[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 2nd 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 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
093/18:00:53
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
0
094/18:43:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 213
9
098/16:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 213
8
104/12:19:00
253 2
9 3
0 3
0
N/A 0
4 0
0 221
4
000/00:08:00
506 -0
9 -0
0 215
1
Coasting Arc #1 (Orbit 3304)
---------------------------------------
Vector Time (GMT): 2016/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907109
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4132380
95 A = 6780235
06 meter
Y = 2889943
36 meter E =
0009837
Z = -4541409
27 I = 51
99378
XDOT = -1288
382955 Wp = 95
64108
YDOT = 6845
260110 meter/sec RA = 79
69796 deg
ZDOT = 3188
644722 TA = 206
22193
MA = 206
27177
Ha = 221
227 n
mi
Hp = 214
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13557680
29 X = 4121817
96
Y = 9481441
47 feet Y = 2936094
93 meter
Z = -14899636
73 Z = -4521361
12
XDOT = -4226
978198 XDOT = -1380
321656
YDOT = 22458
202459 feet/sec YDOT = 6830
338775 meter/sec
ZDOT = 10461
432815 ZDOT = 3182
162177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15021797
39 X = 4578643
85
Y = 7115330
95 feet Y = 2168752
87 meter
Z = -14813010
17 Z = -4515005
50
XDOT = -37
966405 XDOT = -11
572160
YDOT = 21763
784978 feet/sec YDOT = 6633
601661 meter/sec
ZDOT = 10432
021776 ZDOT = 3179
680237
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 16092
51037899
00016717 00000-0 10270-3 0 9007
2 25544 51
6392 80
4699 0002498 17
3246 342
7991 15
54287257 33052
Satellite: ISS
Catalog Number: 25544
Epoch time: 16092
51037899 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 80
4699 deg
Eccentricity:
0002498
Arg of perigee: 17
3246 deg
Mean anomaly: 342
7991 deg
Mean motion: 15
54287257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3305
Checksum: 333
Coasting Arc #2 (Orbit 3320)
---------------------------------------
Vector Time (GMT): 2016/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907109
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3911784
24 A = 6784051
31 meter
Y = -4414352
60 meter E =
0013578
Z = 3342546
36 I = 52
00064
XDOT = 2284
957597 Wp = 81
04244
YDOT = -5605
639389 meter/sec RA = 74
73370 deg
ZDOT = -4710
708343 TA = 60
22612
MA = 60
09113
Ha = 221
203 n
mi
Hp = 214
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12833937
78 X = -3878367
73
Y = -14482784
12 feet Y = -4457909
61 meter
Z = 10966359
46 Z = 3323625
53
XDOT = 7496
580043 XDOT = 2370
353977
YDOT = -18391
205345 feet/sec YDOT = -5579
610452 meter/sec
ZDOT = -15455
079867 ZDOT = -4699
400654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15309436
25 X = -4666316
17
Y = -11910578
61 feet Y = -3630344
36 meter
Z = 10884912
20 Z = 3317721
24
XDOT = 3277
353476 XDOT = 998
937340
YDOT = -18346
276252 feet/sec YDOT = -5591
945002 meter/sec
ZDOT = -15404
908607 ZDOT = -4695
416143
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 16093
53908543
00016717 00000-0 10270-3 0 9014
2 25544 51
6395 75
3399 0002573 18
6252 341
4995 15
54338421 33218
Satellite: ISS
Catalog Number: 25544
Epoch time: 16093
53908543 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 75
3399 deg
Eccentricity:
0002573
Arg of perigee: 18
6252 deg
Mean anomaly: 341
4995 deg
Mean motion: 15
54338421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3321
Checksum: 316
Coasting Arc #3 (Orbit 3324)
---------------------------------------
Vector Time (GMT): 2016/093/18:00:53
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4354940
91 A = 6777395
45 meter
Y = -474571
46 meter E =
0006895
Z = 5168570
92 I = 51
98068
XDOT = -981
169587 Wp = 40
89916
YDOT = -7457
937750 meter/sec RA = 73
50407 deg
ZDOT = -1505
286764 TA = 63
55899
MA = 63
48826
Ha = 221
187 n
mi
Hp = 214
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14287863
89 X = -4374417
11
Y = -1556992
98 feet Y = -523379
68 meter
Z = 16957253
69 Z = 5147368
50
XDOT = -3219
060326 XDOT = -890
388129
YDOT = -24468
299705 feet/sec YDOT = -7468
402402 meter/sec
ZDOT = -4938
604869 ZDOT = -1509
831785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1190455
01 X = 362850
69
Y = 14431371
11 feet Y = 4398681
91 meter
Z = 16865173
56 Z = 5140504
90
XDOT = -22374
647845 XDOT = -6819
792663
YDOT = 7662
617388 feet/sec YDOT = 2335
565780 meter/sec
ZDOT = -4957
006365 ZDOT = -1510
895540
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 16093
79626033
00016717 00000-0 10270-3 0 9024
2 25544 51
6435 74
0590 0002566 15
0194 345
1035 15
54371833 33254
Satellite: ISS
Catalog Number: 25544
Epoch time: 16093
79626033 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 74
0590 deg
Eccentricity:
0002566
Arg of perigee: 15
0194 deg
Mean anomaly: 345
1035 deg
Mean motion: 15
54371833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3325
Checksum: 292
Coasting Arc #4 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2016/094/18:00:53
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4614338
61 A = 6780428
32 meter
Y = 2220005
67 meter E =
0009446
Z = -4453028
80 I = 51
97972
XDOT = -96
579384 Wp = 94
36287
YDOT = 6893
008798 meter/sec RA = 68
53050 deg
ZDOT = 3341
741116 TA = 209
23222
MA = 209
28511
Ha = 221
205 n
mi
Hp = 214
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15138906
20 X = 4610801
86
Y = 7283483
17 feet Y = 2271585
99 meter
Z = -14609674
53 Z = -4430622
39
XDOT = -316
861495 XDOT = -189
884254
YDOT = 22614
858262 feet/sec YDOT = 6891
407470 meter/sec
ZDOT = 10963
717573 ZDOT = 3341
044539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3993858
72 X = 1217328
14
Y = -16404553
81 feet Y = -5000108
00 meter
Z = -14512680
83 Z = -4423465
12
XDOT = 21015
833485 XDOT = 6405
626046
YDOT = -4563
249393 feet/sec YDOT = -1390
878415 meter/sec
ZDOT = 10959
428117 ZDOT = 3340
433690
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 16094
76066658
00016717 00000-0 10270-3 0 9034
2 25544 51
6428 69
2502 0002609 19
5677 340
5575 15
54339429 33408
Satellite: ISS
Catalog Number: 25544
Epoch time: 16094
76066658 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 69
2502 deg
Eccentricity:
0002609
Arg of perigee: 19
5677 deg
Mean anomaly: 340
5575 deg
Mean motion: 15
54339429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3340
Checksum: 326
Coasting Arc #5 (Orbit 3340)
---------------------------------------
Vector Time (GMT): 2016/094/18:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4451502
54 A = 6777733
72 meter
Y = -428705
03 meter E =
0007688
Z = 5089885
79 I = 51
97052
XDOT = -1375
960672 Wp = 43
56772
YDOT = -7325
881035 meter/sec RA = 68
39403 deg
ZDOT = -1813
370922 TA = 63
93501
MA = 63
85589
Ha = 221
230 n
mi
Hp = 213
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14604667
12 X = -4471102
23
Y = -1406512
58 feet Y = -478593
70 meter
Z = 16699100
35 Z = 5068213
99
XDOT = -4514
306666 XDOT = -1285
130024
YDOT = -24035
042767 feet/sec YDOT = -7340
760288 meter/sec
ZDOT = -5949
379665 ZDOT = -1819
833517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4313588
44 X = 1314781
76
Y = 14135147
10 feet Y = 4308392
84 meter
Z = 16604972
24 Z = 5061195
54
XDOT = -19479
578527 XDOT = -5937
375535
YDOT = 12992
197993 feet/sec YDOT = 3960
021948 meter/sec
ZDOT = -5976
131462 ZDOT = -1821
524869
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 16094
82495857
00016717 00000-0 10270-3 0 9049
2 25544 51
6425 68
9294 0002584 18
4151 341
7095 15
54373904 33413
Satellite: ISS
Catalog Number: 25544
Epoch time: 16094
82495857 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 68
9294 deg
Eccentricity:
0002584
Arg of perigee: 18
4151 deg
Mean anomaly: 341
7095 deg
Mean motion: 15
54373904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3341
Checksum: 326
Coasting Arc #6 (Orbit 3355)
---------------------------------------
Vector Time (GMT): 2016/095/18:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4812178
65 A = 6780993
97 meter
Y = 2123146
02 meter E =
0008653
Z = -4287550
57 I = 51
96827
XDOT = 226
578006 Wp = 92
72776
YDOT = 6756
121997 meter/sec RA = 63
42058 deg
ZDOT = 3605
718217 TA = 213
93552
MA = 213
99090
Ha = 221
195 n
mi
Hp = 214
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15787987
70 X = 4808906
53
Y = 6965702
16 feet Y = 2176940
14 meter
Z = -14066766
95 Z = -4264182
44
XDOT = 743
366160 XDOT = 133
497499
YDOT = 22165
754582 feet/sec YDOT = 6758
135771 meter/sec
ZDOT = 11829
784178 ZDOT = 3606
591911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 82215
95 X = 25059
42
Y = -17338146
21 feet Y = -5284666
96 meter
Z = -13965579
88 Z = -4256708
75
XDOT = 18812
474737 XDOT = 5734
042300
YDOT = -9425
935416 feet/sec YDOT = -2873
025115 meter/sec
ZDOT = 11832
337091 ZDOT = 3606
496345
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 16095
78935888
00016717 00000-0 10270-3 0 9059
2 25544 51
6423 64
1201 0002562 21
4599 338
6661 15
54355096 33565
Satellite: ISS
Catalog Number: 25544
Epoch time: 16095
78935888 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 64
1201 deg
Eccentricity:
0002562
Arg of perigee: 21
4599 deg
Mean anomaly: 338
6661 deg
Mean motion: 15
54355096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3356
Checksum: 328
Coasting Arc #7 (Orbit 3371)
---------------------------------------
Vector Time (GMT): 2016/096/18:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4927741
70 A = 6784901
70 meter
Y = -3586362
63 meter E =
0014189
Z = 2970398
47 I = 51
96745
XDOT = 1108
244980 Wp = 86
99697
YDOT = -5695
474895 meter/sec RA = 58
45654 deg
ZDOT = -5016
684476 TA = 59
20811
MA = 59
06851
Ha = 221
212 n
mi
Hp = 213
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16167131
56 X = -4901700
83
Y = -11766281
59 feet Y = -3641321
89 meter
Z = 9745401
79 Z = 2946524
40
XDOT = 3635
974343 XDOT = 1196
219820
YDOT = -18685
941257 feet/sec YDOT = -5682
590573 meter/sec
ZDOT = -16458
938568 ZDOT = -5011
086396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4011098
03 X = -1222582
68
Y = 19640051
88 feet Y = 5986287
81 meter
Z = 9642294
14 Z = 2938971
25
XDOT = -17132
086827 XDOT = -5221
860065
YDOT = 4603
879181 feet/sec YDOT = 1403
262374 meter/sec
ZDOT = -16433
548041 ZDOT = -5008
945443
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 16096
81804322
00016717 00000-0 10270-3 0 9063
2 25544 51
6432 58
9899 0002719 23
2120 336
9155 15
54392041 33721
Satellite: ISS
Catalog Number: 25544
Epoch time: 16096
81804322 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 58
9899 deg
Eccentricity:
0002719
Arg of perigee: 23
2120 deg
Mean anomaly: 336
9155 deg
Mean motion: 15
54392041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3372
Checksum: 308
Coasting Arc #8 (Orbit 3386)
---------------------------------------
Vector Time (GMT): 2016/097/18:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4752613
13 A = 6787936
92 meter
Y = 4647372
28 meter E =
0011470
Z = -1349879
38 I = 51
95827
XDOT = -2527
658376 Wp = 34
99071
YDOT = 4272
843944 meter/sec RA = 53
50147 deg
ZDOT = 5844
918672 TA = 310
37229
MA = 310
47237
Ha = 221
302 n
mi
Hp = 213
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15592562
77 X = 4706849
02
Y = 15247284
40 feet Y = 4700263
09 meter
Z = -4428738
14 Z = -1326903
99
XDOT = -8292
842440 XDOT = -2603
642865
YDOT = 14018
516876 feet/sec YDOT = 4244
153954 meter/sec
ZDOT = 19176
242361 ZDOT = 5832
454677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7079006
81 X = 2157681
27
Y = -20648544
13 feet Y = -6293676
25 meter
Z = -4329746
49 Z = -1319706
73
XDOT = 14768
679403 XDOT = 4501
493482
YDOT = 1077
376166 feet/sec YDOT = 328
384255 meter/sec
ZDOT = 19121
267592 ZDOT = 5828
162362
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 16097
78242951
00016717 00000-0 10270-3 0 9075
2 25544 51
6418 54
1802 0002676 27
1887 332
9405 15
54352247 33876
Satellite: ISS
Catalog Number: 25544
Epoch time: 16097
78242951 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 54
1802 deg
Eccentricity:
0002676
Arg of perigee: 27
1887 deg
Mean anomaly: 332
9405 deg
Mean motion: 15
54352247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3387
Checksum: 325
Coasting Arc #9 (Orbit 3400)
---------------------------------------
Vector Time (GMT): 2016/098/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3245520
72 A = 6776593
18 meter
Y = -2648163
48 meter E =
0016408
Z = -5340915
30 I = 51
90527
XDOT = 4946
175035 Wp = 83
00677
YDOT = 5844
021834 meter/sec RA = 49
10968 deg
ZDOT = 110
265348 TA = 188
02856
MA = 188
05485
Ha = 221
241 n
mi
Hp = 213
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10648033
86 X = 3300836
12
Y = -8688200
40 feet Y = -2611561
32 meter
Z = -17522687
99 Z = -5325014
48
XDOT = 16227
608384 XDOT = 4879
922488
YDOT = 19173
299980 feet/sec YDOT = 5898
962828 meter/sec
ZDOT = 361
762953 ZDOT = 134
131242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5720253
64 X = -1743533
31
Y = -12592807
53 feet Y = -3838287
74 meter
Z = -17453078
31 Z = -5319698
27
XDOT = 21705
453884 XDOT = 6615
822344
YDOT = -10493
074046 feet/sec YDOT = -3198
288969 meter/sec
ZDOT = 464
386185 ZDOT = 141
544909
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 16098
68251913
00016717 00000-0 10270-3 0 9084
2 25544 51
6438 49
6933 0002619 33
1149 327
0167 15
54393259 34012
Satellite: ISS
Catalog Number: 25544
Epoch time: 16098
68251913 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 49
6933 deg
Eccentricity:
0002619
Arg of perigee: 33
1149 deg
Mean anomaly: 327
0167 deg
Mean motion: 15
54393259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3401
Checksum: 320
Coasting Arc #10 (Orbit 3416)
---------------------------------------
Vector Time (GMT): 2016/099/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4435875
77 A = 6777973
14 meter
Y = 1150437
75 meter E =
0008666
Z = 4990126
42 I = 51
88955
XDOT = -3999
238041 Wp = 49
93432
YDOT = -6194
676870 meter/sec RA = 44
12612 deg
ZDOT = -2119
041654 TA = 60
66000
MA = 60
57347
Ha = 221
289 n
mi
Hp = 213
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14553398
20 X = -4472650
82
Y = 3774402
07 feet Y = 1100627
76 meter
Z = 16371805
85 Z = 4968488
27
XDOT = -13120
859716 XDOT = -3919
376839
YDOT = -20323
743012 feet/sec YDOT = -6238
952712 meter/sec
ZDOT = -6952
236398 ZDOT = -2138
274590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 247597
81 X = 75467
81
Y = 15134852
19 feet Y = 4613102
95 meter
Z = 16277545
31 Z = 4961395
81
XDOT = -21712
721208 XDOT = -6618
037424
YDOT = 7948
881800 feet/sec YDOT = 2422
819172 meter/sec
ZDOT = -7034
640214 ZDOT = -2144
158337
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 16099
71118275
00016717 00000-0 10270-3 0 9093
2 25544 51
6447 44
5639 0002563 33
1641 326
9672 15
54437228 34175
Satellite: ISS
Catalog Number: 25544
Epoch time: 16099
71118275 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 44
5639 deg
Eccentricity:
0002563
Arg of perigee: 33
1641 deg
Mean anomaly: 326
9672 deg
Mean motion: 15
54437228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3417
Checksum: 322
Coasting Arc #11 (Orbit 3431)
---------------------------------------
Vector Time (GMT): 2016/100/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5406890
89 A = 6781549
79 meter
Y = 260612
52 meter E =
0008429
Z = -4092327
50 I = 51
87727
XDOT = 2633
954396 Wp = 90
80395
YDOT = 6063
255402 meter/sec RA = 39
14822 deg
ZDOT = 3872
942355 TA = 219
14883
MA = 219
20984
Ha = 221
311 n
mi
Hp = 213
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17739143
35 X = 5423453
88
Y = 855027
95 feet Y = 321168
23 meter
Z = -13426271
33 Z = -4066021
57
XDOT = 8641
582663 XDOT = 2547
144425
YDOT = 19892
570216 feet/sec YDOT = 6092
224977 meter/sec
ZDOT = 12706
503790 ZDOT = 3885
526273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4698259
78 X = 1432029
58
Y = -17215983
49 feet Y = -5247431
77 meter
Z = -13311998
67 Z = -4057497
19
XDOT = 20020
958885 XDOT = 6102
388268
YDOT = -4385
443535 feet/sec YDOT = -1336
683190 meter/sec
ZDOT = 12760
020804 ZDOT = 3889
254341
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 16100
67554908
00016717 00000-0 10270-3 0 9100
2 25544 51
6445 39
7549 0002637 37
3000 322
8335 15
54404760 34329
Satellite: ISS
Catalog Number: 25544
Epoch time: 16100
67554908 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 39
7549 deg
Eccentricity:
0002637
Arg of perigee: 37
3000 deg
Mean anomaly: 322
8335 deg
Mean motion: 15
54404760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3432
Checksum: 293
Coasting Arc #12 (Orbit 3447)
---------------------------------------
Vector Time (GMT): 2016/101/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943973
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6029489
63 A = 6785503
48 meter
Y = -1542388
83 meter E =
0015158
Z = 2689329
67 I = 51
86459
XDOT = -910
901032 Wp = 93
06675
YDOT = -5559
387691 meter/sec RA = 34
18036 deg
ZDOT = -5206
209383 TA = 56
64778
MA = 56
50278
Ha = 221
389 n
mi
Hp = 213
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19781790
12 X = -6024857
91
Y = -5060330
79 feet Y = -1609788
52 meter
Z = 8823260
07 Z = 2660050
87
XDOT = -2988
520447 XDOT = -823
377010
YDOT = -18239
460928 feet/sec YDOT = -5569
084946 meter/sec
ZDOT = -17080
739445 ZDOT = -5210
421431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8924760
34 X = -2720266
95
Y = 18425491
36 feet Y = 5616089
77 meter
Z = 8696321
48 Z = 2650638
79
XDOT = -17104
583865 XDOT = -5213
477162
YDOT = -176
753874 feet/sec YDOT = -53
874581 meter/sec
ZDOT = -17097
959319 ZDOT = -5211
458000
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 16101
70419833
00016717 00000-0 10270-3 0 9113
2 25544 51
6439 34
6257 0002739 43
3186 316
8181 15
54420369 34489
Satellite: ISS
Catalog Number: 25544
Epoch time: 16101
70419833 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 34
6257 deg
Eccentricity:
0002739
Arg of perigee: 43
3186 deg
Mean anomaly: 316
8181 deg
Mean motion: 15
54420369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3448
Checksum: 306
Coasting Arc #13 (Orbit 3462)
---------------------------------------
Vector Time (GMT): 2016/102/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943973
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6199964
43 A = 6788030
64 meter
Y = 2557933
14 meter E =
0012406
Z = -1010839
39 I = 51
84628
XDOT = -1009
031311 Wp = 39
43995
YDOT = 4766
694549 meter/sec RA = 29
21974 deg
ZDOT = 5922
389807 TA = 309
63507
MA = 309
74448
Ha = 221
308 n
mi
Hp = 213
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20341090
66 X = 6175810
46
Y = 8392169
09 feet Y = 2627130
16 meter
Z = -3316402
20 Z = -980780
00
XDOT = -3310
470179 XDOT = -1091
027399
YDOT = 15638
761643 feet/sec YDOT = 4754
952719 meter/sec
ZDOT = 19430
412751 ZDOT = 5917
288736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11978417
45 X = 3651021
64
Y = -18481129
71 feet Y = -5633048
34 meter
Z = -3186275
98 Z = -971176
92
XDOT = 13399
379566 XDOT = 4084
130892
YDOT = 5367
682144 feet/sec YDOT = 1636
069518 meter/sec
ZDOT = 19407
307447 ZDOT = 5915
347310
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 16102
66854832
00016717 00000-0 10270-3 0 9122
2 25544 51
6440 29
8165 0002588 43
9516 316
1842 15
54436695 34633
Satellite: ISS
Catalog Number: 25544
Epoch time: 16102
66854832 = yrday
fracday
Element set: 912
Inclination: 51
6440 deg
RA of node: 29
8165 deg
Eccentricity:
0002588
Arg of perigee: 43
9516 deg
Mean anomaly: 316
1842 deg
Mean motion: 15
54436695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3463
Checksum: 319
Coasting Arc #14 (Orbit 3478)
---------------------------------------
Vector Time (GMT): 2016/103/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943973
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5841511
35 A = 6788172
33 meter
Y = -3349833
59 meter E =
0010285
Z = -831254
83 I = 51
81811
XDOT = 3006
855957 Wp = 126
34688
YDOT = -3780
246588 meter/sec RA = 24
26132 deg
ZDOT = -5953
495161 TA = 62
61982
MA = 62
51519
Ha = 221
278 n
mi
Hp = 213
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19165063
48 X = -5799580
61
Y = -10990267
69 feet Y = -3414922
85 meter
Z = -2727213
99 Z = -859529
62
XDOT = 9865
012981 XDOT = 3077
823855
YDOT = -12402
383818 feet/sec YDOT = -3746
225398 meter/sec
ZDOT = -19532
464439 ZDOT = -5938
715958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14019387
29 X = -4273109
25
Y = 17054644
73 feet Y = 5198255
71 meter
Z = -2849422
96 Z = -868504
12
XDOT = -9327
948665 XDOT = -2843
158753
YDOT = -10890
412430 feet/sec YDOT = -3319
397709 meter/sec
ZDOT = -19467
491918 ZDOT = -5933
691537
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 16103
69717881
00016717 00000-0 10270-3 0 9139
2 25544 51
6439 24
6862 0002486 48
0298 312
1067 15
54415209 34798
Satellite: ISS
Catalog Number: 25544
Epoch time: 16103
69717881 = yrday
fracday
Element set: 913
Inclination: 51
6439 deg
RA of node: 24
6862 deg
Eccentricity:
0002486
Arg of perigee: 48
0298 deg
Mean anomaly: 312
1067 deg
Mean motion: 15
54415209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3479
Checksum: 321
Coasting Arc #15 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2016/104/12:23:00
506
Vector Time (MET): N/A
Weight (LBS) : 943644
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 848517
22 A = 6778112
91 meter
Y = -4144444
88 meter E =
0014751
Z = -5308666
54 I = 51
75420
XDOT = 7312
597623 Wp = 82
48144
YDOT = 2203
684134 meter/sec RA = 20
03043 deg
ZDOT = -551
015420 TA = 182
25806
MA = 182
26473
Ha = 221
355 n
mi
Hp = 215
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2783849
13 X = 920585
69
Y = -13597260
10 feet Y = -4134553
50 meter
Z = -17416884
97 Z = -5304369
38
XDOT = 23991
462018 XDOT = 7290
088597
YDOT = 7229
934823 feet/sec YDOT = 2285
332580 meter/sec
ZDOT = -1807
793373 ZDOT = -515
547283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3599190
17 X = -1097033
16
Y = -13429812
00 feet Y = -4093406
70 meter
Z = -17397389
46 Z = -5302724
31
XDOT = 23687
531510 XDOT = 7219
959604
YDOT = -4203
059084 feet/sec YDOT = -1281
092409 meter/sec
ZDOT = -1654
102937 ZDOT = -504
170575
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 16104
53293718
00016717 00000-0 10270-3 0 9142
2 25544 51
6437 20
5181 0000814 354
9879 5
1265 15
53897721 34928
Satellite: ISS
Catalog Number: 25544
Epoch time: 16104
53293718 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 20
5181 deg
Eccentricity:
0000814
Arg of perigee: 354
9879 deg
Mean anomaly: 5
1265 deg
Mean motion: 15
53897721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 314
Coasting Arc #16 (Orbit 3507)
---------------------------------------
Vector Time (GMT): 2016/105/12:23:00
506
Vector Time (MET): N/A
Weight (LBS) : 943644
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2477597
27 A = 6778505
62 meter
Y = 3578292
66 meter E =
0004658
Z = 5194489
28 I = 51
72516
XDOT = -6967
255102 Wp = 44
57261
YDOT = -2933
202377 meter/sec RA = 15
04079 deg
ZDOT = -1298
624521 TA = 57
90448
MA = 57
85927
Ha = 221
310 n
mi
Hp = 215
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8128599
97 X = -2542659
14
Y = 11739805
30 feet Y = 3550223
05 meter
Z = 17042287
65 Z = 5182295
46
XDOT = -22858
448496 XDOT = -6927
629308
YDOT = -9623
367377 feet/sec YDOT = -3010
893375 meter/sec
ZDOT = -4260
579137 ZDOT = -1332
373348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1759139
48 X = -536185
71
Y = 14234815
61 feet Y = 4338771
80 meter
Z = 16988589
92 Z = 5178122
21
XDOT = -23637
888618 XDOT = -7204
828451
YDOT = 2353
461319 feet/sec YDOT = 717
335010 meter/sec
ZDOT = -4406
647172 ZDOT = -1343
146058
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 16105
56192737
00016717 00000-0 10270-3 0 9156
2 25544 51
6435 15
3913 0000857 341
6152 18
4970 15
53935603 35085
Satellite: ISS
Catalog Number: 25544
Epoch time: 16105
56192737 = yrday
fracday
Element set: 915
Inclination: 51
6435 deg
RA of node: 15
3913 deg
Eccentricity:
0000857
Arg of perigee: 341
6152 deg
Mean anomaly: 18
4970 deg
Mean motion: 15
53935603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3508
Checksum: 305
Coasting Arc #17 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2016/106/12:23:00
506
Vector Time (MET): N/A
Weight (LBS) : 943644
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3992043
08 A = 6781072
16 meter
Y = -2986154
37 meter E =
0009577
Z = -4605925
40 I = 51
70343
XDOT = 6104
211843 Wp = 105
21933
YDOT = 3504
875528 meter/sec RA = 10
05197 deg
ZDOT = 3021
113210 TA = 194
93562
MA = 194
96393
Ha = 221
303 n
mi
Hp = 215
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13097254
21 X = 4047511
94
Y = -9797094
38 feet Y = -2941202
88 meter
Z = -15111303
80 Z = -4586398
08
XDOT = 20026
941742 XDOT = 6049
890486
YDOT = 11498
935458 feet/sec YDOT = 3572
833378 meter/sec
ZDOT = 9911
788748 ZDOT = 3050
633783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6790744
08 X = 2069818
79
Y = -14966025
86 feet Y = -4561644
68 meter
Z = -15025860
83 Z = -4579882
38
XDOT = 21943
697042 XDOT = 6688
438859
YDOT = -113
442552 feet/sec YDOT = -34
577290 meter/sec
ZDOT = 10039
363228 ZDOT = 3059
997912
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 16106
52659810
00016717 00000-0 10270-3 0 9164
2 25544 51
6446 10
5839 0000888 347
3331 12
7800 15
53915251 35230
Satellite: ISS
Catalog Number: 25544
Epoch time: 16106
52659810 = yrday
fracday
Element set: 916
Inclination: 51
6446 deg
RA of node: 10
5839 deg
Eccentricity:
0000888
Arg of perigee: 347
3331 deg
Mean anomaly: 12
7800 deg
Mean motion: 15
53915251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 298
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