364
837603 ZDOT = -720
802501
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 15163
44787430
00016717 00000-0 10270-3 0 9022
2 25544 51
6402 107
7019 0004477 36
9762 323
1699 15
55272608 27306
Satellite: ISS
Catalog Number: 25544
Epoch time: 15163
44787430 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 107
7019 deg
Eccentricity:
0004477
Arg of perigee: 36
9762 deg
Mean anomaly: 323
1699 deg
Mean motion: 15
55272608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 312
Coasting Arc #4 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2015/164/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3534652
24 A = 6774810
65 meter
Y = -2663121
08 meter E =
0009437
Z = 5125087
78 I = 51
97922
XDOT = 2797
737263 Wp = 47
79389
YDOT = -6947
631092 meter/sec RA = 101
87912 deg
ZDOT = -1672
487402 TA = 58
31198
MA = 58
21999
Ha = 220
558 n
mi
Hp = 211
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11596628
09 X = -3529505
91
Y = -8737273
88 feet Y = -2702619
66 meter
Z = 16814592
45 Z = 5107929
14
XDOT = 9178
928027 XDOT = 2883
343807
YDOT = -22794
065264 feet/sec YDOT = -6915
866127 meter/sec
ZDOT = -5487
163393 ZDOT = -1658
689210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13821925
97 X = -4212923
04
Y = 4715413
40 feet Y = 1437258
00 meter
Z = 16741311
05 Z = 5102751
61
XDOT = -13250
271986 XDOT = -4038
682901
YDOT = -19478
270563 feet/sec YDOT = -5936
976868 meter/sec
ZDOT = -5426
529617 ZDOT = -1654
006227
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 15164
47592981
00016717 00000-0 10270-3 0 9032
2 25544 51
6406 102
5678 0004457 39
5764 320
5714 15
55312165 27462
Satellite: ISS
Catalog Number: 25544
Epoch time: 15164
47592981 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 102
5678 deg
Eccentricity:
0004457
Arg of perigee: 39
5764 deg
Mean anomaly: 320
5714 deg
Mean motion: 15
55312165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 318
Coasting Arc #5 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2015/165/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2720383
20 A = 6778542
43 meter
Y = 4611593
22 meter E =
0010244
Z = -4165353
05 I = 51
99805
XDOT = -3654
639774 Wp = 85
78975
YDOT = 5568
999631 meter/sec RA = 96
89806 deg
ZDOT = 3787
504732 TA = 223
01941
MA = 223
09954
Ha = 220
485 n
mi
Hp = 211
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8925141
73 X = 2688846
99
Y = 15129899
01 feet Y = 4641838
52 meter
Z = -13665856
46 Z = -4152213
84
XDOT = -11990
287971 XDOT = -3735
040491
YDOT = 18270
996165 feet/sec YDOT = 5527
681033 meter/sec
ZDOT = 12426
196627 ZDOT = 3769
556445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17590423
27 X = 5361561
01
Y = 816243
91 feet Y = 248791
14 meter
Z = -13610230
96 Z = -4148398
40
XDOT = 8656
700234 XDOT = 2638
562231
YDOT = 18857
373909 feet/sec YDOT = 5747
727568 meter/sec
ZDOT = 12347
957249 ZDOT = 3763
657369
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 15165
43971177
00016717 00000-0 10270-3 0 9048
2 25544 51
6412 97
7544 0004460 42
1980 317
9516 15
55328676 27611
Satellite: ISS
Catalog Number: 25544
Epoch time: 15165
43971177 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 97
7544 deg
Eccentricity:
0004460
Arg of perigee: 42
1980 deg
Mean anomaly: 317
9516 deg
Mean motion: 15
55328676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 323
Coasting Arc #6 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2015/166/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1751698
90 A = 6783050
79 meter
Y = -6049788
09 meter E =
0016457
Z = 2503435
77 I = 52
01746
XDOT = 4286
944899 Wp = 91
32530
YDOT = -3462
436922 meter/sec RA = 91
93208 deg
ZDOT = -5337
858540 TA = 60
72956
MA = 60
56515
Ha = 220
431 n
mi
Hp = 211
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5747043
64 X = -1696079
37
Y = -19848386
11 feet Y = -6069066
09 meter
Z = 8213371
95 Z = 2495060
55
XDOT = 14064
779853 XDOT = 4351
273566
YDOT = -11359
701187 feet/sec YDOT = -3414
137072 meter/sec
ZDOT = -17512
659253 ZDOT = -5316
877487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19859955
13 X = -6053314
32
Y = -5756775
12 feet Y = -1754665
06 meter
Z = 8178517
16 Z = 2492812
03
XDOT = -2400
029073 XDOT = -731
528861
YDOT = -16610
440456 feet/sec YDOT = -5062
862251 meter/sec
ZDOT = -17421
763640 ZDOT = -5310
153557
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 15166
46772532
00016717 00000-0 10270-3 0 9057
2 25544 51
6421 92
6199 0004454 45
7910 314
3608 15
55382605 27778
Satellite: ISS
Catalog Number: 25544
Epoch time: 15166
46772532 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 92
6199 deg
Eccentricity:
0004454
Arg of perigee: 45
7910 deg
Mean anomaly: 314
3608 deg
Mean motion: 15
55382605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 319
Coasting Arc #7 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2015/167/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 727051
15 A = 6785503
73 meter
Y = 6722640
28 meter E =
0015465
Z = -476304
04 I = 52
02629
XDOT = -4660
297582 Wp = 43
78383
YDOT = 921
843292 meter/sec RA = 86
97928 deg
ZDOT = 6024
494029 TA = 311
10223
MA = 311
23567
Ha = 220
394 n
mi
Hp = 211
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2385338
40 X = 654136
65
Y = 22055906
44 feet Y = 6730363
03 meter
Z = -1562677
29 Z = -472948
27
XDOT = -15289
690231 XDOT = -4699
524305
YDOT = 3024
420249 feet/sec YDOT = 869
508580 meter/sec
ZDOT = 19765
400356 ZDOT = 6001
759996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20062562
54 X = 6115069
06
Y = 9470337
06 feet Y = 2886558
74 meter
Z = -1549551
14 Z = -472303
19
XDOT = -4775
029297 XDOT = -1455
428930
YDOT = 13264
927921 feet/sec YDOT = 4043
150030 meter/sec
ZDOT = 19667
445221 ZDOT = 5994
637303
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 15167
43146793
00016717 00000-0 10270-3 0 9060
2 25544 51
6423 87
8068 0004383 49
0936 311
0596 15
55412627 27922
Satellite: ISS
Catalog Number: 25544
Epoch time: 15167
43146793 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 87
8068 deg
Eccentricity:
0004383
Arg of perigee: 49
0936 deg
Mean anomaly: 311
0596 deg
Mean motion: 15
55412627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2792
Checksum: 326
Coasting Arc #8 (Orbit 2807)
---------------------------------------
Vector Time (GMT): 2015/168/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 409824
46 A = 6784290
31 meter
Y = -6558503
94 meter E =
0008870
Z = -1684860
44 I = 52
02114
XDOT = 4768
984603 Wp = 112
46658
YDOT = 1764
600646 meter/sec RA = 82
02890 deg
ZDOT = -5736
200129 TA = 85
89947
MA = 85
79810
Ha = 220
346 n
mi
Hp = 211
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1344568
45 X = 491317
17
Y = -21517401
39 feet Y = -6553465
12 meter
Z = -5527757
36 Z = -1682672
63
XDOT = 15646
274943 XDOT = 4776
762253
YDOT = 5789
372199 feet/sec YDOT = 1817
974889 meter/sec
ZDOT = -18819
554230 ZDOT = -5713
014195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17844111
04 X = -5438885
04
Y = -12104225
27 feet Y = -3689367
86 meter
Z = -5517060
82 Z = -1681600
14
XDOT = 12102
381708 XDOT = 3688
805945
YDOT = -9349
716631 feet/sec YDOT = -2849
793629 meter/sec
ZDOT = -18720
173966 ZDOT = -5705
909025
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 15168
45943940
00016717 00000-0 10270-3 0 9073
2 25544 51
6434 82
6721 0004367 51
9666 308
1881 15
55447892 28081
Satellite: ISS
Catalog Number: 25544
Epoch time: 15168
45943940 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 82
6721 deg
Eccentricity:
0004367
Arg of perigee: 51
9666 deg
Mean anomaly: 308
1881 deg
Mean motion: 15
55447892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2808
Checksum: 338
Coasting Arc #9 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2015/169/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1557250
88 A = 6780121
25 meter
Y = 5561716
40 meter E =
0015852
Z = 3535923
11 I = 52
00213
XDOT = -4586
301466 Wp = 82
77081
YDOT = -4171
841161 meter/sec RA = 77
06891 deg
ZDOT = 4526
760779 TA = 318
72618
MA = 318
84590
Ha = 220
366 n
mi
Hp = 211
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5109090
81 X = -1636503
70
Y = 18247101
06 feet Y = 5543858
57 meter
Z = 11600797
59 Z = 3528166
61
XDOT = -15046
920821 XDOT = -4561
299284
YDOT = -13687
142918 feet/sec YDOT = -4222
989031 meter/sec
ZDOT = 14851
577359 ZDOT = 4504
541648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13331241
03 X = 4063362
27
Y = 13495774
53 feet Y = 4113512
08 meter
Z = 11566334
46 Z = 3525418
74
XDOT = -18382
728495 XDOT = -5603
055645
YDOT = 5468
209148 feet/sec YDOT = 1666
710148 meter/sec
ZDOT = 14756
828532 ZDOT = 4497
881337
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 15169
48738924
00016717 00000-0 10270-3 0 9082
2 25544 51
6433 77
5378 0004314 56
0780 304
0783 15
55479282 28248
Satellite: ISS
Catalog Number: 25544
Epoch time: 15169
48738924 = yrday
fracday
Element set: 908
Inclination: 51
6433 deg
RA of node: 77
5378 deg
Eccentricity:
0004314
Arg of perigee: 56
0780 deg
Mean anomaly: 304
0783 deg
Mean motion: 15
55479282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 334
Coasting Arc #10 (Orbit 2838)
---------------------------------------
Vector Time (GMT): 2015/170/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2727718
36 A = 6775407
08 meter
Y = -3886630
00 meter E =
0015851
Z = -4848217
65 I = 51
97911
XDOT = 4027
136646 Wp = 68
28501
YDOT = 5996
822235 meter/sec RA = 72
09145 deg
ZDOT = -2542
614787 TA = 176
79317
MA = 176
78300
Ha = 220
279 n
mi
Hp = 211
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8949207
21 X = 2794527
52
Y = -12751410
77 feet Y = -3855752
69 meter
Z = -15906225
88 Z = -4834805
24
XDOT = 13212
390572 XDOT = 3972
130424
YDOT = 19674
613631 feet/sec YDOT = 6041
549081 meter/sec
ZDOT = -8341
912032 ZDOT = -2523
184702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6886538
37 X = -2099016
90
Y = -14039905
96 feet Y = -4279363
34 meter
Z = -15847758
13 Z = -4830396
68
XDOT = 22595
914192 XDOT = 6887
234646
YDOT = -1763
712168 feet/sec YDOT = -537
579469 meter/sec
ZDOT = -8259
525041 ZDOT = -2517
503233
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 15170
45107281
00016717 00000-0 10270-3 0 9098
2 25544 51
6437 72
7236 0004346 58
7539 301
4040 15
55520479 28396
Satellite: ISS
Catalog Number: 25544
Epoch time: 15170
45107281 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 72
7236 deg
Eccentricity:
0004346
Arg of perigee: 58
7539 deg
Mean anomaly: 301
4040 deg
Mean motion: 15
55520479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2839
Checksum: 308
Coasting Arc #11 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2015/171/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3778828
53 A = 6773137
00 meter
Y = 1770306
96 meter E =
0006283
Z = 5329743
67 I = 51
96121
XDOT = -3089
888634 Wp = 73
69107
YDOT = -7025
204212 meter/sec RA = 67
10152 deg
ZDOT = 144
289566 TA = 14
95061
MA = 14
93205
Ha = 220
284 n
mi
Hp = 211
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12397731
39 X = -3824233
37
Y = 5808093
71 feet Y = 1727795
16 meter
Z = 17486035
66 Z = 5311276
91
XDOT = -10137
429900 XDOT = -3011
802370
YDOT = -23048
570250 feet/sec YDOT = -7059
320779 meter/sec
ZDOT = 473
390966 ZDOT = 129
468478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -628547
64 X = -191581
32
Y = 13777763
18 feet Y = 4199462
22 meter
Z = 17406243
39 Z = 5305422
99
XDOT = -24121
133992 XDOT = -7352
121641
YDOT = -1613
132314 feet/sec YDOT = -491
682729 meter/sec
ZDOT = 411
041101 ZDOT = 125
285328
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 15171
47897997
00016717 00000-0 10270-3 0 9103
2 25544 51
6434 67
5889 0004140 61
3220 298
8349 15
55575166 28550
Satellite: ISS
Catalog Number: 25544
Epoch time: 15171
47897997 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 67
5889 deg
Eccentricity:
0004140
Arg of perigee: 61
3220 deg
Mean anomaly: 298
8349 deg
Mean motion: 15
55575166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 347
Coasting Arc #12 (Orbit 2869)
---------------------------------------
Vector Time (GMT): 2015/172/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4622214
54 A = 6774905
79 meter
Y = 459278
86 meter E =
0015560
Z = -4945781
09 I = 51
95422
XDOT = 1734
904195 Wp = 95
96964
YDOT = 7101
150085 meter/sec RA = 62
10874 deg
ZDOT = 2285
422235 TA = 196
27157
MA = 196
32159
Ha = 220
222 n
mi
Hp = 211
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15164745
87 X = 4640759
81
Y = 1506820
39 feet Y = 511071
65 meter
Z = -16226315
90 Z = -4923282
34
XDOT = 5691
942898 XDOT = 1644
266853
YDOT = 23297
736498 feet/sec YDOT = 7120
043915 meter/sec
ZDOT = 7498
104446 ZDOT = 2293
630539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8168427
75 X = 2489736
78
Y = -12986351
54 feet Y = -3958239
95 meter
Z = -16129625
37 Z = -4916309
81
XDOT = 22418
335926 XDOT = 6833
108790
YDOT = 4764
902017 feet/sec YDOT = 1452
342135 meter/sec
ZDOT = 7531
985475 ZDOT = 2295
749173
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 15172
44262617
00016717 00000-0 10270-3 0 9117
2 25544 51
6439 62
7741 0004237 64
7120 295
4472 15
55569412 28706
Satellite: ISS
Catalog Number: 25544
Epoch time: 15172
44262617 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 62
7741 deg
Eccentricity:
0004237
Arg of perigee: 64
7120 deg
Mean anomaly: 295
4472 deg
Mean motion: 15
55569412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2870
Checksum: 307
Coasting Arc #13 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2015/173/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5080077
94 A = 6779391
36 meter
Y = -2540714
78 meter E =
0015950
Z = 3689757
43 I = 51
95349
XDOT = -20
379500 Wp = 80
85203
YDOT = -6316
661245 meter/sec RA = 57
12691 deg
ZDOT = -4359
147117 TA = 55
37968
MA = 55
22938
Ha = 220
286 n
mi
Hp = 210
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16666922
37 X = -5069212
84
Y = -8335678
40 feet Y = -2597463
10 meter
Z = 12105503
39 Z = 3665105
72
XDOT = -66
861878 XDOT = 71
431406
YDOT = -20723
954216 feet/sec YDOT = -6316
375426 meter/sec
ZDOT = -14301
663769 ZDOT = -4359
023656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14741712
77 X = -4493274
05
Y = 11510672
27 feet Y = 3508452
91 meter
Z = 11999974
03 Z = 3657592
08
XDOT = -17848
218815 XDOT = -5440
137095
YDOT = -7886
739102 feet/sec YDOT = -2403
878078 meter/sec
ZDOT = -14299
854805 ZDOT = -4358
595744
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 15173
47049427
00016717 00000-0 10270-3 0 9124
2 25544 51
6436 57
6388 0004229 68
9520 291
2085 15
55592132 28860
Satellite: ISS
Catalog Number: 25544
Epoch time: 15173
47049427 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 57
6388 deg
Eccentricity:
0004229
Arg of perigee: 68
9520 deg
Mean anomaly: 291
2085 deg
Mean motion: 15
55592132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 328
Coasting Arc #14 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2015/174/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5041359
91 A = 6783550
32 meter
Y = 4146394
82 meter E =
0011043
Z = -1836829
40 I = 51
95065
XDOT = -1892
469040 Wp = 49
96335
YDOT = 4800
748796 meter/sec RA = 52
15983 deg
ZDOT = 5672
354758 TA = 289
91697
MA = 290
03591
Ha = 220
134 n
mi
Hp = 210
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16539894
71 X = 5003541
84
Y = 13603657
55 feet Y = 4202559
30 meter
Z = -6026343
18 Z = -1812431
08
XDOT = -6208
887926 XDOT = -1973
565575
YDOT = 15750
488176 feet/sec YDOT = 4779
132085 meter/sec
ZDOT = 18610
087789 ZDOT = 5662
964949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19264219
48 X = 5871734
10
Y = -9421326
79 feet Y = -2871620
41 meter
Z = -5922235
83 Z = -1805097
48
XDOT = 11008
490173 XDOT = 3355
387805
YDOT = 10898
943951 feet/sec YDOT = 3321
998116 meter/sec
ZDOT = 18568
720008 ZDOT = 5659
745858
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 15174
43410069
00016717 00000-0 10270-3 0 9136
2 25544 51
6444 52
8239 0004124 71
4186 288
7415 15
55639658 29013
Satellite: ISS
Catalog Number: 25544
Epoch time: 15174
43410069 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 52
8239 deg
Eccentricity:
0004124
Arg of perigee: 71
4186 deg
Mean anomaly: 288
7415 deg
Mean motion: 15
55639658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 313
Coasting Arc #15 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2015/175/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4371146
09 A = 6784878
45 meter
Y = -5168860
71 meter E =
0013616
Z = -388704
87 I = 51
93532
XDOT = 3834
053732 Wp = 122
42248
YDOT = -2801
466642 meter/sec RA = 47
20254 deg
ZDOT = -6022
967369 TA = 61
75310
MA = 61
61572
Ha = 220
076 n
mi
Hp = 210
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14341030
49 X = -4311133
60
Y = -16958204
42 feet Y = -5217406
14 meter
Z = -1275278
44 Z = -409793
65
XDOT = 12578
916445 XDOT = 3894
352725
YDOT = -9191
163525 feet/sec YDOT = -2758
254130 meter/sec
ZDOT = -19760
391629 ZDOT = -6004
196058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21276071
37 X = -6484946
55
Y = 6351215
25 feet Y = 1935850
41 meter
Z = -1364932
15 Z = -416031
32
XDOT = -2879
531685 XDOT = -877
681258
YDOT = -13769
761008 feet/sec YDOT = -4197
023155 meter/sec
ZDOT = -19679
074449 ZDOT = -5998
181892
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 15175
46192863
00016717 00000-0 10270-3 0 9140
2 25544 51
6448 47
6880 0004033 76
1541 284
0061 15
55634833 29170
Satellite: ISS
Catalog Number: 25544
Epoch time: 15175
46192863 = yrday
fracday
Element set: 914
Inclination: 51
6448 deg
RA of node: 47
6880 deg
Eccentricity:
0004033
Arg of perigee: 76
1541 deg
Mean anomaly: 284
0061 deg
Mean motion: 15
55634833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2917
Checksum: 314
Coasting Arc #16 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2015/176/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3105905
92 A = 6782120
91 meter
Y = 5473716
60 meter E =
0017786
Z = 2505664
78 I = 51
90451
XDOT = -5485
376344 Wp = 75
55858
YDOT = 661
123881 meter/sec RA = 42
24102 deg
ZDOT = 5327
981107 TA = 312
47688
MA = 312
62707
Ha = 220
023 n
mi
Hp = 210
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10189980
07 X = 3032295
08
Y = 17958387
80 feet Y = 5508037
09 meter
Z = 8220684
99 Z = 2520574
33
XDOT = -17996
641549 XDOT = -5518
242868
YDOT = 2169
041603 feet/sec YDOT = 599
598621 meter/sec
ZDOT = 17480
252975 ZDOT = 5301
254403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20475717
22 X = 6240998
61
Y = -2458573
20 feet Y = -749373
11 meter
Z = 8283686
97 Z = 2524867
79
XDOT = -5132
910743 XDOT = -1564
511195
YDOT = 16058
409979 feet/sec YDOT = 4894
603362 meter/sec
ZDOT = 17365
157650 ZDOT = 5292
900052
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 15176
48973556
00016717 00000-0 10270-3 0 9150
2 25544 51
6449 42
5522 0004092 76
5567 283
6042 15
55679117 29331
Satellite: ISS
Catalog Number: 25544
Epoch time: 15176
48973556 = yrday
fracday
Element set: 915
Inclination: 51
6449 deg
RA of node: 42
5522 deg
Eccentricity:
0004092
Arg of perigee: 76
5567 deg
Mean anomaly: 283
6042 deg
Mean motion: 15
55679117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2933
Checksum: 335
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