[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 12th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
132/13:18:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 213
2
135/07:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 213
1
Coasting Arc #1 (Orbit 3926)
---------------------------------------
Vector Time (GMT): 2016/132/11:20:16
127
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1459414
30 A = 6785892
12 meter
Y = 6221634
88 meter E =
0007467
Z = -2278815
33 I = 51
33195
XDOT = -5389
337443 Wp = 129
49483
YDOT = -709
422114 meter/sec RA = 240
21844 deg
ZDOT = -5404
875626 TA = 75
98432
MA = 75
90131
Ha = 220
939 n
mi
Hp = 213
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4788104
67 X = 1400803
54
Y = 20412187
93 feet Y = 6237627
42 meter
Z = -7476428
26 Z = -2271867
87
XDOT = -17681
553291 XDOT = -5354
749227
YDOT = -2327
500373 feet/sec YDOT = -769
495606 meter/sec
ZDOT = -17732
531580 ZDOT = -5430
971880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16579862
38 X = 5053542
05
Y = 12850121
77 feet Y = 3916717
12 meter
Z = -7447340
18 Z = -2269949
29
XDOT = -14198
069423 XDOT = -4327
571560
YDOT = 8008
014109 feet/sec YDOT = 2440
842700 meter/sec
ZDOT = -17845
777798 ZDOT = -5439
393073
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 16132
50008382
00016717 00000-0 10270-3 0 9006
2 25544 51
6423 241
0526 0001722 105
2967 254
8376 15
54557745 39279
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
50008382 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 241
0526 deg
Eccentricity:
0001722
Arg of perigee: 105
2967 deg
Mean anomaly: 254
8376 deg
Mean motion: 15
54557745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3927
Checksum: 299
Coasting Arc #2 (Orbit 3927)
---------------------------------------
Vector Time (GMT): 2016/132/13:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4937902
22 A = 6779589
02 meter
Y = -1422172
85 meter E =
0010992
Z = -4433470
42 I = 51
31299
XDOT = -961
824354 Wp = 109
65642
YDOT = -6857
436122 meter/sec RA = 239
76770 deg
ZDOT = 3274
012630 TA = 193
53141
MA = 193
56090
Ha = 220
871 n
mi
Hp = 213
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16200466
59 X = -4900096
10
Y = -4665921
42 feet Y = -1477180
15 meter
Z = -14545506
62 Z = -4457365
91
XDOT = -3155
591713 XDOT = -900
975151
YDOT = -22498
150008 feet/sec YDOT = -6867
851814 meter/sec
ZDOT = 10741
511254 ZDOT = 3269
487758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10267165
38 X = -3129432
01
Y = 13258500
29 feet Y = 4041190
89 meter
Z = -14649067
83 Z = -4465035
87
XDOT = -21138
204693 XDOT = -6442
924791
YDOT = -4532
239544 feet/sec YDOT = -1381
426613 meter/sec
ZDOT = 10723
058346 ZDOT = 3268
388184
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 16132
56436761
00016717 00000-0 10270-3 0 9019
2 25544 51
6428 240
7342 0001643 103
1912 256
9424 15
54575449 39284
Satellite: ISS
Catalog Number: 25544
Epoch time: 16132
56436761 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 240
7342 deg
Eccentricity:
0001643
Arg of perigee: 103
1912 deg
Mean anomaly: 256
9424 deg
Mean motion: 15
54575449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3928
Checksum: 307
Coasting Arc #3 (Orbit 3943)
---------------------------------------
Vector Time (GMT): 2016/133/13:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5200254
42 A = 6783749
79 meter
Y = 2996510
54 meter E =
0014514
Z = 3147861
70 I = 51
34352
XDOT = -506
786694 Wp = 94
95907
YDOT = 5954
169820 meter/sec RA = 234
75701 deg
ZDOT = -4812
728591 TA = 48
54308
MA = 48
41853
Ha = 220
821 n
mi
Hp = 213
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17061202
18 X = 5151069
17
Y = 9831071
32 feet Y = 3054388
12 meter
Z = 10327630
26 Z = 3173004
00
XDOT = -1662
686005 XDOT = -549
951770
YDOT = 19534
677888 feet/sec YDOT = 5948
261414 meter/sec
ZDOT = -15789
791965 ZDOT = -4815
295079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15184361
34 X = 4628193
34
Y = -12446378
97 feet Y = -3793656
31 meter
Z = 10436347
58 Z = 3180998
74
XDOT = 16826
309090 XDOT = 5128
659010
YDOT = 7228
894745 feet/sec YDOT = 2203
367118 meter/sec
ZDOT = -15801
978266 ZDOT = -4816
442976
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 16133
59291572
00016717 00000-0 10270-3 0 9023
2 25544 51
6425 235
6039 0001668 100
8340 259
3000 15
54570922 39449
Satellite: ISS
Catalog Number: 25544
Epoch time: 16133
59291572 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 235
6039 deg
Eccentricity:
0001668
Arg of perigee: 100
8340 deg
Mean anomaly: 259
3000 deg
Mean motion: 15
54570922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3944
Checksum: 296
Coasting Arc #4 (Orbit 3958)
---------------------------------------
Vector Time (GMT): 2016/134/13:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5119942
46 A = 6787110
59 meter
Y = -4189392
56 meter E =
0008980
Z = -1504132
31 I = 51
37299
XDOT = 2102
135783 Wp = 46
49466
YDOT = -4621
593367 meter/sec RA = 229
75929 deg
ZDOT = 5744
473310 TA = 297
01863
MA = 297
11027
Ha = 220
855 n
mi
Hp = 213
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16797711
48 X = -5065408
64
Y = -13744726
24 feet Y = -4246342
21 meter
Z = -4934817
30 Z = -1528871
46
XDOT = 6896
770941 XDOT = 2125
755055
YDOT = -15162
707898 feet/sec YDOT = -4597
953945 meter/sec
ZDOT = 18846
697212 ZDOT = 5754
742277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18577108
55 X = -5662302
69
Y = 11176153
72 feet Y = 3406491
65 meter
Z = -5041592
84 Z = -1536677
50
XDOT = -11190
321375 XDOT = -3410
809955
YDOT = -10118
434306 feet/sec YDOT = -3084
098777 meter/sec
ZDOT = 18892
113563 ZDOT = 5758
316214
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 16134
55716909
00016717 00000-0 10270-3 0 9037
2 25544 51
6417 230
7945 0001507 99
8035 260
3288 15
54545535 39590
Satellite: ISS
Catalog Number: 25544
Epoch time: 16134
55716909 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 230
7945 deg
Eccentricity:
0001507
Arg of perigee: 99
8035 deg
Mean anomaly: 260
3288 deg
Mean motion: 15
54545535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3959
Checksum: 331
Coasting Arc #5 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2016/135/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3693023
78 A = 6776207
71 meter
Y = 2215760
45 meter E =
0016331
Z = -5245861
62 I = 51
35110
XDOT = -4774
211048 Wp = 97
82444
YDOT = -5924
642303 meter/sec RA = 225
95974 deg
ZDOT = 858
643496 TA = 180
43007
MA = 180
43148
Ha = 220
903 n
mi
Hp = 213
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12116219
75 X = -3692044
22
Y = 7269555
28 feet Y = 2174468
14 meter
Z = -17210832
07 Z = -5263799
09
XDOT = -15663
422073 XDOT = -4711
776329
YDOT = -19437
802833 feet/sec YDOT = -5977
681626 meter/sec
ZDOT = 2817
071837 ZDOT = 835
603019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13502382
75 X = -4115526
26
Y = 3825261
71 feet Y = 1165939
77 meter
Z = -17289158
13 Z = -5269735
40
XDOT = -9688
190616 XDOT = -2952
960500
YDOT = -21914
644033 feet/sec YDOT = -6679
583501 meter/sec
ZDOT = 2717
962166 ZDOT = 828
434868
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 16135
32856596
00016717 00000-0 10270-3 0 9041
2 25544 51
6397 226
9444 0001833 106
3364 253
7990 15
54602085 39713
Satellite: ISS
Catalog Number: 25544
Epoch time: 16135
32856596 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 226
9444 deg
Eccentricity:
0001833
Arg of perigee: 106
3364 deg
Mean anomaly: 253
7990 deg
Mean motion: 15
54602085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 328
Coasting Arc #6 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2016/136/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4884227
73 A = 6778723
22 meter
Y = -675547
18 meter E =
0009479
Z = 4645304
52 I = 51
38216
XDOT = 3587
007676 Wp = 72
32273
YDOT = 6146
150150 meter/sec RA = 220
93789 deg
ZDOT = -2870
024529 TA = 46
31778
MA = 46
23927
Ha = 220
818 n
mi
Hp = 213
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16024369
18 X = 4868853
80
Y = -2216362
15 feet Y = -621014
49 meter
Z = 15240500
39 Z = 4668993
71
XDOT = 11768
397888 XDOT = 3531
954742
YDOT = 20164
534613 feet/sec YDOT = 6185
954655 meter/sec
ZDOT = -9416
090975 ZDOT = -2852
733294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15976791
67 X = 4869726
10
Y = 1811811
95 feet Y = 552240
28 meter
Z = 15343564
98 Z = 4676718
61
XDOT = 6579
619937 XDOT = 2005
468157
YDOT = 21305
455083 feet/sec YDOT = 6493
902709 meter/sec
ZDOT = -9341
987492 ZDOT = -2847
437788
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 16136
35708493
00016717 00000-0 10270-3 0 9058
2 25544 51
6395 221
8123 0001895 109
1835 250
9523 15
54579124 39876
Satellite: ISS
Catalog Number: 25544
Epoch time: 16136
35708493 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 221
8123 deg
Eccentricity:
0001895
Arg of perigee: 109
1835 deg
Mean anomaly: 250
9523 deg
Mean motion: 15
54579124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3987
Checksum: 328
Coasting Arc #7 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2016/137/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5772331
62 A = 6782628
99 meter
Y = -745325
29 meter E =
0006933
Z = -3489706
95 I = 51
42126
XDOT = -1966
442102 Wp = 99
51171
YDOT = -5871
050552 meter/sec RA = 215
93010 deg
ZDOT = 4513
178921 TA = 219
35652
MA = 219
40693
Ha = 220
843 n
mi
Hp = 213
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18938095
86 X = -5746616
52
Y = -2445292
94 feet Y = -809731
54 meter
Z = -11449169
79 Z = -3517685
33
XDOT = -6451
581700 XDOT = -1922
567704
YDOT = -19261
976876 feet/sec YDOT = -5892
795321 meter/sec
ZDOT = 14807
017458 ZDOT = 4503
732877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17783249
34 X = -5420334
40
Y = -6752084
48 feet Y = -2058035
35 meter
Z = -11570644
72 Z = -3526732
51
XDOT = -2396
599755 XDOT = -730
483605
YDOT = -18956
754934 feet/sec YDOT = -5778
018904 meter/sec
ZDOT = 14766
951556 ZDOT = 4500
966834
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 16137
32131189
00016717 00000-0 10270-3 0 9069
2 25544 51
6402 217
0031 0001846 111
2950 248
8400 15
54619369 40023
Satellite: ISS
Catalog Number: 25544
Epoch time: 16137
32131189 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 217
0031 deg
Eccentricity:
0001846
Arg of perigee: 111
2950 deg
Mean anomaly: 248
8400 deg
Mean motion: 15
54619369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4002
Checksum: 276
Coasting Arc #8 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2016/138/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6206730
66 A = 6786346
23 meter
Y = 1991784
30 meter E =
0015705
Z = 1860769
46 I = 51
46008
XDOT = 16
252276 Wp = 113
88262
YDOT = 5226
210341 meter/sec RA = 210
93528 deg
ZDOT = -5617
078696 TA = 45
57264
MA = 45
44422
Ha = 220
755 n
mi
Hp = 213
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20363289
56 X = 6174957
79
Y = 6534725
40 feet Y = 2061014
43 meter
Z = 6104886
69 Z = 1890843
46
XDOT = 53
321115 XDOT = -14
904008
YDOT = 17146
359388 feet/sec YDOT = 5226
217932 meter/sec
ZDOT = -18428
735880 ZDOT = -5617
075373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18443014
18 X = 5621430
72
Y = 10752322
70 feet Y = 3277307
96 meter
Z = 6235272
53 Z = 1900511
07
XDOT = -2734
333002 XDOT = -833
424699
YDOT = 15435
744413 feet/sec YDOT = 4704
814897 meter/sec
ZDOT = -18429
597558 ZDOT = -5617
341336
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 16138
34981353
00016717 00000-0 10270-3 0 9079
2 25544 51
6401 211
8719 0001752 117
2045 242
9287 15
54628918 40189
Satellite: ISS
Catalog Number: 25544
Epoch time: 16138
34981353 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 211
8719 deg
Eccentricity:
0001752
Arg of perigee: 117
2045 deg
Mean anomaly: 242
9287 deg
Mean motion: 15
54628918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4018
Checksum: 312
Coasting Arc #9 (Orbit 4032)
---------------------------------------
Vector Time (GMT): 2016/139/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6109338
20 A = 6787816
38 meter
Y = -2946137
80 meter E =
0012667
Z = -30651
35 I = 51
49481
XDOT = 2056
507797 Wp = 53
00299
YDOT = -4309
043984 meter/sec RA = 205
95100 deg
ZDOT = 6001
241250 TA = 306
66614
MA = 306
78250
Ha = 220
764 n
mi
Hp = 213
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20043760
49 X = -6075790
79
Y = -9665806
44 feet Y = -3014268
91 meter
Z = -100562
18 Z = -60248
04
XDOT = 6747
072825 XDOT = 2075
387845
YDOT = -14137
283413 feet/sec YDOT = -4285
941295 meter/sec
ZDOT = 19689
111711 ZDOT = 6011
277187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17729527
94 X = -5403960
12
Y = -13446255
41 feet Y = -4098418
65 meter
Z = -228726
55 Z = -69715
85
XDOT = 8309
753183 XDOT = 2532
812770
YDOT = -11250
204289 feet/sec YDOT = -3429
062267 meter/sec
ZDOT = 19733
458469 ZDOT = 6014
758141
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 16139
31402592
00016717 00000-0 10270-3 0 9081
2 25544 51
6418 207
0622 0001778 116
0505 244
0831 15
54647722 40332
Satellite: ISS
Catalog Number: 25544
Epoch time: 16139
31402592 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 207
0622 deg
Eccentricity:
0001778
Arg of perigee: 116
0505 deg
Mean anomaly: 244
0831 deg
Mean motion: 15
54647722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4033
Checksum: 287
Coasting Arc #10 (Orbit 4048)
---------------------------------------
Vector Time (GMT): 2016/140/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5412290
35 A = 6786358
25 meter
Y = 3647891
60 meter E =
0008981
Z = -1848546
63 I = 51
51850
XDOT = -4087
866452 Wp = 137
31612
YDOT = 3224
470668 meter/sec RA = 200
96922 deg
ZDOT = -5628
108689 TA = 63
05555
MA = 62
96384
Ha = 220
775 n
mi
Hp = 213
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17756858
10 X = 5380076
06
Y = 11968148
30 feet Y = 3708235
37 meter
Z = -6064785
54 Z = -1822332
73
XDOT = -13411
635340 XDOT = -4096
280045
YDOT = 10578
972008 feet/sec YDOT = 3178
710566 meter/sec
ZDOT = -18464
923519 ZDOT = -5647
987213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15330982
14 X = 4672883
36
Y = 14995521
24 feet Y = 4570634
87 meter
Z = -5951431
45 Z = -1813996
31
XDOT = -13896
297711 XDOT = -4235
591542
YDOT = 6874
161381 feet/sec YDOT = 2095
244389 meter/sec
ZDOT = -18551
883078 ZDOT = -5654
613962
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 16140
34251199
00016717 00000-0 10270-3 0 9092
2 25544 51
6409 201
9316 0001781 118
1163 242
0171 15
54669124 40494
Satellite: ISS
Catalog Number: 25544
Epoch time: 16140
34251199 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 201
9316 deg
Eccentricity:
0001781
Arg of perigee: 118
1163 deg
Mean anomaly: 242
0171 deg
Mean motion: 15
54669124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4049
Checksum: 290
Coasting Arc #11 (Orbit 4064)
---------------------------------------
Vector Time (GMT): 2016/141/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4185348
70 A = 6782667
59 meter
Y = -4056304
41 meter E =
0013827
Z = 3458304
26 I = 51
53708
XDOT = 5808
556035 Wp = 95
16991
YDOT = -2097
932375 meter/sec RA = 195
98132 deg
ZDOT = 4552
085741 TA = 305
49959
MA = 305
62851
Ha = 220
702 n
mi
Hp = 213
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13731459
00 X = -4156478
30
Y = -13308085
33 feet Y = -4102946
51 meter
Z = 11346142
58 Z = 3438042
41
XDOT = 19056
942373 XDOT = 5809
471437
YDOT = -6882
980233 feet/sec YDOT = -2032
972341 meter/sec
ZDOT = 14934
664505 ZDOT = 4580
304917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11429485
94 X = -3483707
31
Y = -15394838
34 feet Y = -4692346
73 meter
Z = 11258723
57 Z = 3431658
94
XDOT = 18710
940911 XDOT = 5703
094790
YDOT = -2838
375645 feet/sec YDOT = -865
136896 meter/sec
ZDOT = 15057
710481 ZDOT = 4589
590155
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 16141
37099044
00016717 00000-0 10270-3 0 9107
2 25544 51
6413 196
8012 0001754 127
0067 233
1247 15
54701187 40655
Satellite: ISS
Catalog Number: 25544
Epoch time: 16141
37099044 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 196
8012 deg
Eccentricity:
0001754
Arg of perigee: 127
0067 deg
Mean anomaly: 233
1247 deg
Mean motion: 15
54701187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4065
Checksum: 286
Coasting Arc #12 (Orbit 4079)
---------------------------------------
Vector Time (GMT): 2016/142/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2485442
56 A = 6778603
15 meter
Y = 4255228
07 meter E =
0011477
Z = -4665433
04 I = 51
55485
XDOT = -7034
455099 Wp = 77
84079
YDOT = 960
122774 meter/sec RA = 190
98302 deg
ZDOT = -2875
428048 TA = 163
53821
MA = 163
50091
Ha = 220
680 n
mi
Hp = 213
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8154339
11 X = 2460337
91
Y = 13960722
02 feet Y = 4282881
88 meter
Z = -15306538
83 Z = -4653419
84
XDOT = -23078
920930 XDOT = -7030
700758
YDOT = 3150
009101 feet/sec YDOT = 881
479998 meter/sec
ZDOT = -9433
819055 ZDOT = -2909
591141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6105597
73 X = 1860986
19
Y = 15023029
23 feet Y = 4579019
31 meter
Z = -15255012
47 Z = -4649727
80
XDOT = -22134
962992 XDOT = -6746
736720
YDOT = -722
382691 feet/sec YDOT = -220
182244 meter/sec
ZDOT = -9582
537401 ZDOT = -2920
757400
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 16142
33518485
00016717 00000-0 10270-3 0 9110
2 25544 51
6418 191
9914 0001698 127
1431 232
9877 15
54669228 40802
Satellite: ISS
Catalog Number: 25544
Epoch time: 16142
33518485 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 191
9914 deg
Eccentricity:
0001698
Arg of perigee: 127
1431 deg
Mean anomaly: 232
9877 deg
Mean motion: 15
54669228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4080
Checksum: 326
Coasting Arc #13 (Orbit 4095)
---------------------------------------
Vector Time (GMT): 2016/143/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -518576
88 A = 6775880
27 meter
Y = -4244051
46 meter E =
0005068
Z = 5253264
85 I = 51
57778
XDOT = 7624
787579 Wp = 123
35986
YDOT = 121
909604 meter/sec RA = 185
97562 deg
ZDOT = 847
851149 TA = 318
51262
MA = 318
55108
Ha = 220
597 n
mi
Hp = 213
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1701367
73 X = -496598
84
Y = -13924053
34 feet Y = -4249728
07 meter
Z = 17235120
91 Z = 5250798
73
XDOT = 25015
707279 XDOT = 7618
739094
YDOT = 399
965892 feet/sec YDOT = 207
141163 meter/sec
ZDOT = 2781
663876 ZDOT = 884
876434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17571
02 X = 5355
65
Y = -14039894
83 feet Y = -4279359
95 meter
Z = 17225108
15 Z = 5250212
96
XDOT = 23708
115016 XDOT = 7226
233457
YDOT = 3653
312198 feet/sec YDOT = 1113
529558 meter/sec
ZDOT = 2942
669074 ZDOT = 896
925534
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 16143
36364919
00016717 00000-0 10270-3 0 9126
2 25544 51
6415 186
8602 0001668 127
4560 232
6745 15
54723264 40968
Satellite: ISS
Catalog Number: 25544
Epoch time: 16143
36364919 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 186
8602 deg
Eccentricity:
0001668
Arg of perigee: 127
4560 deg
Mean anomaly: 232
6745 deg
Mean motion: 15
54723264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4096
Checksum: 318
Coasting Arc #14 (Orbit 4110)
---------------------------------------
Vector Time (GMT): 2016/144/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1538839
43 A = 6776164
68 meter
Y = 4089200
87 meter E =
0015608
Z = -5193289
19 I = 51
61040
XDOT = -7457
607682 Wp = 103
10023
YDOT = -1155
790098 meter/sec RA = 180
96805 deg
ZDOT = 1299
553919 TA = 179
40508
MA = 179
40322
Ha = 220
602 n
mi
Hp = 213
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5048685
79 X = -1559224
38
Y = 13416013
36 feet Y = 4071879
05 meter
Z = -17038350
35 Z = -5200813
73
XDOT = -24467
216806 XDOT = -7450
441849
YDOT = -3791
962265 feet/sec YDOT = -1239
146084 meter/sec
ZDOT = 4263
628343 ZDOT = 1263
343469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6426269
15 X = -1958726
84
Y = 12768783
05 feet Y = 3891925
08 meter
Z = -17071768
20 Z = -5203474
95
XDOT = -22976
069151 XDOT = -7003
105877
YDOT = -6072
561074 feet/sec YDOT = -1850
916615 meter/sec
ZDOT = 4106
318026 ZDOT = 1251
605734
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 16144
32783159
00016717 00000-0 10270-3 0 9135
2 25544 51
6412 182
0512 0001732 128
2756 231
8553 15
54716800 41115
Satellite: ISS
Catalog Number: 25544
Epoch time: 16144
32783159 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 182
0512 deg
Eccentricity:
0001732
Arg of perigee: 128
2756 deg
Mean anomaly: 231
8553 deg
Mean motion: 15
54716800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4111
Checksum: 284
Coasting Arc #15 (Orbit 4126)
---------------------------------------
Vector Time (GMT): 2016/145/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3454027
96 A = 6779177
45 meter
Y = -3768761
39 meter E =
0010027
Z = 4445060
47 I = 51
65282
XDOT = 6590
257985 Wp = 77
87690
YDOT = 2146
520323 meter/sec RA = 175
96608 deg
ZDOT = -3292
680944 TA = 45
33505
MA = 45
25337
Ha = 220
537 n
mi
Hp = 213
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11332112
72 X = 3474322
03
Y = -12364702
74 feet Y = -3730023
13 meter
Z = 14583531
71 Z = 4461888
39
XDOT = 21621
581317 XDOT = 6581
759872
YDOT = 7042
389510 feet/sec YDOT = 2220
169786 meter/sec
ZDOT = -10802
759001 ZDOT = -3260
687153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12374543
14 X = 3771760
75
Y = -11225599
63 feet Y = -3421562
77 meter
Z = 14657375
11 Z = 4467567
93
XDOT = 20094
660150 XDOT = 6124
852414
YDOT = 8191
825962 feet/sec YDOT = 2496
868553 meter/sec
ZDOT = -10663
936336 ZDOT = -3250
367795
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 16145
35628579
00016717 00000-0 10270-3 0 9144
2 25544 51
6414 176
9195 0001728 130
2010 229
9295 15
54702670 41275
Satellite: ISS
Catalog Number: 25544
Epoch time: 16145
35628579 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 176
9195 deg
Eccentricity:
0001728
Arg of perigee: 130
2010 deg
Mean anomaly: 229
9295 deg
Mean motion: 15
54702670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4127
Checksum: 313
Coasting Arc #16 (Orbit 4141)
---------------------------------------
Vector Time (GMT): 2016/146/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5014926
52 A = 6783365
82 meter
Y = 3314017
53 meter E =
0005575
Z = -3148575
35 I = 51
69895
XDOT = -5072
884890 Wp = 91
89804
YDOT = -3074
173436 meter/sec RA = 170
97885 deg
ZDOT = 4851
427722 TA = 231
85536
MA = 231
90561
Ha = 220
512 n
mi
Hp = 213
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16453171
01 X = -5036317
42
Y = 10872760
93 feet Y = 3257818
00 meter
Z = -10329971
63 Z = -3172988
45
XDOT = -16643
323130 XDOT = -5061
698035
YDOT = -10085
870854 feet/sec YDOT = -3130
839749 meter/sec
ZDOT = 15916
757617 ZDOT = 4826
811559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17194023
60 X = -5240738
39
Y = 9543154
76 feet Y = 2908753
57 meter
Z = -10436753
82 Z = -3181122
56
XDOT = -15200
511843 XDOT = -4633
116010
YDOT = -10122
079278 feet/sec YDOT = -3085
209764 meter/sec
ZDOT = 15810
171308 ZDOT = 4818
940215
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 16146
32045399
00016717 00000-0 10270-3 0 9156
2 25544 51
6416 172
1095 0001515 132
8606 227
2674 15
54703128 41425
Satellite: ISS
Catalog Number: 25544
Epoch time: 16146
32045399 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 172
1095 deg
Eccentricity:
0001515
Arg of perigee: 132
8606 deg
Mean anomaly: 227
2674 deg
Mean motion: 15
54703128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4142
Checksum: 295
Coasting Arc #17 (Orbit 4157)
---------------------------------------
Vector Time (GMT): 2016/147/07:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 926503
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6073683
88 A = 6786740
22 meter
Y = -2660172
76 meter E =
0015495
Z = 1410717
74 I = 51
74109
XDOT = 3088
054559 Wp = 121
11883
YDOT = 3950
086555 meter/sec RA = 166
00595 deg
ZDOT = -5807
347256 TA = 43
51312
MA = 43
39097
Ha = 220
535 n
mi
Hp = 213
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19926784
38 X = 6096126
49
Y = -8727600
93 feet Y = -2592127
44 meter
Z = 4628339
05 Z = 1440276
61
XDOT = 10131
412594 XDOT = 3071
863941
YDOT = 12959
601559 feet/sec YDOT = 3984
529260 meter/sec
ZDOT = -19052
976561 ZDOT = -5792
385122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20398227
14 X = 6217379
63
Y = -7479877
09 feet Y = -2279866
54 meter
Z = 4757419
93 Z = 1450061
60
XDOT = 8887
440148 XDOT = 2708
891757
YDOT = 12079
741625 feet/sec YDOT = 3681
905247 meter/sec
ZDOT = -18988
534387 ZDOT = -5787
705281
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 16147
34889630
00016717 00000-0 10270-3 0 9164
2 25544 51
6409 166
9787 0001693 136
0598 224
0690 15
54713767 41589
Satellite: ISS
Catalog Number: 25544
Epoch time: 16147
34889630 = yrday
fracday
Element set: 916
Inclination: 51
6409 deg
RA of node: 166
9787 deg
Eccentricity:
0001693
Arg of perigee: 136
0598 deg
Mean anomaly: 224
0690 deg
Mean motion: 15
54713767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4158
Checksum: 347
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