[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 4th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 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
048/10:50:37
738 1
4 2
6 2
7
N/A -2
1 -0
3 222
4
000/00:07:15
477 0
7 0
1 213
2
Coasting Arc #1 (Orbit 2402)
---------------------------------------
Vector Time (GMT): 2016/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 842779
74 A = 6776633
64 meter
Y = -4127520
65 meter E =
0021248
Z = -5326362
88 I = 51
68337
XDOT = 7533
569228 Wp = 84
93740
YDOT = 1338
956180 meter/sec RA = 9
15018 deg
ZDOT = 156
802013 TA = 186
54504
MA = 186
57284
Ha = 222
989 n
mi
Hp = 211
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2765025
39 X = 914744
93
Y = -13541734
41 feet Y = -4117693
77 meter
Z = -17474943
82 Z = -5322094
10
XDOT = 24716
434475 XDOT = 7517
275113
YDOT = 4392
900854 feet/sec YDOT = 1423
110437 meter/sec
ZDOT = 514
442300 ZDOT = 193
358189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11957903
13 X = 3644768
87
Y = -6979170
97 feet Y = -2127251
31 meter
Z = -17455581
42 Z = -5320461
22
XDOT = 12860
209892 XDOT = 3919
791975
YDOT = 20371
320432 feet/sec YDOT = 6209
178468 meter/sec
ZDOT = 672
678475 ZDOT = 205
032399
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 16034
51575389
00016717 00000-0 10270-3 0 9004
2 25544 51
6406 9
6333 0006675 71
5828 288
6050 15
54383520 24037
Satellite: ISS
Catalog Number: 25544
Epoch time: 16034
51575389 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 9
6333 deg
Eccentricity:
0006675
Arg of perigee: 71
5828 deg
Mean anomaly: 288
6050 deg
Mean motion: 15
54383520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2403
Checksum: 305
Coasting Arc #2 (Orbit 2418)
---------------------------------------
Vector Time (GMT): 2016/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2724488
26 A = 6778133
07 meter
Y = 3729777
72 meter E =
0012914
Z = 4952346
36 I = 51
65696
XDOT = -7016
256766 Wp = 65
73034
YDOT = -2230
414296 meter/sec RA = 4
15020 deg
ZDOT = -2170
478735 TA = 45
45603
MA = 45
35063
Ha = 223
014 n
mi
Hp = 211
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8938609
76 X = -2790049
07
Y = 12236803
56 feet Y = 3698944
11 meter
Z = 16247855
50 Z = 4938952
44
XDOT = -23019
215112 XDOT = -6980
251168
YDOT = -7317
632205 feet/sec YDOT = -2308
673406 meter/sec
ZDOT = -7120
993224 ZDOT = -2204
474001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15109978
83 X = -4605521
55
Y = 1798738
64 feet Y = 548255
54 meter
Z = 16189008
41 Z = 4934409
76
XDOT = -10278
720159 XDOT = -3132
953905
YDOT = -20645
620685 feet/sec YDOT = -6292
785185 meter/sec
ZDOT = -7267
936437 ZDOT = -2215
267026
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 16035
54440032
00016717 00000-0 10270-3 0 9015
2 25544 51
6406 4
5028 0006610 74
5711 285
6171 15
54417214 24191
Satellite: ISS
Catalog Number: 25544
Epoch time: 16035
54440032 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 4
5028 deg
Eccentricity:
0006610
Arg of perigee: 74
5711 deg
Mean anomaly: 285
6171 deg
Mean motion: 15
54417214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2419
Checksum: 270
Coasting Arc #3 (Orbit 2433)
---------------------------------------
Vector Time (GMT): 2016/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4373440
17 A = 6781689
57 meter
Y = -3262204
70 meter E =
0013145
Z = -4039499
47 I = 51
63706
XDOT = 5852
933192 Wp = 92
58535
YDOT = 3012
494584 meter/sec RA = 359
15582 deg
ZDOT = 3914
406837 TA = 218
04927
MA = 218
14218
Ha = 222
981 n
mi
Hp = 211
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14348557
00 X = 4429215
70
Y = -10702771
34 feet Y = -3212986
14 meter
Z = -13252951
00 Z = -4018119
31
XDOT = 19202
536718 XDOT = 5799
797580
YDOT = 9883
512416 feet/sec YDOT = 3077
648864 meter/sec
ZDOT = 12842
542115 ZDOT = 3942
709342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17737961
09 X = 5406530
54
Y = 2874271
25 feet Y = 876077
88 meter
Z = -13159574
99 Z = -4011038
46
XDOT = 6465
147047 XDOT = 1970
576820
YDOT = 19301
147220 feet/sec YDOT = 5882
989673 meter/sec
ZDOT = 12964
637650 ZDOT = 3951
621556
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 16036
50874544
00016717 00000-0 10270-3 0 9022
2 25544 51
6409 359
6930 0006642 77
6831 282
5065 15
54412841 24348
Satellite: ISS
Catalog Number: 25544
Epoch time: 16036
50874544 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 359
6930 deg
Eccentricity:
0006642
Arg of perigee: 77
6831 deg
Mean anomaly: 282
5065 deg
Mean motion: 15
54412841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2434
Checksum: 314
Coasting Arc #4 (Orbit 2449)
---------------------------------------
Vector Time (GMT): 2016/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5666857
94 A = 6785588
31 meter
Y = 2652823
66 meter E =
0019941
Z = 2605271
44 I = 51
61911
XDOT = -4175
257841 Wp = 95
82946
YDOT = -3743
559250 meter/sec RA = 354
17019 deg
ZDOT = -5237
433731 TA = 54
80703
MA = 54
62045
Ha = 222
954 n
mi
Hp = 211
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18592053
60 X = -5708756
31
Y = 8703489
70 feet Y = 2589218
86 meter
Z = 8547478
49 Z = 2577642
08
XDOT = -13698
352497 XDOT = -4107
645484
YDOT = -12282
018536 feet/sec YDOT = -3789
871763 meter/sec
ZDOT = -17183
181531 ZDOT = -5257
551386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19366817
46 X = -5903005
96
Y = -6955884
28 feet Y = -2120153
53 meter
Z = 8427136
78 Z = 2568591
29
XDOT = -1499
686993 XDOT = -457
104595
YDOT = -16877
889043 feet/sec YDOT = -5144
380580 meter/sec
ZDOT = -17269
637808 ZDOT = -5263
785604
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 16037
53736857
00016717 00000-0 10270-3 0 9031
2 25544 51
6415 354
5621 0006635 81
2684 278
9220 15
54453981 24505
Satellite: ISS
Catalog Number: 25544
Epoch time: 16037
53736857 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 354
5621 deg
Eccentricity:
0006635
Arg of perigee: 81
2684 deg
Mean anomaly: 278
9220 deg
Mean motion: 15
54453981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2450
Checksum: 320
Coasting Arc #5 (Orbit 2464)
---------------------------------------
Vector Time (GMT): 2016/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6428036
76 A = 6788003
63 meter
Y = -1965526
24 meter E =
0015441
Z = -915050
29 I = 51
59588
XDOT = 2165
920920 Wp = 56
66819
YDOT = 4364
562534 meter/sec RA = 349
19271 deg
ZDOT = 5920
563812 TA = 293
42030
MA = 293
58259
Ha = 222
904 n
mi
Hp = 211
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21089359
47 X = 6453982
83
Y = -6448576
90 feet Y = -1893498
63 meter
Z = -3002133
48 Z = -883762
18
XDOT = 7106
039764 XDOT = 2088
195486
YDOT = 14319
430886 feet/sec YDOT = 4388
348878 meter/sec
ZDOT = 19424
421957 ZDOT = 5930
896150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19699584
20 X = 6004433
26
Y = 9953392
66 feet Y = 3033794
08 meter
Z = -2866075
58 Z = -873579
84
XDOT = -4146
255902 XDOT = -1263
778799
YDOT = 13732
441327 feet/sec YDOT = 4185
648116 meter/sec
ZDOT = 19468
326560 ZDOT = 5933
945935
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 16038
50169127
00016717 00000-0 10270-3 0 9040
2 25544 51
6417 349
7525 0006609 85
1123 275
0784 15
54471680 24653
Satellite: ISS
Catalog Number: 25544
Epoch time: 16038
50169127 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 349
7525 deg
Eccentricity:
0006609
Arg of perigee: 85
1123 deg
Mean anomaly: 275
0784 deg
Mean motion: 15
54471680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2465
Checksum: 317
Coasting Arc #6 (Orbit 2480)
---------------------------------------
Vector Time (GMT): 2016/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6628609
77 A = 6787863
57 meter
Y = 1091482
56 meter E =
0014690
Z = -948438
56 I = 51
56562
XDOT = 30
818502 Wp = 119
96107
YDOT = -4883
011366 meter/sec RA = 344
21670 deg
ZDOT = -5910
681434 TA = 70
31927
MA = 70
16083
Ha = 222
801 n
mi
Hp = 211
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21747407
37 X = -6635715
36
Y = 3580979
54 feet Y = 1017317
28 meter
Z = -3111675
06 Z = -980655
17
XDOT = 101
110572 XDOT = 114
130062
YDOT = -16020
378499 feet/sec YDOT = -4882
201206 meter/sec
ZDOT = -19391
999454 ZDOT = -5910
329137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18372773
15 X = -5600021
26
Y = -12137715
77 feet Y = -3699575
77 meter
Z = -3251572
89 Z = -991079
42
XDOT = 10168
306427 XDOT = 3099
299799
YDOT = -10261
217544 feet/sec YDOT = -3127
619108 meter/sec
ZDOT = -19389
479519 ZDOT = -5909
913358
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 16039
53029063
00016717 00000-0 10270-3 0 9059
2 25544 51
6429 344
6216 0006563 88
4410 271
7495 15
54487977 24817
Satellite: ISS
Catalog Number: 25544
Epoch time: 16039
53029063 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 344
6216 deg
Eccentricity:
0006563
Arg of perigee: 88
4410 deg
Mean anomaly: 271
7495 deg
Mean motion: 15
54487977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2481
Checksum: 330
Coasting Arc #7 (Orbit 2496)
---------------------------------------
Vector Time (GMT): 2016/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6239153
89 A = 6785175
65 meter
Y = -119510
07 meter E =
0019957
Z = 2642898
40 I = 51
52635
XDOT = -2117
754494 Wp = 82
24095
YDOT = 5226
431430 meter/sec RA = 339
23485 deg
ZDOT = 5204
708677 TA = 307
63572
MA = 307
81666
Ha = 222
733 n
mi
Hp = 211
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20469665
00 X = 6227188
83
Y = -392093
42 feet Y = -49806
43 meter
Z = 8670926
52 Z = 2673176
85
XDOT = -6948
013432 XDOT = -2201
321959
YDOT = 17147
084743 feet/sec YDOT = 5202
282409 meter/sec
ZDOT = 17075
815868 ZDOT = 5194
218070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15473285
67 X = 4716257
47
Y = 13320821
96 feet Y = 4060186
53 meter
Z = 8802216
88 Z = 2682915
71
XDOT = -15723
205650 XDOT = -4792
433082
YDOT = 6944
811687 feet/sec YDOT = 2116
778602 meter/sec
ZDOT = 17029
281678 ZDOT = 5190
525056
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 16040
55887757
00016717 00000-0 10270-3 0 9066
2 25544 51
6429 339
4916 0006549 92
3471 267
8431 15
54508297 24973
Satellite: ISS
Catalog Number: 25544
Epoch time: 16040
55887757 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 339
4916 deg
Eccentricity:
0006549
Arg of perigee: 92
3471 deg
Mean anomaly: 267
8431 deg
Mean motion: 15
54508297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2497
Checksum: 353
Coasting Arc #8 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2016/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5329407
09 A = 6780986
32 meter
Y = -1031283
72 meter E =
0013705
Z = -4077111
06 I = 51
48358
XDOT = 3960
940843 Wp = 81
88605
YDOT = -5308
467982 meter/sec RA = 334
23975 deg
ZDOT = -3844
012844 TA = 148
24867
MA = 148
16595
Ha = 222
730 n
mi
Hp = 211
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17484931
40 X = -5297674
51
Y = -3383476
78 feet Y = -1090703
61 meter
Z = -13376348
64 Z = -4102922
26
XDOT = 12995
212739 XDOT = 4038
679215
YDOT = -17416
233538 feet/sec YDOT = -5263
739789 meter/sec
ZDOT = -12611
590695 ZDOT = -3824
582730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10949985
55 X = -3337555
59
Y = -13938012
15 feet Y = -4248306
10 meter
Z = -13488034
61 Z = -4111152
95
XDOT = 20265
930683 XDOT = 6177
055672
YDOT = -3828
419755 feet/sec YDOT = -1166
902341 meter/sec
ZDOT = -12526
297881 ZDOT = -3818
015594
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 16041
52316668
00016717 00000-0 10270-3 0 9073
2 25544 51
6434 334
6814 0006565 95
2654 264
9248 15
54537067 25125
Satellite: ISS
Catalog Number: 25544
Epoch time: 16041
52316668 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 334
6814 deg
Eccentricity:
0006565
Arg of perigee: 95
2654 deg
Mean anomaly: 264
9248 deg
Mean motion: 15
54537067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 322
Coasting Arc #9 (Orbit 2527)
---------------------------------------
Vector Time (GMT): 2016/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4017539
32 A = 6777390
78 meter
Y = 2224063
44 meter E =
0012101
Z = 4976132
77 I = 51
44322
XDOT = -5365
437715 Wp = 110
91248
YDOT = 5093
371851 meter/sec RA = 329
23174 deg
ZDOT = 2047
118497 TA = 319
10188
MA = 319
19261
Ha = 222
520 n
mi
Hp = 211
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13180903
28 X = 3968199
22
Y = 7296796
06 feet Y = 2268714
83 meter
Z = 16325894
91 Z = 4995528
57
XDOT = -17603
142109 XDOT = -5431
938134
YDOT = 16710
537568 feet/sec YDOT = 5033
000338 meter/sec
ZDOT = 6716
268035 ZDOT = 2020
893004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5361583
52 X = 1634210
66
Y = 13981955
62 feet Y = 4261700
07 meter
Z = 16409528
57 Z = 5001624
31
XDOT = -23235
825073 XDOT = -7082
279482
YDOT = 1130
689080 feet/sec YDOT = 344
634032 meter/sec
ZDOT = 6601
574756 ZDOT = 2012
159986
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 16042
55172874
00016717 00000-0 10270-3 0 9087
2 25544 51
6432 329
5513 0006429 100
1652 260
0227 15
54573659 25283
Satellite: ISS
Catalog Number: 25544
Epoch time: 16042
55172874 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 329
5513 deg
Eccentricity:
0006429
Arg of perigee: 100
1652 deg
Mean anomaly: 260
0227 deg
Mean motion: 15
54573659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2528
Checksum: 304
Coasting Arc #10 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2016/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2454303
22 A = 6776096
72 meter
Y = -3451815
41 meter E =
0021273
Z = -5307733
79 I = 51
41184
XDOT = 6219
357753 Wp = 93
77296
YDOT = -4460
301266 meter/sec RA = 324
21246 deg
ZDOT = 23
570623 TA = 176
46033
MA = 176
44526
Ha = 222
668 n
mi
Hp = 211
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8052175
93 X = -2389739
43
Y = -11324853
72 feet Y = -3478900
57 meter
Z = -17413824
78 Z = -5319498
87
XDOT = 20404
717039 XDOT = 6268
657217
YDOT = -14633
534336 feet/sec YDOT = -4390
476630 meter/sec
ZDOT = 77
331441 ZDOT = 53
902448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 925037
00 X = 281951
28
Y = -13801425
12 feet Y = -4206674
38 meter
Z = -17464137
92 Z = -5323069
24
XDOT = 24062
845520 XDOT = 7334
355315
YDOT = 1342
138500 feet/sec YDOT = 409
083815 meter/sec
ZDOT = 209
685139 ZDOT = 63
912030
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 16043
51599686
00016717 00000-0 10270-3 0 9099
2 25544 51
6434 324
7406 0006496 102
6211 257
5668 15
54563478 25430
Satellite: ISS
Catalog Number: 25544
Epoch time: 16043
51599686 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 324
7406 deg
Eccentricity:
0006496
Arg of perigee: 102
6211 deg
Mean anomaly: 257
5668 deg
Mean motion: 15
54563478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 333
Coasting Arc #11 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2016/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 795280
08 A = 6777490
85 meter
Y = 4542951
75 meter E =
0011526
Z = 4956898
46 I = 51
39092
XDOT = -6537
805166 Wp = 81
53963
YDOT = 3435
639039 meter/sec RA = 319
19231 deg
ZDOT = -2093
973384 TA = 28
92274
MA = 28
85892
Ha = 222
541 n
mi
Hp = 211
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2609186
60 X = 720342
34
Y = 14904697
33 feet Y = 4551426
52 meter
Z = 16262790
22 Z = 4960579
29
XDOT = -21449
492015 XDOT = -6565
565920
YDOT = 11271
781625 feet/sec YDOT = 3362
373567 meter/sec
ZDOT = -6869
991416 ZDOT = -2125
799772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7175707
35 X = -2187155
60
Y = 13303270
69 feet Y = 4054836
91 meter
Z = 16277850
47 Z = 4961488
82
XDOT = -22845
343747 XDOT = -6963
260774
YDOT = -3723
509682 feet/sec YDOT = -1134
925751 meter/sec
ZDOT = -7008
610064 ZDOT = -2136
224348
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 16044
54453601
00016717 00000-0 10270-3 0 9101
2 25544 51
6429 319
6100 0006415 106
0754 254
1105 15
54596732 25594
Satellite: ISS
Catalog Number: 25544
Epoch time: 16044
54453601 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 319
6100 deg
Eccentricity:
0006415
Arg of perigee: 106
0754 deg
Mean anomaly: 254
1105 deg
Mean motion: 15
54596732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 289
Coasting Arc #12 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2016/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 771095
48 A = 6781100
19 meter
Y = -5410994
29 meter E =
0013467
Z = -4027974
98 I = 51
37993
XDOT = 6281
937557 Wp = 108
39053
YDOT = -1999
601577 meter/sec RA = 314
17731 deg
ZDOT = 3895
331655 TA = 202
20489
MA = 202
26327
Ha = 222
557 n
mi
Hp = 211
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2529840
80 X = 851111
22
Y = -17752605
95 feet Y = -5401924
28 meter
Z = -13215141
02 Z = -4024034
51
XDOT = 20610
031356 XDOT = 6284
909053
YDOT = -6560
372627 feet/sec YDOT = -1929
335896 meter/sec
ZDOT = 12779
959497 ZDOT = 3925
854790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12749524
90 X = 3886055
19
Y = -12628688
49 feet Y = -3849224
25 meter
Z = -13197003
70 Z = -4022446
73
XDOT = 19433
559733 XDOT = 5923
349007
YDOT = 6148
353993 feet/sec YDOT = 1874
018297 meter/sec
ZDOT = 12912
640536 ZDOT = 3935
772835
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 16045
50878124
00016717 00000-0 10270-3 0 9110
2 25544 51
6434 314
7991 0006449 109
6706 250
5143 15
54603248 25747
Satellite: ISS
Catalog Number: 25544
Epoch time: 16045
50878124 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 314
7991 deg
Eccentricity:
0006449
Arg of perigee: 109
6706 deg
Mean anomaly: 250
5143 deg
Mean motion: 15
54603248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 311
Coasting Arc #13 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2016/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2165938
36 A = 6785237
33 meter
Y = 5889832
12 meter E =
0020097
Z = 2554504
39 I = 51
37179
XDOT = -5596
747564 Wp = 106
85128
YDOT = 230
210457 meter/sec RA = 309
17325 deg
ZDOT = -5247
683479 TA = 44
29259
MA = 44
13194
Ha = 222
560 n
mi
Hp = 211
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7106096
98 X = -2244047
49
Y = 19323596
21 feet Y = 5865174
57 meter
Z = 8380919
91 Z = 2543792
88
XDOT = -18362
032690 XDOT = -5573
415159
YDOT = 755
283652 feet/sec YDOT = 167
754084 meter/sec
ZDOT = -17216
809314 ZDOT = -5274
814127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17132844
53 X = -5222091
01
Y = 11452455
07 feet Y = 3490708
31 meter
Z = 8333349
53 Z = 2540004
94
XDOT = -14389
326285 XDOT = -4385
866652
YDOT = -8844
537964 feet/sec YDOT = -2695
815171 meter/sec
ZDOT = -17334
438509 ZDOT = -5283
536857
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 16046
53729831
00016717 00000-0 10270-3 0 9125
2 25544 51
6432 309
6677 0006488 113
9082 246
2751 15
54595591 25903
Satellite: ISS
Catalog Number: 25544
Epoch time: 16046
53729831 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 309
6677 deg
Eccentricity:
0006488
Arg of perigee: 113
9082 deg
Mean anomaly: 246
2751 deg
Mean motion: 15
54595591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 332
Coasting Arc #14 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2016/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3233509
35 A = 6787577
09 meter
Y = -5910541
57 meter E =
0013227
Z = -807162
63 I = 51
36124
XDOT = 4564
817274 Wp = 67
25273
YDOT = 1700
274480 meter/sec RA = 304
17778 deg
ZDOT = 5918
977324 TA = 283
98743
MA = 284
13448
Ha = 222
411 n
mi
Hp = 211
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10608626
47 X = 3303282
96
Y = -19391540
59 feet Y = -5873992
24 meter
Z = -2648171
36 Z = -791285
52
XDOT = 14976
434626 XDOT = 4516
713656
YDOT = 5578
328346 feet/sec YDOT = 1751
052597 meter/sec
ZDOT = 19419
216943 ZDOT = 5941
034857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19813442
31 X = 6039137
21
Y = -9816716
17 feet Y = -2992135
09 meter
Z = -2578216
73 Z = -785840
46
XDOT = 8266
521546 XDOT = 2519
635767
YDOT = 11632
613845 feet/sec YDOT = 3545
620700 meter/sec
ZDOT = 19514
485549 ZDOT = 5948
015195
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 16047
50152080
00016717 00000-0 10270-3 0 9130
2 25544 51
6438 304
8570 0006322 117
1588 243
0210 15
54639099 26056
Satellite: ISS
Catalog Number: 25544
Epoch time: 16047
50152080 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 304
8570 deg
Eccentricity:
0006322
Arg of perigee: 117
1588 deg
Mean anomaly: 243
0210 deg
Mean motion: 15
54639099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 290
Coasting Arc #15 (Orbit 2619)
---------------------------------------
Vector Time (GMT): 2016/048/10:54:15
477
Vector Time (MET): N/A
Weight (LBS) : 922210
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1852763
02 A = 6779643
84 meter
Y = -4475548
61 meter E =
0015318
Z = -4758267
82 I = 51
31333
XDOT = 5209
089572 Wp = 113
84843
YDOT = -4954
659554 meter/sec RA = 299
38195 deg
ZDOT = 2632
636993 TA = 182
28574
MA = 182
29275
Ha = 222
360 n
mi
Hp = 213
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6078618
83 X = -1779465
39
Y = -14683558
44 feet Y = -4495857
81 meter
Z = -15611114
90 Z = -4767089
71
XDOT = 17090
188886 XDOT = 5251
318648
YDOT = -16255
444732 feet/sec YDOT = -4896
171832 meter/sec
ZDOT = 8637
260475 ZDOT = 2658
043803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7508843
59 X = 2288695
52
Y = -13964433
72 feet Y = -4256359
40 meter
Z = -15648490
75 Z = -4769659
98
XDOT = 22363
331275 XDOT = 6816
343373
YDOT = 2224
143051 feet/sec YDOT = 677
918802 meter/sec
ZDOT = 8748
325795 ZDOT = 2666
489702
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 16048
46573412
00016717 00000-0 10270-3 0 9143
2 25544 51
6437 300
0452 0004318 128
2497 231
9045 15
54152217 26208
Satellite: ISS
Catalog Number: 25544
Epoch time: 16048
46573412 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 300
0452 deg
Eccentricity:
0004318
Arg of perigee: 128
2497 deg
Mean anomaly: 231
9045 deg
Mean motion: 15
54152217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2620
Checksum: 285
Coasting Arc #16 (Orbit 2635)
---------------------------------------
Vector Time (GMT): 2016/049/10:54:15
477
Vector Time (MET): N/A
Weight (LBS) : 922210
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 753804
44 A = 6783270
66 meter
Y = 5598073
84 meter E =
0014890
Z = 3741580
22 I = 51
31028
XDOT = -5327
894829 Wp = 96
08701
YDOT = 3552
968762 meter/sec RA = 294
36891 deg
ZDOT = -4229
508612 TA = 38
88153
MA = 38
77452
Ha = 222
283 n
mi
Hp = 213
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2473111
69 X = 672974
75
Y = 18366383
98 feet Y = 5606051
61 meter
Z = 12275525
65 Z = 3745045
35
XDOT = -17479
969912 XDOT = -5346
684309
YDOT = 11656
721661 feet/sec YDOT = 3493
283451 meter/sec
ZDOT = -13876
340589 ZDOT = -4255
435473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12395752
34 X = -3778225
31
Y = 13763824
35 feet Y = 4195213
66 meter
Z = 12289480
66 Z = 3745833
71
XDOT = -19160
011958 XDOT = -5839
971645
YDOT = -4726
734180 feet/sec YDOT = -1440
708578 meter/sec
ZDOT = -13989
386175 ZDOT = -4263
964906
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 16049
49454609
00016717 00000-0 10270-3 0 9154
2 25544 51
6433 294
9164 0004346 131
6802 228
4723 15
54162829 26365
Satellite: ISS
Catalog Number: 25544
Epoch time: 16049
49454609 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 294
9164 deg
Eccentricity:
0004346
Arg of perigee: 131
6802 deg
Mean anomaly: 228
4723 deg
Mean motion: 15
54162829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 323
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