[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 9th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10 7639 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
070/23:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 215
5
077/03:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
2
078/21:26:42
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
0
079/03:12:07
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
0
080/10:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 214
9
084/04:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 214
6
Coasting Arc #1 (Orbit 2947)
---------------------------------------
Vector Time (GMT): 2016/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3354438
51 A = 6782593
82 meter
Y = -4212817
29 meter E =
0008910
Z = 4118346
05 I = 51
54314
XDOT = 6505
908819 Wp = 109
50502
YDOT = -1469
449447 meter/sec RA = 194
07163 deg
ZDOT = 3786
376756 TA = 301
36849
MA = 301
45564
Ha = 220
602 n
mi
Hp = 215
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11005375
70 X = -3327085
37
Y = -13821579
05 feet Y = -4250175
25 meter
Z = 13511634
04 Z = 4102118
33
XDOT = 21344
845208 XDOT = 6503
464646
YDOT = -4821
028371 feet/sec YDOT = -1396
709105 meter/sec
ZDOT = 12422
495920 ZDOT = 3817
974785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7631786
08 X = -2326168
40
Y = -15993455
99 feet Y = -4874805
39 meter
Z = 13441867
53 Z = 4097081
22
XDOT = 20636
992536 XDOT = 6290
155325
YDOT = 735
056031 feet/sec YDOT = 224
045078 meter/sec
ZDOT = 12559
832249 ZDOT = 3828
236870
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
55530613
00016717 00000-0 10270-3 0 9007
2 25544 51
6423 194
9008 0001926 254
7925 105
3015 15
53996148 29485
Satellite: ISS
Catalog Number: 25544
Epoch time: 16069
55530613 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 194
9008 deg
Eccentricity:
0001926
Arg of perigee: 254
7925 deg
Mean anomaly: 105
3015 deg
Mean motion: 15
53996148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2948
Checksum: 316
Coasting Arc #2 (Orbit 2962)
---------------------------------------
Vector Time (GMT): 2016/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1779058
39 A = 6779363
60 meter
Y = 4272938
18 meter E =
0010566
Z = -4963230
63 I = 51
56447
XDOT = -7330
927043 Wp = 72
97479
YDOT = 556
431529 meter/sec RA = 189
07558 deg
ZDOT = -2149
476948 TA = 176
03678
MA = 176
02841
Ha = 220
562 n
mi
Hp = 215
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5836805
73 X = 1755254
20
Y = 14018826
06 feet Y = 4292698
90 meter
Z = -16283565
05 Z = -4954646
97
XDOT = -24051
597910 XDOT = -7326
163178
YDOT = 1825
562759 feet/sec YDOT = 474
478519 meter/sec
ZDOT = -7052
089725 ZDOT = -2185
077053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2830664
01 X = 862786
39
Y = 14959061
57 feet Y = 4559521
97 meter
Z = -16246971
85 Z = -4952077
02
XDOT = -22755
306963 XDOT = -6935
817562
YDOT = -3518
464423 feet/sec YDOT = -1072
427956 meter/sec
ZDOT = -7206
663456 ZDOT = -2196
591022
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
51992997
00016717 00000-0 10270-3 0 9013
2 25544 51
6432 190
0943 0001825 262
1542 97
9404 15
53986989 29633
Satellite: ISS
Catalog Number: 25544
Epoch time: 16070
51992997 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 190
0943 deg
Eccentricity:
0001825
Arg of perigee: 262
1542 deg
Mean anomaly: 97
9404 deg
Mean motion: 15
53986989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2963
Checksum: 340
Coasting Arc #3 (Orbit 2969)
---------------------------------------
Vector Time (GMT): 2016/070/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6255297
20 A = 6787293
07 meter
Y = 1149789
52 meter E =
0004827
Z = -2364638
50 I = 51
60381
XDOT = -2883
147147 Wp = 29
29826
YDOT = -4634
540866 meter/sec RA = 186
72060 deg
ZDOT = 5382
188529 TA = 304
30086
MA = 304
34655
Ha = 220
556 n
mi
Hp = 215
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20522628
60 X = -6256203
17
Y = 3772275
34 feet Y = 1079833
19 meter
Z = -7758000
32 Z = -2395027
42
XDOT = -9459
144184 XDOT = -2857
252531
YDOT = -15205
186568 feet/sec YDOT = -4666
636496 meter/sec
ZDOT = 17658
098847 ZDOT = 5368
246609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20210968
31 X = 6160303
14
Y = 4985848
87 feet Y = 1519686
74 meter
Z = -7890056
13 Z = -2404889
11
XDOT = 2832
631571 XDOT = 863
386103
YDOT = 16321
836795 feet/sec YDOT = 4974
895855 meter/sec
ZDOT = 17598
306029 ZDOT = 5363
963678
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
97008272
00016717 00000-0 10270-3 0 9028
2 25544 51
6411 187
8542 0001780 283
7398 76
3556 15
53984359 29703
Satellite: ISS
Catalog Number: 25544
Epoch time: 16070
97008272 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 187
8542 deg
Eccentricity:
0001780
Arg of perigee: 283
7398 deg
Mean anomaly: 76
3556 deg
Mean motion: 15
53984359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2970
Checksum: 335
Coasting Arc #4 (Orbit 2985)
---------------------------------------
Vector Time (GMT): 2016/071/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6730970
87 A = 6789385
82 meter
Y = -387127
38 meter E =
0011680
Z = 748417
54 I = 51
64303
XDOT = 940
719366 Wp = 129
71273
YDOT = 4742
007107 meter/sec RA = 181
74806 deg
ZDOT = -5953
113345 TA = 42
19909
MA = 42
10924
Ha = 220
573 n
mi
Hp = 215
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22083237
75 X = 6731164
07
Y = -1270102
95 feet Y = -311856
00 meter
Z = 2455438
12 Z = 781115
40
XDOT = 3086
349627 XDOT = 916
540787
YDOT = 15557
766099 feet/sec YDOT = 4752
390809 meter/sec
ZDOT = -19531
211763 ZDOT = -5948
602980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20768273
42 X = -6330169
74
Y = -7565976
91 feet Y = -2306109
76 meter
Z = 2597410
21 Z = 791690
63
XDOT = 2654
365767 XDOT = 809
050686
YDOT = -14042
754487 feet/sec YDOT = -4280
231568 meter/sec
ZDOT = -19512
365024 ZDOT = -5947
368859
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
99899175
00016717 00000-0 10270-3 0 9032
2 25544 51
6412 182
7265 0001756 288
1131 71
9831 15
54018082 29863
Satellite: ISS
Catalog Number: 25544
Epoch time: 16071
99899175 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 182
7265 deg
Eccentricity:
0001756
Arg of perigee: 288
1131 deg
Mean anomaly: 71
9831 deg
Mean motion: 15
54018082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2986
Checksum: 329
Coasting Arc #5 (Orbit 3001)
---------------------------------------
Vector Time (GMT): 2016/072/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6709809
96 A = 6789213
06 meter
Y = -354650
79 meter E =
0012507
Z = 924695
52 I = 51
67450
XDOT = 1073
560435 Wp = 47
87966
YDOT = -4751
092514 meter/sec RA = 176
78028 deg
ZDOT = 5924
658415 TA = 322
12837
MA = 322
21629
Ha = 220
506 n
mi
Hp = 215
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22013812
20 X = -6709837
25
Y = -1163552
45 feet Y = -429684
38 meter
Z = 3033777
97 Z = 892100
93
XDOT = 3522
179905 XDOT = 1097
829095
YDOT = -15587
573866 feet/sec YDOT = -4738
950815 meter/sec
ZDOT = 19437
855691 ZDOT = 5929
933041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19939501
42 X = 6077560
03
Y = 9445430
99 feet Y = 2878967
37 meter
Z = 2892353
18 Z = 881589
25
XDOT = -8374
173330 XDOT = -2552
448031
YDOT = 11673
141090 feet/sec YDOT = 3557
973404 meter/sec
ZDOT = 19461
483471 ZDOT = 5931
860162
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
02788163
00016717 00000-0 10270-3 0 9043
2 25544 51
6410 177
5987 0001849 291
2100 68
8855 15
54056278 30028
Satellite: ISS
Catalog Number: 25544
Epoch time: 16073
02788163 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 177
5987 deg
Eccentricity:
0001849
Arg of perigee: 291
2100 deg
Mean anomaly: 68
8855 deg
Mean motion: 15
54056278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3002
Checksum: 315
Coasting Arc #6 (Orbit 3016)
---------------------------------------
Vector Time (GMT): 2016/073/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6188442
84 A = 6786784
83 meter
Y = 1137417
21 meter E =
0003477
Z = -2541668
90 I = 51
69937
XDOT = -3023
745589 Wp = 136
34993
YDOT = 4653
343046 meter/sec RA = 171
81062 deg
ZDOT = -5286
565228 TA = 72
15696
MA = 72
11903
Ha = 220
536 n
mi
Hp = 215
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20303290
17 X = 6187610
35
Y = 3731683
75 feet Y = 1206615
56 meter
Z = -8338808
74 Z = -2511609
16
XDOT = -9920
425162 XDOT = -3049
875854
YDOT = 15266
873511 feet/sec YDOT = 4619
382846 meter/sec
ZDOT = -17344
374107 ZDOT = -5301
317780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17603220
84 X = -5365461
71
Y = -10882649
18 feet Y = -3317031
47 meter
Z = -8208492
51 Z = -2501948
52
XDOT = 13897
592455 XDOT = 4235
986180
YDOT = -9365
817462 feet/sec YDOT = -2854
701162 meter/sec
ZDOT = -17409
137512 ZDOT = -5306
305114
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
99244820
00016717 00000-0 10270-3 0 9057
2 25544 51
6418 172
7907 0001879 300
9550 59
1418 15
54090078 30175
Satellite: ISS
Catalog Number: 25544
Epoch time: 16073
99244820 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 172
7907 deg
Eccentricity:
0001879
Arg of perigee: 300
9550 deg
Mean anomaly: 59
1418 deg
Mean motion: 15
54090078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3017
Checksum: 316
Coasting Arc #7 (Orbit 3032)
---------------------------------------
Vector Time (GMT): 2016/074/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5212103
87 A = 6783104
99 meter
Y = -1927295
89 meter E =
0009725
Z = 3881855
06 I = 51
71806
XDOT = 4712
988641 Wp = 93
70911
YDOT = -4437
903626 meter/sec RA = 166
83517 deg
ZDOT = 4115
186242 TA = 313
13828
MA = 313
21957
Ha = 220
635 n
mi
Hp = 215
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17100078
32 X = -5209021
32
Y = -6323149
23 feet Y = -1985563
49 meter
Z = 12735744
95 Z = 3856543
71
XDOT = 15462
561157 XDOT = 4742
274357
YDOT = -14560
051266 feet/sec YDOT = -4385
035719 meter/sec
ZDOT = 13501
267198 ZDOT = 4138
152243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13909947
44 X = 4239751
98
Y = 11903266
71 feet Y = 3628115
69 meter
Z = 12626151
35 Z = 3848450
93
XDOT = -18611
237534 XDOT = -5672
705200
YDOT = 7287
719857 feet/sec YDOT = 2221
297012 meter/sec
ZDOT = 13601
668764 ZDOT = 4145
788639
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
02130175
00016717 00000-0 10270-3 0 9061
2 25544 51
6411 167
6628 0001842 305
0305 55
0675 15
54107912 30339
Satellite: ISS
Catalog Number: 25544
Epoch time: 16075
02130175 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 167
6628 deg
Eccentricity:
0001842
Arg of perigee: 305
0305 deg
Mean anomaly: 55
0675 deg
Mean motion: 15
54107912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3033
Checksum: 274
Coasting Arc #8 (Orbit 3047)
---------------------------------------
Vector Time (GMT): 2016/075/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3868940
51 A = 6779412
66 meter
Y = 2755109
10 meter E =
0010661
Z = -4847588
07 I = 51
73800
XDOT = -6007
928726 Wp = 63
65243
YDOT = 4042
105102 meter/sec RA = 161
85097 deg
ZDOT = -2497
350123 TA = 181
81139
MA = 181
81526
Ha = 220
497 n
mi
Hp = 215
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12693374
39 X = 3861392
01
Y = 9039071
83 feet Y = 2798331
51 meter
Z = -15904160
33 Z = -4828812
43
XDOT = -19711
052252 XDOT = -6040
551049
YDOT = 13261
499677 feet/sec YDOT = 3974
737821 meter/sec
ZDOT = -8193
405914 ZDOT = -2526
614562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9074024
87 X = -2765762
78
Y = -12769560
16 feet Y = -3892161
94 meter
Z = -15823062
12 Z = -4822869
34
XDOT = 22012
048898 XDOT = 6709
272504
YDOT = -5329
357043 feet/sec YDOT = -1624
388027 meter/sec
ZDOT = -8321
111077 ZDOT = -2536
274656
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
98583558
00016717 00000-0 10270-3 0 9074
2 25544 51
6419 162
8549 0001906 310
5395 49
5592 15
54153731 30489
Satellite: ISS
Catalog Number: 25544
Epoch time: 16075
98583558 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 162
8549 deg
Eccentricity:
0001906
Arg of perigee: 310
5395 deg
Mean anomaly: 49
5592 deg
Mean motion: 15
54153731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3048
Checksum: 337
Coasting Arc #9 (Orbit 3063)
---------------------------------------
Vector Time (GMT): 2016/076/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2280089
79 A = 6777286
73 meter
Y = -3562567
90 meter E =
0001153
Z = 5294371
94 I = 51
76189
XDOT = 6823
769547 Wp = 89
46278
YDOT = -3446
783900 meter/sec RA = 156
86100 deg
ZDOT = 619
307763 TA = 354
63608
MA = 354
63732
Ha = 220
474 n
mi
Hp = 215
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7480609
56 X = -2265800
36
Y = -11688214
91 feet Y = -3587984
98 meter
Z = 17369986
67 Z = 5283330
98
XDOT = 22387
695365 XDOT = 6858
796882
YDOT = -11308
346127 feet/sec YDOT = -3370
280066 meter/sec
ZDOT = 2031
849615 ZDOT = 652
541028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3519225
83 X = 1072660
03
Y = 13484548
28 feet Y = 4110090
32 meter
Z = 17322595
98 Z = 5279927
25
XDOT = -23815
285000 XDOT = -7258
898868
YDOT = 3418
651196 feet/sec YDOT = 1042
004884 meter/sec
ZDOT = 2176
715977 ZDOT = 663
463030
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
01465187
00016717 00000-0 10270-3 0 9088
2 25544 51
6422 157
7265 0002035 310
9928 49
1049 15
54198782 30647
Satellite: ISS
Catalog Number: 25544
Epoch time: 16077
01465187 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 157
7265 deg
Eccentricity:
0002035
Arg of perigee: 310
9928 deg
Mean anomaly: 49
1049 deg
Mean motion: 15
54198782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3064
Checksum: 319
Coasting Arc #10 (Orbit 3066)
---------------------------------------
Vector Time (GMT): 2016/077/03:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2231433
12 A = 6781180
50 meter
Y = -4726817
71 meter E =
0008732
Z = 4316207
04 I = 51
77990
XDOT = 6811
038184 Wp = 59
82112
YDOT = -13
010112 meter/sec RA = 155
83264 deg
ZDOT = -3525
874142 TA = 66
03869
MA = 65
94728
Ha = 220
331 n
mi
Hp = 215
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7320974
80 X = 2263157
65
Y = -15507932
13 feet Y = -4701686
54 meter
Z = 14160784
25 Z = 4327124
19
XDOT = 22345
925802 XDOT = 6827
804472
YDOT = -42
684093 feet/sec YDOT = 63
248844 meter/sec
ZDOT = -11567
828551 ZDOT = -3492
747423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8279926
03 X = 2523721
45
Y = 14972286
16 feet Y = 4563552
82 meter
Z = 14208937
82 Z = 4330884
25
XDOT = -12069
863326 XDOT = -3678
894342
YDOT = 17546
170044 feet/sec YDOT = 5348
072629 meter/sec
ZDOT = -11423
959216 ZDOT = -3482
022769
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
20755141
00016717 00000-0 10270-3 0 9092
2 25544 51
6412 156
7628 0002210 310
5397 49
5563 15
54193884 30675
Satellite: ISS
Catalog Number: 25544
Epoch time: 16077
20755141 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 156
7628 deg
Eccentricity:
0002210
Arg of perigee: 310
5397 deg
Mean anomaly: 49
5563 deg
Mean motion: 15
54193884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3067
Checksum: 311
Coasting Arc #11 (Orbit 3081)
---------------------------------------
Vector Time (GMT): 2016/078/03:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3635680
62 A = 6785011
93 meter
Y = 4817593
68 meter E =
0003899
Z = -3099403
35 I = 51
81972
XDOT = -5766
585906 Wp = 50
17259
YDOT = -1200
636621 meter/sec RA = 150
85790 deg
ZDOT = 4904
654545 TA = 274
29679
MA = 274
34134
Ha = 220
446 n
mi
Hp = 215
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11928086
01 X = -3674226
54
Y = 15805753
53 feet Y = 4776721
22 meter
Z = -10168646
16 Z = -3117158
52
XDOT = -18919
245099 XDOT = -5776
555930
YDOT = -3939
096526 feet/sec YDOT = -1265
177627 meter/sec
ZDOT = 16091
386302 ZDOT = 4876
618160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6118165
08 X = -1864816
72
Y = -18790404
12 feet Y = -5727315
18 meter
Z = -10246522
05 Z = -3123139
92
XDOT = 12783
327503 XDOT = 3896
358223
YDOT = -12859
105941 feet/sec YDOT = -3919
455491 meter/sec
ZDOT = 15969
800111 ZDOT = 4867
595074
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
17205094
00016717 00000-0 10270-3 0 9108
2 25544 51
6394 151
9541 0001988 314
9859 45
1132 15
54190182 30826
Satellite: ISS
Catalog Number: 25544
Epoch time: 16078
17205094 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 151
9541 deg
Eccentricity:
0001988
Arg of perigee: 314
9859 deg
Mean anomaly: 45
1132 deg
Mean motion: 15
54190182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3082
Checksum: 308
Coasting Arc #12 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2016/078/21:26:42
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3220975
74 A = 6777408
98 meter
Y = -2833645
04 meter E =
0001852
Z = 5245347
57 I = 51
81693
XDOT = 5909
275407 Wp = 105
34487
YDOT = -4776
622585 meter/sec RA = 147
27431 deg
ZDOT = 1047
453764 TA = 334
64569
MA = 334
65478
Ha = 220
530 n
mi
Hp = 214
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10567505
72 X = -3214529
16
Y = -9296735
69 feet Y = -2869627
46 meter
Z = 17209145
56 Z = 5229717
06
XDOT = 19387
386507 XDOT = 5957
161582
YDOT = -15671
333941 feet/sec YDOT = -4710
273267 meter/sec
ZDOT = 3436
528097 ZDOT = 1076
276069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1640242
20 X = 499945
82
Y = 14061579
81 feet Y = 4285969
53 meter
Z = 17141695
99 Z = 5224788
94
XDOT = -23844
109808 XDOT = -7267
684669
YDOT = -1564
629362 feet/sec YDOT = -476
899029 meter/sec
ZDOT = 3562
478286 ZDOT = 1085
843382
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
94364124
00016717 00000-0 10270-3 0 9114
2 25544 51
6416 148
1104 0002106 319
2505 40
8490 15
54240884 30940
Satellite: ISS
Catalog Number: 25544
Epoch time: 16078
94364124 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 148
1104 deg
Eccentricity:
0002106
Arg of perigee: 319
2505 deg
Mean anomaly: 40
8490 deg
Mean motion: 15
54240884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3094
Checksum: 288
Coasting Arc #13 (Orbit 3096)
---------------------------------------
Vector Time (GMT): 2016/079/03:12:07
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4693100
21 A = 6788009
35 meter
Y = 4641119
27 meter E =
0008616
Z = -1565925
36 I = 51
85738
XDOT = -4392
017970 Wp = 24
10775
YDOT = -2502
083614 meter/sec RA = 146
05663 deg
ZDOT = 5766
046242 TA = 318
82395
MA = 318
88892
Ha = 220
427 n
mi
Hp = 215
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15397310
39 X = -4737043
06
Y = 15226769
26 feet Y = 4588392
01 meter
Z = -5137550
41 Z = -1588830
29
XDOT = -14409
507775 XDOT = -4391
721255
YDOT = -8208
935741 feet/sec YDOT = -2551
195707 meter/sec
ZDOT = 18917
474548 ZDOT = 5744
712213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 367738
21 X = 112086
61
Y = -21627679
97 feet Y = -6592116
86 meter
Z = -5237778
28 Z = -1596474
82
XDOT = 14555
761709 XDOT = 4436
596169
YDOT = -4296
905899 feet/sec YDOT = -1309
696918 meter/sec
ZDOT = 18825
195709 ZDOT = 5737
919652
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
13653690
00016717 00000-0 10270-3 0 9126
2 25544 51
6403 147
1470 0002124 317
7295 42
3694 15
54209633 30973
Satellite: ISS
Catalog Number: 25544
Epoch time: 16079
13653690 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 147
1470 deg
Eccentricity:
0002124
Arg of perigee: 317
7295 deg
Mean anomaly: 42
3694 deg
Mean motion: 15
54209633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3097
Checksum: 303
Coasting Arc #14 (Orbit 3112)
---------------------------------------
Vector Time (GMT): 2016/080/03:12:07
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5368031
13 A = 6788964
66 meter
Y = -4144972
86 meter E =
0009635
Z = -184755
87 I = 51
88738
XDOT = 2767
687811 Wp = 133
88776
YDOT = 3844
099529 meter/sec RA = 141
10165 deg
ZDOT = -6029
220647 TA = 48
09569
MA = 48
01355
Ha = 220
502 n
mi
Hp = 214
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17611650
69 X = 5414879
74
Y = -13598992
33 feet Y = -4084682
05 meter
Z = -606154
44 Z = -158565
26
XDOT = 9080
340587 XDOT = 2753
783461
YDOT = 12611
875096 feet/sec YDOT = 3874
971074 meter/sec
ZDOT = -19780
907635 ZDOT = -6015
810373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2736053
19 X = -833949
01
Y = 22084892
58 feet Y = 6731475
26 meter
Z = -491719
63 Z = -149876
14
XDOT = -13827
929508 XDOT = -4214
752914
YDOT = -2134
082569 feet/sec YDOT = -650
468367 meter/sec
ZDOT = -19723
256873 ZDOT = -6011
648695
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
16530755
00016717 00000-0 10270-3 0 9138
2 25544 51
6407 142
0178 0002215 325
5624 34
5385 15
54250091 31133
Satellite: ISS
Catalog Number: 25544
Epoch time: 16080
16530755 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 142
0178 deg
Eccentricity:
0002215
Arg of perigee: 325
5624 deg
Mean anomaly: 34
5385 deg
Mean motion: 15
54250091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3113
Checksum: 275
Coasting Arc #15 (Orbit 3117)
---------------------------------------
Vector Time (GMT): 2016/080/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4639516
88 A = 6779138
41 meter
Y = -1032686
13 meter E =
0005624
Z = 4830203
17 I = 51
86493
XDOT = 4000
338867 Wp = 113
43583
YDOT = -6028
415654 meter/sec RA = 139
62506 deg
ZDOT = 2549
024519 TA = 311
54919
MA = 311
59741
Ha = 220
544 n
mi
Hp = 214
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15221512
09 X = -4651087
11
Y = -3388077
85 feet Y = -1084632
29 meter
Z = 15847123
25 Z = 4807637
85
XDOT = 13124
471350 XDOT = 4055
070867
YDOT = -19778
266581 feet/sec YDOT = -5983
374816 meter/sec
ZDOT = 8362
941335 ZDOT = 2568
590746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12251196
27 X = -3734164
62
Y = -9806834
78 feet Y = -2989123
24 meter
Z = 15749253
91 Z = 4800372
59
XDOT = 19747
152956 XDOT = 6018
932221
YDOT = -11076
659114 feet/sec YDOT = -3376
165698 meter/sec
ZDOT = 8448
898672 ZDOT = 2575
224315
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
48679488
00016717 00000-0 10270-3 0 9141
2 25544 51
6435 140
4143 0001854 317
8392 42
2618 15
54267818 31187
Satellite: ISS
Catalog Number: 25544
Epoch time: 16080
48679488 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 140
4143 deg
Eccentricity:
0001854
Arg of perigee: 317
8392 deg
Mean anomaly: 42
2618 deg
Mean motion: 15
54267818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3118
Checksum: 322
Coasting Arc #16 (Orbit 3132)
---------------------------------------
Vector Time (GMT): 2016/081/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3463838
82 A = 6777180
56 meter
Y = 2421744
59 meter E =
0013762
Z = -5309710
18 I = 51
88062
XDOT = -5000
161766 Wp = 78
26125
YDOT = 5766
739676 meter/sec RA = 134
64305 deg
ZDOT = -630
361728 TA = 185
72558
MA = 185
74133
Ha = 220
515 n
mi
Hp = 214
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11364300
57 X = 3462292
90
Y = 7945356
28 feet Y = 2460470
08 meter
Z = -17420309
01 Z = -5292888
00
XDOT = -16404
730202 XDOT = -5061
213261
YDOT = 18919
749594 feet/sec YDOT = 5710
483086 meter/sec
ZDOT = -2068
115907 ZDOT = -654
800230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6995642
86 X = 2132271
94
Y = 12077446
17 feet Y = 3681205
59 meter
Z = -17347606
60 Z = -5287550
49
XDOT = -22010
899649 XDOT = -6708
922213
YDOT = 9618
653639 feet/sec YDOT = 2931
765629 meter/sec
ZDOT = -2175
211065 ZDOT = -663
004332
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
45125225
00016717 00000-0 10270-3 0 9155
2 25544 51
6422 135
6068 0001933 324
1823 35
9200 15
54238997 31332
Satellite: ISS
Catalog Number: 25544
Epoch time: 16081
45125225 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 135
6068 deg
Eccentricity:
0001933
Arg of perigee: 324
1823 deg
Mean anomaly: 35
9200 deg
Mean motion: 15
54238997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3133
Checksum: 291
Coasting Arc #17 (Orbit 3148)
---------------------------------------
Vector Time (GMT): 2016/082/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2156479
00 A = 6777412
23 meter
Y = -3779670
50 meter E =
0004777
Z = 5194523
10 I = 51
90401
XDOT = 5591
592788 Wp = 31
56745
YDOT = -5070
148102 meter/sec RA = 129
65934 deg
ZDOT = -1363
318715 TA = 71
51173
MA = 71
45982
Ha = 220
507 n
mi
Hp = 214
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7075062
35 X = -2139286
14
Y = -12400493
77 feet Y = -3803688
71 meter
Z = 17042398
62 Z = 5184089
89
XDOT = 18345
120695 XDOT = 5654
495248
YDOT = -16634
344168 feet/sec YDOT = -5007
267706 meter/sec
ZDOT = -4472
830431 ZDOT = -1336
002703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1459944
26 X = -444991
01
Y = -14255518
98 feet Y = -4345082
18 meter
Z = 16997671
75 Z = 5180890
35
XDOT = 22543
899345 XDOT = 6871
380520
YDOT = -7517
284255 feet/sec YDOT = -2291
268241 meter/sec
ZDOT = -4353
331656 ZDOT = -1326
895489
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
47999336
00016717 00000-0 10270-3 0 9161
2 25544 51
6423 130
4777 0001944 327
0710 33
0321 15
54306725 31497
Satellite: ISS
Catalog Number: 25544
Epoch time: 16082
47999336 = yrday
fracday
Element set: 916
Inclination: 51
6423 deg
RA of node: 130
4777 deg
Eccentricity:
0001944
Arg of perigee: 327
0710 deg
Mean anomaly: 33
0321 deg
Mean motion: 15
54306725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3149
Checksum: 302
Coasting Arc #18 (Orbit 3163)
---------------------------------------
Vector Time (GMT): 2016/083/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 863965
32 A = 6780137
86 meter
Y = 4981118
47 meter E =
0008512
Z = -4526072
83 I = 51
93216
XDOT = -5757
316739 Wp = 101
00556
YDOT = 3908
148257 meter/sec RA = 124
68157 deg
ZDOT = 3205
595116 TA = 201
08132
MA = 201
11642
Ha = 220
580 n
mi
Hp = 214
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2834531
88 X = 830186
68
Y = 16342252
19 feet Y = 4990590
30 meter
Z = -14849320
29 Z = -4521958
76
XDOT = -18888
834446 XDOT = -5816
162108
YDOT = 12822
008718 feet/sec YDOT = 3843
437611 meter/sec
ZDOT = 10517
044343 ZDOT = 3177
483997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3760379
93 X = -1146163
80
Y = 16170035
47 feet Y = 4928626
81 meter
Z = -14832248
20 Z = -4520869
25
XDOT = -21299
790100 XDOT = -6492
176023
YDOT = 4570
401689 feet/sec YDOT = 1393
058435 meter/sec
ZDOT = 10394
265379 ZDOT = 3168
172087
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
44442881
00016717 00000-0 10270-3 0 9178
2 25544 51
6415 125
6692 0001929 338
1438 21
9633 15
54312411 31641
Satellite: ISS
Catalog Number: 25544
Epoch time: 16083
44442881 = yrday
fracday
Element set: 917
Inclination: 51
6415 deg
RA of node: 125
6692 deg
Eccentricity:
0001929
Arg of perigee: 338
1438 deg
Mean anomaly: 21
9633 deg
Mean motion: 15
54312411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3164
Checksum: 303
Coasting Arc #19 (Orbit 3175)
---------------------------------------
Vector Time (GMT): 2016/084/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2226305
91 A = 6787649
00 meter
Y = -6194079
22 meter E =
0012750
Z = 1635819
38 I = 51
96786
XDOT = 5067
758538 Wp = 110
68148
YDOT = 294
883124 meter/sec RA = 120
97915 deg
ZDOT = -5748
800563 TA = 51
48754
MA = 51
37328
Ha = 220
625 n
mi
Hp = 214
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7304153
23 X = 2287458
06
Y = -20321782
23 feet Y = -6168841
01 meter
Z = 5366861
49 Z = 1646783
75
XDOT = 16626
504390 XDOT = 5092
009670
YDOT = 967
464318 feet/sec YDOT = 351
688849 meter/sec
ZDOT = -18860
894235 ZDOT = -5724
123779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15667135
81 X = 4775342
99
Y = 14843913
39 feet Y = 4524424
80 meter
Z = 5415512
97 Z = 1650648
35
XDOT = -6551
977464 XDOT = -1997
042731
YDOT = 13794
868201 feet/sec YDOT = 4204
675828 meter/sec
ZDOT = -18753
713462 ZDOT = -5716
131863
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
21596912
00016717 00000-0 10270-3 0 9180
2 25544 51
6389 121
8184 0001806 342
6450 17
4641 15
54309807 31760
Satellite: ISS
Catalog Number: 25544
Epoch time: 16084
21596912 = yrday
fracday
Element set: 918
Inclination: 51
6389 deg
RA of node: 121
8184 deg
Eccentricity:
0001806
Arg of perigee: 342
6450 deg
Mean anomaly: 17
4641 deg
Mean motion: 15
54309807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3176
Checksum: 314
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