[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 12th 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
169/11:15:28
743 0
9 1
9 1
9
N/A 1
6 -0
2 220
3
000/00:04:57
487 -0
3 -0
2 212
4
Coasting Arc #1 (Orbit 2730)
---------------------------------------
Vector Time (GMT): 2015/163/12:01:57
505
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2512467
50 A = 6776917
55 meter
Y = 4272415
11 meter E =
0012167
Z = -4632193
80 I = 51
97962
XDOT = -4143
145679 Wp = 89
74163
YDOT = 5696
239545 meter/sec RA = 106
48790 deg
ZDOT = 3013
475544 TA = 210
17687
MA = 210
24701
Ha = 220
421 n
mi
Hp = 211
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8243003
61 X = 2487007
30
Y = 14017109
93 feet Y = 4300369
23 meter
Z = -15197486
23 Z = -4620050
04
XDOT = -13592
997634 XDOT = -4221
172955
YDOT = 18688
449951 feet/sec YDOT = 5649
471628 meter/sec
ZDOT = 9886
730788 ZDOT = 2993
159724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15235741
20 X = 4643853
92
Y = -5818849
91 feet Y = -1773585
45 meter
Z = -15146063
60 Z = -4616520
18
XDOT = 15653
429179 XDOT = 4771
165214
YDOT = 15540
541826 feet/sec YDOT = 4736
757149 meter/sec
ZDOT = 9798
324218 ZDOT = 2986
529222
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
51211809
00016717 00000-0 10270-3 0 9000
2 25544 51
6418 107
3804 0004380 35
0551 325
0889 15
55291183 27312
Satellite: ISS
Catalog Number: 25544
Epoch time: 15163
51211809 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 107
3804 deg
Eccentricity:
0004380
Arg of perigee: 35
0551 deg
Mean anomaly: 325
0889 deg
Mean motion: 15
55291183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2731
Checksum: 286
Coasting Arc #2 (Orbit 2746)
---------------------------------------
Vector Time (GMT): 2015/164/12:01:57
505
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1382343
39 A = 6781446
06 meter
Y = -5802000
32 meter E =
0015750
Z = 3216691
30 I = 52
00422
XDOT = 4614
605976 Wp = 80
36510
YDOT = -3784
876075 meter/sec RA = 101
51533 deg
ZDOT = -4821
177138 TA = 62
59683
MA = 62
43669
Ha = 220
396 n
mi
Hp = 211
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4535247
34 X = -1332986
95
Y = -19035434
12 feet Y = -5817182
97 meter
Z = 10553449
15 Z = 3210095
31
XDOT = 15139
783385 XDOT = 4680
006125
YDOT = -12417
572426 feet/sec YDOT = -3732
906327 meter/sec
ZDOT = -15817
510294 ZDOT = -4798
601592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19516296
40 X = -5948567
14
Y = 1614097
21 feet Y = 491976
83 meter
Z = 10526175
68 Z = 3208378
35
XDOT = -9804
503748 XDOT = -2988
412742
YDOT = -15548
673344 feet/sec YDOT = -4739
235635 meter/sec
ZDOT = -15719
726439 ZDOT = -4791
372619
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
54016526
00016717 00000-0 10270-3 0 9014
2 25544 51
6427 102
2461 0004388 38
6464 321
5003 15
55338003 27474
Satellite: ISS
Catalog Number: 25544
Epoch time: 15164
54016526 = yrday
fracday
Element set: 901
Inclination: 51
6427 deg
RA of node: 102
2461 deg
Eccentricity:
0004388
Arg of perigee: 38
6464 deg
Mean anomaly: 321
5003 deg
Mean motion: 15
55338003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2747
Checksum: 282
Coasting Arc #3 (Orbit 2761)
---------------------------------------
Vector Time (GMT): 2015/165/12:01:57
505
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 279187
29 A = 6785030
28 meter
Y = 6642676
08 meter E =
0013172
Z = -1327059
92 I = 52
02184
XDOT = -4760
354371 Wp = 38
97846
YDOT = 1362
222661 meter/sec RA = 96
55787 deg
ZDOT = 5858
584757 TA = 306
64316
MA = 306
76420
Ha = 220
398 n
mi
Hp = 211
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 915968
81 X = 211332
97
Y = 21793556
70 feet Y = 6645418
91 meter
Z = -4353871
12 Z = -1325867
63
XDOT = -15617
960536 XDOT = -4803
692344
YDOT = 4469
234452 feet/sec YDOT = 1308
746201 meter/sec
ZDOT = 19221
078600 ZDOT = 5835
354567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21716771
54 X = 6619271
96
Y = 2052700
76 feet Y = 625663
19 meter
Z = -4350006
85 Z = -1325882
09
XDOT = 2420
860553 XDOT = 737
878296
YDOT = 14620
604559 feet/sec YDOT = 4456
360269 meter/sec
ZDOT = 19120
924130 ZDOT = 5828
057675
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
50393988
00016717 00000-0 10270-3 0 9022
2 25544 51
6427 97
4328 0004363 41
4222 318
7261 15
55350217 27620
Satellite: ISS
Catalog Number: 25544
Epoch time: 15165
50393988 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 97
4328 deg
Eccentricity:
0004363
Arg of perigee: 41
4222 deg
Mean anomaly: 318
7261 deg
Mean motion: 15
55350217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2762
Checksum: 306
Coasting Arc #4 (Orbit 2777)
---------------------------------------
Vector Time (GMT): 2015/166/12:01:57
505
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 835039
24 A = 6785384
76 meter
Y = -6680230
14 meter E =
0010765
Z = -829254
83 I = 52
02745
XDOT = 4626
095009 Wp = 117
10129
YDOT = 1311
623999 meter/sec RA = 91
60808 deg
ZDOT = -5971
807286 TA = 71
82034
MA = 71
70318
Ha = 220
360 n
mi
Hp = 211
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2739630
04 X = 913705
34
Y = -21916765
54 feet Y = -6670452
22 meter
Z = -2720652
34 Z = -825008
21
XDOT = 15177
477064 XDOT = 4640
093277
YDOT = 4303
228342 feet/sec YDOT = 1363
435126 meter/sec
ZDOT = -19592
543589 ZDOT = -5949
300282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21427699
16 X = -6531162
70
Y = -5367483
48 feet Y = -1636008
97 meter
Z = -2701104
09 Z = -823296
53
XDOT = 5715
451692 XDOT = 1742
069676
YDOT = -13112
396331 feet/sec YDOT = -3996
658402 meter/sec
ZDOT = -19496
003110 ZDOT = -5942
381748
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
53194536
00016717 00000-0 10270-3 0 9035
2 25544 51
6441 92
2983 0004296 45
9215 314
2291 15
55385677 27781
Satellite: ISS
Catalog Number: 25544
Epoch time: 15166
53194536 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 92
2983 deg
Eccentricity:
0004296
Arg of perigee: 45
9215 deg
Mean anomaly: 314
2291 deg
Mean motion: 15
55385677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2778
Checksum: 330
Coasting Arc #5 (Orbit 2793)
---------------------------------------
Vector Time (GMT): 2015/167/12:01:57
505
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1859935
31 A = 6782245
90 meter
Y = 5872262
02 meter E =
0017263
Z = 2817016
26 I = 52
01718
XDOT = -4240
206147 Wp = 72
53752
YDOT = -3816
772978 meter/sec RA = 86
65368 deg
ZDOT = 5135
980037 TA = 319
30973
MA = 319
43858
Ha = 220
399 n
mi
Hp = 211
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6102149
97 X = -1939146
16
Y = 19265951
50 feet Y = 5851019
69 meter
Z = 9242179
33 Z = 2807789
50
XDOT = -13911
437489 XDOT = -4222
159664
YDOT = -12522
221058 feet/sec YDOT = -3864
089591 meter/sec
ZDOT = 16850
328207 ZDOT = 5115
425152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18530372
33 X = 5648057
49
Y = 8111188
86 feet Y = 2472290
36 meter
Z = 9201354
07 Z = 2804572
72
XDOT = -13305
538446 XDOT = -4055
528118
YDOT = 11303
926547 feet/sec YDOT = 3445
436811 meter/sec
ZDOT = 16762
666305 ZDOT = 5109
260690
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
55992926
00016717 00000-0 10270-3 0 9048
2 25544 51
6440 87
1641 0004333 49
0639 311
0889 15
55417366 27948
Satellite: ISS
Catalog Number: 25544
Epoch time: 15167
55992926 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 87
1641 deg
Eccentricity:
0004333
Arg of perigee: 49
0639 deg
Mean anomaly: 311
0889 deg
Mean motion: 15
55417366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2794
Checksum: 330
Coasting Arc #6 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2015/168/12:01:57
505
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2838531
16 A = 6777307
22 meter
Y = -4321854
77 meter E =
0013056
Z = -4394872
41 I = 51
99941
XDOT = 3569
076526 Wp = 63
75922
YDOT = 5839
145619 meter/sec RA = 81
68463 deg
ZDOT = -3439
242709 TA = 171
51261
MA = 171
49051
Ha = 220
291 n
mi
Hp = 211
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9312766
28 X = 2907996
82
Y = -14179313
57 feet Y = -4289723
41 meter
Z = -14418872
75 Z = -4380915
31
XDOT = 11709
568656 XDOT = 3520
223070
YDOT = 19157
301901 feet/sec YDOT = 5878
784721 meter/sec
ZDOT = -11283
604688 ZDOT = -3422
022643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13321460
34 X = -4060381
11
Y = -10586367
77 feet Y = -3226724
90 meter
Z = -14357992
62 Z = -4376316
15
XDOT = 19324
477080 XDOT = 5890
100614
YDOT = -9122
607728 feet/sec YDOT = -2780
570836 meter/sec
ZDOT = -11210
684145 ZDOT = -3417
016527
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
52364373
00016717 00000-0 10270-3 0 9056
2 25544 51
6450 82
3505 0004324 52
3142 307
8403 15
55474092 28092
Satellite: ISS
Catalog Number: 25544
Epoch time: 15168
52364373 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 82
3505 deg
Eccentricity:
0004324
Arg of perigee: 52
3142 deg
Mean anomaly: 307
8403 deg
Mean motion: 15
55474092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2809
Checksum: 292
Coasting Arc #7 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2015/169/11:17:57
487
Vector Time (MET): N/A
Weight (LBS) : 877531
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3994976
23 A = 6774423
29 meter
Y = -1252757
07 meter E =
0017089
Z = -5340379
78 I = 51
98072
XDOT = 1950
487876 Wp = 81
22734
YDOT = 7399
960468 meter/sec RA = 76
84379 deg
ZDOT = -275
012539 TA = 186
14931
MA = 186
17031
Ha = 220
262 n
mi
Hp = 212
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13106877
39 X = 4034629
38
Y = -4110095
37 feet Y = -1207860
16 meter
Z = -17520931
05 Z = -5320876
91
XDOT = 6399
238437 XDOT = 1868
930684
YDOT = 24278
085525 feet/sec YDOT = 7421
316125 meter/sec
ZDOT = -902
272108 ZDOT = -265
734536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -558569
98 X = -170252
13
Y = -13831571
61 feet Y = -4215863
03 meter
Z = -17436793
57 Z = -5314734
68
XDOT = 24099
886297 XDOT = 7345
645343
YDOT = 123
157483 feet/sec YDOT = 37
538401 meter/sec
ZDOT = -863
826741 ZDOT = -263
294391
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
48734121
00016717 00000-0 10270-3 0 9065
2 25544 51
6445 77
5361 0002897 45
1645 314
9743 15
55144843 28244
Satellite: ISS
Catalog Number: 25544
Epoch time: 15169
48734121 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 77
5361 deg
Eccentricity:
0002897
Arg of perigee: 45
1645 deg
Mean anomaly: 314
9743 deg
Mean motion: 15
55144843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 323
Coasting Arc #8 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2015/170/11:17:57
487
Vector Time (MET): N/A
Weight (LBS) : 877531
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4443094
20 A = 6775636
20 meter
Y = -946563
65 meter E =
0008819
Z = 5022701
29 I = 51
97676
XDOT = -739
083692 Wp = 53
13027
YDOT = -7362
318707 meter/sec RA = 71
85708 deg
ZDOT = -2033
664759 TA = 56
57069
MA = 56
48638
Ha = 220
326 n
mi
Hp = 212
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14577080
72 X = -4456577
51
Y = -3105523
79 feet Y = -996325
27 meter
Z = 16478678
76 Z = 5001084
87
XDOT = -2424
815261 XDOT = -646
822839
YDOT = -24154
588935 feet/sec YDOT = -7370
067504 meter/sec
ZDOT = -6672
128473 ZDOT = -2037
031910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6559144
67 X = -1999227
30
Y = 13496773
50 feet Y = 4113816
56 meter
Z = 16385882
35 Z = 4994416
94
XDOT = -23031
000353 XDOT = -7019
848908
YDOT = -3045
921109 feet/sec YDOT = -928
396754 meter/sec
ZDOT = -6685
147431 ZDOT = -2037
632937
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
51549405
00016717 00000-0 10270-3 0 9071
2 25544 51
6441 72
4032 0002850 46
5626 313
5764 15
55189381 28404
Satellite: ISS
Catalog Number: 25544
Epoch time: 15170
51549405 = yrday
fracday
Element set: 907
Inclination: 51
6441 deg
RA of node: 72
4032 deg
Eccentricity:
0002850
Arg of perigee: 46
5626 deg
Mean anomaly: 313
5764 deg
Mean motion: 15
55189381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 299
Coasting Arc #9 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2015/171/11:17:57
487
Vector Time (MET): N/A
Weight (LBS) : 877531
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4639470
56 A = 6779580
17 meter
Y = 2944471
15 meter E =
0008616
Z = -3978400
46 I = 51
97992
XDOT = -661
331129 Wp = 90
66878
YDOT = 6481
703170 meter/sec RA = 66
87791 deg
ZDOT = 4033
403845 TA = 221
22290
MA = 221
28799
Ha = 220
228 n
mi
Hp = 212
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15221360
10 X = 4625525
39
Y = 9660338
42 feet Y = 2996275
22 meter
Z = -13052494
95 Z = -3955896
53
XDOT = -2169
721552 XDOT = -753
354543
YDOT = 21265
430349 feet/sec YDOT = 6473
792750 meter/sec
ZDOT = 13232
952247 ZDOT = 4029
968460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12853236
34 X = 3917666
44
Y = -12740043
27 feet Y = -3883165
19 meter
Z = -12956279
52 Z = -3949074
00
XDOT = 19286
123896 XDOT = 5878
410564
YDOT = 6041
224161 feet/sec YDOT = 1841
365124 meter/sec
ZDOT = 13216
877006 ZDOT = 4028
504112
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
47936931
00016717 00000-0 10270-3 0 9082
2 25544 51
6447 67
5901 0002845 50
6426 309
4979 15
55207043 28552
Satellite: ISS
Catalog Number: 25544
Epoch time: 15171
47936931 = yrday
fracday
Element set: 908
Inclination: 51
6447 deg
RA of node: 67
5901 deg
Eccentricity:
0002845
Arg of perigee: 50
6426 deg
Mean anomaly: 309
4979 deg
Mean motion: 15
55207043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 328
Coasting Arc #10 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2015/172/11:17:57
487
Vector Time (MET): N/A
Weight (LBS) : 877531
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4463568
42 A = 6784007
39 meter
Y = -4556011
81 meter E =
0015711
Z = 2293209
47 I = 51
98117
XDOT = 2207
099633 Wp = 99
66202
YDOT = -4922
719792 meter/sec RA = 61
91280 deg
ZDOT = -5455
080910 TA = 54
90422
MA = 54
75702
Ha = 220
240 n
mi
Hp = 212
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14644253
34 X = -4423429
73
Y = -14947545
30 feet Y = -4605702
14 meter
Z = 7523653
11 Z = 2271623
53
XDOT = 7241
140529 XDOT = 2288
481167
YDOT = -16150
655485 feet/sec YDOT = -4897
583004 meter/sec
ZDOT = -17897
247081 ZDOT = -5444
162134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17676774
04 X = -5387880
73
Y = 11260102
80 feet Y = 3432079
33 meter
Z = 7431713
59 Z = 2265186
30
XDOT = -13447
273997 XDOT = -4098
729114
YDOT = -9265
879448 feet/sec YDOT = -2824
240056 meter/sec
ZDOT = -17849
287060 ZDOT = -5440
462696
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
50748316
00016717 00000-0 10270-3 0 9096
2 25544 51
6444 62
4563 0002795 55
3925 304
7492 15
55211613 28711
Satellite: ISS
Catalog Number: 25544
Epoch time: 15172
50748316 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 62
4563 deg
Eccentricity:
0002795
Arg of perigee: 55
3925 deg
Mean anomaly: 304
7492 deg
Mean motion: 15
55211613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 311
Coasting Arc #11 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2015/173/11:17:57
487
Vector Time (MET): N/A
Weight (LBS) : 877531
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3881658
30 A = 6786004
76 meter
Y = 5550746
10 meter E =
0014273
Z = -290617
23 I = 51
97318
XDOT = -3732
675694 Wp = 45
27326
YDOT = 2916
220306 meter/sec RA = 56
95764 deg
ZDOT = 6034
318507 TA = 311
60725
MA = 311
72946
Ha = 220
129 n
mi
Hp = 212
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12735099
41 X = 3820711
73
Y = 18211109
26 feet Y = 5593812
60 meter
Z = -953468
61 Z = -271908
56
XDOT = -12246
311331 XDOT = -3794
320427
YDOT = 9567
651924 feet/sec YDOT = 2874
133895 meter/sec
ZDOT = 19797
632898 ZDOT = 6016
036520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20311347
34 X = 6190898
67
Y = -9023383
76 feet Y = -2750327
37 meter
Z = -874113
37 Z = -266429
76
XDOT = 6369
064715 XDOT = 1941
290925
YDOT = 12492
545012 feet/sec YDOT = 3807
727720 meter/sec
ZDOT = 19718
399840 ZDOT = 6010
168271
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
47131979
00016717 00000-0 10270-3 0 9106
2 25544 51
6449 57
6430 0002745 54
9441 305
1969 15
55262235 28864
Satellite: ISS
Catalog Number: 25544
Epoch time: 15173
47131979 = yrday
fracday
Element set: 910
Inclination: 51
6449 deg
RA of node: 57
6430 deg
Eccentricity:
0002745
Arg of perigee: 54
9441 deg
Mean anomaly: 305
1969 deg
Mean motion: 15
55262235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 324
Coasting Arc #12 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2015/174/11:17:57
487
Vector Time (MET): N/A
Weight (LBS) : 877531
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2814050
17 A = 6784617
61 meter
Y = -5901306
99 meter E =
0008045
Z = -1808355
37 I = 51
95089
XDOT = 5098
859103 Wp = 122
68363
YDOT = -697
093385 meter/sec RA = 52
00328 deg
ZDOT = -5682
210087 TA = 77
10363
MA = 77
01379
Ha = 220
057 n
mi
Hp = 212
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9232448
07 X = -2739066
92
Y = -19361243
40 feet Y = -5932356
14 meter
Z = -5932924
43 Z = -1821843
76
XDOT = 16728
540363 XDOT = 5133
877150
YDOT = -2287
051787 feet/sec YDOT = -639
878360 meter/sec
ZDOT = -18642
421545 ZDOT = -5657
355911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20668103
16 X = -6299637
84
Y = 5678724
05 feet Y = 1730875
09 meter
Z = -5989744
62 Z = -1825674
16
XDOT = 1096
973629 XDOT = 334
357562
YDOT = -15480
747119 feet/sec YDOT = -4718
531722 meter/sec
ZDOT = -18535
367795 ZDOT = -5649
580104
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
49939365
00016717 00000-0 10270-3 0 9115
2 25544 51
6453 52
5089 0002559 59
3290 300
8115 15
55261639 29028
Satellite: ISS
Catalog Number: 25544
Epoch time: 15174
49939365 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 52
5089 deg
Eccentricity:
0002559
Arg of perigee: 59
3290 deg
Mean anomaly: 300
8115 deg
Mean motion: 15
55261639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 317
Coasting Arc #13 (Orbit 2917)
---------------------------------------
Vector Time (GMT): 2015/175/11:17:57
487
Vector Time (MET): N/A
Weight (LBS) : 877531
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1349529
65 A = 6780398
57 meter
Y = 5580850
54 meter E =
0014362
Z = 3593428
55 I = 51
91700
XDOT = -6086
296274 Wp = 87
04820
YDOT = -1408
567030 meter/sec RA = 47
03735 deg
ZDOT = 4458
750798 TA = 315
32812
MA = 315
44374
Ha = 220
068 n
mi
Hp = 211
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4427590
72 X = 1269567
44
Y = 18309877
11 feet Y = 5595494
50 meter
Z = 11789463
74 Z = 3599790
50
XDOT = -19968
163627 XDOT = -6091
751904
YDOT = -4621
282907 feet/sec YDOT = -1476
658826 meter/sec
ZDOT = 14628
447501 ZDOT = 4429
171428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18767743
35 X = 5720408
17
Y = -1417032
17 feet Y = -431911
40 meter
Z = 11815686
35 Z = 3601421
20
XDOT = -7822
265044 XDOT = -2384
226385
YDOT = 17715
453666 feet/sec YDOT = 5399
670277 meter/sec
ZDOT = 14501
502389 ZDOT = 4420
057928
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
52744738
00016717 00000-0 10270-3 0 9129
2 25544 51
6453 47
3745 0002758 59
8331 300
3096 15
55305141 29188
Satellite: ISS
Catalog Number: 25544
Epoch time: 15175
52744738 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 47
3745 deg
Eccentricity:
0002758
Arg of perigee: 59
8331 deg
Mean anomaly: 300
3096 deg
Mean motion: 15
55305141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2918
Checksum: 311
Coasting Arc #14 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2015/176/11:17:57
487
Vector Time (MET): N/A
Weight (LBS) : 877531
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 453259
59 A = 6775783
89 meter
Y = -4720186
18 meter E =
0014243
Z = -4853466
28 I = 51
87973
XDOT = 6489
166062 Wp = 69
76932
YDOT = 3202
188615 meter/sec RA = 42
05469 deg
ZDOT = -2509
403201 TA = 175
62524
MA = 175
61278
Ha = 219
916 n
mi
Hp = 211
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1487072
14 X = 529584
50
Y = -15486175
12 feet Y = -4714690
39 meter
Z = -15923445
79 Z = -4851079
42
XDOT = 21289
914900 XDOT = 6465
065886
YDOT = 10505
868161 feet/sec YDOT = 3274
620167 meter/sec
ZDOT = -8232
950133 ZDOT = -2477
938332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15111482
35 X = -4605979
82
Y = -3746187
97 feet Y = -1141838
09 meter
Z = -15912206
20 Z = -4850040
45
XDOT = 13123
064674 XDOT = 3999
910113
YDOT = -18554
450214 feet/sec YDOT = -5655
396425 meter/sec
ZDOT = -8098
271262 ZDOT = -2468
353081
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
49122799
00016717 00000-0 10270-3 0 9134
2 25544 51
6453 42
5611 0002572 60
0350 300
1059 15
55362167 29331
Satellite: ISS
Catalog Number: 25544
Epoch time: 15176
49122799 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 42
5611 deg
Eccentricity:
0002572
Arg of perigee: 60
0350 deg
Mean anomaly: 300
1059 deg
Mean motion: 15
55362167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2933
Checksum: 289
Coasting Arc #15 (Orbit 2948)
---------------------------------------
Vector Time (GMT): 2015/177/11:17:57
487
Vector Time (MET): N/A
Weight (LBS) : 877531
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2366392
58 A = 6773682
70 meter
Y = 3451833
24 meter E =
0004786
Z = 5322068
69 I = 51
84898
XDOT = -6203
214795 Wp = 79
59923
YDOT = -4515
742660 meter/sec RA = 37
05883 deg
ZDOT = 171
388698 TA = 8
77766
MA = 8
76929
Ha = 219
988 n
mi
Hp = 211
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7763755
18 X = -2430668
63
Y = 11324912
21 feet Y = 3425010
83 meter
Z = 17460855
28 Z = 5310417
36
XDOT = -20351
754576 XDOT = -6153
090186
YDOT = -14815
428673 feet/sec YDOT = -4584
830821 meter/sec
ZDOT = 562
298877 ZDOT = 141
375934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10269285
39 X = 3130078
19
Y = 9211069
70 feet Y = 2807534
05 meter
Z = 17410025
00 Z = 5306575
62
XDOT = -16540
178121 XDOT = -5041
446291
YDOT = 17624
241296 feet/sec YDOT = 5371
868747 meter/sec
ZDOT = 434
147841 ZDOT = 132
328262
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 15177
51924290
00016717 00000-0 10270-3 0 9145
2 25544 51
6456 37
4270 0002551 64
6200 295
5217 15
55387842 29496
Satellite: ISS
Catalog Number: 25544
Epoch time: 15177
51924290 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 37
4270 deg
Eccentricity:
0002551
Arg of perigee: 64
6200 deg
Mean anomaly: 295
5217 deg
Mean motion: 15
55387842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2949
Checksum: 315
Coasting Arc #16 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2015/178/11:17:57
487
Vector Time (MET): N/A
Weight (LBS) : 877531
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4172618
94 A = 6775247
00 meter
Y = -1992254
77 meter E =
0014241
Z = -4965087
54 I = 51
82775
XDOT = 5123
257258 Wp = 99
39223
YDOT = 5251
011632 meter/sec RA = 32
05930 deg
ZDOT = 2201
673693 TA = 192
03713
MA = 192
07120
Ha = 219
823 n
mi
Hp = 211
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13689694
67 X = 4218705
32
Y = -6536268
93 feet Y = -1945335
62 meter
Z = -16289657
29 Z = -4944705
94
XDOT = 16808
586803 XDOT = 5053
463464
YDOT = 17227
728453 feet/sec YDOT = 5307
912784 meter/sec
ZDOT = 7223
338888 ZDOT = 2226
392606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5036011
61 X = -1534976
34
Y = -14409402
43 feet Y = -4391985
86 meter
Z = -16201580
02 Z = -4938241
59
XDOT = 17860
370547 XDOT = 5443
840943
YDOT = -14470
612065 feet/sec YDOT = -4410
642557 meter/sec
ZDOT = 7328
556787 ZDOT = 2233
744109
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 15178
48298860
00016717 00000-0 10270-3 0 9150
2 25544 51
6448 32
6127 0002460 65
2045 294
9364 15
55420184 29648
Satellite: ISS
Catalog Number: 25544
Epoch time: 15178
48298860 = yrday
fracday
Element set: 915
Inclination: 51
6448 deg
RA of node: 32
6127 deg
Eccentricity:
0002460
Arg of perigee: 65
2045 deg
Mean anomaly: 294
9364 deg
Mean motion: 15
55420184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 322
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