[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 14th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 730 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 3213)
---------------------------------------
Vector Time (GMT): 2015/194/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1641979
70 A = 6782290
48 meter
Y = -5727910
43 meter E =
0002774
Z = -3242260
45 I = 51
38094
XDOT = 5945
299409 Wp = 96
65046
YDOT = -975
856868 meter/sec RA = 311
75992 deg
ZDOT = 4738
050999 TA = 225
63459
MA = 225
65731
Ha = 218
991 n
mi
Hp = 213
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5387072
49 X = 1721658
07
Y = -18792357
06 feet Y = -5709102
84 meter
Z = -10637337
42 Z = -3234091
27
XDOT = 19505
575489 XDOT = 5932
754353
YDOT = -3201
630143 feet/sec YDOT = -909
443355 meter/sec
ZDOT = 15544
786742 ZDOT = 4766
901250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18619721
52 X = -5675291
12
Y = 6020804
59 feet Y = 1835141
24 meter
Z = -10601040
70 Z = -3231197
21
XDOT = -13091
771123 XDOT = -3990
371838
YDOT = -12916
577520 feet/sec YDOT = -3936
972828 meter/sec
ZDOT = 15669
023795 ZDOT = 4775
918453
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 15194
54516723
00016717 00000-0 10270-3 0 9000
2 25544 51
6449 312
3947 0002062 240
0645 120
0304 15
55025810 32143
Satellite: ISS
Catalog Number: 25544
Epoch time: 15194
54516723 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 312
3947 deg
Eccentricity:
0002062
Arg of perigee: 240
0645 deg
Mean anomaly: 120
0304 deg
Mean motion: 15
55025810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3214
Checksum: 267
Coasting Arc #2 (Orbit 3229)
---------------------------------------
Vector Time (GMT): 2015/195/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2994628
79 A = 6785770
59 meter
Y = 5912061
00 meter E =
0012962
Z = 1425478
74 I = 51
37226
XDOT = -4933
973968 Wp = 126
65885
YDOT = -1100
738948 meter/sec RA = 306
76054 deg
ZDOT = -5771
098409 TA = 37
72596
MA = 37
63515
Ha = 218
942 n
mi
Hp = 213
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9824897
60 X = -3067440
66
Y = 19396525
59 feet Y = 5878165
81 meter
Z = 4676767
52 Z = 1410755
46
XDOT = -16187
578634 XDOT = -4893
265076
YDOT = -3611
348255 feet/sec YDOT = -1155
685570 meter/sec
ZDOT = -18934
049899 ZDOT = -5794
967640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21536550
96 X = 6564340
73
Y = -3087066
93 feet Y = -940938
00 meter
Z = 4612262
20 Z = 1405817
52
XDOT = 6054
486967 XDOT = 1845
407628
YDOT = 13653
130015 feet/sec YDOT = 4161
474029 meter/sec
ZDOT = -19036
449626 ZDOT = -5802
309846
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 15195
57338149
00016717 00000-0 10270-3 0 9019
2 25544 51
6447 307
2621 0001981 239
8479 120
2478 15
55065539 32307
Satellite: ISS
Catalog Number: 25544
Epoch time: 15195
57338149 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 307
2621 deg
Eccentricity:
0001981
Arg of perigee: 239
8479 deg
Mean anomaly: 120
2478 deg
Mean motion: 15
55065539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3230
Checksum: 320
Coasting Arc #3 (Orbit 3245)
---------------------------------------
Vector Time (GMT): 2015/196/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3944374
06 A = 6786342
51 meter
Y = -5484377
77 meter E =
0011362
Z = 583124
61 I = 51
35695
XDOT = 3599
622005 Wp = 48
21413
YDOT = 3229
106380 meter/sec RA = 301
76642 deg
ZDOT = 5954
058250 TA = 318
10734
MA = 318
19422
Ha = 218
837 n
mi
Hp = 213
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12940859
78 X = 4002575
98
Y = -17993365
38 feet Y = -5439943
83 meter
Z = 1913138
50 Z = 602426
06
XDOT = 11809
783480 XDOT = 3534
323722
YDOT = 10594
181038 feet/sec YDOT = 3268
993945 meter/sec
ZDOT = 19534
311843 ZDOT = 5971
385991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22155741
97 X = -6753070
15
Y = 145981
01 feet Y = 44495
01 meter
Z = 1997232
06 Z = 608756
33
XDOT = 1694
040674 XDOT = 516
343597
YDOT = -14068
229123 feet/sec YDOT = -4287
996237 meter/sec
ZDOT = 19608
161144 ZDOT = 5976
567517
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 15196
60157275
00016717 00000-0 10270-3 0 9024
2 25544 51
6453 302
1290 0001870 250
6774 109
4177 15
55103107 32462
Satellite: ISS
Catalog Number: 25544
Epoch time: 15196
60157275 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 302
1290 deg
Eccentricity:
0001870
Arg of perigee: 250
6774 deg
Mean anomaly: 109
4177 deg
Mean motion: 15
55103107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3246
Checksum: 290
Coasting Arc #4 (Orbit 3260)
---------------------------------------
Vector Time (GMT): 2015/197/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4495519
21 A = 6783591
45 meter
Y = 4396506
54 meter E =
0004334
Z = -2541203
23 I = 51
33130
XDOT = -2097
160817 Wp = 149
48071
YDOT = -5176
248657 meter/sec RA = 296
76862 deg
ZDOT = -5252
999103 TA = 59
19826
MA = 59
15560
Ha = 218
714 n
mi
Hp = 213
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14749078
77 X = -4532003
90
Y = 14424234
05 feet Y = 4346030
95 meter
Z = -8337280
95 Z = -2563129
37
XDOT = -6880
448874 XDOT = -2013
606272
YDOT = -16982
443099 feet/sec YDOT = -5199
232788 meter/sec
ZDOT = -17234
249026 ZDOT = -5262
984080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20366387
43 X = 6207674
89
Y = 3034542
68 feet Y = 924928
61 meter
Z = -8432432
62 Z = -2570205
46
XDOT = -9251
550912 XDOT = -2819
872718
YDOT = 14153
384691 feet/sec YDOT = 4313
951654 meter/sec
ZDOT = -17276
146912 ZDOT = -5265
769579
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 15197
56548200
00016717 00000-0 10270-3 0 9033
2 25544 51
6444 297
3174 0001919 253
9834 106
1108 15
55137338 32613
Satellite: ISS
Catalog Number: 25544
Epoch time: 15197
56548200 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 297
3174 deg
Eccentricity:
0001919
Arg of perigee: 253
9834 deg
Mean anomaly: 106
1108 deg
Mean motion: 15
55137338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3261
Checksum: 310
Coasting Arc #5 (Orbit 3276)
---------------------------------------
Vector Time (GMT): 2015/198/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4637201
25 A = 6778973
58 meter
Y = -2751546
85 meter E =
0008693
Z = 4103322
27 I = 51
30312
XDOT = 599
877104 Wp = 108
71581
YDOT = 6652
375043 meter/sec RA = 291
75612 deg
ZDOT = 3773
610297 TA = 302
17318
MA = 302
25747
Ha = 218
526 n
mi
Hp = 213
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15213914
87 X = 4647693
06
Y = -9027384
69 feet Y = -2699632
30 meter
Z = 13462343
40 Z = 4125873
71
XDOT = 1968
100736 XDOT = 507
113642
YDOT = 21825
377437 feet/sec YDOT = 6658
564285 meter/sec
ZDOT = 12380
611209 ZDOT = 3776
299555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16431473
52 X = -5008313
13
Y = -6350488
37 feet Y = -1935628
85 meter
Z = 13559850
49 Z = 4133042
43
XDOT = 15561
213173 XDOT = 4743
057775
YDOT = -13741
292184 feet/sec YDOT = -4188
345858 meter/sec
ZDOT = 12390
861133 ZDOT = 3776
734473
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 15198
59362995
00016717 00000-0 10270-3 0 9043
2 25544 51
6446 292
1839 0001921 261
0829 99
0107 15
55195001 32770
Satellite: ISS
Catalog Number: 25544
Epoch time: 15198
59362995 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 292
1839 deg
Eccentricity:
0001921
Arg of perigee: 261
0829 deg
Mean anomaly: 99
0107 deg
Mean motion: 15
55195001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3277
Checksum: 327
Coasting Arc #6 (Orbit 3291)
---------------------------------------
Vector Time (GMT): 2015/199/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4451695
59 A = 6775228
03 meter
Y = 683642
43 meter E =
0011504
Z = -5071920
34 I = 51
27844
XDOT = 803
314450 Wp = 75
20122
YDOT = -7425
630933 meter/sec RA = 286
72883 deg
ZDOT = -1706
346401 TA = 178
21406
MA = 178
20995
Ha = 218
625 n
mi
Hp = 213
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14605300
48 X = -4434372
38
Y = 2242921
35 feet Y = 633957
83 meter
Z = -16640158
59 Z = -5093503
27
XDOT = 2635
546097 XDOT = 894
578566
YDOT = -24362
306210 feet/sec YDOT = -7416
137349 meter/sec
ZDOT = -5598
249347 ZDOT = -1702
222933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10871911
13 X = 3313758
51
Y = 9851168
95 feet Y = 3002636
30 meter
Z = -16733092
81 Z = -5100246
69
XDOT = -19888
668540 XDOT = -6062
066171
YDOT = 12474
945157 feet/sec YDOT = 3802
363284 meter/sec
ZDOT = -5579
071550 ZDOT = -1700
501008
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 15199
55750109
00016717 00000-0 10270-3 0 9059
2 25544 51
6435 287
3720 0001922 268
3792 91
7141 15
55188147 32920
Satellite: ISS
Catalog Number: 25544
Epoch time: 15199
55750109 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 287
3720 deg
Eccentricity:
0001922
Arg of perigee: 268
3792 deg
Mean anomaly: 91
7141 deg
Mean motion: 15
55188147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3292
Checksum: 323
Coasting Arc #7 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2015/200/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3984889
92 A = 6774165
59 meter
Y = 1544644
56 meter E =
0001594
Z = 5255371
15 I = 51
26762
XDOT = -2034
644644 Wp = 26
44896
YDOT = 7370
290414 meter/sec RA = 281
69151 deg
ZDOT = -622
008390 TA = 69
52585
MA = 69
50874
Ha = 218
352 n
mi
Hp = 213
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13073785
83 X = 3941793
01
Y = 5067731
49 feet Y = 1588964
99 meter
Z = 17242031
33 Z = 5274624
02
XDOT = -6675
343319 XDOT = -2113
888356
YDOT = 24180
742829 feet/sec YDOT = 7347
094636 meter/sec
ZDOT = -2040
709940 ZDOT = -632
084240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4453643
19 X = -1357470
44
Y = -13187858
17 feet Y = -4019659
17 meter
Z = 17324516
79 Z = 5280512
72
XDOT = 21840
829494 XDOT = 6657
084830
YDOT = -10121
754041 feet/sec YDOT = -3085
110632 meter/sec
ZDOT = -2085
453661 ZDOT = -635
646276
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 15200
58560739
00016717 00000-0 10270-3 0 9064
2 25544 51
6437 282
2381 0001962 275
0698 85
0231 15
55267333 33082
Satellite: ISS
Catalog Number: 25544
Epoch time: 15200
58560739 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 282
2381 deg
Eccentricity:
0001962
Arg of perigee: 275
0698 deg
Mean anomaly: 85
0231 deg
Mean motion: 15
55267333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 310
Coasting Arc #8 (Orbit 3322)
---------------------------------------
Vector Time (GMT): 2015/201/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3324183
10 A = 6776751
72 meter
Y = -3657150
85 meter E =
0008834
Z = -4645404
62 I = 51
26964
XDOT = 3060
024158 Wp = 110
50044
YDOT = -6415
529537 meter/sec RA = 276
65677 deg
ZDOT = 2862
389207 TA = 188
10282
MA = 188
11710
Ha = 218
564 n
mi
Hp = 213
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10906112
54 X = -3260475
63
Y = -11998526
40 feet Y = -3693967
66 meter
Z = -15240828
80 Z = -4661398
00
XDOT = 10039
449337 XDOT = 3117
632532
YDOT = -21048
325254 feet/sec YDOT = -6380
988338 meter/sec
ZDOT = 9391
040705 ZDOT = 2877
393663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1964312
84 X = -598722
55
Y = 16030278
03 feet Y = 4886028
74 meter
Z = -15308901
01 Z = -4666153
03
XDOT = -21262
461671 XDOT = -6480
798317
YDOT = 6421
413168 feet/sec YDOT = 1957
246734 meter/sec
ZDOT = 9456
778553 ZDOT = 2882
426103
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 15201
54944056
00016717 00000-0 10270-3 0 9070
2 25544 51
6425 277
4253 0001751 284
6996 75
3963 15
55280204 33239
Satellite: ISS
Catalog Number: 25544
Epoch time: 15201
54944056 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 277
4253 deg
Eccentricity:
0001751
Arg of perigee: 284
6996 deg
Mean anomaly: 75
3963 deg
Mean motion: 15
55280204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3323
Checksum: 313
Coasting Arc #9 (Orbit 3338)
---------------------------------------
Vector Time (GMT): 2015/202/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2486528
09 A = 6781193
05 meter
Y = 5376477
63 meter E =
0010859
Z = 3291721
53 I = 51
28257
XDOT = -3887
481671 Wp = 88
25701
YDOT = 4672
338230 meter/sec RA = 271
63384 deg
ZDOT = -4681
195045 TA = 53
24070
MA = 53
14106
Ha = 218
444 n
mi
Hp = 213
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8157900
56 X = 2410232
48
Y = 17639362
30 feet Y = 5403856
92 meter
Z = 10799611
32 Z = 3303615
29
XDOT = -12754
204957 XDOT = -3916
700763
YDOT = 15329
193667 feet/sec YDOT = 4628
702629 meter/sec
ZDOT = -15358
251459 ZDOT = -4700
150256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7700203
27 X = 2347021
96
Y = -17813479
52 feet Y = -5429548
56 meter
Z = 10849740
33 Z = 3307000
85
XDOT = 18560
497786 XDOT = 5657
239725
YDOT = -1408
697592 feet/sec YDOT = -429
371026 meter/sec
ZDOT = -15440
636129 ZDOT = -4706
305892
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 15202
57750714
00016717 00000-0 10270-3 0 9081
2 25544 51
6429 272
2909 0001911 292
1643 67
9307 15
55330479 33391
Satellite: ISS
Catalog Number: 25544
Epoch time: 15202
57750714 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 272
2909 deg
Eccentricity:
0001911
Arg of perigee: 292
1643 deg
Mean anomaly: 67
9307 deg
Mean motion: 15
55330479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3339
Checksum: 316
Coasting Arc #10 (Orbit 3353)
---------------------------------------
Vector Time (GMT): 2015/203/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1533967
31 A = 6785016
41 meter
Y = -6446586
78 meter E =
0008390
Z = -1437482
00 I = 51
29450
XDOT = 4485
856706 Wp = 24
95489
YDOT = -2347
583162 meter/sec RA = 266
62567 deg
ZDOT = 5760
896368 TA = 319
28199
MA = 319
34468
Ha = 218
571 n
mi
Hp = 213
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5032701
14 X = -1454783
34
Y = -21150219
09 feet Y = -6463297
82 meter
Z = -4716148
29 Z = -1444741
49
XDOT = 14717
377643 XDOT = 4483
790561
YDOT = -7702
044494 feet/sec YDOT = -2297
431088 meter/sec
ZDOT = 18900
578635 ZDOT = 5782
682479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12064871
89 X = -3677372
95
Y = 18078017
53 feet Y = 5510179
74 meter
Z = -4746161
75 Z = -1446630
10
XDOT = -14265
844595 XDOT = -4348
229433
YDOT = -4550
822991 feet/sec YDOT = -1387
090848 meter/sec
ZDOT = 18994
695247 ZDOT = 5789
583111
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 15203
54130291
00016717 00000-0 10270-3 0 9092
2 25544 51
6422 267
4774 0001857 299
3817 60
7150 15
55306086 33542
Satellite: ISS
Catalog Number: 25544
Epoch time: 15203
54130291 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 267
4774 deg
Eccentricity:
0001857
Arg of perigee: 299
3817 deg
Mean anomaly: 60
7150 deg
Mean motion: 15
55306086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3354
Checksum: 308
Coasting Arc #11 (Orbit 3369)
---------------------------------------
Vector Time (GMT): 2015/204/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 440100
73 A = 6785523
02 meter
Y = 6732651
04 meter E =
0008908
Z = -680463
06 I = 51
30028
XDOT = -4847
887278 Wp = 142
37938
YDOT = -278
197596 meter/sec RA = 261
62555 deg
ZDOT = -5936
116824 TA = 45
00792
MA = 44
93576
Ha = 218
574 n
mi
Hp = 213
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1443900
05 X = 368087
31
Y = 22088750
13 feet Y = 6737169
91 meter
Z = -2232490
35 Z = -678499
85
XDOT = -15905
141987 XDOT = -4815
580896
YDOT = -912
721773 feet/sec YDOT = -332
229026 meter/sec
ZDOT = -19475
448897 ZDOT = -5959
588276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14887643
03 X = 4537753
60
Y = -16382548
70 feet Y = -4993400
84 meter
Z = -2225292
34 Z = -678269
11
XDOT = 9101
396798 XDOT = 2774
105744
YDOT = 10908
495702 feet/sec YDOT = 3324
909490 meter/sec
ZDOT = -19576
326176 ZDOT = -5966
864218
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 15204
56933117
00016717 00000-0 10270-3 0 9105
2 25544 51
6429 262
3426 0001753 306
2703 53
8288 15
55370811 33704
Satellite: ISS
Catalog Number: 25544
Epoch time: 15204
56933117 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 262
3426 deg
Eccentricity:
0001753
Arg of perigee: 306
2703 deg
Mean anomaly: 53
8288 deg
Mean motion: 15
55370811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3370
Checksum: 293
Coasting Arc #12 (Orbit 3385)
---------------------------------------
Vector Time (GMT): 2015/205/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 728979
88 A = 6782699
61 meter
Y = -6184756
93 meter E =
0012737
Z = 2671002
22 I = 51
29540
XDOT = 4924
824303 Wp = 71
59064
YDOT = 2818
367908 meter/sec RA = 256
62165 deg
ZDOT = 5165
549825 TA = 318
74769
MA = 318
84386
Ha = 218
659 n
mi
Hp = 213
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2391666
26 X = 785110
49
Y = -20291197
26 feet Y = -6176291
26 meter
Z = 8763130
66 Z = 2674679
53
XDOT = 16157
560049 XDOT = 4867
850461
YDOT = 9246
613871 feet/sec YDOT = 2873
121755 meter/sec
ZDOT = 16947
341944 ZDOT = 5189
335250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16011084
37 X = -4880178
52
Y = 12680718
93 feet Y = 3865083
13 meter
Z = 8780077
30 Z = 2676167
56
XDOT = -3867
476975 XDOT = -1178
806982
YDOT = -16724
966187 feet/sec YDOT = -5097
769694 meter/sec
ZDOT = 17049
108674 ZDOT = 5196
568324
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 15205
59734062
00016717 00000-0 10270-3 0 9118
2 25544 51
6420 257
2079 0001706 316
4965 43
6053 15
55364326 33861
Satellite: ISS
Catalog Number: 25544
Epoch time: 15205
59734062 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 257
2079 deg
Eccentricity:
0001706
Arg of perigee: 316
4965 deg
Mean anomaly: 43
6053 deg
Mean motion: 15
55364326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3386
Checksum: 303
Coasting Arc #13 (Orbit 3400)
---------------------------------------
Vector Time (GMT): 2015/206/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1973298
18 A = 6777820
22 meter
Y = 4893204
04 meter E =
0007820
Z = -4262998
02 I = 51
28909
XDOT = -4643
043098 Wp = 58
13343
YDOT = -4959
616029 meter/sec RA = 251
60445 deg
ZDOT = -3544
332974 TA = 175
51674
MA = 175
50973
Ha = 218
603 n
mi
Hp = 212
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6474075
39 X = -2007160
57
Y = 16053819
04 feet Y = 4870948
22 meter
Z = -13986213
98 Z = -4272665
85
XDOT = -15233
081031 XDOT = -4570
021455
YDOT = -16271
706131 feet/sec YDOT = -5011
129105 meter/sec
ZDOT = -11628
389022 ZDOT = -3566
710752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15752350
13 X = 4801316
32
Y = -7093132
81 feet Y = -2161986
88 meter
Z = -14028680
33 Z = -4275941
76
XDOT = -943
615524 XDOT = -287
614012
YDOT = 21086
588321 feet/sec YDOT = 6427
192120 meter/sec
ZDOT = -11723
722843 ZDOT = -3573
390722
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 15206
56107952
00016717 00000-0 10270-3 0 9129
2 25544 51
6432 252
3942 0001725 317
0814 43
0205 15
55421352 34014
Satellite: ISS
Catalog Number: 25544
Epoch time: 15206
56107952 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 252
3942 deg
Eccentricity:
0001725
Arg of perigee: 317
0814 deg
Mean anomaly: 43
0205 deg
Mean motion: 15
55421352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3401
Checksum: 267
Coasting Arc #14 (Orbit 3416)
---------------------------------------
Vector Time (GMT): 2015/207/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3176705
46 A = 6774127
88 meter
Y = -3046146
70 meter E =
0002846
Z = 5147558
86 I = 51
28660
XDOT = 3966
867514 Wp = 113
49906
YDOT = 6426
599220 meter/sec RA = 246
57228 deg
ZDOT = 1353
259665 TA = 323
42714
MA = 323
44657
Ha = 218
513 n
mi
Hp = 212
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10422262
00 X = 3185527
36
Y = -9993919
62 feet Y = -3010573
72 meter
Z = 16888316
48 Z = 5163011
80
XDOT = 13014
657198 XDOT = 3888
135325
YDOT = 21084
643111 feet/sec YDOT = 6470
519025 meter/sec
ZDOT = 4439
828298 ZDOT = 1372
339016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14358628
54 X = -4376509
98
Y = 252758
65 feet Y = 77040
84 meter
Z = 16955326
82 Z = 5167983
61
XDOT = 4936
084307 XDOT = 1504
518497
YDOT = -23223
001367 feet/sec YDOT = -7078
370817 meter/sec
ZDOT = 4520
725583 ZDOT = 1377
917158
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 15207
58904931
00016717 00000-0 10270-3 0 9135
2 25544 51
6418 247
2593 0001731 324
5082 35
5956 15
55450479 34178
Satellite: ISS
Catalog Number: 25544
Epoch time: 15207
58904931 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 247
2593 deg
Eccentricity:
0001731
Arg of perigee: 324
5082 deg
Mean anomaly: 35
5956 deg
Mean motion: 15
55450479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3417
Checksum: 317
Coasting Arc #15 (Orbit 3431)
---------------------------------------
Vector Time (GMT): 2015/208/12:55:24
826
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4247030
53 A = 6773854
23 meter
Y = 920177
47 meter E =
0013126
Z = -5207731
07 I = 51
30015
XDOT = -2837
011447 Wp = 92
30658
YDOT = -7035
091500 meter/sec RA = 241
53404 deg
ZDOT = 1072
418093 TA = 188
01581
MA = 188
03680
Ha = 218
612 n
mi
Hp = 212
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13933827
19 X = -4231707
55
Y = 3018954
95 feet Y = 872770
48 meter
Z = -17085731
85 Z = -5228324
84
XDOT = -9307
780339 XDOT = -2763
341866
YDOT = -23081
008858 feet/sec YDOT = -7066
404997 meter/sec
ZDOT = 3518
432065 ZDOT = 1058
814941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12280807
47 X = 3743190
12
Y = 7029012
89 feet Y = 2142443
13 meter
Z = -17174475
47 Z = -5234780
12
XDOT = -8037
573114 XDOT = -2449
852285
YDOT = 22485
284017 feet/sec YDOT = 6853
514568 meter/sec
ZDOT = 3461
181304 ZDOT = 1054
968061
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 15208
55275325
00016717 00000-0 10270-3 0 9142
2 25544 51
6427 242
4457 0001864 325
7054 34
3979 15
55458081 34329
Satellite: ISS
Catalog Number: 25544
Epoch time: 15208
55275325 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 242
4457 deg
Eccentricity:
0001864
Arg of perigee: 325
7054 deg
Mean anomaly: 34
3979 deg
Mean motion: 15
55458081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3432
Checksum: 315
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