[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 24th 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) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
273/17:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 213
6
278/01:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 2028)
---------------------------------------
Vector Time (GMT): 2016/267/13:52:19
901
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1924217
74 A = 6782802
06 meter
Y = 5059089
68 meter E =
0013212
Z = 4085773
28 I = 51
28141
XDOT = -4593
369540 Wp = 46
87101
YDOT = 4825
469298 meter/sec RA = 286
41567 deg
ZDOT = -3795
053593 TA = 82
57890
MA = 82
42879
Ha = 222
376 n
mi
Hp = 214
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6313050
33 X = 1847655
70
Y = 16598063
24 feet Y = 5080179
79 meter
Z = 13404767
98 Z = 4094934
35
XDOT = -15070
110040 XDOT = -4628
552971
YDOT = 15831
592185 feet/sec YDOT = 4773
906157 meter/sec
ZDOT = -12450
963230 ZDOT = -3817
452926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13705556
72 X = -4177453
69
Y = -11245361
75 feet Y = -3427586
26 meter
Z = 13443870
97 Z = 4097691
87
XDOT = 4219
575863 XDOT = 1286
126723
YDOT = -20211
028162 feet/sec YDOT = -6160
321384 meter/sec
ZDOT = -12549
626154 ZDOT = -3825
126052
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 16267
61921095
00016717 00000-0 10270-3 0 9002
2 25544 51
6396 287
0031 0006645 354
8215 5
2868 15
53926117 20294
Satellite: ISS
Catalog Number: 25544
Epoch time: 16267
61921095 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 287
0031 deg
Eccentricity:
0006645
Arg of perigee: 354
8215 deg
Mean anomaly: 5
2868 deg
Mean motion: 15
53926117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2029
Checksum: 310
Coasting Arc #2 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2016/268/13:52:19
901
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1136137
68 A = 6786433
43 meter
Y = -6035734
29 meter E =
0009572
Z = -2879011
40 I = 51
28543
XDOT = 4770
757465 Wp = 25
58052
YDOT = -3286
903520 meter/sec RA = 281
41002 deg
ZDOT = 5022
933824 TA = 301
46530
MA = 301
55883
Ha = 222
515 n
mi
Hp = 214
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3727485
83 X = -1054575
12
Y = -19802277
85 feet Y = -6047983
53 meter
Z = -9445575
46 Z = -2884331
88
XDOT = 15652
091419 XDOT = 4782
758622
YDOT = -10783
804198 feet/sec YDOT = -3233
486204 meter/sec
ZDOT = 16479
441680 ZDOT = 5046
138391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13356821
20 X = 4071159
10
Y = 15073165
88 feet Y = 4594300
96 meter
Z = -9467748
01 Z = -2885769
59
XDOT = -6655
312574 XDOT = -2028
539273
YDOT = 16282
241898 feet/sec YDOT = 4962
827330 meter/sec
ZDOT = 16581
343799 ZDOT = 5053
993590
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 16268
58387757
00016717 00000-0 10270-3 0 9011
2 25544 51
6398 282
1968 0006602
0430
0722 15
53908413 20441
Satellite: ISS
Catalog Number: 25544
Epoch time: 16268
58387757 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 282
1968 deg
Eccentricity:
0006602
Arg of perigee:
0430 deg
Mean anomaly:
0722 deg
Mean motion: 15
53908413 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2044
Checksum: 296
Coasting Arc #3 (Orbit 2059)
---------------------------------------
Vector Time (GMT): 2016/269/13:52:19
901
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 348142
30 A = 6789080
16 meter
Y = 6640728
39 meter E =
0012314
Z = 1356903
35 I = 51
28948
XDOT = -4823
334090 Wp = 90
38480
YDOT = 1443
105613 meter/sec RA = 276
41123 deg
ZDOT = -5779
540043 TA = 74
76946
MA = 74
63334
Ha = 222
643 n
mi
Hp = 214
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1142199
16 X = 267266
87
Y = 21787166
64 feet Y = 6644169
48 meter
Z = 4451782
66 Z = 1358397
49
XDOT = -15824
586908 XDOT = -4811
038315
YDOT = 4734
598467 feet/sec YDOT = 1389
236069 meter/sec
ZDOT = -18961
745548 ZDOT = -5802
940818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12502950
26 X = -3810899
24
Y = -17877740
69 feet Y = -5449135
36 meter
Z = 4457156
09 Z = 1358541
18
XDOT = 9494
882998 XDOT = 2894
040338
YDOT = -11430
480349 feet/sec YDOT = -3484
010410 meter/sec
ZDOT = -19064
180410 ZDOT = -5810
762189
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 16269
61284809
00016717 00000-0 10270-3 0 9021
2 25544 51
6401 277
0682 0006810 3
0117 357
1075 15
53944959 20608
Satellite: ISS
Catalog Number: 25544
Epoch time: 16269
61284809 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 277
0682 deg
Eccentricity:
0006810
Arg of perigee: 3
0117 deg
Mean anomaly: 357
1075 deg
Mean motion: 15
53944959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2060
Checksum: 303
Coasting Arc #4 (Orbit 2075)
---------------------------------------
Vector Time (GMT): 2016/270/13:52:19
901
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 376165
20 A = 6789791
75 meter
Y = -6763853
53 meter E =
0018080
Z = 260315
13 I = 51
28829
XDOT = 4782
191169 Wp = 34
19815
YDOT = 503
347868 meter/sec RA = 271
41826 deg
ZDOT = 5980
366047 TA = 328
62250
MA = 328
73024
Ha = 222
612 n
mi
Hp = 214
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1234137
80 X = 450507
88
Y = -22191120
50 feet Y = -6759231
29 meter
Z = 854052
27 Z = 262323
74
XDOT = 15689
603572 XDOT = 4747
157206
YDOT = 1651
403767 feet/sec YDOT = 556
630299 meter/sec
ZDOT = 19620
623513 ZDOT = 6003
511528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11065029
54 X = 3372621
01
Y = 19274776
02 feet Y = 5874951
73 meter
Z = 863979
61 Z = 263340
99
XDOT = -12543
041372 XDOT = -3823
119010
YDOT = 6289
241703 feet/sec YDOT = 1916
960871 meter/sec
ZDOT = 19721
610056 ZDOT = 6011
146745
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 16270
64181344
00016717 00000-0 10270-3 0 9037
2 25544 51
6390 271
9413 0006583 7
2994 352
8254 15
53961783 20768
Satellite: ISS
Catalog Number: 25544
Epoch time: 16270
64181344 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 271
9413 deg
Eccentricity:
0006583
Arg of perigee: 7
2994 deg
Mean anomaly: 352
8254 deg
Mean motion: 15
53961783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2076
Checksum: 319
Coasting Arc #5 (Orbit 2090)
---------------------------------------
Vector Time (GMT): 2016/271/13:52:19
901
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1117460
47 A = 6788338
15 meter
Y = 6425293
84 meter E =
0005752
Z = -1891397
43 I = 51
28389
XDOT = -4638
095121 Wp = 77
77030
YDOT = -2446
562277 meter/sec RA = 266
42290 deg
ZDOT = -5584
259479 TA = 123
14467
MA = 123
08947
Ha = 222
817 n
mi
Hp = 214
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3666208
88 X = -1180039
10
Y = 21080360
35 feet Y = 6412447
51 meter
Z = -6205372
16 Z = -1896978
56
XDOT = -15216
847509 XDOT = -4583
266431
YDOT = -8026
779123 feet/sec YDOT = -2498
122694 meter/sec
ZDOT = -18321
061284 ZDOT = -5606
656676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8786125
15 X = -2678010
94
Y = -19501541
52 feet Y = -5944069
85 meter
Z = -6230827
16 Z = -1899156
12
XDOT = 15583
706328 XDOT = 4749
913689
YDOT = -1150
059145 feet/sec YDOT = -350
538027 meter/sec
ZDOT = -18418
456117 ZDOT = -5613
945425
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 16271
60646641
00016717 00000-0 10270-3 0 9041
2 25544 51
6394 267
1333 0006790 9
9757 350
1529 15
53941752 20913
Satellite: ISS
Catalog Number: 25544
Epoch time: 16271
60646641 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 267
1333 deg
Eccentricity:
0006790
Arg of perigee: 9
9757 deg
Mean anomaly: 350
1529 deg
Mean motion: 15
53941752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2091
Checksum: 318
Coasting Arc #6 (Orbit 2106)
---------------------------------------
Vector Time (GMT): 2016/272/13:52:19
901
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1834645
40 A = 6785082
56 meter
Y = -5621156
28 meter E =
0015620
Z = 3308201
60 I = 51
27714
XDOT = 4418
091792 Wp = 64
18565
YDOT = 4195
481065 meter/sec RA = 261
42214 deg
ZDOT = 4668
087080 TA = 334
55731
MA = 334
63413
Ha = 222
706 n
mi
Hp = 213
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6019177
83 X = 1881296
41
Y = -18442113
78 feet Y = -5600378
75 meter
Z = 10853679
79 Z = 3317227
94
XDOT = 14495
051812 XDOT = 4348
172908
YDOT = 13764
701656 feet/sec YDOT = 4244
496831 meter/sec
ZDOT = 15315
246324 ZDOT = 4689
378684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5704068
76 X = 1738600
16
Y = 18518317
80 feet Y = 5644383
27 meter
Z = 10894031
97 Z = 3320500
94
XDOT = -18337
654087 XDOT = -5589
316966
YDOT = -3435
841432 feet/sec YDOT = -1047
244468 meter/sec
ZDOT = 15407
529897 ZDOT = 4696
215113
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 16272
63542080
00016717 00000-0 10270-3 0 9058
2 25544 51
6402 262
0059 0006646 12
9506 347
1816 15
53979321 21074
Satellite: ISS
Catalog Number: 25544
Epoch time: 16272
63542080 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 262
0059 deg
Eccentricity:
0006646
Arg of perigee: 12
9506 deg
Mean anomaly: 347
1816 deg
Mean motion: 15
53979321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2107
Checksum: 296
Coasting Arc #7 (Orbit 2121)
---------------------------------------
Vector Time (GMT): 2016/273/13:52:19
901
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2580456
35 A = 6781458
97 meter
Y = 4452066
87 meter E =
0014518
Z = -4431745
73 I = 51
27028
XDOT = -4055
047434 Wp = 47
40417
YDOT = -5609
409134 meter/sec RA = 256
41075 deg
ZDOT = -3271
235659 TA = 189
37030
MA = 189
39742
Ha = 222
990 n
mi
Hp = 213
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8466064
14 X = -2608521
10
Y = 14606518
62 feet Y = 4423052
92 meter
Z = -14539848
20 Z = -4444349
81
XDOT = -13303
961396 XDOT = -3976
129886
YDOT = -18403
573275 feet/sec YDOT = -5654
314617 meter/sec
ZDOT = -10732
400456 ZDOT = -3290
741649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1807293
17 X = -550862
96
Y = -16737184
09 feet Y = -5101493
71 meter
Z = -14595621
73 Z = -4448745
50
XDOT = 20302
194129 XDOT = 6188
108771
YDOT = 7248
316144 feet/sec YDOT = 2209
286761 meter/sec
ZDOT = -10816
664729 ZDOT = -3296
919410
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 16273
60006292
00016717 00000-0 10270-3 0 9067
2 25544 51
6399 257
1977 0006901 17
0339 343
1044 15
53958786 21225
Satellite: ISS
Catalog Number: 25544
Epoch time: 16273
60006292 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 257
1977 deg
Eccentricity:
0006901
Arg of perigee: 17
0339 deg
Mean anomaly: 343
1044 deg
Mean motion: 15
53958786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2122
Checksum: 316
Coasting Arc #8 (Orbit 2123)
---------------------------------------
Vector Time (GMT): 2016/273/17:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3980632
05 A = 6777886
51 meter
Y = 1537195
32 meter E =
0018429
Z = -5281180
56 I = 51
26196
XDOT = -2227
260139 Wp = 66
01140
YDOT = -7310
834900 meter/sec RA = 255
72228 deg
ZDOT = -443
070362 TA = 199
69772
MA = 199
76899
Ha = 222
971 n
mi
Hp = 213
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13059816
43 X = -3971871
68
Y = 5043291
74 feet Y = 1492729
43 meter
Z = -17326707
87 Z = -5300496
51
XDOT = -7307
283922 XDOT = -2143
190731
YDOT = -23985
678806 feet/sec YDOT = -7335
271622 meter/sec
ZDOT = -1453
642921 ZDOT = -453
684620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3727028
29 X = -1135998
22
Y = -13385207
94 feet Y = -4079811
38 meter
Z = -17411314
45 Z = -5306968
64
XDOT = 23617
368224 XDOT = 7198
573835
YDOT = -4600
480875 feet/sec YDOT = -1402
226571 meter/sec
ZDOT = -1498
799167 ZDOT = -456
833986
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 16273
72868167
00016717 00000-0 10270-3 0 9078
2 25544 51
6424 256
5580 0006928 17
5952 342
5439 15
53971620 21247
Satellite: ISS
Catalog Number: 25544
Epoch time: 16273
72868167 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 256
5580 deg
Eccentricity:
0006928
Arg of perigee: 17
5952 deg
Mean anomaly: 342
5439 deg
Mean motion: 15
53971620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2124
Checksum: 329
Coasting Arc #9 (Orbit 2139)
---------------------------------------
Vector Time (GMT): 2016/274/17:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4421557
65 A = 6778381
14 meter
Y = 175326
70 meter E =
0010866
Z = 5131440
45 I = 51
27266
XDOT = 1378
995700 Wp = 33
65895
YDOT = 7409
357913 meter/sec RA = 250
69855 deg
ZDOT = -1431
027386 TA = 70
23416
MA = 70
11701
Ha = 222
830 n
mi
Hp = 213
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14506422
73 X = 4394341
93
Y = 575218
84 feet Y = 224620
11 meter
Z = 16835434
55 Z = 5152853
32
XDOT = 4524
264107 XDOT = 1302
991257
YDOT = 24308
917036 feet/sec YDOT = 7424
353589 meter/sec
ZDOT = -4694
971738 ZDOT = -1424
514218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1762177
15 X = -537111
60
Y = 14300538
99 feet Y = 4358804
28 meter
Z = 16928920
52 Z = 5159934
98
XDOT = -23558
521711 XDOT = -7180
637418
YDOT = 2662
643836 feet/sec YDOT = 811
573841 meter/sec
ZDOT = -4667
727360 ZDOT = -1422
723299
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 16274
75762549
00016717 00000-0 10270-3 0 9080
2 25544 51
6422 251
4305 0006855 19
6630 340
4786 15
54004819 21407
Satellite: ISS
Catalog Number: 25544
Epoch time: 16274
75762549 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 251
4305 deg
Eccentricity:
0006855
Arg of perigee: 19
6630 deg
Mean anomaly: 340
4786 deg
Mean motion: 15
54004819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2140
Checksum: 311
Coasting Arc #10 (Orbit 2154)
---------------------------------------
Vector Time (GMT): 2016/275/17:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4759201
96 A = 6781056
87 meter
Y = -1764009
69 meter E =
0012223
Z = -4505540
43 I = 51
29419
XDOT = -384
653737 Wp = 76
31452
YDOT = -6973
612810 meter/sec RA = 245
67964 deg
ZDOT = 3146
669964 TA = 225
39718
MA = 225
49697
Ha = 223
020 n
mi
Hp = 213
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15614179
67 X = -4717236
40
Y = -5787433
37 feet Y = -1816996
29 meter
Z = -14781956
81 Z = -4528557
54
XDOT = -1261
987327 XDOT = -321
929789
YDOT = -22879
307120 feet/sec YDOT = -6977
563103 meter/sec
ZDOT = 10323
720354 ZDOT = 3144
954744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6790059
68 X = 2069610
19
Y = -15106903
48 feet Y = -4604584
18 meter
Z = -14882197
27 Z = -4536093
73
XDOT = 21814
722808 XDOT = 6649
127512
YDOT = -326
613098 feet/sec YDOT = -99
551672 meter/sec
ZDOT = 10317
347999 ZDOT = 3144
727670
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 16275
72225637
00016717 00000-0 10270-3 0 9091
2 25544 51
6434 246
6229 0006881 23
1679 336
9782 15
53977200 21557
Satellite: ISS
Catalog Number: 25544
Epoch time: 16275
72225637 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 246
6229 deg
Eccentricity:
0006881
Arg of perigee: 23
1679 deg
Mean anomaly: 336
9782 deg
Mean motion: 15
53977200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2155
Checksum: 332
Coasting Arc #11 (Orbit 2170)
---------------------------------------
Vector Time (GMT): 2016/276/17:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4918569
99 A = 6784770
03 meter
Y = 3200866
33 meter E =
0016854
Z = 3397915
09 I = 51
32070
XDOT = -783
996521 Wp = 68
54583
YDOT = 6097
489537 meter/sec RA = 240
67072 deg
ZDOT = -4584
581974 TA = 71
52236
MA = 71
33925
Ha = 223
149 n
mi
Hp = 213
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16137040
64 X = 4865905
66
Y = 10501529
94 feet Y = 3255575
07 meter
Z = 11148015
39 Z = 3421680
28
XDOT = -2572
167063 XDOT = -829
851668
YDOT = 20004
886933 feet/sec YDOT = 6088
465352 meter/sec
ZDOT = -15041
279441 ZDOT = -4588
502690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11263814
34 X = -3433210
61
Y = 15540243
61 feet Y = 4736666
25 meter
Z = 11251300
98 Z = 3429396
54
XDOT = -18727
994325 XDOT = -5708
292670
YDOT = -2613
650662 feet/sec YDOT = -796
640722 meter/sec
ZDOT = -15059
373421 ZDOT = -4590
097019
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 16276
75118932
00016717 00000-0 10270-3 0 9106
2 25544 51
6433 241
4952 0006976 28
2084 331
9445 15
53982768 21717
Satellite: ISS
Catalog Number: 25544
Epoch time: 16276
75118932 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 241
4952 deg
Eccentricity:
0006976
Arg of perigee: 28
2084 deg
Mean anomaly: 331
9445 deg
Mean motion: 15
53982768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2171
Checksum: 327
Coasting Arc #12 (Orbit 2185)
---------------------------------------
Vector Time (GMT): 2016/277/17:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4861487
92 A = 6787942
33 meter
Y = -4288554
12 meter E =
0013503
Z = -1995978
51 I = 51
34830
XDOT = 2040
728433 Wp = 35
62987
YDOT = -4882
593272 meter/sec RA = 235
67232 deg
ZDOT = 5549
989234 TA = 302
23489
MA = 302
36571
Ha = 223
115 n
mi
Hp = 213
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15949763
52 X = -4803475
13
Y = -14070059
45 feet Y = -4342594
42 meter
Z = -6548485
94 Z = -2019453
37
XDOT = 6695
303259 XDOT = 2068
215237
YDOT = -16019
006798 feet/sec YDOT = -4859
618108 meter/sec
ZDOT = 18208
626097 ZDOT = 5559
970114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14556373
71 X = 4436782
71
Y = -15463801
25 feet Y = -4713366
62 meter
Z = -6650340
81 Z = -2027023
88
XDOT = 14678
451363 XDOT = 4473
991975
YDOT = 6008
578575 feet/sec YDOT = 1831
414750 meter/sec
ZDOT = 18252
991806 ZDOT = 5563
511902
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 16277
71580787
00016717 00000-0 10270-3 0 9115
2 25544 51
6435 236
6880 0006895 30
5146 329
6407 15
54004668 21863
Satellite: ISS
Catalog Number: 25544
Epoch time: 16277
71580787 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 236
6880 deg
Eccentricity:
0006895
Arg of perigee: 30
5146 deg
Mean anomaly: 329
6407 deg
Mean motion: 15
54004668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2186
Checksum: 332
Coasting Arc #13 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2016/278/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1174398
76 A = 6780402
15 meter
Y = 4764025
52 meter E =
0016333
Z = -4695582
46 I = 51
32907
XDOT = -5791
896516 Wp = 57
61180
YDOT = -4164
906449 meter/sec RA = 233
86166 deg
ZDOT = -2775
532792 TA = 184
70847
MA = 184
72385
Ha = 223
106 n
mi
Hp = 213
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3853014
32 X = -1204774
50
Y = 15630004
97 feet Y = 4750722
21 meter
Z = -15405454
26 Z = -4701361
84
XDOT = -19002
285156 XDOT = -5731
410418
YDOT = -13664
391237 feet/sec YDOT = -4229
337451 meter/sec
ZDOT = -9106
078715 ZDOT = -2803
521465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7505024
02 X = 2287531
32
Y = 14213225
84 feet Y = 4332191
24 meter
Z = -15431449
10 Z = -4703505
69
XDOT = -22212
231680 XDOT = -6770
288216
YDOT = 1704
878388 feet/sec YDOT = 519
646933 meter/sec
ZDOT = -9227
672835 ZDOT = -2812
594680
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 16278
10165448
00016717 00000-0 10270-3 0 9123
2 25544 51
6431 234
7608 0006366 34
4766 325
6798 15
53984405 21921
Satellite: ISS
Catalog Number: 25544
Epoch time: 16278
10165448 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 234
7608 deg
Eccentricity:
0006366
Arg of perigee: 34
4766 deg
Mean anomaly: 325
6798 deg
Mean motion: 15
53984405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 328
Coasting Arc #14 (Orbit 2207)
---------------------------------------
Vector Time (GMT): 2016/279/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2405845
94 A = 6777938
21 meter
Y = -3588083
27 meter E =
0007682
Z = 5216282
82 I = 51
34199
XDOT = 5577
700018 Wp = 66
29507
YDOT = 5177
276585 meter/sec RA = 228
84462 deg
ZDOT = 990
590676 TA = 14
20131
MA = 14
17972
Ha = 222
990 n
mi
Hp = 213
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7893195
33 X = 2420451
06
Y = -11771926
73 feet Y = -3561097
28 meter
Z = 17113788
78 Z = 5228005
88
XDOT = 18299
540743 XDOT = 5514
579892
YDOT = 16985
815566 feet/sec YDOT = 5239
297345 meter/sec
ZDOT = 3249
969409 ZDOT = 1017
532389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2171698
07 X = -661933
57
Y = -13942375
30 feet Y = -4249635
99 meter
Z = 17165560
18 Z = 5232062
74
XDOT = 23934
351617 XDOT = 7295
190373
YDOT = 409
559065 feet/sec YDOT = 124
833603 meter/sec
ZDOT = 3366
844658 ZDOT = 1026
214252
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 16279
13057100
00016717 00000-0 10270-3 0 9133
2 25544 51
6438 229
6325 0006434 37
8877 322
2727 15
54042426 22085
Satellite: ISS
Catalog Number: 25544
Epoch time: 16279
13057100 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 229
6325 deg
Eccentricity:
0006434
Arg of perigee: 37
8877 deg
Mean anomaly: 322
2727 deg
Mean motion: 15
54042426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2208
Checksum: 302
Coasting Arc #15 (Orbit 2222)
---------------------------------------
Vector Time (GMT): 2016/280/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3634144
52 A = 6777887
48 meter
Y = 2322519
72 meter E =
0019044
Z = -5244522
42 I = 51
36339
XDOT = -4964
129421 Wp = 80
40361
YDOT = -5757
713018 meter/sec RA = 223
82743 deg
ZDOT = 895
963798 TA = 198
18010
MA = 198
24828
Ha = 223
206 n
mi
Hp = 212
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11923046
33 X = -3634369
34
Y = 7619815
36 feet Y = 2281878
55 meter
Z = -17206438
39 Z = -5262177
26
XDOT = -16286
513847 XDOT = -4903
728544
YDOT = -18890
134574 feet/sec YDOT = -5812
887440 meter/sec
ZDOT = 2939
513772 ZDOT = 871
996101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3368761
78 X = -1026798
59
Y = 13645491
11 feet Y = 4159145
69 meter
Z = -17283927
75 Z = -5268141
18
XDOT = -23826
935435 XDOT = -7262
449920
YDOT = -2314
916357 feet/sec YDOT = -705
586506 meter/sec
ZDOT = 2835
706141 ZDOT = 864
323232
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 16280
09517518
00016717 00000-0 10270-3 0 9145
2 25544 51
6435 224
8264 0006611 41
3824 318
7828 15
54031173 22236
Satellite: ISS
Catalog Number: 25544
Epoch time: 16280
09517518 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 224
8264 deg
Eccentricity:
0006611
Arg of perigee: 41
3824 deg
Mean anomaly: 318
7828 deg
Mean motion: 15
54031173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2223
Checksum: 295
Coasting Arc #16 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2016/281/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4758087
64 A = 6779989
29 meter
Y = -1006763
07 meter E =
0014096
Z = 4717547
09 I = 51
39427
XDOT = 3970
896255 Wp = 54
53853
YDOT = 5976
995528 meter/sec RA = 218
81297 deg
ZDOT = -2715
715535 TA = 62
46549
MA = 62
32232
Ha = 223
124 n
mi
Hp = 212
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15610523
74 X = 4746075
69
Y = -3303028
46 feet Y = -953621
73 meter
Z = 15477516
71 Z = 4740631
98
XDOT = 13027
874851 XDOT = 3916
956836
YDOT = 19609
565382 feet/sec YDOT = 6021
098944 meter/sec
ZDOT = -8909
827871 ZDOT = -2696
557088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8795366
51 X = 2680827
71
Y = -13194803
10 feet Y = -4021775
98 meter
Z = 15578532
38 Z = 4748336
67
XDOT = 22097
601330 XDOT = 6735
348885
YDOT = 4255
086372 feet/sec YDOT = 1296
950326 meter/sec
ZDOT = -8827
050276 ZDOT = -2690
484924
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 16281
12407871
00016717 00000-0 10270-3 0 9151
2 25544 51
6432 219
6982 0006605 45
0863 315
0824 15
54047327 22390
Satellite: ISS
Catalog Number: 25544
Epoch time: 16281
12407871 = yrday
fracday
Element set: 915
Inclination: 51
6432 deg
RA of node: 219
6982 deg
Eccentricity:
0006605
Arg of perigee: 45
0863 deg
Mean anomaly: 315
0824 deg
Mean motion: 15
54047327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2239
Checksum: 305
Coasting Arc #17 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2016/282/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5653025
20 A = 6783468
34 meter
Y = -185233
58 meter E =
0011120
Z = -3751755
28 I = 51
43139
XDOT = -2614
669039 Wp = 75
09463
YDOT = -5820
449086 meter/sec RA = 213
80951 deg
ZDOT = 4240
413726 TA = 239
91515
MA = 240
02546
Ha = 223
189 n
mi
Hp = 212
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18546670
61 X = -5632309
05
Y = -607721
71 feet Y = -248333
94 meter
Z = -12308908
39 Z = -3779166
32
XDOT = -8578
310494 XDOT = -2569
987365
YDOT = -19095
961568 feet/sec YDOT = -5849
437931 meter/sec
ZDOT = 13912
118522 ZDOT = 4227
821086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13426102
89 X = -4092276
16
Y = 12693535
86 feet Y = 3868989
73 meter
Z = -12428654
42 Z = -3788253
87
XDOT = -18741
741247 XDOT = -5712
482732
YDOT = -6297
002089 feet/sec YDOT = -1919
326237 meter/sec
ZDOT = 13857
991507 ZDOT = 4223
915811
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 16282
08866842
00016717 00000-0 10270-3 0 9165
2 25544 51
6428 214
8917 0006508 48
5089 311
6622 15
54052537 22544
Satellite: ISS
Catalog Number: 25544
Epoch time: 16282
08866842 = yrday
fracday
Element set: 916
Inclination: 51
6428 deg
RA of node: 214
8917 deg
Eccentricity:
0006508
Arg of perigee: 48
5089 deg
Mean anomaly: 311
6622 deg
Mean motion: 15
54052537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 323
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