[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 19th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3569)
---------------------------------------
Vector Time (GMT): 2016/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 299695
30 A = 6776841
72 meter
Y = 4197677
41 meter E =
0003646
Z = 5308942
74 I = 51
59859
XDOT = -7647
704583 Wp = 65
64791
YDOT = 606
212268 meter/sec RA = 355
19488 deg
ZDOT = -46
102685 TA = 24
80021
MA = 24
78269
Ha = 221
113 n
mi
Hp = 214
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 983252
29 X = 226944
81
Y = 13771907
53 feet Y = 4200622
57 meter
Z = 17417791
15 Z = 5310221
47
XDOT = -25090
894301 XDOT = -7653
691056
YDOT = 1988
885394 feet/sec YDOT = 520
657069 meter/sec
ZDOT = -151
255528 ZDOT = -83
268179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6859463
09 X = 2090764
35
Y = 11975620
02 feet Y = 3650168
98 meter
Z = 17422513
07 Z = 5310381
98
XDOT = -20763
842499 XDOT = -6328
819194
YDOT = 12355
489829 feet/sec YDOT = 3765
953300 meter/sec
ZDOT = -312
831499 ZDOT = -95
351041
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 16109
54808289
00016717 00000-0 10270-3 0 9008
2 25544 51
6452 355
5140 0001582 35
9564 324
1695 15
54301648 35708
Satellite: ISS
Catalog Number: 25544
Epoch time: 16109
54808289 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 355
5140 deg
Eccentricity:
0001582
Arg of perigee: 35
9564 deg
Mean anomaly: 324
1695 deg
Mean motion: 15
54301648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3570
Checksum: 310
Coasting Arc #2 (Orbit 3584)
---------------------------------------
Vector Time (GMT): 2016/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1556925
35 A = 6778240
87 meter
Y = -4304338
53 meter E =
0013438
Z = -5011413
14 I = 51
57082
XDOT = 7383
308784 Wp = 97
97102
YDOT = 338
526452 meter/sec RA = 350
19061 deg
ZDOT = 2005
846932 TA = 191
54595
MA = 191
57681
Ha = 221
162 n
mi
Hp = 214
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5108022
80 X = 1629285
37
Y = -14121845
57 feet Y = -4286523
86 meter
Z = -16441644
17 Z = -5003673
73
XDOT = 24223
454015 XDOT = 7369
230908
YDOT = 1110
651090 feet/sec YDOT = 421
013008 meter/sec
ZDOT = 6580
862637 ZDOT = 2041
679342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1810749
74 X = -551916
52
Y = -14945634
86 feet Y = -4555429
50 meter
Z = -16407171
18 Z = -5000905
78
XDOT = 20930
031860 XDOT = 6379
473711
YDOT = -9920
916798 feet/sec YDOT = -3023
895440 meter/sec
ZDOT = 6736
447032 ZDOT = 2053
269055
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 16110
51251979
00016717 00000-0 10270-3 0 9016
2 25544 51
6447 350
7055 0001708 37
8022 322
3250 15
54303054 35850
Satellite: ISS
Catalog Number: 25544
Epoch time: 16110
51251979 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 350
7055 deg
Eccentricity:
0001708
Arg of perigee: 37
8022 deg
Mean anomaly: 322
3250 deg
Mean motion: 15
54303054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3585
Checksum: 280
Coasting Arc #3 (Orbit 3600)
---------------------------------------
Vector Time (GMT): 2016/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3270282
63 A = 6781520
71 meter
Y = 4259807
27 meter E =
0011927
Z = 4134028
95 I = 51
54999
XDOT = -6545
189813 Wp = 70
78656
YDOT = -1360
342205 meter/sec RA = 345
19149 deg
ZDOT = -3763
214697 TA = 58
05448
MA = 57
93856
Ha = 221
177 n
mi
Hp = 213
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10729273
70 X = -3337755
41
Y = 13975745
65 feet Y = 4222859
91 meter
Z = 13563087
11 Z = 4117978
24
XDOT = -21473
719859 XDOT = -6511
211341
YDOT = -4463
064976 feet/sec YDOT = -1433
345232 meter/sec
ZDOT = -12346
504911 ZDOT = -3794
927374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2941159
30 X = -896465
36
Y = 17426917
38 feet Y = 5311724
42 meter
Z = 13492525
53 Z = 4112521
78
XDOT = -19698
037181 XDOT = -6003
961733
YDOT = 6373
553313 feet/sec YDOT = 1942
659050 meter/sec
ZDOT = -12483
979857 ZDOT = -3805
117060
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 16111
54124134
00016717 00000-0 10270-3 0 9023
2 25544 51
6440 345
5768 0001763 38
1276 322
0001 15
54344890 36015
Satellite: ISS
Catalog Number: 25544
Epoch time: 16111
54124134 = yrday
fracday
Element set: 902
Inclination: 51
6440 deg
RA of node: 345
5768 deg
Eccentricity:
0001763
Arg of perigee: 38
1276 deg
Mean anomaly: 322
0001 deg
Mean motion: 15
54344890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3601
Checksum: 272
Coasting Arc #4 (Orbit 3615)
---------------------------------------
Vector Time (GMT): 2016/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4648320
75 A = 6785484
18 meter
Y = -4057378
65 meter E =
0006288
Z = -2823029
25 I = 51
53189
XDOT = 5197
123317 Wp = 53
88162
YDOT = 2423
580799 meter/sec RA = 340
20028 deg
ZDOT = 5085
718035 TA = 274
01863
MA = 274
09051
Ha = 221
164 n
mi
Hp = 214
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15250396
18 X = 4707059
19
Y = -13311609
76 feet Y = -4005069
84 meter
Z = -9261906
99 Z = -2800305
50
XDOT = 17050
929518 XDOT = 5144
931323
YDOT = 7951
380575 feet/sec YDOT = 2481
407073 meter/sec
ZDOT = 16685
426625 ZDOT = 5110
837819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6889162
93 X = 2099816
86
Y = -19082614
19 feet Y = -5816380
80 meter
Z = -9162408
46 Z = -2792702
10
XDOT = 17279
855624 XDOT = 5266
899994
YDOT = -1806
830781 feet/sec YDOT = -550
722022 meter/sec
ZDOT = 16794
046081 ZDOT = 5118
825245
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 16112
50565980
00016717 00000-0 10270-3 0 9039
2 25544 51
6437 340
7681 0001640 38
4789 321
6480 15
54312224 36166
Satellite: ISS
Catalog Number: 25544
Epoch time: 16112
50565980 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 340
7681 deg
Eccentricity:
0001640
Arg of perigee: 38
4789 deg
Mean anomaly: 321
6480 deg
Mean motion: 15
54312224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3616
Checksum: 299
Coasting Arc #5 (Orbit 3631)
---------------------------------------
Vector Time (GMT): 2016/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5624318
05 A = 6788246
72 meter
Y = 3609587
65 meter E =
0014154
Z = 1156419
97 I = 51
51150
XDOT = -3476
718299 Wp = 115
70884
YDOT = -3524
659301 meter/sec RA = 335
21652 deg
ZDOT = -5857
617047 TA = 51
70931
MA = 51
58209
Ha = 221
191 n
mi
Hp = 213
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18452487
03 X = -5669880
84
Y = 11842479
17 feet Y = 3546438
10 meter
Z = 3794028
76 Z = 1128987
02
XDOT = -11406
556099 XDOT = -3408
591960
YDOT = -11563
842850 feet/sec YDOT = -3563
157739 meter/sec
ZDOT = -19217
903698 ZDOT = -5874
340692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10036588
88 X = -3059152
29
Y = 19516674
26 feet Y = 5948682
32 meter
Z = 3674173
91 Z = 1119888
21
XDOT = -14140
353536 XDOT = -4309
979758
YDOT = -3608
464666 feet/sec YDOT = -1099
860030 meter/sec
ZDOT = -19289
833915 ZDOT = -5879
541377
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 16113
53436167
00016717 00000-0 10270-3 0 9048
2 25544 51
6438 335
6382 0001687 46
6899 313
4394 15
54318716 36325
Satellite: ISS
Catalog Number: 25544
Epoch time: 16113
53436167 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 335
6382 deg
Eccentricity:
0001687
Arg of perigee: 46
6899 deg
Mean anomaly: 313
4394 deg
Mean motion: 15
54318716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3632
Checksum: 327
Coasting Arc #6 (Orbit 3647)
---------------------------------------
Vector Time (GMT): 2016/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6087396
77 A = 6788464
97 meter
Y = -2926283
78 meter E =
0014791
Z = 605358
98 I = 51
48232
XDOT = 1589
185397 Wp = 51
06142
YDOT = 4557
641156 meter/sec RA = 330
23504 deg
ZDOT = 5961
867518 TA = 315
48995
MA = 315
60867
Ha = 221
098 n
mi
Hp = 213
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19971774
17 X = 6116726
14
Y = -9600668
57 feet Y = -2858046
44 meter
Z = 1986085
91 Z = 635002
00
XDOT = 5213
862850 XDOT = 1509
141843
YDOT = 14952
890931 feet/sec YDOT = 4574
965219 meter/sec
ZDOT = 19559
932803 ZDOT = 5969
392899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12126930
65 X = 3696288
46
Y = -18532452
33 feet Y = -5648691
47 meter
Z = 2115396
30 Z = 644772
79
XDOT = 10731
988775 XDOT = 3271
110179
YDOT = 9290
204113 feet/sec YDOT = 2831
654214 meter/sec
ZDOT = 19591
709473 ZDOT = 5971
553048
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 16114
56305163
00016717 00000-0 10270-3 0 9054
2 25544 51
6421 330
5081 0001637 48
1749 311
9544 15
54366537 36484
Satellite: ISS
Catalog Number: 25544
Epoch time: 16114
56305163 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 330
5081 deg
Eccentricity:
0001637
Arg of perigee: 48
1749 deg
Mean anomaly: 311
9544 deg
Mean motion: 15
54366537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3648
Checksum: 302
Coasting Arc #7 (Orbit 3662)
---------------------------------------
Vector Time (GMT): 2016/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6067464
10 A = 6786282
86 meter
Y = 1939785
09 meter E =
0005913
Z = -2339746
53 I = 51
44727
XDOT = 328
528305 Wp = 118
58292
YDOT = -5447
343018 meter/sec RA = 325
24981 deg
ZDOT = -5381
238342 TA = 87
57721
MA = 87
50951
Ha = 221
057 n
mi
Hp = 213
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19906378
28 X = -6077338
61
Y = 6364124
31 feet Y = 1871879
38 meter
Z = -7676333
75 Z = -2369245
37
XDOT = 1077
848770 XDOT = 415
557686
YDOT = -17871
860296 feet/sec YDOT = -5443
182754 meter/sec
ZDOT = -17654
981436 ZDOT = -5379
430845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13440015
23 X = -4096516
64
Y = 15941859
88 feet Y = 4859078
89 meter
Z = -7804816
99 Z = -2378908
22
XDOT = -7325
600337 XDOT = -2232
842983
YDOT = -14794
363752 feet/sec YDOT = -4509
322072 meter/sec
ZDOT = -17646
053464 ZDOT = -5378
517096
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 16115
52744295
00016717 00000-0 10270-3 0 9065
2 25544 51
6417 325
6994 0001515 47
0488 313
0791 15
54349714 36632
Satellite: ISS
Catalog Number: 25544
Epoch time: 16115
52744295 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 325
6994 deg
Eccentricity:
0001515
Arg of perigee: 47
0488 deg
Mean anomaly: 313
0791 deg
Mean motion: 15
54349714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3663
Checksum: 321
Coasting Arc #8 (Orbit 3678)
---------------------------------------
Vector Time (GMT): 2016/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5581001
68 A = 6782471
63 meter
Y = -722999
53 meter E =
0012539
Z = 3775104
99 I = 51
40880
XDOT = -2063
789018 Wp = 91
44603
YDOT = 6078
581359 meter/sec RA = 320
25194 deg
ZDOT = 4202
789717 TA = 314
01161
MA = 314
11489
Ha = 220
977 n
mi
Hp = 213
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18310372
98 X = 5570333
49
Y = -2372045
69 feet Y = -660648
64 meter
Z = 12385515
06 Z = 3802190
69
XDOT = -6770
961344 XDOT = -2152
023557
YDOT = 19942
852227 feet/sec YDOT = 6055
009419 meter/sec
ZDOT = 13788
680175 ZDOT = 4192
549748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13980548
87 X = 4261271
30
Y = -11937743
23 feet Y = -3638624
14 meter
Z = 12503274
88 Z = 3810998
18
XDOT = 4268
767792 XDOT = 1301
120423
YDOT = 19435
554773 feet/sec YDOT = 5923
957095 meter/sec
ZDOT = 13743
012839 ZDOT = 4188
870313
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 16116
55611721
00016717 00000-0 10270-3 0 9077
2 25544 51
6416 320
5683 0001607 47
8988 312
2301 15
54366443 36798
Satellite: ISS
Catalog Number: 25544
Epoch time: 16116
55611721 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 320
5683 deg
Eccentricity:
0001607
Arg of perigee: 47
8988 deg
Mean anomaly: 312
2301 deg
Mean motion: 15
54366443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3679
Checksum: 309
Coasting Arc #9 (Orbit 3693)
---------------------------------------
Vector Time (GMT): 2016/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4736433
20 A = 6778670
36 meter
Y = -715394
09 meter E =
0013235
Z = -4808957
14 I = 51
37047
XDOT = 3513
032862 Wp = 69
85625
YDOT = -6320
649730 meter/sec RA = 315
24161 deg
ZDOT = -2520
966714 TA = 175
22786
MA = 175
21523
Ha = 221
114 n
mi
Hp = 213
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15539479
02 X = -4704721
26
Y = -2347093
46 feet Y = -768182
75 meter
Z = -15777418
44 Z = -4831888
88
XDOT = 11525
698366 XDOT = 3595
696810
YDOT = -20737
039795 feet/sec YDOT = -6280
902475 meter/sec
ZDOT = -8270
888169 ZDOT = -2503
700185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14103601
80 X = -4298777
83
Y = 6702617
40 feet Y = 2042957
78 meter
Z = -15876854
99 Z = -4839265
40
XDOT = -1537
069124 XDOT = -468
498669
YDOT = -22636
239744 feet/sec YDOT = -6899
525874 meter/sec
ZDOT = -8194
666366 ZDOT = -2497
734308
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 16117
52049069
00016717 00000-0 10270-3 0 9086
2 25544 51
6399 315
7587 0001657 56
2439 303
8872 15
54387014 36940
Satellite: ISS
Catalog Number: 25544
Epoch time: 16117
52049069 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 315
7587 deg
Eccentricity:
0001657
Arg of perigee: 56
2439 deg
Mean anomaly: 303
8872 deg
Mean motion: 15
54387014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3694
Checksum: 340
Coasting Arc #10 (Orbit 3709)
---------------------------------------
Vector Time (GMT): 2016/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3627526
16 A = 6776745
42 meter
Y = 2234718
82 meter E =
0003980
Z = 5266426
63 I = 51
34201
XDOT = -4589
100956 Wp = 93
49618
YDOT = 6122
842229 meter/sec RA = 310
22156 deg
ZDOT = 562
252053 TA = 351
11544
MA = 351
12248
Ha = 221
023 n
mi
Hp = 213
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11901332
56 X = 3576685
01
Y = 7331754
64 feet Y = 2274999
97 meter
Z = 17278302
59 Z = 5283924
98
XDOT = -15056
105499 XDOT = -4659
958246
YDOT = 20088
065056 feet/sec YDOT = 6071
127665 meter/sec
ZDOT = 1844
658966 ZDOT = 539
786944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13863238
11 X = 4225514
98
Y = -768544
86 feet Y = -234252
47 meter
Z = 17353848
30 Z = 5289452
96
XDOT = -852
629193 XDOT = -259
881378
YDOT = 24087
616319 feet/sec YDOT = 7341
905454 meter/sec
ZDOT = 1745
908816 ZDOT = 532
153007
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 16118
54914922
00016717 00000-0 10270-3 0 9099
2 25544 51
6402 310
6290 0001594 60
2643 299
8669 15
54366337 37104
Satellite: ISS
Catalog Number: 25544
Epoch time: 16118
54914922 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 310
6290 deg
Eccentricity:
0001594
Arg of perigee: 60
2643 deg
Mean anomaly: 299
8669 deg
Mean motion: 15
54366337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3710
Checksum: 317
Coasting Arc #11 (Orbit 3724)
---------------------------------------
Vector Time (GMT): 2016/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2401031
66 A = 6777261
77 meter
Y = -3730159
92 meter E =
0015043
Z = -5137080
50 I = 51
32386
XDOT = 5238
293998 Wp = 97
55373
YDOT = -5389
558746 meter/sec RA = 305
19623 deg
ZDOT = 1466
915163 TA = 186
64038
MA = 186
66033
Ha = 221
087 n
mi
Hp = 213
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7877400
47 X = -2334187
66
Y = -12238057
49 feet Y = -3756636
13 meter
Z = -16853938
64 Z = -5148581
86
XDOT = 17186
003931 XDOT = 5291
046354
YDOT = -17682
279350 feet/sec YDOT = -5330
685697 meter/sec
ZDOT = 4812
713789 ZDOT = 1492
489885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13483100
43 X = -4109649
01
Y = -5326168
18 feet Y = -1623416
06 meter
Z = -16903155
69 Z = -5152081
85
XDOT = 3079
733929 XDOT = 938
702902
YDOT = -23407
414839 feet/sec YDOT = -7134
580043 meter/sec
ZDOT = 4924
816098 ZDOT = 1501
083947
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 16119
51350644
00016717 00000-0 10270-3 0 9104
2 25544 51
6399 305
8184 0001608 65
8773 294
2548 15
54417483 37258
Satellite: ISS
Catalog Number: 25544
Epoch time: 16119
51350644 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 305
8184 deg
Eccentricity:
0001608
Arg of perigee: 65
8773 deg
Mean anomaly: 294
2548 deg
Mean motion: 15
54417483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3725
Checksum: 326
Coasting Arc #12 (Orbit 3740)
---------------------------------------
Vector Time (GMT): 2016/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1133012
65 A = 6780302
45 meter
Y = 5038676
22 meter E =
0010959
Z = 4386511
85 I = 51
31615
XDOT = -5513
597384 Wp = 69
80192
YDOT = 4158
564860 meter/sec RA = 300
17638 deg
ZDOT = -3342
182669 TA = 54
17013
MA = 54
06837
Ha = 221
047 n
mi
Hp = 213
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3717233
11 X = 1055276
76
Y = 16531089
95 feet Y = 5050911
71 meter
Z = 14391443
06 Z = 4391826
92
XDOT = -18089
230261 XDOT = -5543
454698
YDOT = 13643
585499 feet/sec YDOT = 4096
741173 meter/sec
ZDOT = -10965
166236 ZDOT = -3369
039116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12849145
00 X = 3916419
40
Y = 11016233
84 feet Y = 3357748
08 meter
Z = 14413551
08 Z = 4393250
37
XDOT = -5366
571291 XDOT = -1635
730929
YDOT = 20804
949809 feet/sec YDOT = 6341
348702 meter/sec
ZDOT = -11082
588238 ZDOT = -3377
972895
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 16120
54214564
00016717 00000-0 10270-3 0 9110
2 25544 51
6398 300
6884 0001548 67
8637 292
2680 15
54413741 37417
Satellite: ISS
Catalog Number: 25544
Epoch time: 16120
54214564 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 300
6884 deg
Eccentricity:
0001548
Arg of perigee: 67
8637 deg
Mean anomaly: 292
2680 deg
Mean motion: 15
54413741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3741
Checksum: 311
Coasting Arc #13 (Orbit 3755)
---------------------------------------
Vector Time (GMT): 2016/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 36914
11 A = 6784218
27 meter
Y = -6010338
32 meter E =
0006187
Z = -3150025
37 I = 51
31351
XDOT = 5423
301169 Wp = 76
88861
YDOT = -2483
268736 meter/sec RA = 295
16587 deg
ZDOT = 4811
078635 TA = 246
62076
MA = 246
68585
Ha = 221
098 n
mi
Hp = 213
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 121109
28 X = 119422
04
Y = -19718957
76 feet Y = -6009464
26 meter
Z = -10334728
91 Z = -3149645
53
XDOT = 17792
982839 XDOT = 5427
296312
YDOT = -8147
207139 feet/sec YDOT = -2422
599342 meter/sec
ZDOT = 15784
378725 ZDOT = 4837
433616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11996113
95 X = -3656415
53
Y = -15652572
47 feet Y = -4770904
09 meter
Z = -10331931
53 Z = -3149172
73
XDOT = 7780
796854 XDOT = 2371
586881
YDOT = -16437
669438 feet/sec YDOT = -5010
201645 meter/sec
ZDOT = 15899
295535 ZDOT = 4846
105279
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 16121
50648826
00016717 00000-0 10270-3 0 9120
2 25544 51
6391 295
8790 0001655 77
2120 282
9217 15
54439297 37564
Satellite: ISS
Catalog Number: 25544
Epoch time: 16121
50648826 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 295
8790 deg
Eccentricity:
0001655
Arg of perigee: 77
2120 deg
Mean anomaly: 282
9217 deg
Mean motion: 15
54439297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3756
Checksum: 328
Coasting Arc #14 (Orbit 3771)
---------------------------------------
Vector Time (GMT): 2016/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1109246
35 A = 6787350
92 meter
Y = 6517816
12 meter E =
0014944
Z = 1505548
28 I = 51
31185
XDOT = -5068
623785 Wp = 113
75781
YDOT = 471
943163 meter/sec RA = 290
16554 deg
ZDOT = -5738
210241 TA = 49
71611
MA = 49
58557
Ha = 220
962 n
mi
Hp = 213
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3639259
69 X = -1189361
12
Y = 21383911
15 feet Y = 6504963
89 meter
Z = 4939462
87 Z = 1499965
00
XDOT = -16629
343126 XDOT = -5045
650483
YDOT = 1548
369958 feet/sec YDOT = 415
390711 meter/sec
ZDOT = -18826
149085 ZDOT = -5762
776757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10603812
37 X = 3232042
01
Y = 18929502
39 feet Y = 5769712
33 meter
Z = 4913986
47 Z = 1497783
07
XDOT = -10475
878973 XDOT = -3193
047911
YDOT = 10816
870676 feet/sec YDOT = 3296
982182 meter/sec
ZDOT = -18932
914358 ZDOT = -5770
752296
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 16122
53510951
00016717 00000-0 10270-3 0 9132
2 25544 51
6393 290
7487 0001512 70
5117 289
6199 15
54482876 37729
Satellite: ISS
Catalog Number: 25544
Epoch time: 16122
53510951 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 290
7487 deg
Eccentricity:
0001512
Arg of perigee: 70
5117 deg
Mean anomaly: 289
6199 deg
Mean motion: 15
54482876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3772
Checksum: 325
Coasting Arc #15 (Orbit 3787)
---------------------------------------
Vector Time (GMT): 2016/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1989537
71 A = 6788284
81 meter
Y = -6477562
53 meter E =
0014078
Z = 281034
92 I = 51
30524
XDOT = 4512
405036 Wp = 52
29622
YDOT = 1653
847918 meter/sec RA = 285
17023 deg
ZDOT = 5977
460862 TA = 310
74719
MA = 310
86933
Ha = 221
072 n
mi
Hp = 213
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6527354
69 X = 2060458
40
Y = -21251845
56 feet Y = -6454917
64 meter
Z = 922030
59 Z = 290872
23
XDOT = 14804
478465 XDOT = 4464
539694
YDOT = 5426
010231 feet/sec YDOT = 1704
041252 meter/sec
ZDOT = 19611
092067 ZDOT = 5999
264891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8658633
88 X = -2639151
61
Y = -20474189
17 feet Y = -6240532
86 meter
Z = 965958
85 Z = 294424
26
XDOT = 13241
484432 XDOT = 4036
004455
YDOT = -4641
056915 feet/sec YDOT = -1414
594148 meter/sec
ZDOT = 19705
462476 ZDOT = 6006
224963
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 16123
56372384
00016717 00000-0 10270-3 0 9143
2 25544 51
6398 285
6182 0001724 84
2459 275
8891 15
54476055 37880
Satellite: ISS
Catalog Number: 25544
Epoch time: 16123
56372384 = yrday
fracday
Element set: 914
Inclination: 51
6398 deg
RA of node: 285
6182 deg
Eccentricity:
0001724
Arg of perigee: 84
2459 deg
Mean anomaly: 275
8891 deg
Mean motion: 15
54476055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3788
Checksum: 347
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