[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 17th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 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
There are no maneuvers
Coasting Arc #1 (Orbit 3056)
---------------------------------------
Vector Time (GMT): 2016/076/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4889725
62 A = 6786545
02 meter
Y = -3980980
84 meter E =
0011910
Z = 2495860
25 I = 51
77943
XDOT = 4861
230793 Wp = 101
84622
YDOT = 2623
067750 meter/sec RA = 159
01200 deg
ZDOT = -5320
864135 TA = 50
21872
MA = 50
11389
Ha = 220
389 n
mi
Hp = 215
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16042406
90 X = 4921754
80
Y = -13060960
78 feet Y = -3926121
37 meter
Z = 8188517
89 Z = 2519691
29
XDOT = 15948
919924 XDOT = 4857
383968
YDOT = 8605
865320 feet/sec YDOT = 2677
407258 meter/sec
ZDOT = -17456
903329 ZDOT = -5297
259267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15157058
80 X = 4619871
52
Y = -14017674
96 feet Y = -4272587
33 meter
Z = 8292629
14 Z = 2527593
36
XDOT = 15536
781123 XDOT = 4735
610886
YDOT = 6496
290767 feet/sec YDOT = 1980
069426 meter/sec
ZDOT = -17354
807709 ZDOT = -5289
745390
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 16076
56457247
00016717 00000-0 10270-3 0 9007
2 25544 51
6421 159
9689 0001878 302
5802 57
5169 15
54155039 30578
Satellite: ISS
Catalog Number: 25544
Epoch time: 16076
56457247 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 159
9689 deg
Eccentricity:
0001878
Arg of perigee: 302
5802 deg
Mean anomaly: 57
5169 deg
Mean motion: 15
54155039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3057
Checksum: 329
Coasting Arc #2 (Orbit 3071)
---------------------------------------
Vector Time (GMT): 2016/077/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5715309
41 A = 6788994
95 meter
Y = 3547400
37 meter E =
0010229
Z = -875686
54 I = 51
81661
XDOT = -3174
745262 Wp = 28
04159
YDOT = -3656
100120 meter/sec RA = 154
04907 deg
ZDOT = 5946
604501 TA = 322
50588
MA = 322
57718
Ha = 220
493 n
mi
Hp = 215
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18751015
12 X = -5750298
88
Y = 11638452
65 feet Y = 3483292
26 meter
Z = -2872987
32 Z = -903535
13
XDOT = -10415
830912 XDOT = -3162
511631
YDOT = -11995
079135 feet/sec YDOT = -3691
533227 meter/sec
ZDOT = 19509
857288 ZDOT = 5931
212632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17759674
67 X = -5413148
84
Y = 13074217
59 feet Y = 3985021
52 meter
Z = -2994494
01 Z = -912721
78
XDOT = -10497
499937 XDOT = -3199
637981
YDOT = -9832
850294 feet/sec YDOT = -2997
052769 meter/sec
ZDOT = 19443
581973 ZDOT = 5926
403785
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 16077
52908853
00016717 00000-0 10270-3 0 9019
2 25544 51
6420 155
1603 0002026 310
2523 49
8452 15
54121272 30721
Satellite: ISS
Catalog Number: 25544
Epoch time: 16077
52908853 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 155
1603 deg
Eccentricity:
0002026
Arg of perigee: 310
2523 deg
Mean anomaly: 49
8452 deg
Mean motion: 15
54121272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3072
Checksum: 274
Coasting Arc #3 (Orbit 3087)
---------------------------------------
Vector Time (GMT): 2016/078/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6095516
75 A = 6788846
97 meter
Y = -2849147
50 meter E =
0008321
Z = -873818
71 I = 51
84516
XDOT = 1326
983708 Wp = 142
00444
YDOT = 4652
000019 meter/sec RA = 149
09172 deg
ZDOT = -5947
961650 TA = 47
42186
MA = 47
35167
Ha = 220
522 n
mi
Hp = 215
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19998414
54 X = 6131168
18
Y = -9347596
77 feet Y = -2780784
14 meter
Z = -2866859
30 Z = -844121
66
XDOT = 4353
621088 XDOT = 1303
757554
YDOT = 15262
467253 feet/sec YDOT = 4666
708687 meter/sec
ZDOT = -19514
309874 ZDOT = -5941
572518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19029753
17 X = 5800268
77
Y = -11220876
43 feet Y = -3420123
13 meter
Z = -2737418
19 Z = -834365
06
XDOT = 5100
903170 XDOT = 1554
755286
YDOT = 13374
256418 feet/sec YDOT = 4076
473356 meter/sec
ZDOT = -19487
289450 ZDOT = -5939
725824
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 16078
55789122
00016717 00000-0 10270-3 0 9020
2 25544 51
6420 150
0311 0001878 316
1072 43
9931 15
54191960 30884
Satellite: ISS
Catalog Number: 25544
Epoch time: 16078
55789122 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 150
0311 deg
Eccentricity:
0001878
Arg of perigee: 316
1072 deg
Mean anomaly: 43
9931 deg
Mean motion: 15
54191960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3088
Checksum: 298
Coasting Arc #4 (Orbit 3103)
---------------------------------------
Vector Time (GMT): 2016/079/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6002012
93 A = 6786549
26 meter
Y = 1907891
62 meter E =
0013146
Z = 2509903
64 I = 51
86426
XDOT = 482
784790 Wp = 67
60021
YDOT = -5504
674394 meter/sec RA = 144
13254 deg
ZDOT = 5321
533524 TA = 320
47802
MA = 320
57381
Ha = 220
653 n
mi
Hp = 214
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19691643
47 X = -6035093
25
Y = 6259486
94 feet Y = 1840588
48 meter
Z = 8234591
98 Z = 2480667
12
XDOT = 1583
939600 XDOT = 518
454138
YDOT = -18059
955362 feet/sec YDOT = -5499
075445 meter/sec
ZDOT = 17459
099489 ZDOT = 5323
966091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18911770
45 X = -5764307
63
Y = 8447920
44 feet Y = 2574926
15 meter
Z = 8107285
81 Z = 2471100
71
XDOT = 40
834847 XDOT = 12
446461
YDOT = -16730
061373 feet/sec YDOT = -5099
322706 meter/sec
ZDOT = 17470
534795 ZDOT = 5325
019005
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 16079
58667827
00016717 00000-0 10270-3 0 9032
2 25544 51
6419 144
9016 0001901 323
6116 36
4907 15
54194913 31045
Satellite: ISS
Catalog Number: 25544
Epoch time: 16079
58667827 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 144
9016 deg
Eccentricity:
0001901
Arg of perigee: 323
6116 deg
Mean anomaly: 36
4907 deg
Mean motion: 15
54194913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3104
Checksum: 311
Coasting Arc #5 (Orbit 3118)
---------------------------------------
Vector Time (GMT): 2016/080/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5503283
86 A = 6782680
55 meter
Y = -701464
36 meter E =
0006099
Z = -3909185
13 I = 51
87742
XDOT = -2137
133548 Wp = 57
74779
YDOT = 6105
194570 meter/sec RA = 139
16620 deg
ZDOT = -4105
640365 TA = 169
32198
MA = 169
30903
Ha = 220
588 n
mi
Hp = 214
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18055393
24 X = 5529707
73
Y = -2301392
26 feet Y = -639775
80 meter
Z = -12825410
53 Z = -3882387
57
XDOT = -7011
593006 XDOT = -2185
301295
YDOT = 20030
165911 feet/sec YDOT = 6081
025807 meter/sec
ZDOT = -13469
948704 ZDOT = -4116
139784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17684677
16 X = 5390289
60
Y = -4639112
70 feet Y = -1414001
55 meter
Z = -12708879
33 Z = -3873666
42
XDOT = -4602
671256 XDOT = -1402
894199
YDOT = 19469
218135 feet/sec YDOT = 5934
217688 meter/sec
ZDOT = -13516
529036 ZDOT = -4119
838050
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 16080
55115210
00016717 00000-0 10270-3 0 9046
2 25544 51
6422 140
0927 0001896 328
2885 31
8162 15
54229279 31196
Satellite: ISS
Catalog Number: 25544
Epoch time: 16080
55115210 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 140
0927 deg
Eccentricity:
0001896
Arg of perigee: 328
2885 deg
Mean anomaly: 31
8162 deg
Mean motion: 15
54229279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3119
Checksum: 296
Coasting Arc #6 (Orbit 3134)
---------------------------------------
Vector Time (GMT): 2016/081/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4662285
10 A = 6778994
56 meter
Y = -684077
45 meter E =
0005597
Z = 4869528
66 I = 51
88837
XDOT = 3503
404965 Wp = 109
02715
YDOT = -6367
341184 meter/sec RA = 134
19089 deg
ZDOT = 2455
733105 TA = 316
94308
MA = 316
98686
Ha = 220
747 n
mi
Hp = 214
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15296210
96 X = -4677942
95
Y = -2244348
59 feet Y = -736301
01 meter
Z = 15976143
90 Z = 4846842
71
XDOT = 11494
110778 XDOT = 3562
416980
YDOT = -20890
226981 feet/sec YDOT = -6327
833442 meter/sec
ZDOT = 8056
867141 ZDOT = 2472
895950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15561022
37 X = -4742999
62
Y = 44058
85 feet Y = 13429
14 meter
Z = 15877688
31 Z = 4839519
40
XDOT = 8251
626336 XDOT = 2515
095707
YDOT = -21209
314839 feet/sec YDOT = -6464
599163 meter/sec
ZDOT = 8132
448152 ZDOT = 2478
770197
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 16081
57990839
00016717 00000-0 10270-3 0 9058
2 25544 51
6415 134
9632 0001955 334
4197 25
6858 15
54261677 31353
Satellite: ISS
Catalog Number: 25544
Epoch time: 16081
57990839 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 134
9632 deg
Eccentricity:
0001955
Arg of perigee: 334
4197 deg
Mean anomaly: 25
6858 deg
Mean motion: 15
54261677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3135
Checksum: 335
Coasting Arc #7 (Orbit 3149)
---------------------------------------
Vector Time (GMT): 2016/082/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3604722
64 A = 6777074
43 meter
Y = 2180319
91 meter E =
0014239
Z = -5320798
27 I = 51
90426
XDOT = -4505
656799 Wp = 78
27157
YDOT = 6170
591122 meter/sec RA = 129
20838 deg
ZDOT = -522
303811 TA = 186
74727
MA = 186
76646
Ha = 220
655 n
mi
Hp = 214
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11826517
85 X = 3605919
87
Y = 7153280
56 feet Y = 2220636
15 meter
Z = -17456687
22 Z = -5303284
96
XDOT = -14782
338579 XDOT = -4571
785899
YDOT = 20244
721530 feet/sec YDOT = 6119
836037 meter/sec
ZDOT = -1713
595180 ZDOT = -544
352672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12949373
77 X = 3946969
12
Y = 5097888
78 feet Y = 1553836
50 meter
Z = -17380941
43 Z = -5297710
95
XDOT = -10880
728441 XDOT = -3316
446029
YDOT = 21447
837279 feet/sec YDOT = 6537
300803 meter/sec
ZDOT = -1810
385677 ZDOT = -551
805554
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 16082
54435497
00016717 00000-0 10270-3 0 9061
2 25544 51
6422 130
1539 0002014 338
1166 21
9900 15
54260205 31509
Satellite: ISS
Catalog Number: 25544
Epoch time: 16082
54435497 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 130
1539 deg
Eccentricity:
0002014
Arg of perigee: 338
1166 deg
Mean anomaly: 21
9900 deg
Mean motion: 15
54260205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3150
Checksum: 274
Coasting Arc #8 (Orbit 3165)
---------------------------------------
Vector Time (GMT): 2016/083/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2414522
75 A = 6777500
92 meter
Y = -3653138
29 meter E =
0005643
Z = 5171118
70 I = 51
92449
XDOT = 5140
549787 Wp = 35
32999
YDOT = -5497
771157 meter/sec RA = 124
22526 deg
ZDOT = -1478
362821 TA = 68
87227
MA = 68
81196
Ha = 220
745 n
mi
Hp = 214
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7921662
56 X = -2398612
04
Y = -11985361
85 feet Y = -3680049
29 meter
Z = 16965612
52 Z = 5159428
80
XDOT = 16865
320822 XDOT = 5208
826417
YDOT = -18037
306947 feet/sec YDOT = -5439
904594 meter/sec
ZDOT = -4850
271724 ZDOT = -1453
224623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10065688
75 X = -3068021
93
Y = -10333659
90 feet Y = -3149699
54 meter
Z = 16915407
99 Z = 5155816
36
XDOT = 12601
333658 XDOT = 3840
886499
YDOT = -20062
316862 feet/sec YDOT = -6114
994180 meter/sec
ZDOT = -4740
152740 ZDOT = -1444
798555
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 16083
57308188
00016717 00000-0 10270-3 0 9072
2 25544 51
6408 125
0240 0002054 345
9224 14
1871 15
54313706 31663
Satellite: ISS
Catalog Number: 25544
Epoch time: 16083
57308188 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 125
0240 deg
Eccentricity:
0002054
Arg of perigee: 345
9224 deg
Mean anomaly: 14
1871 deg
Mean motion: 15
54313706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3166
Checksum: 289
Coasting Arc #9 (Orbit 3180)
---------------------------------------
Vector Time (GMT): 2016/084/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1230717
10 A = 6780379
91 meter
Y = 4957367
36 meter E =
0008434
Z = -4466938
08 I = 51
95224
XDOT = -5390
790601 Wp = 98
00825
YDOT = 4319
825480 meter/sec RA = 119
24822 deg
ZDOT = 3313
043690 TA = 205
27776
MA = 205
31906
Ha = 220
754 n
mi
Hp = 214
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4037785
78 X = 1196889
64
Y = 16264328
60 feet Y = 4970940
21 meter
Z = -14655308
67 Z = -4461042
50
XDOT = -17686
320871 XDOT = -5454
788690
YDOT = 14172
655774 feet/sec YDOT = 4259
184760 meter/sec
ZDOT = 10869
565911 ZDOT = 3286
700398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7266583
52 X = 2214854
66
Y = 15124662
42 feet Y = 4609997
10 meter
Z = -14630499
71 Z = -4459376
31
XDOT = -13499
157577 XDOT = -4114
543229
YDOT = 16875
295380 feet/sec YDOT = 5143
590032 meter/sec
ZDOT = 10754
388482 ZDOT = 3277
937609
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 16084
53750059
00016717 00000-0 10270-3 0 9088
2 25544 51
6417 120
2145 0002166 349
8600 10
2509 15
54309398 31813
Satellite: ISS
Catalog Number: 25544
Epoch time: 16084
53750059 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 120
2145 deg
Eccentricity:
0002166
Arg of perigee: 349
8600 deg
Mean anomaly: 10
2509 deg
Mean motion: 15
54309398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3181
Checksum: 295
Coasting Arc #10 (Orbit 3196)
---------------------------------------
Vector Time (GMT): 2016/085/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -86857
27 A = 6784205
58 meter
Y = -5957771
47 meter E =
0012687
Z = 3234711
60 I = 51
97887
XDOT = 5336
970787 Wp = 83
30457
YDOT = -2695
713133 meter/sec RA = 114
28178 deg
ZDOT = -4804
176740 TA = 59
42092
MA = 59
29582
Ha = 220
749 n
mi
Hp = 214
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -284964
79 X = -35942
45
Y = -19546494
31 feet Y = -5958457
61 meter
Z = 10612570
87 Z = 3234414
21
XDOT = 17509
746678 XDOT = 5390
055017
YDOT = -8844
203193 feet/sec YDOT = -2635
735471 meter/sec
ZDOT = -15761
734710 ZDOT = -4778
121604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4539404
30 X = -1383610
43
Y = -19014388
75 feet Y = -5795585
69 meter
Z = 10612263
39 Z = 3234617
88
XDOT = 13915
606495 XDOT = 4241
476860
YDOT = -12087
736811 feet/sec YDOT = -3684
342180 meter/sec
ZDOT = -15648
064625 ZDOT = -4769
530098
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 16085
56619825
00016717 00000-0 10270-3 0 9098
2 25544 51
6402 115
0838 0002203 356
2553 3
8583 15
54364858 31978
Satellite: ISS
Catalog Number: 25544
Epoch time: 16085
56619825 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 115
0838 deg
Eccentricity:
0002203
Arg of perigee: 356
2553 deg
Mean anomaly: 3
8583 deg
Mean motion: 15
54364858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3197
Checksum: 320
Coasting Arc #11 (Orbit 3211)
---------------------------------------
Vector Time (GMT): 2016/086/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -908257
14 A = 6787339
85 meter
Y = 6513224
18 meter E =
0009497
Z = -1662295
84 I = 52
00283
XDOT = -5022
275450 Wp = 30
62000
YDOT = 760
070044 meter/sec RA = 109
32751 deg
ZDOT = 5744
544366 TA = 311
26171
MA = 311
34348
Ha = 220
726 n
mi
Hp = 214
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2979846
27 X = -972947
35
Y = 21368845
74 feet Y = 6502705
52 meter
Z = -5453726
52 Z = -1666865
96
XDOT = -16477
281660 XDOT = -5058
306208
YDOT = 2493
668122 feet/sec YDOT = 703
706929 meter/sec
ZDOT = 18846
930336 ZDOT = 5720
059616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2079123
88 X = 633716
96
Y = 21469870
27 feet Y = 6544016
46 meter
Z = -5474678
00 Z = -1668681
85
XDOT = -14004
777329 XDOT = -4268
656130
YDOT = 6116
286849 feet/sec YDOT = 1864
244231 meter/sec
ZDOT = 18740
398304 ZDOT = 5712
073403
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 16086
53058908
00016717 00000-0 10270-3 0 9107
2 25544 51
6410 110
2745 0002061 1
0028 359
1129 15
54405328 32124
Satellite: ISS
Catalog Number: 25544
Epoch time: 16086
53058908 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 110
2745 deg
Eccentricity:
0002061
Arg of perigee: 1
0028 deg
Mean anomaly: 359
1129 deg
Mean motion: 15
54405328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3212
Checksum: 265
Coasting Arc #12 (Orbit 3227)
---------------------------------------
Vector Time (GMT): 2016/087/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1790902
29 A = 6788578
68 meter
Y = -6542302
57 meter E =
0010538
Z = -140928
96 I = 52
01528
XDOT = 4520
992616 Wp = 126
59852
YDOT = 1360
867911 meter/sec RA = 104
37962 deg
ZDOT = -6041
216282 TA = 54
91169
MA = 54
81292
Ha = 220
829 n
mi
Hp = 214
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5875663
67 X = 1864611
41
Y = -21464247
28 feet Y = -6521863
39 meter
Z = -462365
35 Z = -132049
32
XDOT = 14832
652938 XDOT = 4534
784915
YDOT = 4464
789735 feet/sec YDOT = 1411
501052 meter/sec
ZDOT = -19820
263393 ZDOT = -6019
220915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 370161
58 X = 112825
25
Y = -22251639
31 feet Y = -6782299
66 meter
Z = -422664
13 Z = -128828
03
XDOT = 13976
673854 XDOT = 4260
090191
YDOT = 585
489671 feet/sec YDOT = 178
457252 meter/sec
ZDOT = -19724
903783 ZDOT = -6012
150673
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 16087
55925766
00016717 00000-0 10270-3 0 9116
2 25544 51
6399 105
1432 0002207 4
6109 355
5064 15
54383645 32289
Satellite: ISS
Catalog Number: 25544
Epoch time: 16087
55925766 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 105
1432 deg
Eccentricity:
0002207
Arg of perigee: 4
6109 deg
Mean anomaly: 355
5064 deg
Mean motion: 15
54383645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3228
Checksum: 309
Coasting Arc #13 (Orbit 3243)
---------------------------------------
Vector Time (GMT): 2016/088/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2501982
18 A = 6786938
82 meter
Y = 6006917
62 meter E =
0015104
Z = 1900226
22 I = 52
01737
XDOT = -3903
672854 Wp = 59
47172
YDOT = -3421
470620 meter/sec RA = 99
43263 deg
ZDOT = 5650
156803 TA = 321
36090
MA = 321
46887
Ha = 220
781 n
mi
Hp = 214
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8208602
94 X = -2578197
63
Y = 19707734
98 feet Y = 5978512
85 meter
Z = 6234337
99 Z = 1887886
37
XDOT = -12807
325635 XDOT = -3892
569238
YDOT = -11225
297311 feet/sec YDOT = -3465
061403 meter/sec
ZDOT = 18537
259853 ZDOT = 5631
220920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2737616
40 X = -834425
48
Y = 21188677
26 feet Y = 6458308
83 meter
Z = 6179673
35 Z = 1883564
44
XDOT = -13890
918374 XDOT = -4233
951920
YDOT = -7202
180136 feet/sec YDOT = -2195
224505 meter/sec
ZDOT = 18455
550633 ZDOT = 5625
251833
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 16088
58790915
00016717 00000-0 10270-3 0 9127
2 25544 51
6399 100
0132 0002188 4
8561 355
2613 15
54434706 32442
Satellite: ISS
Catalog Number: 25544
Epoch time: 16088
58790915 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 100
0132 deg
Eccentricity:
0002188
Arg of perigee: 4
8561 deg
Mean anomaly: 355
2613 deg
Mean motion: 15
54434706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3244
Checksum: 303
Coasting Arc #14 (Orbit 3258)
---------------------------------------
Vector Time (GMT): 2016/089/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3111426
38 A = 6783407
21 meter
Y = -4927307
05 meter E =
0005900
Z = -3479144
58 I = 52
00930
XDOT = 3182
952662 Wp = 65
70720
YDOT = 5246
335878 meter/sec RA = 94
47718 deg
ZDOT = -4587
283153 TA = 154
86739
MA = 154
83867
Ha = 220
855 n
mi
Hp = 214
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10208091
79 X = 3183193
80
Y = -16165705
53 feet Y = -4892112
06 meter
Z = -11414516
33 Z = -3463855
17
XDOT = 10442
758078 XDOT = 3146
333459
YDOT = 17212
388051 feet/sec YDOT = 5281
724587 meter/sec
ZDOT = -15050
141579 ZDOT = -4571
910506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5319482
72 X = 1621378
33
Y = -18405717
05 feet Y = -5610062
56 meter
Z = -11347204
04 Z = -3458627
79
XDOT = 13612
223999 XDOT = 4149
005875
YDOT = 13164
328906 feet/sec YDOT = 4012
487451 meter/sec
ZDOT = -14984
241496 ZDOT = -4567
196808
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 16089
55225807
00016717 00000-0 10270-3 0 9139
2 25544 51
6394 95
2024 0002295 10
3882 349
7318 15
54421803 32599
Satellite: ISS
Catalog Number: 25544
Epoch time: 16089
55225807 = yrday
fracday
Element set: 913
Inclination: 51
6394 deg
RA of node: 95
2024 deg
Eccentricity:
0002295
Arg of perigee: 10
3882 deg
Mean anomaly: 349
7318 deg
Mean motion: 15
54421803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3259
Checksum: 312
Coasting Arc #15 (Orbit 3274)
---------------------------------------
Vector Time (GMT): 2016/090/12:39:20
524
Vector Time (MET): N/A
Weight (LBS) : 890089
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3589653
24 A = 6779342
53 meter
Y = 3401160
50 meter E =
0008164
Z = 4631080
71 I = 51
99749
XDOT = -2404
783140 Wp = 98
24385
YDOT = -6637
623455 meter/sec RA = 89
51145 deg
ZDOT = 3005
158147 TA = 321
92264
MA = 321
98030
Ha = 220
931 n
mi
Hp = 213
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11777077
57 X = -3649914
97
Y = 11158663
05 feet Y = 3360682
07 meter
Z = 15193834
36 Z = 4613496
34
XDOT = -7889
708463 XDOT = -2344
978681
YDOT = -21776
979838 feet/sec YDOT = -6664
180690 meter/sec
ZDOT = 9859
442740 ZDOT = 2993
622099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8013644
36 X = -2442558
80
Y = 14189140
14 feet Y = 4324849
91 meter
Z = 15116802
76 Z = 4607601
48
XDOT = -13040
574830 XDOT = -3974
767208
YDOT = -17836
671661 feet/sec YDOT = -5436
617522 meter/sec
ZDOT = 9810
472178 ZDOT = 2990
231920
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 16090
58087979
00016717 00000-0 10270-3 0 9141
2 25544 51
6393 90
0720 0002363 10
5749 349
5453 15
54460629 32759
Satellite: ISS
Catalog Number: 25544
Epoch time: 16090
58087979 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 90
0720 deg
Eccentricity:
0002363
Arg of perigee: 10
5749 deg
Mean anomaly: 349
5453 deg
Mean motion: 15
54460629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3275
Checksum: 324
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