[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 29th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 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
062/01:02:30
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
4
065/04:04:36
784 -1
5 3
0 3
0
N/A -2
4 0
3 220
4
000/00:09:13
568 0
9 0
3 216
2
Coasting Arc #1 (Orbit 2807)
---------------------------------------
Vector Time (GMT): 2016/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1645408
50 A = 6779359
28 meter
Y = -4589664
53 meter E =
0009650
Z = 4707604
03 I = 51
30774
XDOT = 5382
595565 Wp = 136
01398
YDOT = 4735
802895 meter/sec RA = 239
07020 deg
ZDOT = 2725
628404 TA = 286
84947
MA = 286
95529
Ha = 220
974 n
mi
Hp = 214
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5398321
84 X = 1673741
60
Y = -15057954
49 feet Y = -4571105
56 meter
Z = 15444895
11 Z = 4715666
27
XDOT = 17659
434268 XDOT = 5315
998750
YDOT = 15537
411073 feet/sec YDOT = 4795
622579 meter/sec
ZDOT = 8942
350407 ZDOT = 2751
613280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10576551
99 X = 3223733
05
Y = -11954739
93 feet Y = -3643804
73 meter
Z = 15480613
63 Z = 4718491
03
XDOT = 9586
851739 XDOT = 2922
072410
YDOT = 20249
478603 feet/sec YDOT = 6172
041078 meter/sec
ZDOT = 9054
212113 ZDOT = 2759
723852
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 16060
55311402
00016717 00000-0 10270-3 0 9001
2 25544 51
6380 239
7789 0003355 184
2963 175
8161 15
54307213 28087
Satellite: ISS
Catalog Number: 25544
Epoch time: 16060
55311402 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 239
7789 deg
Eccentricity:
0003355
Arg of perigee: 184
2963 deg
Mean anomaly: 175
8161 deg
Mean motion: 15
54307213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2808
Checksum: 302
Coasting Arc #2 (Orbit 2822)
---------------------------------------
Vector Time (GMT): 2016/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906097
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2870545
58 A = 6776969
82 meter
Y = 3201661
96 meter E =
0014286
Z = -5250079
61 I = 51
31761
XDOT = -4974
977171 Wp = 97
55410
YDOT = -5767
445149 meter/sec RA = 234
04758 deg
ZDOT = -800
757860 TA = 164
77016
MA = 164
72711
Ha = 220
952 n
mi
Hp = 214
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9417800
45 X = -2880631
56
Y = 10504140
29 feet Y = 3169504
72 meter
Z = -17224670
63 Z = -5264048
71
XDOT = -16322
103578 XDOT = -4906
224709
YDOT = -18922
064137 feet/sec YDOT = -5822
694305 meter/sec
ZDOT = -2627
158332 ZDOT = -824
757340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12466673
82 X = -3799842
18
Y = 6442479
06 feet Y = 1963667
62 meter
Z = -17285766
23 Z = -5268701
55
XDOT = -7919
617640 XDOT = -2413
899457
YDOT = -22617
943380 feet/sec YDOT = -6893
949142 meter/sec
ZDOT = -2730
256286 ZDOT = -832
182116
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 16061
51752129
00016717 00000-0 10270-3 0 9014
2 25544 51
6382 234
9693 0003444 184
3473 175
7651 15
54339926 28232
Satellite: ISS
Catalog Number: 25544
Epoch time: 16061
51752129 = yrday
fracday
Element set: 901
Inclination: 51
6382 deg
RA of node: 234
9693 deg
Eccentricity:
0003444
Arg of perigee: 184
3473 deg
Mean anomaly: 175
7651 deg
Mean motion: 15
54339926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2823
Checksum: 320
Coasting Arc #3 (Orbit 2831)
---------------------------------------
Vector Time (GMT): 2016/062/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 890989
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1198855
82 A = 6778878
26 meter
Y = -4639839
74 meter E =
0008919
Z = 4792218
96 I = 51
33476
XDOT = 5924
825198 Wp = 139
05017
YDOT = 4159
059205 meter/sec RA = 231
34247 deg
ZDOT = 2535
311771 TA = 285
85500
MA = 285
95330
Ha = 220
762 n
mi
Hp = 214
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3933254
01 X = 1227372
20
Y = -15222571
32 feet Y = -4626273
46 meter
Z = 15722503
14 Z = 4798112
33
XDOT = 19438
402882 XDOT = 5865
561866
YDOT = 13645
207365 feet/sec YDOT = 4224
983402 meter/sec
ZDOT = 8317
952004 ZDOT = 2563
948542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5135016
55 X = -1565153
04
Y = 14832413
71 feet Y = 4520919
70 meter
Z = 15748821
49 Z = 4800240
79
XDOT = -17049
329245 XDOT = -5196
635554
YDOT = -14897
853057 feet/sec YDOT = -4540
865612 meter/sec
ZDOT = 8441
431162 ZDOT = 2572
948218
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 16062
09616032
00016717 00000-0 10270-3 0 9021
2 25544 51
6385 232
0867 0003183 190
1071 170
0019 15
54358692 28323
Satellite: ISS
Catalog Number: 25544
Epoch time: 16062
09616032 = yrday
fracday
Element set: 902
Inclination: 51
6385 deg
RA of node: 232
0867 deg
Eccentricity:
0003183
Arg of perigee: 190
1071 deg
Mean anomaly: 170
0019 deg
Mean motion: 15
54358692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2832
Checksum: 288
Coasting Arc #4 (Orbit 2846)
---------------------------------------
Vector Time (GMT): 2016/063/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 890989
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2597087
19 A = 6776842
28 meter
Y = 3388697
33 meter E =
0014108
Z = -5274819
17 I = 51
34872
XDOT = -5600
423338 Wp = 97
60116
YDOT = -5191
749449 meter/sec RA = 226
32032 deg
ZDOT = -581
099347 TA = 166
84194
MA = 166
80510
Ha = 220
735 n
mi
Hp = 214
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8520627
27 X = -2609164
88
Y = 11117773
39 feet Y = 3359587
01 meter
Z = -17305837
18 Z = -5287464
66
XDOT = -18374
092317 XDOT = -5539
128973
YDOT = -17033
298717 feet/sec YDOT = -5254
034432 meter/sec
ZDOT = -1906
493919 ZDOT = -608
155216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9160347
28 X = 2792073
85
Y = -10505894
99 feet Y = -3202196
79 meter
Z = -17361226
42 Z = -5291701
81
XDOT = 16369
153865 XDOT = 4989
318098
YDOT = 17598
539993 feet/sec YDOT = 5364
034990 meter/sec
ZDOT = -2022
967053 ZDOT = -616
600358
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 16063
06055218
00016717 00000-0 10270-3 0 9033
2 25544 51
6386 227
2763 0003075 191
9980 168
1100 15
54348334 28470
Satellite: ISS
Catalog Number: 25544
Epoch time: 16063
06055218 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 227
2763 deg
Eccentricity:
0003075
Arg of perigee: 191
9980 deg
Mean anomaly: 168
1100 deg
Mean motion: 15
54348334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2847
Checksum: 307
Coasting Arc #5 (Orbit 2862)
---------------------------------------
Vector Time (GMT): 2016/064/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 890989
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3930184
10 A = 6777299
01 meter
Y = -2012998
92 meter E =
0002805
Z = 5138845
69 I = 51
37346
XDOT = 4837
747455 Wp = 96
16079
YDOT = 5777
537126 meter/sec RA = 221
29872 deg
ZDOT = -1436
335578 TA = 7
70847
MA = 7
70416
Ha = 220
487 n
mi
Hp = 214
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12894304
80 X = 3927439
88
Y = -6604327
15 feet Y = -1969063
91 meter
Z = 16859729
94 Z = 5157930
79
XDOT = 15871
874851 XDOT = 4779
759062
YDOT = 18955
174297 feet/sec YDOT = 5831
311679 meter/sec
ZDOT = -4712
387066 ZDOT = -1412
976638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13113065
03 X = -3996862
22
Y = 5926124
42 feet Y = 1806282
72 meter
Z = 16942824
50 Z = 5164172
91
XDOT = -14458
177124 XDOT = -4406
852387
YDOT = -18803
065570 feet/sec YDOT = -5731
174386 meter/sec
ZDOT = -4612
021120 ZDOT = -1405
744037
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 16064
08922496
00016717 00000-0 10270-3 0 9048
2 25544 51
6387 222
1464 0002987 197
3421 162
7630 15
54369183 28635
Satellite: ISS
Catalog Number: 25544
Epoch time: 16064
08922496 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 222
1464 deg
Eccentricity:
0002987
Arg of perigee: 197
3421 deg
Mean anomaly: 162
7630 deg
Mean motion: 15
54369183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2863
Checksum: 327
Coasting Arc #6 (Orbit 2877)
---------------------------------------
Vector Time (GMT): 2016/065/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 890989
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5103015
55 A = 6780178
62 meter
Y = 638110
61 meter E =
0009681
Z = -4428497
21 I = 51
40797
XDOT = -3598
976258 Wp = 128
36520
YDOT = -5904
553816 meter/sec RA = 216
28299 deg
ZDOT = 3295
364624 TA = 175
03467
MA = 175
02506
Ha = 220
489 n
mi
Hp = 214
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16742177
02 X = -5088260
40
Y = 2093538
76 feet Y = 581127
41 meter
Z = -14529190
33 Z = -4453250
21
XDOT = -11807
664889 XDOT = -3548
689804
YDOT = -19371
895721 feet/sec YDOT = -5944
518495 meter/sec
ZDOT = 10811
563727 ZDOT = 3278
004638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16711554
67 X = 5093681
86
Y = -1507671
70 feet Y = -459538
33 meter
Z = -14636653
78 Z = -4461252
07
XDOT = 11081
014245 XDOT = 3377
493142
YDOT = 18556
507671 feet/sec YDOT = 5656
023538 meter/sec
ZDOT = 10737
216456 ZDOT = 3272
703576
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 16065
05359421
00016717 00000-0 10270-3 0 9059
2 25544 51
6387 217
3363 0002908 202
5748 157
5277 15
54377923 28789
Satellite: ISS
Catalog Number: 25544
Epoch time: 16065
05359421 = yrday
fracday
Element set: 905
Inclination: 51
6387 deg
RA of node: 217
3363 deg
Eccentricity:
0002908
Arg of perigee: 202
5748 deg
Mean anomaly: 157
5277 deg
Mean motion: 15
54377923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2878
Checksum: 332
Coasting Arc #7 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2016/065/04:09:13
568
Vector Time (MET): N/A
Weight (LBS) : 890679
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5410991
32 A = 6782974
17 meter
Y = 139948
72 meter E =
0005655
Z = -4094120
30 I = 51
41759
XDOT = -3035
452401 Wp = 137
85578
YDOT = -5914
376040 meter/sec RA = 215
63426 deg
ZDOT = 3808
588206 TA = 171
63707
MA = 171
62764
Ha = 220
449 n
mi
Hp = 216
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17752596
19 X = -5392266
95
Y = 459149
34 feet Y = 79543
74 meter
Z = -13432153
21 Z = -4120359
65
XDOT = -9958
833335 XDOT = -2987
590969
YDOT = -19404
120866 feet/sec YDOT = -5948
052529 meter/sec
ZDOT = 12495
368129 ZDOT = 3793
959759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12212187
32 X = 3722274
69
Y = -12773292
39 feet Y = -3893299
52 meter
Z = -13545985
09 Z = -4128816
25
XDOT = 19864
085652 XDOT = 6054
573307
YDOT = 5802
923337 feet/sec YDOT = 1768
731033 meter/sec
ZDOT = 12432
867677 ZDOT = 3789
538068
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 16065
18217601
00016717 00000-0 10270-3 0 9067
2 25544 51
6410 216
6966 0003710 242
9121 117
1654 15
53831800 28804
Satellite: ISS
Catalog Number: 25544
Epoch time: 16065
18217601 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 216
6966 deg
Eccentricity:
0003710
Arg of perigee: 242
9121 deg
Mean anomaly: 117
1654 deg
Mean motion: 15
53831800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 285
Coasting Arc #8 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2016/066/04:09:13
568
Vector Time (MET): N/A
Weight (LBS) : 890679
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6068191
19 A = 6786593
74 meter
Y = 926334
33 meter E =
0010313
Z = 2881244
92 I = 51
45601
XDOT = 1544
541267 Wp = 109
46228
YDOT = 5576
550492 meter/sec RA = 210
63858 deg
ZDOT = -5034
489042 TA = 37
63216
MA = 37
56004
Ha = 220
292 n
mi
Hp = 216
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19908763
74 X = 6043386
09
Y = 3039154
63 feet Y = 994054
49 meter
Z = 9452903
29 Z = 2910661
80
XDOT = 5067
392607 XDOT = 1506
523050
YDOT = 18295
769332 feet/sec YDOT = 5593
609471 meter/sec
ZDOT = -16517
352499 ZDOT = -5027
079114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16019179
21 X = -4882645
82
Y = 12106001
45 feet Y = 3689909
24 meter
Z = 9580362
28 Z = 2920094
42
XDOT = -15837
299845 XDOT = -4827
208993
YDOT = -7880
845989 feet/sec YDOT = -2402
081857 meter/sec
ZDOT = -16486
093976 ZDOT = -5024
961444
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 16066
21120417
00016717 00000-0 10270-3 0 9071
2 25544 51
6408 211
5687 0003679 246
4719 113
6047 15
53826163 28961
Satellite: ISS
Catalog Number: 25544
Epoch time: 16066
21120417 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 211
5687 deg
Eccentricity:
0003679
Arg of perigee: 246
4719 deg
Mean anomaly: 113
6047 deg
Mean motion: 15
53826163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 316
Coasting Arc #9 (Orbit 2910)
---------------------------------------
Vector Time (GMT): 2016/067/04:09:13
568
Vector Time (MET): N/A
Weight (LBS) : 890679
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6383097
74 A = 6789179
99 meter
Y = -1820406
17 meter E =
0005764
Z = -1410654
97 I = 51
49401
XDOT = 158
405121 Wp = 16
30807
YDOT = -5028
850675 meter/sec RA = 205
65239 deg
ZDOT = 5783
973429 TA = 328
28641
MA = 328
32112
Ha = 220
173 n
mi
Hp = 216
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20941921
72 X = -6355414
87
Y = -5972461
18 feet Y = -1891631
60 meter
Z = -4628133
11 Z = -1441594
43
XDOT = 519
701842 XDOT = 186
531656
YDOT = -16498
853919 feet/sec YDOT = -5026
921288 meter/sec
ZDOT = 18976
290779 ZDOT = 5784
811857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18674410
36 X = 5691960
28
Y = -11146437
09 feet Y = -3397434
02 meter
Z = -4762072
23 Z = -1451479
62
XDOT = 10935
324913 XDOT = 3333
087034
YDOT = 10226
836382 feet/sec YDOT = 3117
139729 meter/sec
ZDOT = 18980
717311 ZDOT = 5785
322636
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 16067
17590594
00016717 00000-0 10270-3 0 9085
2 25544 51
6417 206
7606 0003745 252
3644 107
7100 15
53871476 29114
Satellite: ISS
Catalog Number: 25544
Epoch time: 16067
17590594 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 206
7606 deg
Eccentricity:
0003745
Arg of perigee: 252
3644 deg
Mean anomaly: 107
7100 deg
Mean motion: 15
53871476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2911
Checksum: 313
Coasting Arc #10 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2016/068/04:09:13
568
Vector Time (MET): N/A
Weight (LBS) : 890679
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6280473
50 A = 6790143
40 meter
Y = 2555132
08 meter E =
0010445
Z = -218057
58 I = 51
52660
XDOT = -1974
216315 Wp = 154
89527
YDOT = 4350
428348 meter/sec RA = 200
67386 deg
ZDOT = -5999
001822 TA = 27
45780
MA = 27
40265
Ha = 220
192 n
mi
Hp = 216
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20605228
01 X = 6252493
81
Y = 8382979
27 feet Y = 2625208
03 meter
Z = -715412
00 Z = -187617
44
XDOT = -6477
087648 XDOT = -1993
577058
YDOT = 14273
058885 feet/sec YDOT = 4328
242223 meter/sec
ZDOT = -19681
764509 ZDOT = -6008
639572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20060850
73 X = -6114547
30
Y = 9622010
96 feet Y = 2932788
94 meter
Z = -583738
03 Z = -177923
35
XDOT = -5594
482188 XDOT = -1705
198171
YDOT = -12832
495369 feet/sec YDOT = -3911
344589 meter/sec
ZDOT = -19724
256056 ZDOT = -6011
953246
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 16068
20491152
00016717 00000-0 10270-3 0 9091
2 25544 51
6422 201
6325 0003790 255
1876 104
8857 15
53844061 29274
Satellite: ISS
Catalog Number: 25544
Epoch time: 16068
20491152 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 201
6325 deg
Eccentricity:
0003790
Arg of perigee: 255
1876 deg
Mean anomaly: 104
8857 deg
Mean motion: 15
53844061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 309
Coasting Arc #11 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2016/069/04:09:13
568
Vector Time (MET): N/A
Weight (LBS) : 890679
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5749077
70 A = 6788697
31 meter
Y = -3110386
52 meter E =
0010451
Z = 1812598
16 I = 51
55270
XDOT = 3735
900743 Wp = 59
30067
YDOT = -3604
931961 meter/sec RA = 195
69600 deg
ZDOT = 5644
278281 TA = 320
64912
MA = 320
72501
Ha = 220
047 n
mi
Hp = 216
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18861803
49 X = -5722674
02
Y = -10204680
19 feet Y = -3174528
61 meter
Z = 5946844
37 Z = 1784735
56
XDOT = 12256
892203 XDOT = 3748
517191
YDOT = -11827
204595 feet/sec YDOT = -3563
083193 meter/sec
ZDOT = 18517
973363 ZDOT = 5662
457342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20134058
95 X = 6136861
17
Y = -7479339
27 feet Y = -2279702
61 meter
Z = 5826426
07 Z = 1775894
67
XDOT = 340
858168 XDOT = 103
893570
YDOT = 15454
578827 feet/sec YDOT = 4710
555626 meter/sec
ZDOT = 18597
409874 ZDOT = 5668
490530
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 16069
23390419
00016717 00000-0 10270-3 0 9101
2 25544 51
6426 196
5039 0003753 263
8230 96
2495 15
53886921 29432
Satellite: ISS
Catalog Number: 25544
Epoch time: 16069
23390419 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 196
5039 deg
Eccentricity:
0003753
Arg of perigee: 263
8230 deg
Mean anomaly: 96
2495 deg
Mean motion: 15
53886921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 327
Coasting Arc #12 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2016/070/04:09:13
568
Vector Time (MET): N/A
Weight (LBS) : 890679
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4785842
33 A = 6785597
37 meter
Y = 3537313
94 meter E =
0001115
Z = -3259426
59 I = 51
57365
XDOT = -5316
874319 Wp = 148
29498
YDOT = 2824
040237 meter/sec RA = 190
71505 deg
ZDOT = -4743
668169 TA = 69
52423
MA = 69
51226
Ha = 219
960 n
mi
Hp = 216
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15701582
44 X = 4761764
28
Y = 11605360
70 feet Y = 3590697
25 meter
Z = -10693656
80 Z = -3236237
41
XDOT = -17443
813383 XDOT = -5325
015753
YDOT = 9265
223876 feet/sec YDOT = 2764
537120 meter/sec
ZDOT = -15563
215779 ZDOT = -4769
516248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19047834
64 X = -5805780
00
Y = 4531512
40 feet Y = 1381204
98 meter
Z = -10593572
32 Z = -3228920
84
XDOT = 4472
821508 XDOT = 1363
315996
YDOT = -17832
201247 feet/sec YDOT = -5435
254940 meter/sec
ZDOT = -15675
815482 ZDOT = -4777
988559
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 16070
19857413
00016717 00000-0 10270-3 0 9111
2 25544 51
6428 191
6967 0003947 266
6169 93
4532 15
53892006 29585
Satellite: ISS
Catalog Number: 25544
Epoch time: 16070
19857413 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 191
6967 deg
Eccentricity:
0003947
Arg of perigee: 266
6169 deg
Mean anomaly: 93
4532 deg
Mean motion: 15
53892006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 340
Coasting Arc #13 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2016/071/04:09:13
568
Vector Time (MET): N/A
Weight (LBS) : 890679
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3466937
47 A = 6781898
15 meter
Y = -3839557
75 meter E =
0006042
Z = 4382611
29 I = 51
59303
XDOT = 6564
926661 Wp = 118
86996
YDOT = -2046
144763 meter/sec RA = 185
72623 deg
ZDOT = 3394
288068 TA = 296
70726
MA = 296
76910
Ha = 220
051 n
mi
Hp = 216
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11374466
78 X = -3445033
69
Y = -12596974
24 feet Y = -3878204
19 meter
Z = 14378645
96 Z = 4365823
63
XDOT = 21538
473296 XDOT = 6570
831303
YDOT = -6713
073370 feet/sec YDOT = -1972
697846 meter/sec
ZDOT = 11136
115710 ZDOT = 3426
193389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17009561
61 X = 5184514
38
Y = -900006
15 feet Y = -274321
88 meter
Z = 14306380
29 Z = 4360584
71
XDOT = -8462
442159 XDOT = -2579
352370
YDOT = 19624
795939 feet/sec YDOT = 5981
637802 meter/sec
ZDOT = 11274
892302 ZDOT = 3436
587174
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 16071
22754535
00016717 00000-0 10270-3 0 9128
2 25544 51
6427 186
5681 0003743 273
3490 86
7235 15
53910631 29744
Satellite: ISS
Catalog Number: 25544
Epoch time: 16071
22754535 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 186
5681 deg
Eccentricity:
0003743
Arg of perigee: 273
3490 deg
Mean anomaly: 86
7235 deg
Mean motion: 15
53910631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 316
Coasting Arc #14 (Orbit 2988)
---------------------------------------
Vector Time (GMT): 2016/072/04:09:13
568
Vector Time (MET): N/A
Weight (LBS) : 890679
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1873863
13 A = 6778857
18 meter
Y = 4064420
94 meter E =
0009706
Z = -5100098
72 I = 51
61440
XDOT = -7362
582934 Wp = 69
07218
YDOT = 1255
794945 meter/sec RA = 180
73044 deg
ZDOT = -1703
590871 TA = 184
44225
MA = 184
45087
Ha = 219
858 n
mi
Hp = 216
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6147844
90 X = 1853048
57
Y = 13334714
36 feet Y = 4085258
63 meter
Z = -16732607
35 Z = -5091047
09
XDOT = -24155
455819 XDOT = -7367
803035
YDOT = 4120
062157 feet/sec YDOT = 1173
432225 meter/sec
ZDOT = -5589
208893 ZDOT = -1739
369285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14340520
19 X = -4370990
55
Y = -3354457
07 feet Y = -1022438
51 meter
Z = -16693946
55 Z = -5088314
91
XDOT = 11470
599669 XDOT = 3496
238779
YDOT = -20435
720982 feet/sec YDOT = -6228
807755 meter/sec
ZDOT = -5744
687817 ZDOT = -1750
980847
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 16072
19219303
00016717 00000-0 10270-3 0 9135
2 25544 51
6418 181
7601 0003929 277
6390 82
4317 15
53961101 29893
Satellite: ISS
Catalog Number: 25544
Epoch time: 16072
19219303 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 181
7601 deg
Eccentricity:
0003929
Arg of perigee: 277
6390 deg
Mean anomaly: 82
4317 deg
Mean motion: 15
53961101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2989
Checksum: 312
Coasting Arc #15 (Orbit 3004)
---------------------------------------
Vector Time (GMT): 2016/073/04:09:13
568
Vector Time (MET): N/A
Weight (LBS) : 890679
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -139505
45 A = 6777833
56 meter
Y = -4206534
07 meter E =
0001696
Z = 5313912
69 I = 51
64310
XDOT = 7652
934044 Wp = 304
71045
YDOT = -449
150212 meter/sec RA = 175
73188 deg
ZDOT = -153
729965 TA = 146
75995
MA = 146
74930
Ha = 219
899 n
mi
Hp = 216
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -457695
06 X = -118269
28
Y = -13800964
79 feet Y = -4207974
73 meter
Z = 17434096
76 Z = 5313287
10
XDOT = 25108
051325 XDOT = 7658
134525
YDOT = -1473
589933 feet/sec YDOT = -363
540959 meter/sec
ZDOT = -504
363403 ZDOT = -116
541242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11320444
16 X = 3450471
38
Y = 7911743
80 feet Y = 2411499
51 meter
Z = 17432030
80 Z = 5313282
99
XDOT = -13472
587548 XDOT = -4106
444685
YDOT = 20039
147090 feet/sec YDOT = 6107
932033 meter/sec
ZDOT = -342
869488 ZDOT = -104
506620
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 16073
22114106
00016717 00000-0 10270-3 0 9146
2 25544 51
6417 176
6318 0003888 281
2023 78
8693 15
53962948 30054
Satellite: ISS
Catalog Number: 25544
Epoch time: 16073
22114106 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 176
6318 deg
Eccentricity:
0003888
Arg of perigee: 281
2023 deg
Mean anomaly: 78
8693 deg
Mean motion: 15
53962948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3005
Checksum: 314
Coasting Arc #16 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2016/074/04:09:13
568
Vector Time (MET): N/A
Weight (LBS) : 890679
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1590733
51 A = 6779012
02 meter
Y = 4279224
47 meter E =
0008929
Z = -5019423
22 I = 51
67783
XDOT = -7384
435859 Wp = 104
56658
YDOT = -398
187030 meter/sec RA = 170
73418 deg
ZDOT = 2001
562675 TA = 184
88061
MA = 184
88932
Ha = 219
898 n
mi
Hp = 216
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5218941
97 X = -1614084
46
Y = 14039450
37 feet Y = 4261304
75 meter
Z = -16467923
95 Z = -5027207
76
XDOT = -24227
151768 XDOT = -7389
157126
YDOT = -1306
387893 feet/sec YDOT = -480
790888 meter/sec
ZDOT = 6566
806678 ZDOT = 1965
679550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8280585
35 X = -2523922
41
Y = -12435406
34 feet Y = -3790311
85 meter
Z = -16502382
15 Z = -5029926
08
XDOT = 14522
203943 XDOT = 4426
367762
YDOT = -18174
564494 feet/sec YDOT = -5539
607258 meter/sec
ZDOT = 6411
091825 ZDOT = 1954
100788
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
18576850
00016717 00000-0 10270-3 0 9151
2 25544 51
6403 171
8225 0003964 285
5227 74
5487 15
53992922 30207
Satellite: ISS
Catalog Number: 25544
Epoch time: 16074
18576850 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 171
8225 deg
Eccentricity:
0003964
Arg of perigee: 285
5227 deg
Mean anomaly: 74
5487 deg
Mean motion: 15
53992922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 322
Coasting Arc #17 (Orbit 3035)
---------------------------------------
Vector Time (GMT): 2016/075/04:09:13
568
Vector Time (MET): N/A
Weight (LBS) : 890679
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3189588
00 A = 6781997
64 meter
Y = -4244432
08 meter E =
0007147
Z = 4217538
74 I = 51
71997
XDOT = 6604
793456 Wp = 54
51974
YDOT = 1309
434870 meter/sec RA = 165
74609 deg
ZDOT = -3668
779420 TA = 73
07296
MA = 72
99462
Ha = 219
838 n
mi
Hp = 216
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10464527
54 X = 3216326
32
Y = -13925302
11 feet Y = -4208614
09 meter
Z = 13837069
37 Z = 4233098
25
XDOT = 21669
269869 XDOT = 6607
481437
YDOT = 4296
046162 feet/sec YDOT = 1383
308744 meter/sec
ZDOT = -12036
677888 ZDOT = -3636
688698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5356269
35 X = 1632590
90
Y = 16517815
92 feet Y = 5034630
29 meter
Z = 13905286
77 Z = 4238331
41
XDOT = -14878
245358 XDOT = -4534
889185
YDOT = 14863
546486 feet/sec YDOT = 4530
408969 meter/sec
ZDOT = -11897
550483 ZDOT = -3626
373387
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
21469268
00016717 00000-0 10270-3 0 9161
2 25544 51
6406 166
6940 0004115 290
1791 69
8919 15
54030119 30369
Satellite: ISS
Catalog Number: 25544
Epoch time: 16075
21469268 = yrday
fracday
Element set: 916
Inclination: 51
6406 deg
RA of node: 166
6940 deg
Eccentricity:
0004115
Arg of perigee: 290
1791 deg
Mean anomaly: 69
8919 deg
Mean motion: 15
54030119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3036
Checksum: 314
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