[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 16th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 819 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
233/11:54:08
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 212
4
Coasting Arc #1 (Orbit 3711)
---------------------------------------
Vector Time (GMT): 2015/226/12:30:39
716
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6163908
97 A = 6783287
17 meter
Y = -927558
28 meter E =
0005459
Z = -2676980
57 I = 51
82200
XDOT = -1442
075717 Wp = 111
65585
YDOT = 5431
309389 meter/sec RA = 151
70615 deg
ZDOT = -5212
872471 TA = 98
47594
MA = 98
41406
Ha = 219
773 n
mi
Hp = 212
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20222798
47 X = 6186826
53
Y = -3043170
19 feet Y = -858501
33 meter
Z = -8782744
65 Z = -2646982
46
XDOT = -4731
219544 XDOT = -1477
381121
YDOT = 17819
256524 feet/sec YDOT = 5414
985608 meter/sec
ZDOT = -17102
599971 ZDOT = -5219
963538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19009201
61 X = -5794004
65
Y = -7689590
94 feet Y = -2343787
32 meter
Z = -8653294
86 Z = -2637524
27
XDOT = 12478
775936 XDOT = 3803
530905
YDOT = -11606
309971 feet/sec YDOT = -3537
603279 meter/sec
ZDOT = -17134
055037 ZDOT = -5222
459975
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 15226
54815471
00016717 00000-0 10270-3 0 9008
2 25544 51
6439 152
6468 0001442 46
9757 313
1517 15
55190839 37121
Satellite: ISS
Catalog Number: 25544
Epoch time: 15226
54815471 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 152
6468 deg
Eccentricity:
0001442
Arg of perigee: 46
9757 deg
Mean anomaly: 313
1517 deg
Mean motion: 15
55190839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3712
Checksum: 313
Coasting Arc #2 (Orbit 3727)
---------------------------------------
Vector Time (GMT): 2015/227/12:30:39
716
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5275531
09 A = 6778760
65 meter
Y = -504044
90 meter E =
0011144
Z = 4218596
32 I = 51
83432
XDOT = 3499
462234 Wp = 99
48429
YDOT = -5754
315722 meter/sec RA = 146
72846 deg
ZDOT = 3678
637875 TA = 312
90124
MA = 312
99473
Ha = 219
872 n
mi
Hp = 212
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17308172
85 X = -5289994
59
Y = -1653690
62 feet Y = -563120
05 meter
Z = 13840539
09 Z = 4192934
22
XDOT = 11481
175310 XDOT = 3545
679212
YDOT = -18878
988590 feet/sec YDOT = -5714
923864 meter/sec
ZDOT = 12069
021901 ZDOT = 3695
749739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14313900
99 X = 4362877
02
Y = 10023338
71 feet Y = 3055113
64 meter
Z = 13730002
99 Z = 4184904
91
XDOT = -18504
736713 XDOT = -5640
243750
YDOT = 9745
768672 feet/sec YDOT = 2970
510291 meter/sec
ZDOT = 12143
729162 ZDOT = 3701
408649
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 15227
57628040
00016717 00000-0 10270-3 0 9017
2 25544 51
6436 147
5133 0001435 51
4508 308
6774 15
55203442 37283
Satellite: ISS
Catalog Number: 25544
Epoch time: 15227
57628040 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 147
5133 deg
Eccentricity:
0001435
Arg of perigee: 51
4508 deg
Mean anomaly: 308
6774 deg
Mean motion: 15
55203442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3728
Checksum: 294
Coasting Arc #3 (Orbit 3742)
---------------------------------------
Vector Time (GMT): 2015/228/12:30:39
716
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3890196
11 A = 6774955
97 meter
Y = 2086756
22 meter E =
0014889
Z = -5152535
22 I = 51
84885
XDOT = -5046
231555 Wp = 75
89000
YDOT = 5545
043607 meter/sec RA = 141
73782 deg
ZDOT = -1564
463418 TA = 179
05596
MA = 179
05315
Ha = 219
693 n
mi
Hp = 212
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12763110
61 X = 3891601
02
Y = 6846313
05 feet Y = 2130266
52 meter
Z = -16904643
11 Z = -5133634
44
XDOT = -16555
877804 XDOT = -5100
263083
YDOT = 18192
400284 feet/sec YDOT = 5488
311133 meter/sec
ZDOT = -5132
753995 ZDOT = -1589
108139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8025842
65 X = -2446276
84
Y = -12169282
46 feet Y = -3709197
29 meter
Z = -16823506
40 Z = -5127804
75
XDOT = 22326
243616 XDOT = 6805
039054
YDOT = -7481
708351 feet/sec YDOT = -2280
424705 meter/sec
ZDOT = -5239
908755 ZDOT = -1597
124189
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 15228
54013552
00016717 00000-0 10270-3 0 9022
2 25544 51
6444 142
7005 0001456 52
7229 307
4057 15
55243794 37436
Satellite: ISS
Catalog Number: 25544
Epoch time: 15228
54013552 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 142
7005 deg
Eccentricity:
0001456
Arg of perigee: 52
7229 deg
Mean anomaly: 307
4057 deg
Mean motion: 15
55243794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3743
Checksum: 292
Coasting Arc #4 (Orbit 3758)
---------------------------------------
Vector Time (GMT): 2015/229/12:30:39
716
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2197093
84 A = 6774165
62 meter
Y = -3624706
13 meter E =
0004413
Z = 5281278
93 I = 51
87074
XDOT = 5963
636874 Wp = 58
99296
YDOT = -4764
327650 meter/sec RA = 136
74131 deg
ZDOT = -786
238472 TA = 38
50718
MA = 38
47570
Ha = 219
648 n
mi
Hp = 212
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7208313
12 X = -2182052
31
Y = -11892080
48 feet Y = -3649191
03 meter
Z = 17327030
60 Z = 5270642
80
XDOT = 19565
737777 XDOT = 6020
288704
YDOT = -15630
996226 feet/sec YDOT = -4697
321633 meter/sec
ZDOT = -2579
522546 ZDOT = -757
130801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 975982
61 X = 297479
50
Y = 13928211
23 feet Y = 4245318
78 meter
Z = 17281774
66 Z = 5267484
92
XDOT = -23580
034421 XDOT = -7187
194491
YDOT = 4707
263287 feet/sec YDOT = 1434
773850 meter/sec
ZDOT = -2453
244528 ZDOT = -747
748932
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 15229
56823376
00016717 00000-0 10270-3 0 9039
2 25544 51
6440 137
5669 0001298 50
6425 309
4843 15
55284351 37595
Satellite: ISS
Catalog Number: 25544
Epoch time: 15229
56823376 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 137
5669 deg
Eccentricity:
0001298
Arg of perigee: 50
6425 deg
Mean anomaly: 309
4843 deg
Mean motion: 15
55284351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3759
Checksum: 328
Coasting Arc #5 (Orbit 3773)
---------------------------------------
Vector Time (GMT): 2015/230/12:30:39
716
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 442638
97 A = 6776973
74 meter
Y = 4946259
00 meter E =
0011101
Z = -4622144
10 I = 51
90294
XDOT = -6181
543298 Wp = 104
42777
YDOT = 3371
242529 meter/sec RA = 131
74972 deg
ZDOT = 3019
028195 TA = 195
60496
MA = 195
63921
Ha = 219
629 n
mi
Hp = 212
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1452227
59 X = 409748
20
Y = 16227883
86 feet Y = 4951024
66 meter
Z = -15164514
78 Z = -4620074
10
XDOT = -20280
653864 XDOT = -6233
447064
YDOT = 11060
506984 feet/sec YDOT = 3301
826443 meter/sec
ZDOT = 9904
948145 ZDOT = 2988
873502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5885538
68 X = 1793912
19
Y = -15200634
45 feet Y = -4633153
38 meter
Z = -15156412
33 Z = -4619674
48
XDOT = 22034
804250 XDOT = 6716
208335
YDOT = -1203
273753 feet/sec YDOT = -366
757840 meter/sec
ZDOT = 9774
374609 ZDOT = 2979
229381
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 15230
53206591
00016717 00000-0 10270-3 0 9043
2 25544 51
6443 132
7538 0001354 53
8798 306
2480 15
55268171 37742
Satellite: ISS
Catalog Number: 25544
Epoch time: 15230
53206591 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 132
7538 deg
Eccentricity:
0001354
Arg of perigee: 53
8798 deg
Mean anomaly: 306
2480 deg
Mean motion: 15
55268171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3774
Checksum: 309
Coasting Arc #6 (Orbit 3789)
---------------------------------------
Vector Time (GMT): 2015/231/12:30:39
716
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1214127
62 A = 6781557
29 meter
Y = -5836705
39 meter E =
0013969
Z = 3220304
05 I = 51
93847
XDOT = 5795
289887 Wp = 90
16097
YDOT = -1459
639491 meter/sec RA = 126
77260 deg
ZDOT = -4812
581624 TA = 52
70896
MA = 52
58169
Ha = 219
644 n
mi
Hp = 212
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3983358
35 X = 1263661
94
Y = -19149295
88 feet Y = -5822851
03 meter
Z = 10565302
01 Z = 3226322
71
XDOT = 19013
418266 XDOT = 5834
558738
YDOT = -4788
843476 feet/sec YDOT = -1394
613509 meter/sec
ZDOT = -15789
309790 ZDOT = -4784
333988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11814178
98 X = -3600961
75
Y = 15569781
47 feet Y = 4745669
39 meter
Z = 10592231
26 Z = 3228512
09
XDOT = -18169
565050 XDOT = -5538
083427
YDOT = -3088
403330 feet/sec YDOT = -941
345335 meter/sec
ZDOT = -15667
267069 ZDOT = -4775
383003
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 15231
56014010
00016717 00000-0 10270-3 0 9051
2 25544 51
6439 127
6198 0001410 59
3551 300
7741 15
55280152 37903
Satellite: ISS
Catalog Number: 25544
Epoch time: 15231
56014010 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 127
6198 deg
Eccentricity:
0001410
Arg of perigee: 59
3551 deg
Mean anomaly: 300
7741 deg
Mean motion: 15
55280152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3790
Checksum: 278
Coasting Arc #7 (Orbit 3804)
---------------------------------------
Vector Time (GMT): 2015/232/12:30:39
716
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2564883
63 A = 6785079
67 meter
Y = 6131545
79 meter E =
0009927
Z = -1345511
84 I = 51
96928
XDOT = -4901
527225 Wp = 40
44856
YDOT = -774
144792 meter/sec RA = 121
81060 deg
ZDOT = 5847
163679 TA = 304
96141
MA = 305
05460
Ha = 219
534 n
mi
Hp = 212
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8414972
53 X = -2626721
47
Y = 20116620
06 feet Y = 6102517
74 meter
Z = -4414408
92 Z = -1358122
05
XDOT = -16081
126067 XDOT = -4920
909426
YDOT = -2539
845118 feet/sec YDOT = -829
064902 meter/sec
ZDOT = 19183
607871 ZDOT = 5823
306122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16011682
12 X = 4880360
71
Y = -14785935
88 feet Y = -4506753
26 meter
Z = -4469821
84 Z = -1362401
70
XDOT = 12590
232091 XDOT = 3837
502741
YDOT = 7896
550439 feet/sec YDOT = 2406
868574 meter/sec
ZDOT = 19080
863514 ZDOT = 5815
847199
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 15232
52394610
00016717 00000-0 10270-3 0 9066
2 25544 51
6443 122
8060 0001290 57
7290 302
3988 15
55318607 38056
Satellite: ISS
Catalog Number: 25544
Epoch time: 15232
52394610 = yrday
fracday
Element set: 906
Inclination: 51
6443 deg
RA of node: 122
8060 deg
Eccentricity:
0001290
Arg of perigee: 57
7290 deg
Mean anomaly: 302
3988 deg
Mean motion: 15
55318607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3805
Checksum: 296
Coasting Arc #8 (Orbit 3820)
---------------------------------------
Vector Time (GMT): 2015/233/11:54:08
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4812148
53 A = 6779707
65 meter
Y = 2818069
75 meter E =
0012562
Z = 3845590
64 I = 51
96656
XDOT = -403
959135 Wp = 93
94242
YDOT = -6419
251470 meter/sec RA = 117
00193 deg
ZDOT = 4185
997292 TA = 312
17405
MA = 312
28067
Ha = 219
705 n
mi
Hp = 212
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15787888
87 X = -4861983
57
Y = 9245635
68 feet Y = 2763978
70 meter
Z = 12616767
20 Z = 3822093
07
XDOT = -1325
325245 XDOT = -352
481409
YDOT = -21060
536318 feet/sec YDOT = -6423
480758 meter/sec
ZDOT = 13733
586916 ZDOT = 4184
160317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18346933
38 X = 5592145
30
Y = 829410
41 feet Y = 252804
29 meter
Z = 12514956
75 Z = 3814558
82
XDOT = -10165
986664 XDOT = -3098
592735
YDOT = 17125
853772 feet/sec YDOT = 5219
960230 meter/sec
ZDOT = 13726
761728 ZDOT = 4183
916975
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 15233
55199495
00016717 00000-0 10270-3 0 9075
2 25544 51
6441 117
6715 0001381 60
6635 299
4657 15
55311664 38213
Satellite: ISS
Catalog Number: 25544
Epoch time: 15233
55199495 = yrday
fracday
Element set: 907
Inclination: 51
6441 deg
RA of node: 117
6715 deg
Eccentricity:
0001381
Arg of perigee: 60
6635 deg
Mean anomaly: 299
4657 deg
Mean motion: 15
55311664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3821
Checksum: 322
Coasting Arc #9 (Orbit 3835)
---------------------------------------
Vector Time (GMT): 2015/234/11:54:08
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4527588
43 A = 6775316
86 meter
Y = -778606
79 meter E =
0013660
Z = -4992481
07 I = 51
96604
XDOT = -1122
581996 Wp = 72
83016
YDOT = 7264
975810 meter/sec RA = 112
02166 deg
ZDOT = -2151
988892 TA = 176
27757
MA = 176
26740
Ha = 219
464 n
mi
Hp = 212
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14854292
74 X = 4560210
00
Y = -2554484
20 feet Y = -727794
12 meter
Z = -16379531
08 Z = -4970407
76
XDOT = -3683
011797 XDOT = -1193
283766
YDOT = 23835
222474 feet/sec YDOT = 7252
026957 meter/sec
ZDOT = -7060
331012 ZDOT = -2157
614174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14056655
49 X = -4284468
59
Y = -5718357
03 feet Y = -1742955
22 meter
Z = -16284203
09 Z = -4963425
10
XDOT = 15245
283475 XDOT = 4646
762403
YDOT = -17305
676135 feet/sec YDOT = -5274
770086 meter/sec
ZDOT = -7085
845024 ZDOT = -2159
765563
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 15234
51577696
00016717 00000-0 10270-3 0 9086
2 25544 51
6441 112
8580 0001246 57
6645 302
4628 15
55360024 38360
Satellite: ISS
Catalog Number: 25544
Epoch time: 15234
51577696 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 112
8580 deg
Eccentricity:
0001246
Arg of perigee: 57
6645 deg
Mean anomaly: 302
4628 deg
Mean motion: 15
55360024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3836
Checksum: 310
Coasting Arc #10 (Orbit 3851)
---------------------------------------
Vector Time (GMT): 2015/235/11:54:08
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3915408
58 A = 6773719
84 meter
Y = -1451430
60 meter E =
0003609
Z = 5330533
23 I = 51
97233
XDOT = 2406
595910 Wp = 74
79009
YDOT = -7283
409542 meter/sec RA = 107
03199 deg
ZDOT = -214
424899 TA = 17
24894
MA = 17
23668
Ha = 219
573 n
mi
Hp = 212
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12845828
68 X = -3924780
92
Y = -4761911
40 feet Y = -1495267
52 meter
Z = 17488626
07 Z = 5311490
31
XDOT = 7895
655872 XDOT = 2488
903482
YDOT = -23895
700596 feet/sec YDOT = -7256
037202 meter/sec
ZDOT = -703
493764 ZDOT = -202
534068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8683226
84 X = 2646647
54
Y = 10730788
28 feet Y = 3270744
27 meter
Z = 17406749
00 Z = 5305577
10
XDOT = -18252
653752 XDOT = -5563
408864
YDOT = 15831
314498 feet/sec YDOT = 4825
384659 meter/sec
ZDOT = -650
938560 ZDOT = -198
406073
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 15235
54379999
00016717 00000-0 10270-3 0 9097
2 25544 51
6444 107
7236 0001190 62
3443 297
7831 15
55378099 38522
Satellite: ISS
Catalog Number: 25544
Epoch time: 15235
54379999 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 107
7236 deg
Eccentricity:
0001190
Arg of perigee: 62
3443 deg
Mean anomaly: 297
7831 deg
Mean motion: 15
55378099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3852
Checksum: 343
Coasting Arc #11 (Orbit 3866)
---------------------------------------
Vector Time (GMT): 2015/236/11:54:08
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3105020
32 A = 6775796
85 meter
Y = 3593674
37 meter E =
0012356
Z = -4844303
98 I = 51
98741
XDOT = -3399
129231 Wp = 104
18543
YDOT = 6373
315351 meter/sec RA = 102
04323 deg
ZDOT = 2551
721445 TA = 190
81147
MA = 190
83806
Ha = 219
393 n
mi
Hp = 212
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10187074
55 X = 3088135
84
Y = 11790270
25 feet Y = 3628302
25 meter
Z = -15893385
76 Z = -4829261
60
XDOT = -11151
998789 XDOT = -3482
539761
YDOT = 20909
827267 feet/sec YDOT = 6334
837729 meter/sec
ZDOT = 8371
789517 ZDOT = 2535
006547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3052414
15 X = -930375
83
Y = -15346264
25 feet Y = -4677541
34 meter
Z = -15829138
09 Z = -4824721
29
XDOT = 19010
050253 XDOT = 5794
263317
YDOT = -12332
380049 feet/sec YDOT = -3758
909439 meter/sec
ZDOT = 8298
570955 ZDOT = 2529
404427
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 15236
50756050
00016717 00000-0 10270-3 0 9103
2 25544 51
6440 102
9095 0001136 60
1947 299
9319 15
55391334 38671
Satellite: ISS
Catalog Number: 25544
Epoch time: 15236
50756050 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 102
9095 deg
Eccentricity:
0001136
Arg of perigee: 60
1947 deg
Mean anomaly: 299
9319 deg
Mean motion: 15
55391334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3867
Checksum: 308
Coasting Arc #12 (Orbit 3882)
---------------------------------------
Vector Time (GMT): 2015/237/11:54:08
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2136090
57 A = 6780187
49 meter
Y = -5355186
05 meter E =
0013142
Z = 3557767
39 I = 52
00862
XDOT = 4121
764183 Wp = 84
94494
YDOT = -4647
285477 meter/sec RA = 97
06767 deg
ZDOT = -4505
045817 TA = 53
27000
MA = 53
14938
Ha = 219
360 n
mi
Hp = 212
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7008171
18 X = -2093330
94
Y = -17569508
04 feet Y = -5378834
07 meter
Z = 11672465
18 Z = 3547494
75
XDOT = 13522
848371 XDOT = 4195
308495
YDOT = -15246
999597 feet/sec YDOT = -4600
782076 meter/sec
ZDOT = -14780
334046 ZDOT = -4484
844593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2282345
00 X = -695658
76
Y = 18804342
87 feet Y = 5731563
71 meter
Z = 11629106
16 Z = 3544551
56
XDOT = -17916
336609 XDOT = -5460
899398
YDOT = 6942
905156 feet/sec YDOT = 2116
197492 meter/sec
ZDOT = -14692
369022 ZDOT = -4478
234078
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 15237
53555872
00016717 00000-0 10270-3 0 9117
2 25544 51
6443 97
7753 0001173 56
2476 303
8789 15
55437825 38830
Satellite: ISS
Catalog Number: 25544
Epoch time: 15237
53555872 = yrday
fracday
Element set: 911
Inclination: 51
6443 deg
RA of node: 97
7753 deg
Eccentricity:
0001173
Arg of perigee: 56
2476 deg
Mean anomaly: 303
8789 deg
Mean motion: 15
55437825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3883
Checksum: 341
Coasting Arc #13 (Orbit 3897)
---------------------------------------
Vector Time (GMT): 2015/238/11:54:08
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1110470
31 A = 6784355
21 meter
Y = 6463353
38 meter E =
0008628
Z = -1726002
23 I = 52
02419
XDOT = -4554
790080 Wp = 40
69686
YDOT = 2304
729054 meter/sec RA = 92
10680 deg
ZDOT = 5722
457076 TA = 300
46566
MA = 300
55085
Ha = 219
352 n
mi
Hp = 212
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3643275
29 X = 1046497
15
Y = 21205227
62 feet Y = 6475413
65 meter
Z = -5662736
96 Z = -1720763
42
XDOT = -14943
537009 XDOT = -4608
020747
YDOT = 7561
447026 feet/sec YDOT = 2253
496927 meter/sec
ZDOT = 18774
465474 ZDOT = 5700
201758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6667411
62 X = 2032227
06
Y = -20462725
42 feet Y = -6237038
71 meter
Z = -5641295
43 Z = -1719466
85
XDOT = 15359
096373 XDOT = 4681
452574
YDOT = -124
464992 feet/sec YDOT = -37
936930 meter/sec
ZDOT = 18678
047483 ZDOT = 5693
068873
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 15238
49929693
00016717 00000-0 10270-3 0 9120
2 25544 51
6433 92
9610 0001076 59
0005 301
1254 15
55406985 38986
Satellite: ISS
Catalog Number: 25544
Epoch time: 15238
49929693 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 92
9610 deg
Eccentricity:
0001076
Arg of perigee: 59
0005 deg
Mean anomaly: 301
1254 deg
Mean motion: 15
55406985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3898
Checksum: 320
Coasting Arc #14 (Orbit 3913)
---------------------------------------
Vector Time (GMT): 2015/239/11:54:08
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2640
41 A = 6785521
29 meter
Y = -6767148
02 meter E =
0011632
Z = -426710
23 I = 52
02800
XDOT = 4728
660268 Wp = 133
20415
YDOT = 371
244057 meter/sec RA = 87
15668 deg
ZDOT = -6027
456862 TA = 51
37466
MA = 51
27058
Ha = 219
347 n
mi
Hp = 212
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8662
75 X = 75104
44
Y = -22201929
20 feet Y = -6766742
87 meter
Z = -1399967
94 Z = -426533
91
XDOT = 15513
977257 XDOT = 4753
436110
YDOT = 1217
992314 feet/sec YDOT = 424
261297 meter/sec
ZDOT = -19775
120937 ZDOT = -6004
426184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10047059
78 X = -3062343
82
Y = 19798683
39 feet Y = 6034638
70 meter
Z = -1397988
30 Z = -426106
83
XDOT = -11952
819492 XDOT = -3643
219381
YDOT = -7429
227009 feet/sec YDOT = -2264
428392 meter/sec
ZDOT = -19675
832839 ZDOT = -5997
193849
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 15239
52727206
00016717 00000-0 10270-3 0 9132
2 25544 51
6429 87
8265 0001031 69
5961 290
5303 15
55412396 39146
Satellite: ISS
Catalog Number: 25544
Epoch time: 15239
52727206 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 87
8265 deg
Eccentricity:
0001031
Arg of perigee: 69
5961 deg
Mean anomaly: 290
5303 deg
Mean motion: 15
55412396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3914
Checksum: 312
Coasting Arc #15 (Orbit 3929)
---------------------------------------
Vector Time (GMT): 2015/240/11:54:08
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1102700
99 A = 6782828
70 meter
Y = 6209459
57 meter E =
0014646
Z = 2478125
64 I = 52
01603
XDOT = -4626
563774 Wp = 74
43852
YDOT = -2967
536905 meter/sec RA = 82
20202 deg
ZDOT = 5354
705586 TA = 313
20725
MA = 313
32949
Ha = 219
226 n
mi
Hp = 212
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3617785
42 X = -1184092
31
Y = 20372242
69 feet Y = 6196673
53 meter
Z = 8130333
45 Z = 2472570
90
XDOT = -15179
015007 XDOT = -4619
046886
YDOT = -9736
013469 feet/sec YDOT = -3019
231780 meter/sec
ZDOT = 17567
931712 ZDOT = 5332
249513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12205713
96 X = 3720301
61
Y = -16719584
49 feet Y = -5096129
35 meter
Z = 8105245
62 Z = 2470478
87
XDOT = 8278
427834 XDOT = 2523
264804
YDOT = 14548
956979 feet/sec YDOT = 4434
522087 meter/sec
ZDOT = 17471
589717 ZDOT = 5325
340546
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 15240
55523223
00016717 00000-0 10270-3 0 9141
2 25544 51
6418 82
6903 0000917 67
8607 292
2644 15
55475093 39304
Satellite: ISS
Catalog Number: 25544
Epoch time: 15240
55523223 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 82
6903 deg
Eccentricity:
0000917
Arg of perigee: 67
8607 deg
Mean anomaly: 292
2644 deg
Mean motion: 15
55475093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3930
Checksum: 309
Coasting Arc #16 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2015/241/11:54:08
000
Vector Time (MET): N/A
Weight (LBS) : 924404
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2232463
60 A = 6778125
03 meter
Y = -4868803
55 meter E =
0008695
Z = -4162847
45 I = 51
99382
XDOT = 4205
587302 Wp = 70
37233
YDOT = 5164
426121 meter/sec RA = 77
23455 deg
ZDOT = -3788
427609 TA = 160
77901
MA = 160
74619
Ha = 219
254 n
mi
Hp = 212
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7324355
65 X = 2306963
04
Y = -15973764
94 feet Y = -4843422
52 meter
Z = -13657635
99 Z = -4151821
36
XDOT = 13797
858603 XDOT = 4165
927326
YDOT = 16943
655253 feet/sec YDOT = 5211
233659 meter/sec
ZDOT = -12429
224439 ZDOT = -3768
094841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13455236
76 X = -4101156
16
Y = 11361564
20 feet Y = 3463004
77 meter
Z = -13609182
04 Z = -4148078
69
XDOT = -4612
414668 XDOT = -1405
863991
YDOT = -20232
374228 feet/sec YDOT = -6166
827665 meter/sec
ZDOT = -12342
444036 ZDOT = -3761
976942
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 15241
51893562
00016717 00000-0 10270-3 0 9155
2 25544 51
6406 77
8756 0001042 69
5981 290
5284 15
55473545 39454
Satellite: ISS
Catalog Number: 25544
Epoch time: 15241
51893562 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 77
8756 deg
Eccentricity:
0001042
Arg of perigee: 69
5981 deg
Mean anomaly: 290
5284 deg
Mean motion: 15
55473545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3945
Checksum: 333
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