[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 15th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 76 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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
077/03:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
2
078/21:26:42
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 215
0
079/03:11:47
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
1
080/10:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 215
0
083/03:23:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 214
8
084/04:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 214
6
Coasting Arc #1 (Orbit 3024)
---------------------------------------
Vector Time (GMT): 2016/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4756709
42 A = 6784816
77 meter
Y = 3555240
71 meter E =
0003065
Z = -3282803
11 I = 51
71104
XDOT = -5344
345613 Wp = 70
73067
YDOT = -2779
818145 meter/sec RA = 169
09944 deg
ZDOT = 4737
922949 TA = 251
21672
MA = 251
24998
Ha = 220
407 n
mi
Hp = 215
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15606002
04 X = -4780165
06
Y = 11664175
54 feet Y = 3501916
55 meter
Z = -10770351
39 Z = -3305967
29
XDOT = -17533
942299 XDOT = -5335
878544
YDOT = -9120
138272 feet/sec YDOT = -2839
534354 meter/sec
ZDOT = 15544
366629 ZDOT = 4711
982346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17059362
08 X = -5199693
56
Y = 9294627
00 feet Y = 2833002
31 meter
Z = -10871468
81 Z = -3313623
69
XDOT = -15452
198010 XDOT = -4709
829954
YDOT = -10328
184872 feet/sec YDOT = -3148
030749 meter/sec
ZDOT = 15432
179684 ZDOT = 4703
728368
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 16074
50688678
00016717 00000-0 10270-3 0 9003
2 25544 51
6428 170
2249 0001909 290
1223 69
9724 15
54079183 30251
Satellite: ISS
Catalog Number: 25544
Epoch time: 16074
50688678 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 170
2249 deg
Eccentricity:
0001909
Arg of perigee: 290
1223 deg
Mean anomaly: 69
9724 deg
Mean motion: 15
54079183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3025
Checksum: 318
Coasting Arc #2 (Orbit 3040)
---------------------------------------
Vector Time (GMT): 2016/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5769203
92 A = 6788015
33 meter
Y = -3093511
79 meter E =
0012203
Z = 1773413
53 I = 51
75230
XDOT = 3686
220829 Wp = 114
88570
YDOT = 3605
005731 meter/sec RA = 164
12956 deg
ZDOT = -5677
787982 TA = 45
66636
MA = 45
56640
Ha = 220
447 n
mi
Hp = 215
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18927834
39 X = 5794753
12
Y = -10149316
90 feet Y = -3028853
70 meter
Z = 5818285
86 Z = 1801501
09
XDOT = 12093
900356 XDOT = 3673
214917
YDOT = 11827
446623 feet/sec YDOT = 3646
154258 meter/sec
ZDOT = -18627
913326 ZDOT = -5659
913248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20030039
22 X = 6105155
95
Y = -7656978
79 feet Y = -2333847
13 meter
Z = 5940724
16 Z = 1810732
72
XDOT = 10047
220759 XDOT = 3062
392887
YDOT = 11826
119660 feet/sec YDOT = 3604
601272 meter/sec
ZDOT = -18550
863683 ZDOT = -5654
303250
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 16075
53573899
00016717 00000-0 10270-3 0 9016
2 25544 51
6420 165
0969 0001749 292
9264 67
1704 15
54103050 30418
Satellite: ISS
Catalog Number: 25544
Epoch time: 16075
53573899 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 165
0969 deg
Eccentricity:
0001749
Arg of perigee: 292
9264 deg
Mean anomaly: 67
1704 deg
Mean motion: 15
54103050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3041
Checksum: 308
Coasting Arc #3 (Orbit 3055)
---------------------------------------
Vector Time (GMT): 2016/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6310809
99 A = 6789367
86 meter
Y = 2484644
25 meter E =
0011591
Z = -98867
47 I = 51
78807
XDOT = -1814
942806 Wp = 35
38343
YDOT = -4384
475964 meter/sec RA = 159
16737 deg
ZDOT = 6025
074913 TA = 323
55364
MA = 323
63249
Ha = 220
459 n
mi
Hp = 215
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20704757
18 X = -6337644
61
Y = 8151719
97 feet Y = 2413922
53 meter
Z = -324368
34 Z = -129588
97
XDOT = -5954
536765 XDOT = -1795
046612
YDOT = -14384
763661 feet/sec YDOT = -4404
660054 meter/sec
ZDOT = 19767
306145 ZDOT = 6016
307176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21475904
06 X = -6545855
56
Y = 5815354
74 feet Y = 1772520
13 meter
Z = -458167
29 Z = -139649
39
XDOT = -4031
669341 XDOT = -1228
852815
YDOT = -13400
619602 feet/sec YDOT = -4084
508855 meter/sec
ZDOT = 19729
917693 ZDOT = 6013
678913
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 16076
50027161
00016717 00000-0 10270-3 0 9021
2 25544 51
6427 160
2888 0001936 302
5119 57
5846 15
54112176 30562
Satellite: ISS
Catalog Number: 25544
Epoch time: 16076
50027161 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 160
2888 deg
Eccentricity:
0001936
Arg of perigee: 302
5119 deg
Mean anomaly: 57
5846 deg
Mean motion: 15
54112176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3056
Checksum: 297
Coasting Arc #4 (Orbit 3066)
---------------------------------------
Vector Time (GMT): 2016/077/03:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2211787
17 A = 6781195
25 meter
Y = -4726814
15 meter E =
0008694
Z = 4326441
15 I = 51
77981
XDOT = 6819
173226 Wp = 59
02017
YDOT = -30
454927 meter/sec RA = 155
83308 deg
ZDOT = -3509
820000 TA = 66
65214
MA = 66
56069
Ha = 220
352 n
mi
Hp = 215
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7256519
57 X = 2243463
40
Y = -15507920
44 feet Y = -4701902
94 meter
Z = 14194360
72 Z = 4337262
75
XDOT = 22372
615571 XDOT = 6836
055998
YDOT = -99
917739 feet/sec YDOT = 45
895653 meter/sec
ZDOT = -11515
157480 ZDOT = -3476
653478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8317980
75 X = 2535320
53
Y = 14919998
41 feet Y = 4547615
51 meter
Z = 14242099
31 Z = 4340991
87
XDOT = -12042
923070 XDOT = -3670
682952
YDOT = 17598
383687 feet/sec YDOT = 5363
987348 meter/sec
ZDOT = -11371
112553 ZDOT = -3465
915106
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 16077
20758532
00016717 00000-0 10270-3 0 9033
2 25544 51
6412 156
7633 0002285 311
0063 49
0892 15
54176111 30673
Satellite: ISS
Catalog Number: 25544
Epoch time: 16077
20758532 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 156
7633 deg
Eccentricity:
0002285
Arg of perigee: 311
0063 deg
Mean anomaly: 49
0892 deg
Mean motion: 15
54176111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3067
Checksum: 290
Coasting Arc #5 (Orbit 3081)
---------------------------------------
Vector Time (GMT): 2016/078/03:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3612911
71 A = 6785019
55 meter
Y = 4822269
36 meter E =
0003880
Z = -3118737
68 I = 51
81959
XDOT = -5784
851971 Wp = 50
13826
YDOT = -1176
391644 meter/sec RA = 150
85836 deg
ZDOT = 4888
968172 TA = 274
07553
MA = 274
11988
Ha = 220
472 n
mi
Hp = 215
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11853384
87 X = -3651417
69
Y = 15821093
70 feet Y = 4781651
74 meter
Z = -10232078
99 Z = -3136382
14
XDOT = -18979
173133 XDOT = -5795
015553
YDOT = -3859
552637 feet/sec YDOT = -1241
137997 meter/sec
ZDOT = 16039
921825 ZDOT = 4860
842584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6173874
51 X = -1881796
95
Y = -18737747
52 feet Y = -5711265
45 meter
Z = -10309474
78 Z = -3142327
91
XDOT = 12756
317894 XDOT = 3888
125694
YDOT = -12949
523647 feet/sec YDOT = -3947
014808 meter/sec
ZDOT = 15917
944372 ZDOT = 4851
789445
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 16078
17209663
00016717 00000-0 10270-3 0 9047
2 25544 51
6394 151
9546 0002062 315
4376 44
6611 15
54170069 30823
Satellite: ISS
Catalog Number: 25544
Epoch time: 16078
17209663 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 151
9546 deg
Eccentricity:
0002062
Arg of perigee: 315
4376 deg
Mean anomaly: 44
6611 deg
Mean motion: 15
54170069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3082
Checksum: 304
Coasting Arc #6 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2016/078/21:26:42
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3249256
58 A = 6777496
85 meter
Y = -2810773
10 meter E =
0001855
Z = 5240318
77 I = 51
81704
XDOT = 5889
440548 Wp = 104
97962
YDOT = -4793
841731 meter/sec RA = 147
27521 deg
ZDOT = 1079
663644 TA = 334
69993
MA = 334
70901
Ha = 220
561 n
mi
Hp = 215
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10660290
62 X = -3243039
23
Y = -9221696
53 feet Y = -2847073
06 meter
Z = 17192646
87 Z = 5224550
32
XDOT = 19322
311508 XDOT = 5937
364286
YDOT = -15727
827201 feet/sec YDOT = -4727
714006 meter/sec
ZDOT = 3542
203555 ZDOT = 1108
389690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1759289
38 X = 536231
40
Y = 14068466
62 feet Y = 4288068
63 meter
Z = 17124594
51 Z = 5219576
41
XDOT = -23832
999328 XDOT = -7264
298195
YDOT = -1487
279410 feet/sec YDOT = -453
322764 meter/sec
ZDOT = 3667
738326 ZDOT = 1117
926642
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 16078
94369747
00016717 00000-0 10270-3 0 9053
2 25544 51
6415 148
1109 0002180 319
5852 40
5138 15
54218754 30941
Satellite: ISS
Catalog Number: 25544
Epoch time: 16078
94369747 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 148
1109 deg
Eccentricity:
0002180
Arg of perigee: 319
5852 deg
Mean anomaly: 40
5138 deg
Mean motion: 15
54218754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3094
Checksum: 318
Coasting Arc #7 (Orbit 3096)
---------------------------------------
Vector Time (GMT): 2016/079/03:11:47
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4581031
74 A = 6787871
69 meter
Y = 4702021
93 meter E =
0008215
Z = -1710003
16 I = 51
85674
XDOT = -4540
789296 Wp = 23
35293
YDOT = -2352
231554 meter/sec RA = 146
05730 deg
ZDOT = 5713
356792 TA = 317
95307
MA = 318
01609
Ha = 220
458 n
mi
Hp = 215
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15029631
69 X = -4624964
09
Y = 15426581
13 feet Y = 4650547
93 meter
Z = -5610246
59 Z = -1732363
68
XDOT = -14897
602676 XDOT = -4541
901267
YDOT = -7717
295126 feet/sec YDOT = -2403
015190 meter/sec
ZDOT = 18744
608896 ZDOT = 5691
296637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5757
63 X = -1754
92
Y = -21511890
74 feet Y = -6556824
30 meter
Z = -5708119
19 Z = -1739834
73
XDOT = 14576
786386 XDOT = 4443
004490
YDOT = -4938
089191 feet/sec YDOT = -1505
129585 meter/sec
ZDOT = 18649
152239 ZDOT = 5684
261602
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 16079
13659593
00016717 00000-0 10270-3 0 9067
2 25544 51
6403 147
1476 0002196 318
1509 41
9475 15
54187173 30977
Satellite: ISS
Catalog Number: 25544
Epoch time: 16079
13659593 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 147
1476 deg
Eccentricity:
0002196
Arg of perigee: 318
1509 deg
Mean anomaly: 41
9475 deg
Mean motion: 15
54187173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3097
Checksum: 328
Coasting Arc #8 (Orbit 3112)
---------------------------------------
Vector Time (GMT): 2016/080/03:11:47
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5292583
19 A = 6789039
20 meter
Y = -4244788
26 meter E =
0009883
Z = -25258
30 I = 51
88750
XDOT = 2947
774317 Wp = 132
07010
YDOT = 3702
285013 meter/sec RA = 141
10216 deg
ZDOT = -6032
707040 TA = 48
20101
MA = 48
11662
Ha = 220
535 n
mi
Hp = 214
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17364118
08 X = 5339778
81
Y = -13926470
68 feet Y = -4185339
20 meter
Z = -82868
44 Z = 566
67
XDOT = 9671
175581 XDOT = 2935
459323
YDOT = 12146
604372 feet/sec YDOT = 3735
179291 meter/sec
ZDOT = -19792
345932 ZDOT = -6018
418081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2359149
98 X = -719068
91
Y = 22133674
82 feet Y = 6746344
09 meter
Z = 29993
67 Z = 9142
07
XDOT = -13907
360551 XDOT = -4238
963496
YDOT = -1436
972535 feet/sec YDOT = -437
989229 meter/sec
ZDOT = -19730
855491 ZDOT = -6013
964754
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 16080
16538245
00016717 00000-0 10270-3 0 9073
2 25544 51
6408 142
0185 0002302 325
9294 34
1711 15
54227814 31132
Satellite: ISS
Catalog Number: 25544
Epoch time: 16080
16538245 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 142
0185 deg
Eccentricity:
0002302
Arg of perigee: 325
9294 deg
Mean anomaly: 34
1711 deg
Mean motion: 15
54227814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3113
Checksum: 279
Coasting Arc #9 (Orbit 3117)
---------------------------------------
Vector Time (GMT): 2016/080/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4666838
38 A = 6779287
00 meter
Y = -991388
42 meter E =
0005680
Z = 4812643
76 I = 51
86520
XDOT = 3959
571272 Wp = 112
51470
YDOT = -6037
216722 meter/sec RA = 139
62624 deg
ZDOT = 2591
408867 TA = 312
02538
MA = 312
07372
Ha = 220
582 n
mi
Hp = 214
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15311149
54 X = -4678783
08
Y = -3252586
69 feet Y = -1043642
21 meter
Z = 15789513
64 Z = 4789944
81
XDOT = 12990
719395 XDOT = 4014
198835
YDOT = -19807
141478 feet/sec YDOT = -5992
632353 meter/sec
ZDOT = 8501
997596 ZDOT = 2610
776805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12391127
53 X = -3776815
67
Y = -9724713
05 feet Y = -2964092
54 meter
Z = 15691057
21 Z = 4782634
24
XDOT = 19645
094906 XDOT = 5987
824927
YDOT = -11151
823546 feet/sec YDOT = -3399
075817 meter/sec
ZDOT = 8587
094876 ZDOT = 2617
346518
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 16080
48687519
00016717 00000-0 10270-3 0 9088
2 25544 51
6435 140
4150 0001926 318
4223 41
6783 15
54241672 31181
Satellite: ISS
Catalog Number: 25544
Epoch time: 16080
48687519 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 140
4150 deg
Eccentricity:
0001926
Arg of perigee: 318
4223 deg
Mean anomaly: 41
6783 deg
Mean motion: 15
54241672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3118
Checksum: 303
Coasting Arc #10 (Orbit 3132)
---------------------------------------
Vector Time (GMT): 2016/081/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3505636
19 A = 6777289
37 meter
Y = 2373318
39 meter E =
0013718
Z = -5304238
48 I = 51
88074
XDOT = -4963
064843 Wp = 77
47875
YDOT = 5792
218184 meter/sec RA = 134
64465 deg
ZDOT = -687
092427 TA = 185
96503
MA = 185
98139
Ha = 220
557 n
mi
Hp = 215
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11501431
07 X = 3504602
10
Y = 7786477
65 feet Y = 2412514
14 meter
Z = -17402357
23 Z = -5287212
01
XDOT = -16283
021137 XDOT = -5024
128431
YDOT = 19003
340498 feet/sec YDOT = 5736
376359 meter/sec
ZDOT = -2254
240245 ZDOT = -711
350756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7187303
38 X = 2190690
07
Y = 11992120
37 feet Y = 3655198
29 meter
Z = -17328759
54 Z = -5281805
91
XDOT = -21941
562358 XDOT = -6687
788207
YDOT = 9732
664265 feet/sec YDOT = 2966
516068 meter/sec
ZDOT = -2360
556652 ZDOT = -719
497667
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 16081
45134945
00016717 00000-0 10270-3 0 9097
2 25544 51
6422 135
6076 0002007 324
5642 35
5377 15
54210528 31338
Satellite: ISS
Catalog Number: 25544
Epoch time: 16081
45134945 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 135
6076 deg
Eccentricity:
0002007
Arg of perigee: 324
5642 deg
Mean anomaly: 35
5377 deg
Mean motion: 15
54210528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3133
Checksum: 289
Coasting Arc #11 (Orbit 3148)
---------------------------------------
Vector Time (GMT): 2016/082/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2212210
76 A = 6777444
86 meter
Y = -3728848
62 meter E =
0004680
Z = 5207908
72 I = 51
90385
XDOT = 5563
700237 Wp = 30
36548
YDOT = -5117
976392 meter/sec RA = 129
66123 deg
ZDOT = -1296
670551 TA = 72
06484
MA = 72
01382
Ha = 220
557 n
mi
Hp = 214
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7257909
32 X = -2195647
08
Y = -12233755
30 feet Y = -3753493
57 meter
Z = 17086314
70 Z = 5197203
25
XDOT = 18253
609701 XDOT = 5626
815851
YDOT = -16791
261129 feet/sec YDOT = -5055
406706 meter/sec
ZDOT = -4254
168473 ZDOT = -1269
489507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1695385
01 X = -516753
35
Y = -14178671
17 feet Y = -4321658
97 meter
Z = 17040396
71 Z = 5193912
92
XDOT = 22529
203524 XDOT = 6866
901234
YDOT = -7681
327950 feet/sec YDOT = -2341
268759 meter/sec
ZDOT = -4135
248482 ZDOT = -1260
423737
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 16082
48011003
00016717 00000-0 10270-3 0 9102
2 25544 51
6422 130
4787 0002016 327
5184 32
5845 15
54275918 31492
Satellite: ISS
Catalog Number: 25544
Epoch time: 16082
48011003 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 130
4787 deg
Eccentricity:
0002016
Arg of perigee: 327
5184 deg
Mean anomaly: 32
5845 deg
Mean motion: 15
54275918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3149
Checksum: 288
Coasting Arc #12 (Orbit 3159)
---------------------------------------
Vector Time (GMT): 2016/083/03:23:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2582466
70 A = 6777464
24 meter
Y = -3430027
96 meter E =
0004583
Z = 5242553
81 I = 51
91379
XDOT = 5148
867350 Wp = 32
06710
YDOT = -5576
231337 meter/sec RA = 126
14973 deg
ZDOT = -1107
797327 TA = 68
53091
MA = 68
48204
Ha = 220
797 n
mi
Hp = 214
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8472659
76 X = -2569385
34
Y = -11253372
58 feet Y = -3458832
82 meter
Z = 17199979
70 Z = 5230041
21
XDOT = 16892
609417 XDOT = 5216
220670
YDOT = -18294
722235 feet/sec YDOT = -5518
276864 meter/sec
ZDOT = -3634
505665 ZDOT = -1082
620987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14145482
76 X = 4311543
14
Y = 421975
52 feet Y = 128618
14 meter
Z = 17146163
24 Z = 5226150
56
XDOT = 3583
740808 XDOT = 1092
324198
YDOT = 23630
674053 feet/sec YDOT = 7202
629451 meter/sec
ZDOT = -3524
213510 ZDOT = -1074
180278
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 16083
18737993
00016717 00000-0 10270-3 0 9114
2 25544 51
6385 126
9502 0001990 338
2547 21
8521 15
54220003 31607
Satellite: ISS
Catalog Number: 25544
Epoch time: 16083
18737993 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 126
9502 deg
Eccentricity:
0001990
Arg of perigee: 338
2547 deg
Mean anomaly: 21
8521 deg
Mean motion: 15
54220003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3160
Checksum: 295
Coasting Arc #13 (Orbit 3174)
---------------------------------------
Vector Time (GMT): 2016/084/03:23:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1383007
11 A = 6779793
24 meter
Y = 4745901
61 meter E =
0009474
Z = -4648834
80 I = 51
94088
XDOT = -5442
289538 Wp = 100
49036
YDOT = 4496
556222 meter/sec RA = 121
17120 deg
ZDOT = 2974
846869 TA = 199
04215
MA = 199
07759
Ha = 220
740 n
mi
Hp = 214
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4537424
90 X = 1352416
53
Y = 15570543
34 feet Y = 4761195
53 meter
Z = -15252082
66 Z = -4642191
55
XDOT = -17855
280636 XDOT = -5506
617207
YDOT = 14752
481043 feet/sec YDOT = 4435
337719 meter/sec
ZDOT = 9759
996291 ZDOT = 2948
252604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15116295
33 X = -4607446
82
Y = -5948436
08 feet Y = -1813083
32 meter
Z = -15223987
45 Z = -4640271
38
XDOT = -1004
085932 XDOT = -306
045392
YDOT = -22100
675669 feet/sec YDOT = -6736
285944 meter/sec
ZDOT = 9643
704468 ZDOT = 2939
401122
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 16084
15182610
00016717 00000-0 10270-3 0 9123
2 25544 51
6391 122
1409 0001893 345
8721 14
2379 15
54272361 31755
Satellite: ISS
Catalog Number: 25544
Epoch time: 16084
15182610 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 122
1409 deg
Eccentricity:
0001893
Arg of perigee: 345
8721 deg
Mean anomaly: 14
2379 deg
Mean motion: 15
54272361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3175
Checksum: 292
Coasting Arc #14 (Orbit 3175)
---------------------------------------
Vector Time (GMT): 2016/084/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2159635
48 A = 6787644
05 meter
Y = -6197368
77 meter E =
0012746
Z = 1711211
37 I = 51
96755
XDOT = 5104
529415 Wp = 109
37392
YDOT = 190
847592 meter/sec RA = 120
98033 deg
ZDOT = -5720
513456 TA = 51
94369
MA = 51
82875
Ha = 220
682 n
mi
Hp = 214
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7085418
25 X = 2220463
15
Y = -20332574
70 feet Y = -6172877
91 meter
Z = 5614210
52 Z = 1721851
08
XDOT = 16747
143751 XDOT = 5129
803759
YDOT = 626
140393 feet/sec YDOT = 248
070239 meter/sec
ZDOT = -18768
088767 ZDOT = -5695
655547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15765799
54 X = 4805415
70
Y = 14646625
34 feet Y = 4464291
40 meter
Z = 5661451
79 Z = 1725610
50
XDOT = -6302
389955 XDOT = -1920
968458
YDOT = 14035
107846 feet/sec YDOT = 4277
900871 meter/sec
ZDOT = -18660
104020 ZDOT = -5687
599705
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 16084
21612197
00016717 00000-0 10270-3 0 9139
2 25544 51
6389 121
8197 0001878 342
7111 17
3978 15
54274614 31767
Satellite: ISS
Catalog Number: 25544
Epoch time: 16084
21612197 = yrday
fracday
Element set: 913
Inclination: 51
6389 deg
RA of node: 121
8197 deg
Eccentricity:
0001878
Arg of perigee: 342
7111 deg
Mean anomaly: 17
3978 deg
Mean motion: 15
54274614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3176
Checksum: 320
Coasting Arc #15 (Orbit 3190)
---------------------------------------
Vector Time (GMT): 2016/085/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2989829
79 A = 6788855
86 meter
Y = 6087283
08 meter E =
0013145
Z = 19101
54 I = 51
98821
XDOT = -4229
491425 Wp = 39
26345
YDOT = -2103
391361 meter/sec RA = 116
03229 deg
ZDOT = 6043
275168 TA = 320
94138
MA = 321
03622
Ha = 220
723 n
mi
Hp = 214
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9809152
86 X = -3057769
88
Y = 19971401
17 feet Y = 6053468
94 meter
Z = 62669
10 Z = 4411
70
XDOT = -13876
284204 XDOT = -4235
012198
YDOT = -6900
890292 feet/sec YDOT = -2150
718304 meter/sec
ZDOT = 19827
018267 ZDOT = 6022
716177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14613929
02 X = -4454325
57
Y = -16778359
44 feet Y = -5114043
96 meter
Z = -2167
61 Z = -660
69
XDOT = 10560
483389 XDOT = 3218
835337
YDOT = -9173
103324 feet/sec YDOT = -2795
961893 meter/sec
ZDOT = 19738
025120 ZDOT = 6016
150057
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 16085
18055971
00016717 00000-0 10270-3 0 9148
2 25544 51
6397 117
0114 0001767 348
0499 12
0611 15
54291452 31919
Satellite: ISS
Catalog Number: 25544
Epoch time: 16085
18055971 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 117
0114 deg
Eccentricity:
0001767
Arg of perigee: 348
0499 deg
Mean anomaly: 12
0611 deg
Mean motion: 15
54291452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3191
Checksum: 301
Coasting Arc #16 (Orbit 3206)
---------------------------------------
Vector Time (GMT): 2016/086/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3603012
23 A = 6787460
03 meter
Y = -5465964
71 meter E =
0005901
Z = -1785922
51 I = 51
99700
XDOT = 3231
812157 Wp = 132
92285
YDOT = 3985
654174 meter/sec RA = 111
08430 deg
ZDOT = -5694
169646 TA = 66
58872
MA = 66
52668
Ha = 220
729 n
mi
Hp = 214
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11820906
26 X = 3672541
52
Y = -17932955
09 feet Y = -5425284
92 meter
Z = -5859325
84 Z = -1768250
23
XDOT = 10603
058258 XDOT = 3214
663402
YDOT = 13076
293223 feet/sec YDOT = 4021
697774 meter/sec
ZDOT = -18681
658944 ZDOT = -5678
512411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12247271
54 X = 3732968
36
Y = 17670134
52 feet Y = 5385857
00 meter
Z = -5781616
39 Z = -1762236
68
XDOT = -14833
205540 XDOT = -4521
161049
YDOT = 4207
594707 feet/sec YDOT = 1282
474867 meter/sec
ZDOT = -18614
281858 ZDOT = -5673
633110
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 16086
20928279
00016717 00000-0 10270-3 0 9153
2 25544 51
6397 111
8814 0001886 350
8231 9
2887 15
54317162 32073
Satellite: ISS
Catalog Number: 25544
Epoch time: 16086
20928279 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 111
8814 deg
Eccentricity:
0001886
Arg of perigee: 350
8231 deg
Mean anomaly: 9
2887 deg
Mean motion: 15
54317162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3207
Checksum: 320
Coasting Arc #17 (Orbit 3222)
---------------------------------------
Vector Time (GMT): 2016/087/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 918408
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3970993
70 A = 6784058
87 meter
Y = 4368914
74 meter E =
0012603
Z = 3328704
18 I = 51
99794
XDOT = -2216
338439 Wp = 80
00222
YDOT = -5624
190388 meter/sec RA = 106
13051 deg
ZDOT = 4724
722458 TA = 318
55312
MA = 318
64865
Ha = 220
779 n
mi
Hp = 214
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13028194
56 X = -4035722
40
Y = 14333709
77 feet Y = 4324146
94 meter
Z = 10920945
48 Z = 3309256
17
XDOT = -7271
451573 XDOT = -2176
233476
YDOT = -18452
068201 feet/sec YDOT = -5648
750129 meter/sec
ZDOT = 15501
057932 ZDOT = 4714
054065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8744932
89 X = -2665455
55
Y = -17336958
79 feet Y = -5284305
04 meter
Z = 10835688
63 Z = 3302717
89
XDOT = 18601
501095 XDOT = 5669
737534
YDOT = 303
984761 feet/sec YDOT = 92
654555 meter/sec
ZDOT = 15455
644752 ZDOT = 4710
880520
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 16087
23799420
00016717 00000-0 10270-3 0 9162
2 25544 51
6411 106
7518 0001823 353
2612 6
8516 15
54349423 32230
Satellite: ISS
Catalog Number: 25544
Epoch time: 16087
23799420 = yrday
fracday
Element set: 916
Inclination: 51
6411 deg
RA of node: 106
7518 deg
Eccentricity:
0001823
Arg of perigee: 353
2612 deg
Mean anomaly: 6
8516 deg
Mean motion: 15
54349423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3223
Checksum: 296
Coasting Arc #18 (Orbit 3237)
---------------------------------------
Vector Time (GMT): 2016/088/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 918408
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4171847
90 A = 6780174
49 meter
Y = -2852909
96 meter E =
0010340
Z = -4530167
70 I = 51
99240
XDOT = 1202
505516 Wp = 59
79685
YDOT = 6850
867219 meter/sec RA = 101
16729 deg
ZDOT = -3207
391187 TA = 178
10142
MA = 178
09749
Ha = 220
793 n
mi
Hp = 214
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13687165
04 X = 4225445
58
Y = -9359940
83 feet Y = -2805958
41 meter
Z = -14862754
92 Z = -4509771
24
XDOT = 3945
228071 XDOT = 1141
388297
YDOT = 22476
598486 feet/sec YDOT = 6863
972354 meter/sec
ZDOT = -10522
936965 ZDOT = -3201
698873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4131187
44 X = 1259185
93
Y = 16140689
36 feet Y = 4919682
12 meter
Z = -14773621
77 Z = -4502999
91
XDOT = -21327
293039 XDOT = -6500
558918
YDOT = -4150
225893 feet/sec YDOT = -1264
988852 meter/sec
ZDOT = -10499
371346 ZDOT = -3200
208386
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 16088
20240437
00016717 00000-0 10270-3 0 9170
2 25544 51
6408 101
9436 0001872 358
6642 1
4505 15
54325465 32383
Satellite: ISS
Catalog Number: 25544
Epoch time: 16088
20240437 = yrday
fracday
Element set: 917
Inclination: 51
6408 deg
RA of node: 101
9436 deg
Eccentricity:
0001872
Arg of perigee: 358
6642 deg
Mean anomaly: 1
4505 deg
Mean motion: 15
54325465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3238
Checksum: 297
Coasting Arc #19 (Orbit 3253)
---------------------------------------
Vector Time (GMT): 2016/089/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 918408
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4206477
28 A = 6777205
25 meter
Y = 1057478
91 meter E =
0003583
Z = 5204558
10 I = 51
98913
XDOT = -235
781141 Wp = 99
81103
YDOT = -7549
649156 meter/sec RA = 96
19350 deg
ZDOT = 1342
019470 TA = 337
35302
MA = 337
36882
Ha = 220
864 n
mi
Hp = 214
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13800778
48 X = -4243271
32
Y = 3469418
99 feet Y = 1010234
07 meter
Z = 17075321
86 Z = 5184034
47
XDOT = -773
560174 XDOT = -157
860562
YDOT = -24769
190143 feet/sec YDOT = -7551
850006 meter/sec
ZDOT = 4402
951017 ZDOT = 1341
064097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1207718
18 X = 368112
50
Y = -14285808
84 feet Y = -4354314
53 meter
Z = 16985936
95 Z = 5177313
58
XDOT = 22658
625122 XDOT = 6906
348937
YDOT = 7152
718807 feet/sec YDOT = 2180
148693 meter/sec
ZDOT = 4400
109345 ZDOT = 1341
153328
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 16089
23109627
00016717 00000-0 10270-3 0 9180
2 25544 51
6416 96
8138 0001869 359
2725
8424 15
54381022 32540
Satellite: ISS
Catalog Number: 25544
Epoch time: 16089
23109627 = yrday
fracday
Element set: 918
Inclination: 51
6416 deg
RA of node: 96
8138 deg
Eccentricity:
0001869
Arg of perigee: 359
2725 deg
Mean anomaly:
8424 deg
Mean motion: 15
54381022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3254
Checksum: 314
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