[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 21st 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 ET - UTC (sec) : 68 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
217/02:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 212
7
Coasting Arc #1 (Orbit 1015)
---------------------------------------
Vector Time (GMT): 2016/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2226869
66 A = 6787354
07 meter
Y = -6404861
95 meter E =
0013900
Z = -8595
91 I = 51
30901
XDOT = 4529
175644 Wp = 47
21215
YDOT = -1574
469750 meter/sec RA = 250
88641 deg
ZDOT = 5987
111106 TA = 312
69479
MA = 312
81178
Ha = 220
516 n
mi
Hp = 213
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7306002
81 X = -2155041
62
Y = -21013326
60 feet Y = -6429362
67 meter
Z = -28201
80 Z = -19239
36
XDOT = 14859
500145 XDOT = 4517
362921
YDOT = -5165
583169 feet/sec YDOT = -1523
888045 meter/sec
ZDOT = 19642
752973 ZDOT = 6009
083447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15167612
41 X = -4623088
26
Y = 16275027
16 feet Y = 4960628
28 meter
Z = -73429
42 Z = -22381
29
XDOT = -10260
482026 XDOT = -3127
394921
YDOT = -9508
373138 feet/sec YDOT = -2898
152133 meter/sec
ZDOT = 19738
790621 ZDOT = 6016
383381
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 16202
50004597
00016717 00000-0 10270-3 0 9008
2 25544 51
6405 251
8313 0001866 58
1247 302
0088 15
54808031 10168
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
50004597 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 251
8313 deg
Eccentricity:
0001866
Arg of perigee: 58
1247 deg
Mean anomaly: 302
0088 deg
Mean motion: 15
54808031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1016
Checksum: 270
Coasting Arc #2 (Orbit 1031)
---------------------------------------
Vector Time (GMT): 2016/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1171151
85 A = 6785598
36 meter
Y = 6397819
82 meter E =
0007695
Z = -1929020
93 I = 51
31570
XDOT = -5212
691129 Wp = 127
31834
YDOT = -720
576254 meter/sec RA = 245
88901 deg
ZDOT = -5574
557648 TA = 74
04370
MA = 73
95894
Ha = 220
471 n
mi
Hp = 212
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3842361
72 X = 1108892
93
Y = 20990222
52 feet Y = 6410568
44 meter
Z = -6328808
83 Z = -1923482
67
XDOT = -17102
005018 XDOT = -5177
167820
YDOT = -2364
095320 feet/sec YDOT = -778
669049 meter/sec
ZDOT = -18289
231130 ZDOT = -5599
792835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16515129
47 X = 5033811
46
Y = -13523840
96 feet Y = -4122066
72 meter
Z = -6305809
27 Z = -1922010
66
XDOT = 5131
426121 XDOT = 1564
058682
YDOT = 14814
815931 feet/sec YDOT = 4515
555896 meter/sec
ZDOT = -18399
084710 ZDOT = -5608
041020
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 16203
52839707
00016717 00000-0 10270-3 0 9011
2 25544 51
6410 246
6989 0001865 66
2452 293
8897 15
54871509 10325
Satellite: ISS
Catalog Number: 25544
Epoch time: 16203
52839707 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 246
6989 deg
Eccentricity:
0001865
Arg of perigee: 66
2452 deg
Mean anomaly: 293
8897 deg
Mean motion: 15
54871509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1032
Checksum: 330
Coasting Arc #3 (Orbit 1047)
---------------------------------------
Vector Time (GMT): 2016/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 63429
94 A = 6781786
35 meter
Y = -5758842
56 meter E =
0013919
Z = 3568934
84 I = 51
31634
XDOT = 5611
931598 Wp = 89
64381
YDOT = 2808
171586 meter/sec RA = 240
88358 deg
ZDOT = 4416
667651 TA = 312
79450
MA = 312
91146
Ha = 220
526 n
mi
Hp = 212
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 208103
47 X = 110486
06
Y = -18893840
41 feet Y = -5757870
31 meter
Z = 11709103
80 Z = 3569356
97
XDOT = 18411
849074 XDOT = 5558
659000
YDOT = 9213
161371 feet/sec YDOT = 2870
629874 meter/sec
ZDOT = 14490
379432 ZDOT = 4443
799197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16457496
07 X = -5016244
80
Y = 9279256
68 feet Y = 2828317
44 meter
Z = 11711952
99 Z = 3569803
27
XDOT = -437
040117 XDOT = -133
209828
YDOT = -19274
554862 feet/sec YDOT = -5874
884322 meter/sec
ZDOT = 14608
142807 ZDOT = 4452
561928
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 16204
55674254
00016717 00000-0 10270-3 0 9020
2 25544 51
6405 241
5669 0002015 68
2966 291
8401 15
54861853 10485
Satellite: ISS
Catalog Number: 25544
Epoch time: 16204
55674254 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 241
5669 deg
Eccentricity:
0002015
Arg of perigee: 68
2966 deg
Mean anomaly: 291
8401 deg
Mean motion: 15
54861853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1048
Checksum: 309
Coasting Arc #4 (Orbit 1062)
---------------------------------------
Vector Time (GMT): 2016/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1473731
78 A = 6777569
38 meter
Y = 4611398
46 meter E =
0013064
Z = -4755791
15 I = 51
31954
XDOT = -5604
008742 Wp = 71
67124
YDOT = -4506
698292 meter/sec RA = 235
86598 deg
ZDOT = -2635
233198 TA = 172
18695
MA = 172
16658
Ha = 220
501 n
mi
Hp = 212
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4835078
02 X = -1502086
91
Y = 15129260
05 feet Y = 4594759
81 meter
Z = -15602989
34 Z = -4763018
77
XDOT = -18385
855454 XDOT = -5540
396613
YDOT = -14785
755552 feet/sec YDOT = -4569
010301 meter/sec
ZDOT = -8645
778208 ZDOT = -2662
301209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15418104
52 X = 4699438
26
Y = -3680419
75 feet Y = -1121791
94 meter
Z = -15635291
14 Z = -4765636
74
XDOT = -3582
657874 XDOT = -1091
994120
YDOT = 22191
640777 feet/sec YDOT = 6764
012109 meter/sec
ZDOT = -8762
985956 ZDOT = -2670
958119
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 16205
52081238
00016717 00000-0 10270-3 0 9033
2 25544 51
6413 236
7559 0001889 72
1523 287
9836 15
54866774 10631
Satellite: ISS
Catalog Number: 25544
Epoch time: 16205
52081238 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 236
7559 deg
Eccentricity:
0001889
Arg of perigee: 72
1523 deg
Mean anomaly: 287
9836 deg
Mean motion: 15
54866774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1063
Checksum: 328
Coasting Arc #5 (Orbit 1078)
---------------------------------------
Vector Time (GMT): 2016/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2905509
09 A = 6775236
46 meter
Y = -3109003
71 meter E =
0004574
Z = 5268286
45 I = 51
32976
XDOT = 5144
180252 Wp = 96
92396
YDOT = 5671
261222 meter/sec RA = 230
83869 deg
ZDOT = 508
827708 TA = 348
19875
MA = 348
20947
Ha = 220
420 n
mi
Hp = 212
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9532510
15 X = 2914468
13
Y = -10200143
40 feet Y = -3076462
38 meter
Z = 17284404
35 Z = 5282422
17
XDOT = 16877
231799 XDOT = 5077
908825
YDOT = 18606
500072 feet/sec YDOT = 5728
416325 meter/sec
ZDOT = 1669
382243 ZDOT = 533
655628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13631421
84 X = -4154857
38
Y = -2635078
45 feet Y = -803171
91 meter
Z = 17346556
12 Z = 5287230
30
XDOT = 6738
611959 XDOT = 2053
928925
YDOT = -23143
869739 feet/sec YDOT = -7054
251496 meter/sec
ZDOT = 1776
643262 ZDOT = 541
520866
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 16206
54914947
00016717 00000-0 10270-3 0 9049
2 25544 51
6402 231
6238 0002024 74
4266 285
7110 15
54885870 10794
Satellite: ISS
Catalog Number: 25544
Epoch time: 16206
54914947 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 231
6238 deg
Eccentricity:
0002024
Arg of perigee: 74
4266 deg
Mean anomaly: 285
7110 deg
Mean motion: 15
54885870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1079
Checksum: 307
Coasting Arc #6 (Orbit 1093)
---------------------------------------
Vector Time (GMT): 2016/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4252702
43 A = 6776120
07 meter
Y = 1456867
05 meter E =
0015096
Z = -5083852
48 I = 51
35558
XDOT = -4149
095998 Wp = 99
40568
YDOT = -6210
237079 meter/sec RA = 225
81069 deg
ZDOT = 1693
005860 TA = 187
02589
MA = 187
04708
Ha = 220
491 n
mi
Hp = 212
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13952435
81 X = -4243982
53
Y = 4779747
54 feet Y = 1409359
34 meter
Z = -16679306
03 Z = -5104489
61
XDOT = -13612
519678 XDOT = -4087
566994
YDOT = -20374
793567 feet/sec YDOT = -6256
291042 meter/sec
ZDOT = 5554
481169 ZDOT = 1673
000144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11511960
00 X = 3508845
41
Y = 9053930
40 feet Y = 2759637
98 meter
Z = -16769520
64 Z = -5111349
89
XDOT = -9082
542335 XDOT = -2768
358904
YDOT = 21665
227476 feet/sec YDOT = 6603
561335 meter/sec
ZDOT = 5468
316789 ZDOT = 1666
742957
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 16207
51321055
00016717 00000-0 10270-3 0 9050
2 25544 51
6421 226
8129 0001871 73
2044 286
9314 15
54869253 10943
Satellite: ISS
Catalog Number: 25544
Epoch time: 16207
51321055 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 226
8129 deg
Eccentricity:
0001871
Arg of perigee: 73
2044 deg
Mean anomaly: 286
9314 deg
Mean motion: 15
54869253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1094
Checksum: 297
Coasting Arc #7 (Orbit 1109)
---------------------------------------
Vector Time (GMT): 2016/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5330369
39 A = 6779493
31 meter
Y = 194093
14 meter E =
0012183
Z = 4176538
08 I = 51
38881
XDOT = 2667
332131 Wp = 74
96723
YDOT = 6182
914832 meter/sec RA = 220
79141 deg
ZDOT = -3679
464377 TA = 52
94249
MA = 52
83114
Ha = 220
364 n
mi
Hp = 212
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17488088
56 X = 5307515
17
Y = 636788
51 feet Y = 253572
99 meter
Z = 13702552
76 Z = 4202375
98
XDOT = 8751
089668 XDOT = 2615
868089
YDOT = 20285
153648 feet/sec YDOT = 6212
455066 meter/sec
ZDOT = -12071
733520 ZDOT = -3666
632080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9138508
37 X = -2785417
35
Y = -14819832
13 feet Y = -4517084
83 meter
Z = 13815170
42 Z = 4210863
94
XDOT = 10876
618716 XDOT = 3315
193385
YDOT = -17945
829136 feet/sec YDOT = -5469
888721 meter/sec
ZDOT = -12016
825010 ZDOT = -3662
728263
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 16208
54153786
00016717 00000-0 10270-3 0 9069
2 25544 51
6403 221
6810 0002044 75
7708 284
3672 15
54920230 11101
Satellite: ISS
Catalog Number: 25544
Epoch time: 16208
54153786 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 221
6810 deg
Eccentricity:
0002044
Arg of perigee: 75
7708 deg
Mean anomaly: 284
3672 deg
Mean motion: 15
54920230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1110
Checksum: 284
Coasting Arc #8 (Orbit 1124)
---------------------------------------
Vector Time (GMT): 2016/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5992519
40 A = 6783808
79 meter
Y = -1641876
33 meter E =
0006698
Z = -2724123
67 I = 51
42824
XDOT = -790
823996 Wp = 65
50004
YDOT = -5627
068567 meter/sec RA = 215
78758 deg
ZDOT = 5143
891320 TA = 263
59724
MA = 263
67352
Ha = 220
461 n
mi
Hp = 212
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19660496
73 X = -5960481
62
Y = -5386733
38 feet Y = -1708709
44 meter
Z = -8937413
61 Z = -2753155
90
XDOT = -2594
566917 XDOT = -752
828569
YDOT = -18461
511045 feet/sec YDOT = -5635
699862 meter/sec
ZDOT = 16876
283859 ZDOT = 5140
141765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6745085
61 X = 2055902
09
Y = 19177643
94 feet Y = 5845345
87 meter
Z = -9063728
99 Z = -2762624
60
XDOT = -12229
113950 XDOT = -3727
433932
YDOT = 12250
524935 feet/sec YDOT = 3733
960000 meter/sec
ZDOT = 16860
875013 ZDOT = 5139
194704
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 16209
50559217
00016717 00000-0 10270-3 0 9076
2 25544 51
6404 216
8707 0002029 80
9058 279
2325 15
54912491 11256
Satellite: ISS
Catalog Number: 25544
Epoch time: 16209
50559217 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 216
8707 deg
Eccentricity:
0002029
Arg of perigee: 80
9058 deg
Mean anomaly: 279
2325 deg
Mean motion: 15
54912491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1125
Checksum: 306
Coasting Arc #9 (Orbit 1140)
---------------------------------------
Vector Time (GMT): 2016/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6096810
02 A = 6786707
29 meter
Y = 2840436
32 meter E =
0014998
Z = 855732
65 I = 51
46371
XDOT = -1343
619554 Wp = 120
20576
YDOT = 4688
866999 meter/sec RA = 210
79622 deg
ZDOT = -5920
647828 TA = 50
50899
MA = 50
37645
Ha = 220
503 n
mi
Hp = 212
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20002657
53 X = 6060437
66
Y = 9319016
81 feet Y = 2908411
50 meter
Z = 2807521
82 Z = 885261
05
XDOT = -4408
200635 XDOT = -1367
192038
YDOT = 15383
421912 feet/sec YDOT = 4673
710300 meter/sec
ZDOT = -19424
697598 ZDOT = -5927
231723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4105265
17 X = -1251284
82
Y = -21664725
58 feet Y = -6603408
36 meter
Z = 2935817
55 Z = 894837
19
XDOT = 13407
451877 XDOT = 4086
591332
YDOT = -5206
734425 feet/sec YDOT = -1587
012653 meter/sec
ZDOT = -19454
189157 ZDOT = -5929
636855
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 16210
53391131
00016717 00000-0 10270-3 0 9081
2 25544 51
6395 211
7379 0002069 80
8710 279
2677 15
54914806 11412
Satellite: ISS
Catalog Number: 25544
Epoch time: 16210
53391131 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 211
7379 deg
Eccentricity:
0002069
Arg of perigee: 80
8710 deg
Mean anomaly: 279
2677 deg
Mean motion: 15
54914806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1141
Checksum: 307
Coasting Arc #10 (Orbit 1156)
---------------------------------------
Vector Time (GMT): 2016/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5593621
00 A = 6786443
08 meter
Y = -3671548
11 meter E =
0015278
Z = 1092874
06 I = 51
49041
XDOT = 3465
255029 Wp = 60
79336
YDOT = -3514
924307 meter/sec RA = 205
81240 deg
ZDOT = 5872
852103 TA = 311
09499
MA = 311
22683
Ha = 220
400 n
mi
Hp = 212
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18351774
92 X = -5557457
75
Y = -12045761
53 feet Y = -3733897
59 meter
Z = 3585544
80 Z = 1065789
48
XDOT = 11368
946944 XDOT = 3475
774756
YDOT = -11531
903894 feet/sec YDOT = -3476
115114 meter/sec
ZDOT = 19267
887477 ZDOT = 5889
710577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1329748
91 X = 405307
47
Y = 21930542
83 feet Y = 6684429
45 meter
Z = 3468025
96 Z = 1057054
31
XDOT = -14365
822426 XDOT = -4378
702675
YDOT = -2216
977882 feet/sec YDOT = -675
734858 meter/sec
ZDOT = 19341
997002 ZDOT = 5895
440686
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 16211
56222321
00016717 00000-0 10270-3 0 9090
2 25544 51
6386 206
6066 0001932 89
1438 270
9937 15
54960078 11571
Satellite: ISS
Catalog Number: 25544
Epoch time: 16211
56222321 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 206
6066 deg
Eccentricity:
0001932
Arg of perigee: 89
1438 deg
Mean anomaly: 270
9937 deg
Mean motion: 15
54960078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1157
Checksum: 315
Coasting Arc #11 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2016/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4456179
66 A = 6783462
85 meter
Y = 4191127
31 meter E =
0006427
Z = -2934149
51 I = 51
50847
XDOT = -5368
347806 Wp = 106
85524
YDOT = 2213
704244 meter/sec RA = 200
82364 deg
ZDOT = -5001
935553 TA = 106
68548
MA = 106
61491
Ha = 220
522 n
mi
Hp = 212
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14620011
99 X = 4423234
85
Y = 13750417
69 feet Y = 4240775
30 meter
Z = -9626474
76 Z = -2912582
50
XDOT = -17612
689653 XDOT = -5368
406113
YDOT = 7262
809199 feet/sec YDOT = 2153
671845 meter/sec
ZDOT = -16410
549715 ZDOT = -5028
013257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1899768
54 X = 579049
45
Y = -20024955
47 feet Y = -6103606
43 meter
Z = -9533089
28 Z = -2905685
61
XDOT = 14991
010579 XDOT = 4569
260024
YDOT = 9271
726714 feet/sec YDOT = 2826
022303 meter/sec
ZDOT = -16524
667755 ZDOT = -5036
718732
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 16212
52626612
00016717 00000-0 10270-3 0 9100
2 25544 51
6377 201
7944 0002013 86
2273 273
9110 15
54913715 11727
Satellite: ISS
Catalog Number: 25544
Epoch time: 16212
52626612 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 201
7944 deg
Eccentricity:
0002013
Arg of perigee: 86
2273 deg
Mean anomaly: 273
9110 deg
Mean motion: 15
54913715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1172
Checksum: 281
Coasting Arc #12 (Orbit 1187)
---------------------------------------
Vector Time (GMT): 2016/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2814196
13 A = 6779021
68 meter
Y = -4378813
84 meter E =
0011453
Z = 4335289
83 I = 51
52475
XDOT = 6787
944672 Wp = 105
55510
YDOT = -930
558709 meter/sec RA = 195
82549 deg
ZDOT = 3455
781342 TA = 309
27743
MA = 309
37896
Ha = 220
427 n
mi
Hp = 212
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9232926
92 X = -2786080
56
Y = -14366187
14 feet Y = -4410127
16 meter
Z = 14223391
83 Z = 4321687
40
XDOT = 22270
159685 XDOT = 6781
059530
YDOT = -3053
014137 feet/sec YDOT = -854
690118 meter/sec
ZDOT = 11337
865294 ZDOT = 3488
738097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5384056
05 X = -1641060
28
Y = 16257628
61 feet Y = 4955325
20 meter
Z = 14164766
14 Z = 4317420
72
XDOT = -15071
226139 XDOT = -4593
709727
YDOT = -15025
378297 feet/sec YDOT = -4579
735305 meter/sec
ZDOT = 11481
799866 ZDOT = 3499
652599
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 16213
55456991
00016717 00000-0 10270-3 0 9116
2 25544 51
6381 196
6626 0001803 89
9570 270
1790 15
54949260 11881
Satellite: ISS
Catalog Number: 25544
Epoch time: 16213
55456991 = yrday
fracday
Element set: 911
Inclination: 51
6381 deg
RA of node: 196
6626 deg
Eccentricity:
0001803
Arg of perigee: 89
9570 deg
Mean anomaly: 270
1790 deg
Mean motion: 15
54949260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1188
Checksum: 331
Coasting Arc #13 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2016/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 794324
80 A = 6775735
75 meter
Y = 4328526
81 meter E =
0015724
Z = -5166003
24 I = 51
54506
XDOT = -7521
452450 Wp = 80
69973
YDOT = -298
581496 meter/sec RA = 190
81513 deg
ZDOT = -1407
856100 TA = 175
72924
MA = 175
71581
Ha = 220
465 n
mi
Hp = 212
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2606052
48 X = 770956
76
Y = 14201203
45 feet Y = 4337279
12 meter
Z = -16948829
52 Z = -5162201
20
XDOT = -24676
681266 XDOT = -7510
716018
YDOT = -979
598084 feet/sec YDOT = -382
631288 meter/sec
ZDOT = -4618
950460 ZDOT = -1444
366594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9195769
58 X = 2802870
57
Y = -11155344
26 feet Y = -3400148
93 meter
Z = -16932945
03 Z = -5161161
65
XDOT = 14166
727377 XDOT = 4318
018504
YDOT = 18925
238912 feet/sec YDOT = 5768
412820 meter/sec
ZDOT = -4778
211955 ZDOT = -1456
399004
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 16214
51860147
00016717 00000-0 10270-3 0 9126
2 25544 51
6383 191
8503 0001976 89
5281 270
6099 15
54927452 12034
Satellite: ISS
Catalog Number: 25544
Epoch time: 16214
51860147 = yrday
fracday
Element set: 912
Inclination: 51
6383 deg
RA of node: 191
8503 deg
Eccentricity:
0001976
Arg of perigee: 89
5281 deg
Mean anomaly: 270
6099 deg
Mean motion: 15
54927452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1203
Checksum: 314
Coasting Arc #14 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2016/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1351051
83 A = 6775200
81 meter
Y = -4052766
53 meter E =
0004882
Z = 5254746
49 I = 51
57509
XDOT = 7495
083190 Wp = 73
28441
YDOT = 1422
034871 meter/sec RA = 185
80183 deg
ZDOT = -828
298023 TA = 24
64671
MA = 24
62339
Ha = 220
370 n
mi
Hp = 212
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4432584
73 X = 1370745
77
Y = -13296478
10 feet Y = -4037548
26 meter
Z = 17239981
92 Z = 5261357
08
XDOT = 24590
167945 XDOT = 7482
648011
YDOT = 4665
468738 feet/sec YDOT = 1505
780402 meter/sec
ZDOT = -2717
513200 ZDOT = -791
919780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12900931
27 X = -3932203
85
Y = 5384414
60 feet Y = 1641169
57 meter
Z = 17269486
56 Z = 5263739
50
XDOT = -12101
342327 XDOT = -3688
489141
YDOT = -20765
927510 feet/sec YDOT = -6329
454705 meter/sec
ZDOT = -2558
987536 ZDOT = -779
979401
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 16215
54689694
00016717 00000-0 10270-3 0 9137
2 25544 51
6381 186
7183 0001864 92
8133 267
3234 15
54934398 12196
Satellite: ISS
Catalog Number: 25544
Epoch time: 16215
54689694 = yrday
fracday
Element set: 913
Inclination: 51
6381 deg
RA of node: 186
7183 deg
Eccentricity:
0001864
Arg of perigee: 92
8133 deg
Mean anomaly: 267
3234 deg
Mean motion: 15
54934398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1219
Checksum: 337
Coasting Arc #15 (Orbit 1233)
---------------------------------------
Vector Time (GMT): 2016/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3381835
42 A = 6777808
56 meter
Y = 3624335
75 meter E =
0012290
Z = -4634306
96 I = 51
61706
XDOT = -6639
131224 Wp = 107
95545
YDOT = -2427
966678 meter/sec RA = 180
79415 deg
ZDOT = 2948
741483 TA = 191
44472
MA = 191
47269
Ha = 220
396 n
mi
Hp = 212
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11095260
58 X = -3399601
39
Y = 11890865
31 feet Y = 3586418
56 meter
Z = -15204419
15 Z = -4650777
75
XDOT = -21781
926589 XDOT = -6625
811032
YDOT = -7965
769940 feet/sec YDOT = -2502
135460 meter/sec
ZDOT = 9674
348696 ZDOT = 2916
523313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16192220
06 X = 4935388
67
Y = 316989
62 feet Y = 96618
44 meter
Z = -15276890
19 Z = -4656396
13
XDOT = 8586
669327 XDOT = 2617
216811
YDOT = 20435
556694 feet/sec YDOT = 6228
757680 meter/sec
ZDOT = 9534
119535 ZDOT = 2905
999634
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 16216
51091880
00016717 00000-0 10270-3 0 9140
2 25544 51
6391 181
9069 0001841 94
9322 265
2042 15
54933418 12348
Satellite: ISS
Catalog Number: 25544
Epoch time: 16216
51091880 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 181
9069 deg
Eccentricity:
0001841
Arg of perigee: 94
9322 deg
Mean anomaly: 265
2042 deg
Mean motion: 15
54933418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1234
Checksum: 302
Coasting Arc #16 (Orbit 1243)
---------------------------------------
Vector Time (GMT): 2016/217/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3088695
53 A = 6777192
48 meter
Y = -3670671
56 meter E =
0009405
Z = 4781720
55 I = 51
63832
XDOT = 6828
009874 Wp = 117
54631
YDOT = -2328
965942 meter/sec RA = 177
83487 deg
ZDOT = 2614
452267 TA = 306
65532
MA = 306
74174
Ha = 220
371 n
mi
Hp = 212
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10133515
52 X = -3070646
60
Y = -12042885
70 feet Y = -3705110
54 meter
Z = 15688059
54 Z = 4766760
59
XDOT = 22401
607197 XDOT = 6840
845903
YDOT = -7640
964375 feet/sec YDOT = -2252
538822 meter/sec
ZDOT = 8577
599301 ZDOT = 2647
651420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7625354
82 X = -2324208
15
Y = -13841942
98 feet Y = -4219024
22 meter
Z = 15623348
66 Z = 4761996
67
XDOT = 22411
642934 XDOT = 6831
068766
YDOT = -2470
331677 feet/sec YDOT = -752
957095 meter/sec
ZDOT = 8722
883746 ZDOT = 2658
734966
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 16217
15359589
00016717 00000-0 10270-3 0 9155
2 25544 51
6428 178
6961 0001846 112
4868 247
6480 15
54987152 12444
Satellite: ISS
Catalog Number: 25544
Epoch time: 16217
15359589 = yrday
fracday
Element set: 915
Inclination: 51
6428 deg
RA of node: 178
6961 deg
Eccentricity:
0001846
Arg of perigee: 112
4868 deg
Mean anomaly: 247
6480 deg
Mean motion: 15
54987152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1244
Checksum: 343
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