[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 21st 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) : 96 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 743 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
187/04:14:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
5
Coasting Arc #1 (Orbit 549)
---------------------------------------
Vector Time (GMT): 2016/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3288706
00 A = 6775993
17 meter
Y = 2651606
28 meter E =
0003174
Z = 5296084
83 I = 51
87015
XDOT = -5421
996068 Wp = 46
96064
YDOT = -5385
662759 meter/sec RA = 40
87273 deg
ZDOT = -668
072955 TA = 49
40947
MA = 49
38185
Ha = 220
178 n
mi
Hp = 213
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10789717
83 X = -3343838
60
Y = 8699495
67 feet Y = 2614520
72 meter
Z = 17375606
40 Z = 5279975
60
XDOT = -17788
701010 XDOT = -5358
124050
YDOT = -17669
497242 feet/sec YDOT = -5445
937900 meter/sec
ZDOT = -2191
840404 ZDOT = -694
257334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8369578
10 X = 2551047
41
Y = 11158119
32 feet Y = 3400994
77 meter
Z = 17304839
47 Z = 5274515
07
XDOT = -17382
240814 XDOT = -5298
107000
YDOT = 16624
818640 feet/sec YDOT = 5067
244721 meter/sec
ZDOT = -2304
840477 ZDOT = -702
515377
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 16172
54703394
00016717 00000-0 10270-3 0 9009
2 25544 51
6442 41
2776 0000862 332
9699 27
1409 15
54648981 5502
Satellite: ISS
Catalog Number: 25544
Epoch time: 16172
54703394 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 41
2776 deg
Eccentricity:
0000862
Arg of perigee: 332
9699 deg
Mean anomaly: 27
1409 deg
Mean motion: 15
54648981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 550
Checksum: 315
Coasting Arc #2 (Orbit 564)
---------------------------------------
Vector Time (GMT): 2016/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4663034
61 A = 6778311
79 meter
Y = -1249024
49 meter E =
0010434
Z = -4768173
99 I = 51
85147
XDOT = 4299
916501 Wp = 104
97086
YDOT = 5733
810988 meter/sec RA = 35
88524 deg
ZDOT = 2705
438105 TA = 191
70162
MA = 191
72589
Ha = 220
095 n
mi
Hp = 214
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15298669
97 X = 4699816
60
Y = -4097849
37 feet Y = -1196672
96 meter
Z = -15643615
44 Z = -4745433
05
XDOT = 14107
337602 XDOT = 4222
338202
YDOT = 18811
715840 feet/sec YDOT = 5781
461351 meter/sec
ZDOT = 8876
109269 ZDOT = 2726
138378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3901022
91 X = -1189031
78
Y = -15450667
95 feet Y = -4709363
59 meter
Z = -15544235
48 Z = -4737882
97
XDOT = 17864
940638 XDOT = 5445
233906
YDOT = -13522
333728 feet/sec YDOT = -4121
607320 meter/sec
ZDOT = 8965
128045 ZDOT = 2732
571028
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 16173
51125244
00016717 00000-0 10270-3 0 9010
2 25544 51
6428 36
4673 0000887 336
9857 23
1256 15
54648193 5652
Satellite: ISS
Catalog Number: 25544
Epoch time: 16173
51125244 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 36
4673 deg
Eccentricity:
0000887
Arg of perigee: 336
9857 deg
Mean anomaly: 23
1256 deg
Mean motion: 15
54648193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 565
Checksum: 316
Coasting Arc #3 (Orbit 580)
---------------------------------------
Vector Time (GMT): 2016/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5728499
32 A = 6782263
23 meter
Y = -113160
91 meter E =
0011688
Z = 3620775
06 I = 51
83928
XDOT = -2691
841104 Wp = 81
44547
YDOT = -5661
224758 meter/sec RA = 30
90611 deg
ZDOT = -4421
880804 TA = 55
75655
MA = 55
64589
Ha = 220
096 n
mi
Hp = 213
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18794289
09 X = -5744396
22
Y = -371262
82 feet Y = -177310
19 meter
Z = 11879183
25 Z = 3592908
99
XDOT = -8831
499686 XDOT = -2606
856356
YDOT = -18573
572042 feet/sec YDOT = -5690
850922 meter/sec
ZDOT = -14507
482954 ZDOT = -4434
751387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -288122
91 X = -87819
86
Y = 18871947
16 feet Y = 5752169
49 meter
Z = 11757751
87 Z = 3583762
77
XDOT = -17160
628540 XDOT = -5230
559579
YDOT = 8839
413583 feet/sec YDOT = 2694
253260 meter/sec
ZDOT = -14562
386738 ZDOT = -4438
615478
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 16174
53974520
00016717 00000-0 10270-3 0 9023
2 25544 51
6437 31
3365 0001094 336
1420 23
9683 15
54684159 5815
Satellite: ISS
Catalog Number: 25544
Epoch time: 16174
53974520 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 31
3365 deg
Eccentricity:
0001094
Arg of perigee: 336
1420 deg
Mean anomaly: 23
9683 deg
Mean motion: 15
54684159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 581
Checksum: 302
Coasting Arc #4 (Orbit 595)
---------------------------------------
Vector Time (GMT): 2016/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6337139
87 A = 6786106
03 meter
Y = 1295538
07 meter E =
0007280
Z = -2043298
98 I = 51
82258
XDOT = 723
301128 Wp = 32
54908
YDOT = 5220
621965 meter/sec RA = 25
93614 deg
ZDOT = 5568
546658 TA = 304
91949
MA = 304
98787
Ha = 220
124 n
mi
Hp = 214
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20791141
30 X = 6332107
23
Y = 4250452
98 feet Y = 1366376
31 meter
Z = -6703736
81 Z = -2012527
07
XDOT = 2373
035198 XDOT = 637
819708
YDOT = 17128
024819 feet/sec YDOT = 5228
231740 meter/sec
ZDOT = 18269
510033 ZDOT = 5571
853283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3799931
90 X = 1158219
24
Y = -20920684
33 feet Y = -6376624
58 meter
Z = -6569891
89 Z = -2002503
05
XDOT = 15551
620941 XDOT = 4740
134063
YDOT = -2900
815059 feet/sec YDOT = -884
168430 meter/sec
ZDOT = 18282
819806 ZDOT = 5572
603477
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 16175
50395285
00016717 00000-0 10270-3 0 9037
2 25544 51
6425 26
5252 0001029 338
4530 21
6579 15
54650732 5963
Satellite: ISS
Catalog Number: 25544
Epoch time: 16175
50395285 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 26
5252 deg
Eccentricity:
0001029
Arg of perigee: 338
4530 deg
Mean anomaly: 21
6579 deg
Mean motion: 15
54650732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 596
Checksum: 304
Coasting Arc #5 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2016/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6379000
37 A = 6787801
44 meter
Y = -2297881
26 meter E =
0011584
Z = 175103
11 I = 51
79843
XDOT = 1455
358819 Wp = 130
27311
YDOT = -4518
534564 meter/sec RA = 20
97488 deg
ZDOT = -6023
232556 TA = 47
84424
MA = 47
74589
Ha = 220
112 n
mi
Hp = 213
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20928478
89 X = -6353681
35
Y = -7538980
51 feet Y = -2369073
94 meter
Z = 574485
28 Z = 144177
07
XDOT = 4774
799274 XDOT = 1535
036021
YDOT = -14824
588463 feet/sec YDOT = -4501
813606 meter/sec
ZDOT = -19761
261666 ZDOT = -6015
969829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6722354
09 X = -2048973
53
Y = 21208104
17 feet Y = 6464230
15 meter
Z = 440184
31 Z = 134168
18
XDOT = -13458
714015 XDOT = -4102
216032
YDOT = -3833
890704 feet/sec YDOT = -1168
569887 meter/sec
ZDOT = -19728
654001 ZDOT = -6013
293740
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 16176
53243574
00016717 00000-0 10270-3 0 9045
2 25544 51
6419 21
3949 0000939 345
8185 14
2942 15
54651520 6126
Satellite: ISS
Catalog Number: 25544
Epoch time: 16176
53243574 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 21
3949 deg
Eccentricity:
0000939
Arg of perigee: 345
8185 deg
Mean anomaly: 14
2942 deg
Mean motion: 15
54651520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 305
Coasting Arc #6 (Orbit 627)
---------------------------------------
Vector Time (GMT): 2016/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5816645
42 A = 6786443
45 meter
Y = 3048636
46 meter E =
0014036
Z = 1682923
67 I = 51
76358
XDOT = -3579
279459 Wp = 60
47580
YDOT = 3658
067253 meter/sec RA = 16
01060 deg
ZDOT = 5715
312964 TA = 317
94813
MA = 318
05578
Ha = 219
995 n
mi
Hp = 213
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19083482
35 X = 5773947
65
Y = 10002088
13 feet Y = 3113443
17 meter
Z = 5521403
11 Z = 1711075
80
XDOT = -11743
042846 XDOT = -3647
681144
YDOT = 12001
532981 feet/sec YDOT = 3617
658374 meter/sec
ZDOT = 18751
026785 ZDOT = 5697
760078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8921752
77 X = 2719350
24
Y = -19577046
53 feet Y = -5967083
78 meter
Z = 5643450
61 Z = 1720123
74
XDOT = 11220
393195 XDOT = 3419
975846
YDOT = 10523
332947 feet/sec YDOT = 3207
511882 meter/sec
ZDOT = 18673
756407 ZDOT = 5691
760953
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 16177
56091175
00016717 00000-0 10270-3 0 9058
2 25544 51
6415 16
2630 0000901 338
4928 21
6187 15
54690951 6285
Satellite: ISS
Catalog Number: 25544
Epoch time: 16177
56091175 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 16
2630 deg
Eccentricity:
0000901
Arg of perigee: 338
4928 deg
Mean anomaly: 21
6187 deg
Mean motion: 15
54690951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 628
Checksum: 307
Coasting Arc #7 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2016/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4660026
85 A = 6782836
55 meter
Y = -3610543
08 meter E =
0004787
Z = -3359948
24 I = 51
71981
XDOT = 5448
099362 Wp = 78
06663
YDOT = -2691
329361 meter/sec RA = 11
03691 deg
ZDOT = -4668
758042 TA = 141
04291
MA = 141
00841
Ha = 220
096 n
mi
Hp = 213
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15288801
99 X = -4602985
43
Y = -11845613
79 feet Y = -3662335
40 meter
Z = -11023452
22 Z = -3382447
08
XDOT = 17874
341739 XDOT = 5500
468237
YDOT = -8829
820737 feet/sec YDOT = -2630
111895 meter/sec
ZDOT = -15317
447644 ZDOT = -4642
165727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10702731
19 X = -3262192
47
Y = 16042545
51 feet Y = 4889767
87 meter
Z = -11120737
83 Z = -3389600
89
XDOT = -8951
421389 XDOT = -2728
393239
YDOT = -16498
777443 feet/sec YDOT = -5028
827365 meter/sec
ZDOT = -15200
993013 ZDOT = -4633
262670
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 16178
52510438
00016717 00000-0 10270-3 0 9064
2 25544 51
6409 11
4521 0001047 352
9348 7
1790 15
54686008 6437
Satellite: ISS
Catalog Number: 25544
Epoch time: 16178
52510438 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 11
4521 deg
Eccentricity:
0001047
Arg of perigee: 352
9348 deg
Mean anomaly: 7
1790 deg
Mean motion: 15
54686008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 295
Coasting Arc #8 (Orbit 658)
---------------------------------------
Vector Time (GMT): 2016/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3030544
32 A = 6778769
39 meter
Y = 3964240
90 meter E =
0007968
Z = 4582932
80 I = 51
67365
XDOT = -6834
620587 Wp = 107
55461
YDOT = 1696
521499 meter/sec RA = 6
04912 deg
ZDOT = 3045
308347 TA = 312
01626
MA = 312
08407
Ha = 220
083 n
mi
Hp = 213
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9942730
72 X = 2963728
10
Y = 13006039
71 feet Y = 3997756
53 meter
Z = 15035868
78 Z = 4597492
40
XDOT = -22423
295888 XDOT = -6867
876305
YDOT = 5566
015418 feet/sec YDOT = 1619
906042 meter/sec
ZDOT = 9991
169119 ZDOT = 3012
026921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12065984
75 X = 3677712
15
Y = -10979085
38 feet Y = -3346425
22 meter
Z = 15098477
05 Z = 4602015
80
XDOT = 6772
755724 XDOT = 2064
335945
YDOT = 21013
350463 feet/sec YDOT = 6404
869221 meter/sec
ZDOT = 9845
783359 ZDOT = 3000
994768
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 16179
55357127
00016717 00000-0 10270-3 0 9073
2 25544 51
6403 6
3208 0001030 353
9604 6
1536 15
54665560 6598
Satellite: ISS
Catalog Number: 25544
Epoch time: 16179
55357127 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 6
3208 deg
Eccentricity:
0001030
Arg of perigee: 353
9604 deg
Mean anomaly: 6
1536 deg
Mean motion: 15
54665560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 659
Checksum: 295
Coasting Arc #9 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2016/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1076876
72 A = 6776020
14 meter
Y = -4171214
69 meter E =
0014591
Z = -5243070
61 I = 51
63214
XDOT = 7560
778199 Wp = 78
71262
YDOT = -669
348653 meter/sec RA = 1
04802 deg
ZDOT = -1020
019612 TA = 181
50482
MA = 181
50922
Ha = 220
154 n
mi
Hp = 213
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3533060
11 X = -1004684
53
Y = -13685087
55 feet Y = -4182852
96 meter
Z = -17201675
24 Z = -5248126
81
XDOT = 24805
702754 XDOT = 7572
655909
YDOT = -2196
025764 feet/sec YDOT = -584
732497 meter/sec
ZDOT = -3346
521037 ZDOT = -983
262429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13240247
17 X = -4035627
34
Y = 4871540
31 feet Y = 1484845
49 meter
Z = -17222825
44 Z = -5249517
19
XDOT = -4493
611477 XDOT = -1369
652778
YDOT = -23482
027308 feet/sec YDOT = -7157
321924 meter/sec
ZDOT = -3186
216466 ZDOT = -971
158779
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 16180
51775339
00016717 00000-0 10270-3 0 9081
2 25544 51
6399 1
5103 0000866 4
2878 355
8282 15
54695378 6747
Satellite: ISS
Catalog Number: 25544
Epoch time: 16180
51775339 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 1
5103 deg
Eccentricity:
0000866
Arg of perigee: 4
2878 deg
Mean anomaly: 355
8282 deg
Mean motion: 15
54695378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 332
Coasting Arc #10 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2016/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -990733
48 A = 6776231
84 meter
Y = 4210608
05 meter E =
0004627
Z = 5213589
75 I = 51
60068
XDOT = -7578
296462 Wp = 46
95345
YDOT = -375
581601 meter/sec RA = 356
04020 deg
ZDOT = -1133
041464 TA = 53
93047
MA = 53
88762
Ha = 220
246 n
mi
Hp = 213
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3250437
93 X = -1063069
36
Y = 13814330
88 feet Y = 4199124
06 meter
Z = 17104953
25 Z = 5208601
71
XDOT = -24863
177370 XDOT = -7568
029538
YDOT = -1232
223102 feet/sec YDOT = -460
269649 meter/sec
ZDOT = -3717
327639 ZDOT = -1169
830133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14126752
60 X = 4305834
19
Y = 1615365
49 feet Y = 492363
40 meter
Z = 17082329
03 Z = 5206693
89
XDOT = 1985
677229 XDOT = 605
234420
YDOT = 23768
856694 feet/sec YDOT = 7244
747520 meter/sec
ZDOT = -3877
539193 ZDOT = -1181
873946
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 16181
54620922
00016717 00000-0 10270-3 0 9093
2 25544 51
6403 356
3786 0000908 6
3226 353
7938 15
54670454 6909
Satellite: ISS
Catalog Number: 25544
Epoch time: 16181
54620922 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 356
3786 deg
Eccentricity:
0000908
Arg of perigee: 6
3226 deg
Mean anomaly: 353
7938 deg
Mean motion: 15
54670454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 316
Coasting Arc #11 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2016/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2937936
01 A = 6779000
15 meter
Y = -4104683
77 meter E =
0009701
Z = -4534358
70 I = 51
57811
XDOT = 6841
029962 Wp = 104
83892
YDOT = 1437
640471 meter/sec RA = 351
03486 deg
ZDOT = 3134
266674 TA = 196
62525
MA = 196
65708
Ha = 220
225 n
mi
Hp = 213
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9638897
68 X = 3005643
29
Y = -13466810
26 feet Y = -4071450
72 meter
Z = -14876504
92 Z = -4519922
91
XDOT = 22444
324023 XDOT = 6809
220504
YDOT = 4716
668212 feet/sec YDOT = 1513
963210 meter/sec
ZDOT = 10283
027147 ZDOT = 3167
421692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14710052
08 X = -4483623
87
Y = -7731159
49 feet Y = -2356457
41 meter
Z = -14812740
02 Z = -4514923
16
XDOT = 940
279658 XDOT = 286
597240
YDOT = -21747
211208 feet/sec YDOT = -6628
549976 meter/sec
ZDOT = 10427
175011 ZDOT = 3178
202943
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 16182
51038021
00016717 00000-0 10270-3 0 9106
2 25544 51
6402 351
5677 0000862 20
7896 339
3292 15
54711265 7052
Satellite: ISS
Catalog Number: 25544
Epoch time: 16182
51038021 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 351
5677 deg
Eccentricity:
0000862
Arg of perigee: 20
7896 deg
Mean anomaly: 339
3292 deg
Mean motion: 15
54711265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 292
Coasting Arc #12 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2016/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4583829
40 A = 6783253
41 meter
Y = 3794105
53 meter E =
0012954
Z = 3245600
07 I = 51
55965
XDOT = -5467
505584 Wp = 89
35248
YDOT = -2526
907418 meter/sec RA = 346
03929 deg
ZDOT = -4751
366364 TA = 52
96004
MA = 52
84163
Ha = 220
230 n
mi
Hp = 213
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15038810
36 X = -4641681
10
Y = 12447852
78 feet Y = 3742522
20 meter
Z = 10648294
19 Z = 3223192
93
XDOT = -17938
010445 XDOT = -5415
762599
YDOT = -8290
378668 feet/sec YDOT = -2587
758769 meter/sec
ZDOT = -15588
472322 ZDOT = -4777
800828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14685908
85 X = 4476265
02
Y = 12943160
97 feet Y = 3945075
46 meter
Z = 10549866
83 Z = 3215599
41
XDOT = -4416
130011 XDOT = -1346
036427
YDOT = 17854
899251 feet/sec YDOT = 5442
173292 meter/sec
ZDOT = -15703
105080 ZDOT = -4786
306428
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 16183
53882446
00016717 00000-0 10270-3 0 9118
2 25544 51
6391 346
4366 0000808 12
8539 347
2634 15
54709430 7210
Satellite: ISS
Catalog Number: 25544
Epoch time: 16183
53882446 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 346
4366 deg
Eccentricity:
0000808
Arg of perigee: 12
8539 deg
Mean anomaly: 347
2634 deg
Mean motion: 15
54709430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 312
Coasting Arc #13 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2016/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5726289
73 A = 6786579
58 meter
Y = -3280934
17 meter E =
0009028
Z = -1566153
47 I = 51
54226
XDOT = 3613
419996 Wp = 36
00412
YDOT = 3578
602194 meter/sec RA = 341
05306 deg
ZDOT = 5738
828116 TA = 306
84658
MA = 306
92933
Ha = 220
232 n
mi
Hp = 213
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18787039
80 X = 5770160
05
Y = -10764219
72 feet Y = -3216653
47 meter
Z = -5138298
80 Z = -1538230
57
XDOT = 11855
052479 XDOT = 3545
257929
YDOT = 11740
820845 feet/sec YDOT = 3618
627921 meter/sec
ZDOT = 18828
176233 ZDOT = 5756
216123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13899744
14 X = -4236642
01
Y = -16639133
13 feet Y = -5071607
78 meter
Z = -5015951
28 Z = -1528861
95
XDOT = 8288
424609 XDOT = 2526
311821
YDOT = -12598
020767 feet/sec YDOT = -3839
876730 meter/sec
ZDOT = 18903
172266 ZDOT = 5761
686907
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 16184
50298634
00016717 00000-0 10270-3 0 9127
2 25544 51
6413 341
6256 0000847 24
7548 335
3645 15
54731980 7366
Satellite: ISS
Catalog Number: 25544
Epoch time: 16184
50298634 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 341
6256 deg
Eccentricity:
0000847
Arg of perigee: 24
7548 deg
Mean anomaly: 335
3645 deg
Mean motion: 15
54731980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 317
Coasting Arc #14 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2016/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6300096
29 A = 6787416
79 meter
Y = 2488031
70 meter E =
0010916
Z = -353479
99 I = 51
51443
XDOT = -1470
681113 Wp = 132
24781
YDOT = -4557
101244 meter/sec RA = 336
07217 deg
ZDOT = -5989
672133 TA = 51
56959
MA = 51
47165
Ha = 220
165 n
mi
Hp = 213
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20669607
24 X = -6325732
81
Y = 8162833
65 feet Y = 2417436
53 meter
Z = -1159711
26 Z = -384145
97
XDOT = -4825
069268 XDOT = -1390
518124
YDOT = -14951
119566 feet/sec YDOT = -4573
098276 meter/sec
ZDOT = -19651
155293 ZDOT = -5996
622254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11984830
49 X = 3652976
33
Y = 18705594
45 feet Y = 5701465
19 meter
Z = -1293839
91 Z = -394362
41
XDOT = -12405
918557 XDOT = -3781
323976
YDOT = 6612
882699 feet/sec YDOT = 2015
606647 meter/sec
ZDOT = -19680
471699 ZDOT = -5998
607774
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 16185
53141848
00016717 00000-0 10270-3 0 9136
2 25544 51
6404 336
4938 0001040 24
6708 335
4495 15
54763342 7527
Satellite: ISS
Catalog Number: 25544
Epoch time: 16185
53141848 = yrday
fracday
Element set: 913
Inclination: 51
6404 deg
RA of node: 336
4938 deg
Eccentricity:
0001040
Arg of perigee: 24
6708 deg
Mean anomaly: 335
4495 deg
Mean motion: 15
54763342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 307
Coasting Arc #15 (Orbit 767)
---------------------------------------
Vector Time (GMT): 2016/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6246576
30 A = 6785356
13 meter
Y = -1456781
74 meter E =
0014483
Z = 2191883
98 I = 51
47963
XDOT = -679
419900 Wp = 69
15417
YDOT = 5343
540693 meter/sec RA = 331
08815 deg
ZDOT = 5463
544541 TA = 315
25846
MA = 315
37519
Ha = 220
101 n
mi
Hp = 213
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20494016
74 X = 6251755
04
Y = -4779467
65 feet Y = -1386899
72 meter
Z = 7191220
40 Z = 2222240
30
XDOT = -2229
067912 XDOT = -765
661448
YDOT = 17531
301485 feet/sec YDOT = 5335
459977 meter/sec
ZDOT = 17925
014898 ZDOT = 5460
035427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8950892
69 X = -2728232
09
Y = -18994879
30 feet Y = -5789639
21 meter
Z = 7323780
75 Z = 2232288
37
XDOT = 16250
396602 XDOT = 4953
120884
YDOT = -722
656029 feet/sec YDOT = -220
265558 meter/sec
ZDOT = 17908
602960 ZDOT = 5458
542182
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 16186
55984622
00016717 00000-0 10270-3 0 9145
2 25544 51
6414 331
3630 0000777 32
4292 327
6909 15
54769339 7684
Satellite: ISS
Catalog Number: 25544
Epoch time: 16186
55984622 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 331
3630 deg
Eccentricity:
0000777
Arg of perigee: 32
4292 deg
Mean anomaly: 327
6909 deg
Mean motion: 15
54769339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 333
Coasting Arc #16 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2016/187/04:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 876584
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6042500
78 A = 6783933
53 meter
Y = 1100381
60 meter E =
0004501
Z = -2883828
77 I = 51
45875
XDOT = 1376
615814 Wp = 98
10654
YDOT = -5612
796709 meter/sec RA = 327
71430 deg
ZDOT = -5033
471819 TA = 114
80807
MA = 114
76124
Ha = 220
170 n
mi
Hp = 213
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19824477
63 X = -6040348
24
Y = 3610175
86 feet Y = 1032822
76 meter
Z = -9461380
47 Z = -2913175
93
XDOT = 4516
456082 XDOT = 1463
727289
YDOT = -18414
687366 feet/sec YDOT = -5596
914720 meter/sec
ZDOT = -16514
015153 ZDOT = -5026
573841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20054364
04 X = -6112570
16
Y = -1193979
61 feet Y = -363924
99 meter
Z = -9589468
13 Z = -2922869
89
XDOT = 8782
706762 XDOT = 2676
969021
YDOT = -15326
198509 feet/sec YDOT = -4671
425305 meter/sec
ZDOT = -16482
787791 ZDOT = -5023
953719
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 16187
20261189
00016717 00000-0 10270-3 0 9155
2 25544 51
6444 328
1616 0001252 13
0399 347
0786 15
54737591 7782
Satellite: ISS
Catalog Number: 25544
Epoch time: 16187
20261189 = yrday
fracday
Element set: 915
Inclination: 51
6444 deg
RA of node: 328
1616 deg
Eccentricity:
0001252
Arg of perigee: 13
0399 deg
Mean anomaly: 347
0786 deg
Mean motion: 15
54737591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 321
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