[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 1st 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) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 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
217/02:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 212
7
220/05:58:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 212
7
223/08:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 212
8
Coasting Arc #1 (Orbit 1203)
---------------------------------------
Vector Time (GMT): 2016/214/12:34:23
421
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5412298
63 A = 6784174
34 meter
Y = -3132626
90 meter E =
0015479
Z = 2612550
48 I = 51
57452
XDOT = 4488
218695 Wp = 78
62786
YDOT = -3373
595575 meter/sec RA = 190
70681 deg
ZDOT = 5229
577304 TA = 310
84799
MA = 310
98207
Ha = 220
471 n
mi
Hp = 212
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17756885
28 X = -5389556
93
Y = -10277647
32 feet Y = -3193023
83 meter
Z = 8571359
83 Z = 2586314
50
XDOT = 14725
126951 XDOT = 4500
207034
YDOT = -11068
226952 feet/sec YDOT = -3323
338585 meter/sec
ZDOT = 17157
405854 ZDOT = 5251
408405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6460741
80 X = 1969234
10
Y = 19522719
13 feet Y = 5950524
79 meter
Z = 8457391
58 Z = 2577812
95
XDOT = -16849
446425 XDOT = -5135
711270
YDOT = -1931
699113 feet/sec YDOT = -588
781890 meter/sec
ZDOT = 17253
213726 ZDOT = 5258
779544
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 16214
58297527
00016717 00000-0 10270-3 0 9006
2 25544 51
6387 191
5305 0001882 90
2779 269
8590 15
54933053 12043
Satellite: ISS
Catalog Number: 25544
Epoch time: 16214
58297527 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 191
5305 deg
Eccentricity:
0001882
Arg of perigee: 90
2779 deg
Mean anomaly: 269
8590 deg
Mean motion: 15
54933053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1204
Checksum: 323
Coasting Arc #2 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2016/215/12:34:23
421
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3921338
93 A = 6779928
72 meter
Y = 3685752
33 meter E =
0009332
Z = -4133308
81 I = 51
59191
XDOT = -6221
991403 Wp = 74
88591
YDOT = 2387
869482 meter/sec RA = 185
71465 deg
ZDOT = -3778
350522 TA = 156
13073
MA = 156
08743
Ha = 220
508 n
mi
Hp = 212
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12865285
21 X = 3899909
84
Y = 12092363
29 feet Y = 3729483
71 meter
Z = -13560724
44 Z = -4114312
27
XDOT = -20413
357621 XDOT = -6229
877566
YDOT = 7834
217462 feet/sec YDOT = 2318
247075 meter/sec
ZDOT = -12396
163129 ZDOT = -3808
593751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1929178
70 X = -588013
67
Y = -17613760
27 feet Y = -5368674
13 meter
Z = -13478419
03 Z = -4108222
12
XDOT = 19236
009504 XDOT = 5863
135697
YDOT = 7468
230350 feet/sec YDOT = 2276
316611 meter/sec
ZDOT = -12528
532186 ZDOT = -3818
696610
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 16215
54702927
00016717 00000-0 10270-3 0 9019
2 25544 51
6388 186
7185 0001951 87
5972 272
5405 15
54902300 12190
Satellite: ISS
Catalog Number: 25544
Epoch time: 16215
54702927 = yrday
fracday
Element set: 901
Inclination: 51
6388 deg
RA of node: 186
7185 deg
Eccentricity:
0001951
Arg of perigee: 87
5972 deg
Mean anomaly: 272
5405 deg
Mean motion: 15
54902300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1219
Checksum: 313
Coasting Arc #3 (Orbit 1234)
---------------------------------------
Vector Time (GMT): 2016/216/12:34:23
421
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2011278
28 A = 6776158
70 meter
Y = -4031485
03 meter E =
0007120
Z = 5056882
62 I = 51
61318
XDOT = 7328
133060 Wp = 117
39419
YDOT = -1356
853991 meter/sec RA = 180
71308 deg
ZDOT = 1827
721904 TA = 314
88667
MA = 314
94445
Ha = 220
418 n
mi
Hp = 212
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6598682
02 X = -1990611
29
Y = -13226656
94 feet Y = -4053861
03 meter
Z = 16590822
24 Z = 5047162
68
XDOT = 24042
431299 XDOT = 7333
883031
YDOT = -4451
620706 feet/sec YDOT = -1274
873797 meter/sec
ZDOT = 5996
462940 ZDOT = 1863
333236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3296995
09 X = -1004924
10
Y = 14456878
13 feet Y = 4406456
45 meter
Z = 16549046
45 Z = 5044149
36
XDOT = -20249
922840 XDOT = -6172
176482
YDOT = -11680
081100 feet/sec YDOT = -3560
088719 meter/sec
ZDOT = 6152
110614 ZDOT = 1875
163315
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 16216
57534739
00016717 00000-0 10270-3 0 9028
2 25544 51
6401 181
5872 0001726 92
3765 267
7586 15
54937015 12351
Satellite: ISS
Catalog Number: 25544
Epoch time: 16216
57534739 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 181
5872 deg
Eccentricity:
0001726
Arg of perigee: 92
3765 deg
Mean anomaly: 267
7586 deg
Mean motion: 15
54937015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1235
Checksum: 323
Coasting Arc #4 (Orbit 1243)
---------------------------------------
Vector Time (GMT): 2016/217/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3192603
52 A = 6777493
58 meter
Y = -3634556
86 meter E =
0009656
Z = 4741092
34 I = 51
63905
XDOT = 6766
560900 Wp = 115
95106
YDOT = -2400
421237 meter/sec RA = 177
83661 deg
ZDOT = 2707
932237 TA = 307
25752
MA = 307
34555
Ha = 220
466 n
mi
Hp = 212
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10474421
01 X = -3174753
36
Y = -11924399
15 feet Y = -3670158
92 meter
Z = 15554764
91 Z = 4725627
16
XDOT = 22200
002954 XDOT = 6779
746453
YDOT = -7875
397760 feet/sec YDOT = -2324
679327 meter/sec
ZDOT = 8884
292117 ZDOT = 2740
833742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7982196
51 X = -2432973
50
Y = -13793721
80 feet Y = -4204326
40 meter
Z = 15487842
97 Z = 4720694
54
XDOT = 22262
459411 XDOT = 6785
597628
YDOT = -2714
632906 feet/sec YDOT = -827
420110 meter/sec
ZDOT = 9028
288793 ZDOT = 2751
822424
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 16217
15377472
00016717 00000-0 10270-3 0 9033
2 25544 51
6428 178
6970 0001869 108
2514 251
8842 15
54941059 12445
Satellite: ISS
Catalog Number: 25544
Epoch time: 16217
15377472 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 178
6970 deg
Eccentricity:
0001869
Arg of perigee: 108
2514 deg
Mean anomaly: 251
8842 deg
Mean motion: 15
54941059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1244
Checksum: 322
Coasting Arc #5 (Orbit 1258)
---------------------------------------
Vector Time (GMT): 2016/218/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1145014
36 A = 6775196
30 meter
Y = 4080426
48 meter E =
0016394
Z = -5300253
10 I = 51
66333
XDOT = -7510
472370 Wp = 88
29664
YDOT = 1387
183953 meter/sec RA = 172
83310 deg
ZDOT = -555
568127 TA = 176
40217
MA = 176
39036
Ha = 220
409 n
mi
Hp = 212
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3756608
80 X = 1125046
70
Y = 13387226
00 feet Y = 4093119
09 meter
Z = -17389281
84 Z = -5294739
57
XDOT = -24640
657383 XDOT = -7522
727368
YDOT = 4551
128454 feet/sec YDOT = 1303
128303 meter/sec
ZDOT = -1822
730074 ZDOT = -592
081127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1358109
60 X = 413951
81
Y = 13867204
54 feet Y = 4226723
94 meter
Z = -17365863
90 Z = -5293115
32
XDOT = -24034
081865 XDOT = -7325
588152
YDOT = -124
507698 feet/sec YDOT = -37
949946 meter/sec
ZDOT = -1982
344967 ZDOT = -604
218746
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 16218
11781911
00016717 00000-0 10270-3 0 9048
2 25544 51
6429 173
8869 0001831 108
4674 251
6679 15
54912662 12598
Satellite: ISS
Catalog Number: 25544
Epoch time: 16218
11781911 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 173
8869 deg
Eccentricity:
0001831
Arg of perigee: 108
4674 deg
Mean anomaly: 251
6679 deg
Mean motion: 15
54912662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1259
Checksum: 330
Coasting Arc #6 (Orbit 1274)
---------------------------------------
Vector Time (GMT): 2016/219/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 988526
69 A = 6775823
63 meter
Y = -4338408
55 meter E =
0006175
Z = 5105609
86 I = 51
69805
XDOT = 7484
967700 Wp = 69
58965
YDOT = -264
786979 meter/sec RA = 167
82802 deg
ZDOT = -1670
466197 TA = 36
53624
MA = 36
49413
Ha = 220
316 n
mi
Hp = 212
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3243197
81 X = 1012166
01
Y = -14233623
86 feet Y = -4327221
89 meter
Z = 16750688
52 Z = 5110469
31
XDOT = 24556
980644 XDOT = 7495
486576
YDOT = -868
723686 feet/sec YDOT = -181
026293 meter/sec
ZDOT = -5480
532143 ZDOT = -1634
081212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5450758
04 X = 1661391
05
Y = -13515519
10 feet Y = -4119530
22 meter
Z = 16772594
51 Z = 5112286
81
XDOT = 23410
165386 XDOT = 7135
418410
YDOT = 2821
934368 feet/sec YDOT = 860
125595 meter/sec
ZDOT = -5321
639069 ZDOT = -1622
035588
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 16219
14612886
00016717 00000-0 10270-3 0 9057
2 25544 51
6431 168
7548 0001817 111
7048 248
4299 15
54950456 12757
Satellite: ISS
Catalog Number: 25544
Epoch time: 16219
14612886 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 168
7548 deg
Eccentricity:
0001817
Arg of perigee: 111
7048 deg
Mean anomaly: 248
4299 deg
Mean motion: 15
54950456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1275
Checksum: 328
Coasting Arc #7 (Orbit 1289)
---------------------------------------
Vector Time (GMT): 2016/220/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2960652
52 A = 6779297
14 meter
Y = 4404673
80 meter E =
0010015
Z = -4228569
05 I = 51
74104
XDOT = -6659
464716 Wp = 111
50477
YDOT = -964
637912 meter/sec RA = 162
83339 deg
ZDOT = 3661
235207 TA = 195
97239
MA = 196
00400
Ha = 220
332 n
mi
Hp = 212
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9713426
90 X = -2989146
40
Y = 14451029
52 feet Y = 4371406
36 meter
Z = -13873258
05 Z = -4243020
28
XDOT = -21848
637521 XDOT = -6665
967381
YDOT = -3164
822545 feet/sec YDOT = -1039
144748 meter/sec
ZDOT = 12011
926531 ZDOT = 3628
869923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11666320
64 X = -3555894
53
Y = 12857123
02 feet Y = 3918851
10 meter
Z = -13937056
94 Z = -4248014
96
XDOT = -20273
511695 XDOT = -6179
366365
YDOT = -5539
973300 feet/sec YDOT = -1688
583862 meter/sec
ZDOT = 11870
764925 ZDOT = 3618
209149
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 16220
11016644
00016717 00000-0 10270-3 0 9067
2 25544 51
6431 163
9447 0001858 115
2183 244
9163 15
54949716 12901
Satellite: ISS
Catalog Number: 25544
Epoch time: 16220
11016644 = yrday
fracday
Element set: 906
Inclination: 51
6431 deg
RA of node: 163
9447 deg
Eccentricity:
0001858
Arg of perigee: 115
2183 deg
Mean anomaly: 244
9163 deg
Mean motion: 15
54949716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1290
Checksum: 302
Coasting Arc #8 (Orbit 1292)
---------------------------------------
Vector Time (GMT): 2016/220/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4672222
28 A = 6778836
75 meter
Y = -2148157
04 meter E =
0011513
Z = 4409604
32 I = 51
74239
XDOT = 5244
963168 Wp = 108
96652
YDOT = -4477
454743 meter/sec RA = 162
14555 deg
ZDOT = 3365
293226 TA = 307
02808
MA = 307
13335
Ha = 220
579 n
mi
Hp = 212
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15328813
25 X = -4669273
44
Y = -7047759
31 feet Y = -2200388
33 meter
Z = 14467205
78 Z = 4386915
40
XDOT = 17207
884409 XDOT = 5278
294480
YDOT = -14689
812148 feet/sec YDOT = -4418
615591 meter/sec
ZDOT = 11040
988274 ZDOT = 3390
852657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15904120
67 X = -4847575
98
Y = 5877854
61 feet Y = 1791570
08 meter
Z = 14368480
82 Z = 4379512
95
XDOT = 2222
228625 XDOT = 677
335285
YDOT = -21338
966933 feet/sec YDOT = -6504
117121 meter/sec
ZDOT = 11153
301638 ZDOT = 3399
526339
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 16220
30297362
00016717 00000-0 10270-3 0 9077
2 25544 51
6419 162
9833 0002049 105
0914 255
0466 15
54933962 12935
Satellite: ISS
Catalog Number: 25544
Epoch time: 16220
30297362 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 162
9833 deg
Eccentricity:
0002049
Arg of perigee: 105
0914 deg
Mean anomaly: 255
0466 deg
Mean motion: 15
54933962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1293
Checksum: 306
Coasting Arc #9 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2016/221/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2939430
08 A = 6775632
15 meter
Y = 3212187
88 meter E =
0015673
Z = -5205188
49 I = 51
76301
XDOT = -6494
612488 Wp = 83
67779
YDOT = 3845
111603 meter/sec RA = 157
15102 deg
ZDOT = -1296
384872 TA = 173
88557
MA = 173
86641
Ha = 220
429 n
mi
Hp = 212
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9643799
49 X = 2928576
39
Y = 10538674
16 feet Y = 3244997
72 meter
Z = -17077390
07 Z = -5190936
10
XDOT = -21307
783753 XDOT = -6530
829602
YDOT = 12615
195548 feet/sec YDOT = 3772
281966 meter/sec
ZDOT = -4253
231207 ZDOT = -1328
021772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14354454
60 X = 4375237
76
Y = 347119
96 feet Y = 105802
17 meter
Z = -17015666
73 Z = -5186375
22
XDOT = -5756
058475 XDOT = -1754
446623
YDOT = 23006
134116 feet/sec YDOT = 7012
269678 meter/sec
ZDOT = -4391
994887 ZDOT = -1338
680041
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 16221
26700629
00016717 00000-0 10270-3 0 9089
2 25544 51
6429 158
1726 0001938 109
0642 251
0721 15
54924931 13085
Satellite: ISS
Catalog Number: 25544
Epoch time: 16221
26700629 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 158
1726 deg
Eccentricity:
0001938
Arg of perigee: 109
0642 deg
Mean anomaly: 251
0721 deg
Mean motion: 15
54924931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 298
Coasting Arc #10 (Orbit 1323)
---------------------------------------
Vector Time (GMT): 2016/222/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -993650
96 A = 6775225
35 meter
Y = -4153976
66 meter E =
0004955
Z = 5255305
49 I = 51
78952
XDOT = 7048
628808 Wp = 78
43292
YDOT = -2882
998615 meter/sec RA = 152
15246 deg
ZDOT = -944
375458 TA = 20
58798
MA = 20
56802
Ha = 220
471 n
mi
Hp = 212
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3260009
71 X = -972654
06
Y = -13628532
36 feet Y = -4164970
81 meter
Z = 17241815
93 Z = 5250529
73
XDOT = 23125
422598 XDOT = 7084
930685
YDOT = -9458
656872 feet/sec YDOT = -2803
973180 meter/sec
ZDOT = -3098
344680 ZDOT = -910
047079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12242773
12 X = -3731597
25
Y = -6868396
78 feet Y = -2093487
34 meter
Z = 17221626
12 Z = 5249151
64
XDOT = 8443
359906 XDOT = 2573
536099
YDOT = -22455
940636 feet/sec YDOT = -6844
570706 meter/sec
ZDOT = -2947
964963 ZDOT = -898
539721
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 16222
29530383
00016717 00000-0 10270-3 0 9092
2 25544 51
6410 153
0407 0002047 110
5928 249
5445 15
54948197 13244
Satellite: ISS
Catalog Number: 25544
Epoch time: 16222
29530383 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 153
0407 deg
Eccentricity:
0002047
Arg of perigee: 110
5928 deg
Mean anomaly: 249
5445 deg
Mean motion: 15
54948197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1324
Checksum: 300
Coasting Arc #11 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2016/223/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -930104
91 A = 6778015
50 meter
Y = 4902954
33 meter E =
0012022
Z = -4598518
42 I = 51
82820
XDOT = -6848
364163 Wp = 110
74603
YDOT = 1562
906478 meter/sec RA = 147
16000 deg
ZDOT = 3053
834500 TA = 189
71607
MA = 189
73934
Ha = 220
368 n
mi
Hp = 212
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3051525
30 X = -962524
42
Y = 16085808
17 feet Y = 4892371
94 meter
Z = -15087002
68 Z = -4603115
41
XDOT = -22468
386362 XDOT = -6880
166085
YDOT = 5127
645926 feet/sec YDOT = 1486
145720 meter/sec
ZDOT = 10019
142059 ZDOT = 3020
489871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9930346
80 X = 3026769
71
Y = 12993193
74 feet Y = 3960325
45 meter
Z = -15107872
45 Z = -4604879
52
XDOT = -10390
238504 XDOT = -3166
944696
YDOT = 19412
385943 feet/sec YDOT = 5916
895235 meter/sec
ZDOT = 9873
254172 ZDOT = 3009
367872
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 16223
25932805
00016717 00000-0 10270-3 0 9106
2 25544 51
6424 148
2297 0001834 112
2268 247
9080 15
54931683 13396
Satellite: ISS
Catalog Number: 25544
Epoch time: 16223
25932805 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 148
2297 deg
Eccentricity:
0001834
Arg of perigee: 112
2268 deg
Mean anomaly: 247
9080 deg
Mean motion: 15
54931683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 306
Coasting Arc #12 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2016/223/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5581638
77 A = 6780759
54 meter
Y = -46302
85 meter E =
0007764
Z = -3857239
73 I = 51
83793
XDOT = -2825
163018 Wp = 84
07797
YDOT = 5778
579387 meter/sec RA = 146
63317 deg
ZDOT = -4163
947545 TA = 142
22809
MA = 142
17356
Ha = 220
397 n
mi
Hp = 212
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18312463
17 X = 5600478
36
Y = -151912
22 feet Y = 16220
06 meter
Z = -12654985
99 Z = -3830079
99
XDOT = -9268
907540 XDOT = -2869
344084
YDOT = 18958
593790 feet/sec YDOT = 5746
739440 meter/sec
ZDOT = -13661
245226 ZDOT = -4177
778753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 36394
47 X = 11093
03
Y = -18394470
36 feet Y = -5606634
56 meter
Z = -12536354
76 Z = -3821080
93
XDOT = 17520
444958 XDOT = 5340
231623
YDOT = 9372
522897 feet/sec YDOT = 2856
744979 meter/sec
ZDOT = -13722
589024 ZDOT = -4182
645135
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 16223
38786522
00016717 00000-0 10270-3 0 9114
2 25544 51
6399 147
5875 0001869 110
3024 249
8330 15
54947069 13415
Satellite: ISS
Catalog Number: 25544
Epoch time: 16223
38786522 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 147
5875 deg
Eccentricity:
0001869
Arg of perigee: 110
3024 deg
Mean anomaly: 249
8330 deg
Mean motion: 15
54947069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1341
Checksum: 323
Coasting Arc #13 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2016/224/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4417964
06 A = 6776652
86 meter
Y = -1440366
07 meter E =
0008354
Z = 4927836
64 I = 51
85072
XDOT = 4454
268598 Wp = 120
51922
YDOT = -5814
554783 meter/sec RA = 141
65013 deg
ZDOT = 2286
831581 TA = 307
17261
MA = 307
24886
Ha = 220
365 n
mi
Hp = 212
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14494632
73 X = -4425466
29
Y = -4725610
45 feet Y = -1489812
63 meter
Z = 16167443
05 Z = 4906357
23
XDOT = 14613
742118 XDOT = 4507
849014
YDOT = -19076
623304 feet/sec YDOT = -5764
444582 meter/sec
ZDOT = 7502
728284 ZDOT = 2308
599288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4623260
69 X = -1409169
86
Y = 14631085
87 feet Y = 4459554
97 meter
Z = 16073853
74 Z = 4899310
62
XDOT = -18109
102470 XDOT = -5519
654433
YDOT = -14095
785139 feet/sec YDOT = -4296
395310 meter/sec
ZDOT = 7598
758893 ZDOT = 2316
101711
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 16224
41615124
00016717 00000-0 10270-3 0 9129
2 25544 51
6397 142
4560 0001666 115
1028 245
0298 15
54978464 13571
Satellite: ISS
Catalog Number: 25544
Epoch time: 16224
41615124 = yrday
fracday
Element set: 912
Inclination: 51
6397 deg
RA of node: 142
4560 deg
Eccentricity:
0001666
Arg of perigee: 115
1028 deg
Mean anomaly: 245
0298 deg
Mean motion: 15
54978464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 304
Coasting Arc #14 (Orbit 1371)
---------------------------------------
Vector Time (GMT): 2016/225/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2935203
70 A = 6774964
19 meter
Y = 2990914
37 meter E =
0016406
Z = -5337572
69 I = 51
86948
XDOT = -5529
429062 Wp = 92
28147
YDOT = 5297
352008 meter/sec RA = 136
65768 deg
ZDOT = -73
161136 TA = 177
02750
MA = 177
01774
Ha = 220
276 n
mi
Hp = 212
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9629933
40 X = 2927467
79
Y = 9812711
19 feet Y = 3023694
57 meter
Z = -17511721
43 Z = -5323333
10
XDOT = -18141
171464 XDOT = -5587
899052
YDOT = 17379
763805 feet/sec YDOT = 5235
191311 meter/sec
ZDOT = -240
029974 ZDOT = -100
163456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9573440
76 X = 2917984
74
Y = -9976563
76 feet Y = -3040856
63 meter
Z = -17450006
11 Z = -5318761
86
XDOT = 17084
386517 XDOT = 5207
321010
YDOT = 17016
964487 feet/sec YDOT = 5186
770776 meter/sec
ZDOT = -358
861580 ZDOT = -109
381010
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 16225
38016697
00016717 00000-0 10270-3 0 9137
2 25544 51
6396 137
6441 0001708 117
0165 243
1163 15
54952667 13728
Satellite: ISS
Catalog Number: 25544
Epoch time: 16225
38016697 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 137
6441 deg
Eccentricity:
0001708
Arg of perigee: 117
0165 deg
Mean anomaly: 243
1163 deg
Mean motion: 15
54952667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1372
Checksum: 309
Coasting Arc #15 (Orbit 1387)
---------------------------------------
Vector Time (GMT): 2016/226/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1309269
95 A = 6776368
43 meter
Y = -4401126
01 meter E =
0007057
Z = 4978614
85 I = 51
89854
XDOT = 6027
226326 Wp = 69
29733
YDOT = -4233
580195 meter/sec RA = 131
66738 deg
ZDOT = -2152
588282 TA = 41
61348
MA = 41
55979
Ha = 220
262 n
mi
Hp = 212
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4295505
08 X = -1284141
84
Y = -14439389
78 feet Y = -4415626
72 meter
Z = 16334038
22 Z = 4972315
77
XDOT = 19774
364587 XDOT = 6084
575570
YDOT = -13889
698801 feet/sec YDOT = -4165
859026 meter/sec
ZDOT = -7062
297514 ZDOT = -2123
170618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14243848
08 X = -4341524
89
Y = 4993462
36 feet Y = 1522007
33 meter
Z = 16307245
97 Z = 4970448
57
XDOT = -14332
814103 XDOT = -4368
641739
YDOT = -18190
406698 feet/sec YDOT = -5544
435962 meter/sec
ZDOT = -6933
068997 ZDOT = -2113
199430
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 16226
40844363
00016717 00000-0 10270-3 0 9141
2 25544 51
6409 132
5122 0001631 120
9864 239
1449 15
54972740 13880
Satellite: ISS
Catalog Number: 25544
Epoch time: 16226
40844363 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 132
5122 deg
Eccentricity:
0001631
Arg of perigee: 120
9864 deg
Mean anomaly: 239
1449 deg
Mean motion: 15
54972740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1388
Checksum: 305
Coasting Arc #16 (Orbit 1402)
---------------------------------------
Vector Time (GMT): 2016/227/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -257774
91 A = 6780290
65 meter
Y = 5515717
12 meter E =
0008228
Z = -3943673
89 I = 51
93242
XDOT = -5934
396279 Wp = 109
71556
YDOT = 2629
778095 meter/sec RA = 126
68723 deg
ZDOT = 4070
157073 TA = 202
70358
MA = 202
73999
Ha = 220
195 n
mi
Hp = 212
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -845718
21 X = -300277
49
Y = 18096184
77 feet Y = 5512596
94 meter
Z = -12938562
64 Z = -3945029
21
XDOT = -19469
804065 XDOT = -5983
132867
YDOT = 8627
880888 feet/sec YDOT = 2563
143129 meter/sec
ZDOT = 13353
533705 ZDOT = 4041
211330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18108605
98 X = 5519503
10
Y = -297365
81 feet Y = -90637
10 meter
Z = -12945404
92 Z = -3945759
42
XDOT = 9736
176337 XDOT = 2967
586548
YDOT = 17697
156350 feet/sec YDOT = 5394
093255 meter/sec
ZDOT = 13226
615204 ZDOT = 4031
472314
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 16227
37244729
00016717 00000-0 10270-3 0 9159
2 25544 51
6409 127
7008 0001588 121
0735 239
0574 15
54967797 14031
Satellite: ISS
Catalog Number: 25544
Epoch time: 16227
37244729 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 127
7008 deg
Eccentricity:
0001588
Arg of perigee: 121
0735 deg
Mean anomaly: 239
0574 deg
Mean motion: 15
54967797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1403
Checksum: 324
Coasting Arc #17 (Orbit 1418)
---------------------------------------
Vector Time (GMT): 2016/228/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1663324
04 A = 6784535
55 meter
Y = -6145757
35 meter E =
0015362
Z = 2322332
32 I = 51
96563
XDOT = 5378
272600 Wp = 109
01745
YDOT = -608
856500 meter/sec RA = 121
72256 deg
ZDOT = -5438
962291 TA = 45
19359
MA = 45
06880
Ha = 220
165 n
mi
Hp = 212
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5457099
86 X = 1720643
13
Y = -20163245
89 feet Y = -6126836
49 meter
Z = 7619200
52 Z = 2330551
34
XDOT = 17645
251312 XDOT = 5411
100956
YDOT = -1997
560694 feet/sec YDOT = -548
529439 meter/sec
ZDOT = -17844
364471 ZDOT = -5412
756700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20513827
21 X = -6252614
53
Y = -3867157
22 feet Y = -1178709
52 meter
Z = 7656149
72 Z = 2333594
43
XDOT = -3618
814735 XDOT = -1103
014731
YDOT = -16062
249681 feet/sec YDOT = -4895
773703 meter/sec
ZDOT = -17729
743406 ZDOT = -5404
025790
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 16228
40071384
00016717 00000-0 10270-3 0 9160
2 25544 51
6414 122
5689 0001601 123
9461 236
1844 15
54983757 14197
Satellite: ISS
Catalog Number: 25544
Epoch time: 16228
40071384 = yrday
fracday
Element set: 916
Inclination: 51
6414 deg
RA of node: 122
5689 deg
Eccentricity:
0001601
Arg of perigee: 123
9461 deg
Mean anomaly: 236
1844 deg
Mean motion: 15
54983757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1419
Checksum: 311
Coasting Arc #18 (Orbit 1433)
---------------------------------------
Vector Time (GMT): 2016/229/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2763047
64 A = 6786728
81 meter
Y = 6180615
92 meter E =
0011365
Z = -405440
22 I = 51
98940
XDOT = -4463
367322 Wp = 50
14521
YDOT = -1607
886044 meter/sec RA = 116
76985 deg
ZDOT = 6025
205671 TA = 305
50344
MA = 305
60941
Ha = 220
093 n
mi
Hp = 212
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9065116
92 X = -2829986
08
Y = 20277611
27 feet Y = 6149343
39 meter
Z = -1330184
45 Z = -419024
75
XDOT = -14643
593575 XDOT = -4474
323090
YDOT = -5275
216680 feet/sec YDOT = -1657
859641 meter/sec
ZDOT = 19767
735142 ZDOT = 6003
497568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21030268
97 X = 6410025
98
Y = 7135914
63 feet Y = 2175026
78 meter
Z = -1390598
39 Z = -423854
39
XDOT = -3359
863576 XDOT = -1024
086418
YDOT = 13663
086945 feet/sec YDOT = 4164
508901 meter/sec
ZDOT = 19673
132706 ZDOT = 5996
370849
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 16229
36470814
00016717 00000-0 10270-3 0 9178
2 25544 51
6416 117
7580 0001553 130
5735 229
5554 15
54996195 14340
Satellite: ISS
Catalog Number: 25544
Epoch time: 16229
36470814 = yrday
fracday
Element set: 917
Inclination: 51
6416 deg
RA of node: 117
7580 deg
Eccentricity:
0001553
Arg of perigee: 130
5735 deg
Mean anomaly: 229
5554 deg
Mean motion: 15
54996195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1434
Checksum: 322
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