[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 26th 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
0 222
9
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
0
000/00:00:00
000 0
0 0
0 213
2
Coasting Arc #1 (Orbit 2073)
---------------------------------------
Vector Time (GMT): 2016/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4018107
22 A = 6778903
03 meter
Y = -2020217
64 meter E =
0014308
Z = -5083264
47 I = 51
25282
XDOT = 1570
102762 Wp = 75
01180
YDOT = -7307
533936 meter/sec RA = 271
79269 deg
ZDOT = 1670
684400 TA = 211
18787
MA = 211
27285
Ha = 222
679 n
mi
Hp = 214
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13182766
46 X = -3970525
74
Y = -6628010
64 feet Y = -2064885
31 meter
Z = -16677376
86 Z = -5102667
59
XDOT = 5151
255782 XDOT = 1643
585327
YDOT = -23974
848872 feet/sec YDOT = -7289
564949 meter/sec
ZDOT = 5481
248031 ZDOT = 1678
490810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13589957
62 X = 4142219
08
Y = 5496104
10 feet Y = 1675212
53 meter
Z = -16761761
46 Z = -5108984
89
XDOT = -2662
035419 XDOT = -811
388396
YDOT = 23330
996811 feet/sec YDOT = 7111
287828 meter/sec
ZDOT = 5516
587663 ZDOT = 1681
455920
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
51318479
00016717 00000-0 10270-3 0 9001
2 25544 51
6402 272
5824 0006674 6
3910 353
7327 15
53916628 20741
Satellite: ISS
Catalog Number: 25544
Epoch time: 16270
51318479 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 272
5824 deg
Eccentricity:
0006674
Arg of perigee: 6
3910 deg
Mean anomaly: 353
7327 deg
Mean motion: 15
53916628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2074
Checksum: 306
Coasting Arc #2 (Orbit 2089)
---------------------------------------
Vector Time (GMT): 2016/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3711162
82 A = 6781632
87 meter
Y = 3625959
28 meter E =
0013953
Z = 4364065
44 I = 51
26105
XDOT = -2344
018815 Wp = 45
61941
YDOT = 6476
625586 meter/sec RA = 266
77275 deg
ZDOT = -3371
583189 TA = 78
76813
MA = 78
61134
Ha = 222
670 n
mi
Hp = 214
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12175731
05 X = 3649141
88
Y = 11896191
85 feet Y = 3667113
74 meter
Z = 14317799
99 Z = 4381942
22
XDOT = -7690
350443 XDOT = -2399
890202
YDOT = 21248
771609 feet/sec YDOT = 6450
100386 meter/sec
ZDOT = -11061
624637 ZDOT = -3383
106328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13233162
79 X = -4033468
02
Y = -10603171
08 feet Y = -3231846
54 meter
Z = 14395255
09 Z = 4387673
75
XDOT = 4638
738997 XDOT = 1413
887646
YDOT = -20949
006249 feet/sec YDOT = -6385
257105 meter/sec
ZDOT = -11113
037735 ZDOT = -3387
253902
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
54213945
00016717 00000-0 10270-3 0 9018
2 25544 51
6389 267
4540 0006712 9
2268 350
9007 15
53967877 20908
Satellite: ISS
Catalog Number: 25544
Epoch time: 16271
54213945 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 267
4540 deg
Eccentricity:
0006712
Arg of perigee: 9
2268 deg
Mean anomaly: 350
9007 deg
Mean motion: 15
53967877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2090
Checksum: 320
Coasting Arc #3 (Orbit 2104)
---------------------------------------
Vector Time (GMT): 2016/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3345894
09 A = 6785301
47 meter
Y = -4926433
90 meter E =
0009511
Z = -3249538
91 I = 51
27644
XDOT = 3075
444807 Wp = 41
61284
YDOT = -5195
046978 meter/sec RA = 261
76289 deg
ZDOT = 4724
228737 TA = 280
51106
MA = 280
61820
Ha = 222
841 n
mi
Hp = 213
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10977342
81 X = -3274771
90
Y = -16162840
87 feet Y = -4963452
70 meter
Z = -10661216
88 Z = -3265619
01
XDOT = 10090
042018 XDOT = 3110
360280
YDOT = -17044
117381 feet/sec YDOT = -5160
459423 meter/sec
ZDOT = 15499
438114 ZDOT = 4739
254002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12755291
20 X = 3887812
76
Y = 14749826
37 feet Y = 4495747
08 meter
Z = -10730619
47 Z = -3270692
81
XDOT = -6813
397510 XDOT = -2076
723561
YDOT = 17180
910280 feet/sec YDOT = 5236
741453 meter/sec
ZDOT = 15565
917628 ZDOT = 4744
491693
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
50677814
00016717 00000-0 10270-3 0 9025
2 25544 51
6393 262
6471 0006793 14
5438 345
5909 15
53952373 21053
Satellite: ISS
Catalog Number: 25544
Epoch time: 16272
50677814 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 262
6471 deg
Eccentricity:
0006793
Arg of perigee: 14
5438 deg
Mean anomaly: 345
5909 deg
Mean motion: 15
53952373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2105
Checksum: 322
Coasting Arc #4 (Orbit 2120)
---------------------------------------
Vector Time (GMT): 2016/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2846895
11 A = 6788354
43 meter
Y = 5898937
23 meter E =
0014721
Z = 1772368
28 I = 51
29206
XDOT = -3805
167548 Wp = 86
71709
YDOT = 3541
697190 meter/sec RA = 256
76136 deg
ZDOT = -5634
188531 TA = 73
72730
MA = 73
56542
Ha = 222
933 n
mi
Hp = 213
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9340207
06 X = 2772110
67
Y = 19353468
60 feet Y = 5930355
23 meter
Z = 5814856
56 Z = 1786015
34
XDOT = -12484
145500 XDOT = -3817
120322
YDOT = 11619
741436 feet/sec YDOT = 3499
077603 meter/sec
ZDOT = -18484
870508 ZDOT = -5652
702701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11850656
65 X = -3612080
15
Y = -17907341
28 feet Y = -5458157
62 meter
Z = 5873485
90 Z = 1790238
50
XDOT = 9361
588317 XDOT = 2853
412119
YDOT = -12329
067843 feet/sec YDOT = -3757
899878 meter/sec
ZDOT = -18566
304942 ZDOT = -5659
009746
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
53571637
00016717 00000-0 10270-3 0 9036
2 25544 51
6388 257
5180 0006949 16
8587 343
2796 15
53997165 21215
Satellite: ISS
Catalog Number: 25544
Epoch time: 16273
53571637 = yrday
fracday
Element set: 903
Inclination: 51
6388 deg
RA of node: 257
5180 deg
Eccentricity:
0006949
Arg of perigee: 16
8587 deg
Mean anomaly: 343
2796 deg
Mean motion: 15
53997165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2121
Checksum: 345
Coasting Arc #5 (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 = -3987984
91 A = 6777819
48 meter
Y = 1512896
44 meter E =
0018423
Z = -5282551
30 I = 51
26169
XDOT = -2210
500516 Wp = 66
15569
YDOT = -7317
290637 meter/sec RA = 255
72151 deg
ZDOT = -420
709099 TA = 199
76845
MA = 199
83994
Ha = 222
938 n
mi
Hp = 213
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13083939
99 X = -3978945
62
Y = 4963570
99 feet Y = 1468349
88 meter
Z = -17331205
04 Z = -5301902
29
XDOT = -7252
298280 XDOT = -2126
468785
YDOT = -24006
859044 feet/sec YDOT = -7341
540149 meter/sec
ZDOT = -1380
279195 ZDOT = -431
242032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3645303
67 X = -1111088
56
Y = -13401241
24 feet Y = -4084698
33 meter
Z = -17415960
65 Z = -5308384
81
XDOT = 23631
837938 XDOT = 7202
984204
YDOT = -4550
092687 feet/sec YDOT = -1386
868251 meter/sec
ZDOT = -1425
079236 ZDOT = -434
364151
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
72864296
00016717 00000-0 10270-3 0 9044
2 25544 51
6422 256
5577 0006927 17
5933 342
5458 15
53992351 21244
Satellite: ISS
Catalog Number: 25544
Epoch time: 16273
72864296 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 256
5577 deg
Eccentricity:
0006927
Arg of perigee: 17
5933 deg
Mean anomaly: 342
5458 deg
Mean motion: 15
53992351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2124
Checksum: 332
Coasting Arc #6 (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 = 4427819
87 A = 6778337
32 meter
Y = 209386
36 meter E =
0010928
Z = 5124709
13 I = 51
27251
XDOT = 1353
030938 Wp = 33
79412
YDOT = 7408
257768 meter/sec RA = 250
69754 deg
ZDOT = -1461
287201 TA = 70
39793
MA = 70
27999
Ha = 222
790 n
mi
Hp = 213
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14526968
06 X = 4400255
52
Y = 686963
14 feet Y = 258747
85 meter
Z = 16813350
17 Z = 5146151
57
XDOT = 4439
077880 XDOT = 1277
187718
YDOT = 24305
307639 feet/sec YDOT = 7422
963987 meter/sec
ZDOT = -4794
249347 ZDOT = -1454
899773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1875245
09 X = -571574
70
Y = 14311940
16 feet Y = 4362279
36 meter
Z = 16906959
76 Z = 5153241
33
XDOT = -23547
111713 XDOT = -7177
159650
YDOT = 2586
933441 feet/sec YDOT = 788
497313 meter/sec
ZDOT = -4767
553918 ZDOT = -1453
150434
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
75757145
00016717 00000-0 10270-3 0 9053
2 25544 51
6419 251
4300 0006850 19
6850 340
4565 15
54029908 21408
Satellite: ISS
Catalog Number: 25544
Epoch time: 16274
75757145 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 251
4300 deg
Eccentricity:
0006850
Arg of perigee: 19
6850 deg
Mean anomaly: 340
4565 deg
Mean motion: 15
54029908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2140
Checksum: 305
Coasting Arc #7 (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 = -4761427
12 A = 6781044
70 meter
Y = -1806633
88 meter E =
0012121
Z = -4486073
88 I = 51
29420
XDOT = -347
583795 Wp = 76
11532
YDOT = -6959
724294 meter/sec RA = 245
67847 deg
ZDOT = 3181
853886 TA = 225
99315
MA = 226
09311
Ha = 222
970 n
mi
Hp = 213
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15621480
07 X = -4719079
32
Y = -5927276
51 feet Y = -1859643
22 meter
Z = -14718090
14 Z = -4509100
86
XDOT = -1140
366781 XDOT = -285
188817
YDOT = -22833
741121 feet/sec YDOT = -6963
261880 meter/sec
ZDOT = 10439
153170 ZDOT = 3180
317944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6930102
41 X = 2112295
21
Y = -15105466
13 feet Y = -4604146
08 meter
Z = -14818366
90 Z = -4516638
23
XDOT = 21761
453196 XDOT = 6632
890934
YDOT = -219
189578 feet/sec YDOT = -66
808983 meter/sec
ZDOT = 10433
561550 ZDOT = 3180
149560
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
72218524
00016717 00000-0 10270-3 0 9065
2 25544 51
6432 246
6224 0006870 23
2187 336
9274 15
54006814 21554
Satellite: ISS
Catalog Number: 25544
Epoch time: 16275
72218524 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 246
6224 deg
Eccentricity:
0006870
Arg of perigee: 23
2187 deg
Mean anomaly: 336
9274 deg
Mean motion: 15
54006814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2155
Checksum: 303
Coasting Arc #8 (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 = 4912163
02 A = 6784778
66 meter
Y = 3248756
77 meter E =
0016867
Z = 3361512
68 I = 51
32080
XDOT = -833
539467 Wp = 69
15496
YDOT = 6065
021935 meter/sec RA = 240
66953 deg
ZDOT = -4618
812956 TA = 71
42512
MA = 71
24198
Ha = 223
092 n
mi
Hp = 213
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16116020
40 X = 4859140
48
Y = 10658650
81 feet Y = 3303391
86 meter
Z = 11028584
91 Z = 3385245
87
XDOT = -2734
709539 XDOT = -878
861590
YDOT = 19898
365930 feet/sec YDOT = 6055
446704 meter/sec
ZDOT = -15153
585813 ZDOT = -4622
973044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11419767
62 X = -3480745
17
Y = 15512455
75 feet Y = 4728196
51 meter
Z = 11131723
13 Z = 3392949
21
XDOT = -18615
822300 XDOT = -5674
102637
YDOT = -2758
773650 feet/sec YDOT = -840
874208 meter/sec
ZDOT = -15172
720085 ZDOT = -4624
645082
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
75109706
00016717 00000-0 10270-3 0 9071
2 25544 51
6431 241
4945 0006956 28
3041 331
8489 15
54016038 21715
Satellite: ISS
Catalog Number: 25544
Epoch time: 16276
75109706 = yrday
fracday
Element set: 907
Inclination: 51
6431 deg
RA of node: 241
4945 deg
Eccentricity:
0006956
Arg of perigee: 28
3041 deg
Mean anomaly: 331
8489 deg
Mean motion: 15
54016038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2171
Checksum: 310
Coasting Arc #9 (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 = -4840946
28 A = 6787923
35 meter
Y = -4336581
88 meter E =
0013653
Z = -1940748
41 I = 51
34837
XDOT = 2102
202941 Wp = 35
46711
YDOT = -4827
975532 meter/sec RA = 235
67116 deg
ZDOT = 5575
040216 TA = 303
04052
MA = 303
17160
Ha = 223
048 n
mi
Hp = 213
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15882369
70 X = -4782666
25
Y = -14227630
85 feet Y = -4390390
97 meter
Z = -6367284
80 Z = -1964122
83
XDOT = 6896
991275 XDOT = 2128
952737
YDOT = -15839
814738 feet/sec YDOT = -4804
317037 meter/sec
ZDOT = 18290
814358 ZDOT = 5585
317932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14711803
44 X = 4484157
69
Y = -15392735
56 feet Y = -4691705
80 meter
Z = -6468693
38 Z = -1971657
74
XDOT = 14498
292492 XDOT = 4419
079552
YDOT = 6192
751968 feet/sec YDOT = 1887
550800 meter/sec
ZDOT = 18336
467943 ZDOT = 5588
955429
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
71569294
00016717 00000-0 10270-3 0 9081
2 25544 51
6433 236
6871 0006869 30
6097 329
5455 15
54043509 21867
Satellite: ISS
Catalog Number: 25544
Epoch time: 16277
71569294 = yrday
fracday
Element set: 908
Inclination: 51
6433 deg
RA of node: 236
6871 deg
Eccentricity:
0006869
Arg of perigee: 30
6097 deg
Mean anomaly: 329
5455 deg
Mean motion: 15
54043509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2186
Checksum: 342
Coasting Arc #10 (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 = -1236393
75 A = 6780166
13 meter
Y = 4718911
93 meter E =
0016483
Z = -4724927
98 I = 51
32844
XDOT = -5775
611408 Wp = 58
00692
YDOT = -4229
464980 meter/sec RA = 233
85962 deg
ZDOT = -2711
163336 TA = 185
00723
MA = 185
02374
Ha = 223
035 n
mi
Hp = 213
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4056409
95 X = -1266117
86
Y = 15481994
52 feet Y = 4704918
99 meter
Z = -15501732
22 Z = -4731006
93
XDOT = -18948
856327 XDOT = -5714
717296
YDOT = -13876
197440 feet/sec YDOT = -4293
711582 meter/sec
ZDOT = -8894
892834 ZDOT = -2739
071900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7255014
29 X = 2211328
35
Y = 14236023
36 feet Y = 4339139
92 meter
Z = -15529028
45 Z = -4733247
87
XDOT = -22311
370693 XDOT = -6800
505787
YDOT = 1529
709900 feet/sec YDOT = 466
255578 meter/sec
ZDOT = -9016
126873 ZDOT = -2748
115471
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
10152972
00016717 00000-0 10270-3 0 9097
2 25544 51
6429 234
7598 0006341 34
5819 325
5745 15
54024719 21924
Satellite: ISS
Catalog Number: 25544
Epoch time: 16278
10152972 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 234
7598 deg
Eccentricity:
0006341
Arg of perigee: 34
5819 deg
Mean anomaly: 325
5745 deg
Mean motion: 15
54024719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 325
Coasting Arc #11 (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 = 2478665
23 A = 6777745
26 meter
Y = -3519755
11 meter E =
0007622
Z = 5228590
66 I = 51
34156
XDOT = 5536
854917 Wp = 65
11282
YDOT = 5236
871484 meter/sec RA = 228
84184 deg
ZDOT = 902
645546 TA = 16
23644
MA = 16
21203
Ha = 222
905 n
mi
Hp = 213
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8132103
79 X = 2492441
10
Y = -11547753
00 feet Y = -3491959
45 meter
Z = 17154168
83 Z = 5240665
44
XDOT = 18165
534504 XDOT = 5473
498628
YDOT = 17181
336890 feet/sec YDOT = 5298
434158 meter/sec
ZDOT = 2961
435520 ZDOT = 929
388260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1844314
51 X = -562147
06
Y = -13937318
26 feet Y = -4248094
61 meter
Z = 17207465
91 Z = 5244835
61
XDOT = 23968
661264 XDOT = 7305
647953
YDOT = 619
194959 feet/sec YDOT = 188
730623 meter/sec
ZDOT = 3077
432164 ZDOT = 938
001324
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
13041753
00016717 00000-0 10270-3 0 9107
2 25544 51
6435 229
6313 0006400 38
0132 322
1471 15
54089042 22089
Satellite: ISS
Catalog Number: 25544
Epoch time: 16279
13041753 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 229
6313 deg
Eccentricity:
0006400
Arg of perigee: 38
0132 deg
Mean anomaly: 322
1471 deg
Mean motion: 15
54089042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2208
Checksum: 270
Coasting Arc #12 (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 = -3712081
13 A = 6777798
07 meter
Y = 2231000
95 meter E =
0018878
Z = -5229355
97 I = 51
36337
XDOT = -4890
467796 Wp = 81
04022
YDOT = -5803
433693 meter/sec RA = 223
82414 deg
ZDOT = 1001
585625 TA = 198
56793
MA = 198
63691
Ha = 223
112 n
mi
Hp = 212
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12178743
86 X = -3711350
44
Y = 7319556
91 feet Y = 2189493
57 meter
Z = -17156679
68 Z = -5247387
08
XDOT = -16044
841852 XDOT = -4830
074209
YDOT = -19040
136787 feet/sec YDOT = -5857
784412 meter/sec
ZDOT = 3286
042077 ZDOT = 977
975751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3761009
71 X = -1146355
76
Y = 13602625
73 feet Y = 4146080
32 meter
Z = -17235798
57 Z = -5253471
40
XDOT = -23758
718438 XDOT = -7241
657380
YDOT = -2559
672737 feet/sec YDOT = -780
188250 meter/sec
ZDOT = 3183
804756 ZDOT = 970
423689
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
09499141
00016717 00000-0 10270-3 0 9113
2 25544 51
6433 224
8250 0006574 41
6221 318
5431 15
54083881 22232
Satellite: ISS
Catalog Number: 25544
Epoch time: 16280
09499141 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 224
8250 deg
Eccentricity:
0006574
Arg of perigee: 41
6221 deg
Mean anomaly: 318
5431 deg
Mean motion: 15
54083881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2223
Checksum: 289
Coasting Arc #13 (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 = 4831682
63 A = 6780037
00 meter
Y = -894066
80 meter E =
0014324
Z = 4665171
88 I = 51
39471
XDOT = 3855
558184 Wp = 55
54270
YDOT = 5999
874835 meter/sec RA = 218
80951 deg
ZDOT = -2829
140420 TA = 62
68484
MA = 62
53907
Ha = 223
026 n
mi
Hp = 212
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15851977
14 X = 4818659
44
Y = -2933290
02 feet Y = -840108
13 meter
Z = 15305682
03 Z = 4688611
81
XDOT = 12649
469108 XDOT = 3801
922474
YDOT = 19684
628725 feet/sec YDOT = 6042
690152 meter/sec
ZDOT = -9281
956757 ZDOT = -2810
541529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9227179
44 X = 2812444
29
Y = -13099573
86 feet Y = -3992750
11 meter
Z = 15408231
45 Z = 4696428
94
XDOT = 21887
833910 XDOT = 6671
411776
YDOT = 4539
878531 feet/sec YDOT = 1383
754976 meter/sec
ZDOT = -9201
627445 ZDOT = -2804
656045
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
12385897
00016717 00000-0 10270-3 0 9121
2 25544 51
6429 219
6966 0006560 45
3847 314
7840 15
54102562 22390
Satellite: ISS
Catalog Number: 25544
Epoch time: 16281
12385897 = yrday
fracday
Element set: 912
Inclination: 51
6429 deg
RA of node: 219
6966 deg
Eccentricity:
0006560
Arg of perigee: 45
3847 deg
Mean anomaly: 314
7840 deg
Mean motion: 15
54102562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2239
Checksum: 325
Coasting Arc #14 (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 = -5709191
04 A = 6783592
99 meter
Y = -314197
19 meter E =
0010892
Z = -3656310
48 I = 51
43217
XDOT = -2454
194156 Wp = 73
20447
YDOT = -5813
375001 meter/sec RA = 213
80618 deg
ZDOT = 4345
529862 TA = 243
24244
MA = 243
35392
Ha = 223
074 n
mi
Hp = 212
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18730941
72 X = -5687492
24
Y = -1030830
67 feet Y = -377920
13 meter
Z = -11995769
28 Z = -3683991
97
XDOT = -8051
818096 XDOT = -2410
114130
YDOT = -19072
752629 feet/sec YDOT = -5840
572665 meter/sec
ZDOT = 14256
987736 ZDOT = 4333
715319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13857814
67 X = -4223861
91
Y = 12528223
22 feet Y = 3818602
44 meter
Z = -12116677
17 Z = -3693163
20
XDOT = -18368
409889 XDOT = -5598
691334
YDOT = -6621
687630 feet/sec YDOT = -2018
290390 meter/sec
ZDOT = 14206
259570 ZDOT = 4330
067917
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
08841113
00016717 00000-0 10270-3 0 9136
2 25544 51
6426 214
8897 0006449 48
6670 311
5037 15
54112854 22548
Satellite: ISS
Catalog Number: 25544
Epoch time: 16282
08841113 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 214
8897 deg
Eccentricity:
0006449
Arg of perigee: 48
6670 deg
Mean anomaly: 311
5037 deg
Mean motion: 15
54112854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 308
Coasting Arc #15 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2016/283/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6249255
34 A = 6787166
29 meter
Y = 1423499
91 meter E =
0018416
Z = 2216228
73 I = 51
47141
XDOT = 726
886254 Wp = 91
23743
YDOT = 5350
066300 meter/sec RA = 208
81390 deg
ZDOT = -5447
200156 TA = 64
07063
MA = 63
88096
Ha = 223
172 n
mi
Hp = 212
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20502806
24 X = 6222107
33
Y = 4670275
29 feet Y = 1493231
64 meter
Z = 7271091
64 Z = 2246520
36
XDOT = 2384
797420 XDOT = 693
466890
YDOT = 17552
710958 feet/sec YDOT = 5358
007582 meter/sec
ZDOT = -17871
391588 ZDOT = -5443
750638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17515721
71 X = 5338791
98
Y = -11551479
32 feet Y = -3520890
90 meter
Z = 7403251
11 Z = 2256510
94
XDOT = 13568
173235 XDOT = 4135
579202
YDOT = 9048
968754 feet/sec YDOT = 2758
125676 meter/sec
ZDOT = -17857
136474 ZDOT = -5442
855197
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 16283
11725257
00016717 00000-0 10270-3 0 9142
2 25544 51
6425 209
7612 0006628 52
4488 307
7266 15
54131404 22705
Satellite: ISS
Catalog Number: 25544
Epoch time: 16283
11725257 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 209
7612 deg
Eccentricity:
0006628
Arg of perigee: 52
4488 deg
Mean anomaly: 307
7266 deg
Mean motion: 15
54131404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 301
Coasting Arc #16 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2016/284/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6355352
82 A = 6789226
84 meter
Y = -2292722
81 meter E =
0017255
Z = -591795
92 I = 51
50614
XDOT = 1144
636718 Wp = 46
40125
YDOT = -4681
899570 meter/sec RA = 203
83152 deg
ZDOT = 5966
843448 TA = 307
19770
MA = 307
35508
Ha = 223
244 n
mi
Hp = 212
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20850895
07 X = -6326367
94
Y = -7522056
48 feet Y = -2363630
61 meter
Z = -1941587
65 Z = -622598
34
XDOT = 3755
369809 XDOT = 1167
921208
YDOT = -15360
562893 feet/sec YDOT = -4668
968819 meter/sec
ZDOT = 19576
258031 ZDOT = 5972
460779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19667992
54 X = -5994804
13
Y = 10196655
10 feet Y = 3107940
47 meter
Z = -2075865
06 Z = -632723
67
XDOT = -8072
394562 XDOT = -2460
465862
YDOT = -11655
440148 feet/sec YDOT = -3552
578157 meter/sec
ZDOT = 19601
521670 ZDOT = 5974
543805
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 16284
08177833
00016717 00000-0 10270-3 0 9151
2 25544 51
6419 204
9536 0006664 54
5631 305
6143 15
54105041 22858
Satellite: ISS
Catalog Number: 25544
Epoch time: 16284
08177833 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 204
9536 deg
Eccentricity:
0006664
Arg of perigee: 54
5631 deg
Mean anomaly: 305
6143 deg
Mean motion: 15
54105041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 303
Coasting Arc #17 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2016/285/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5970934
30 A = 6788668
88 meter
Y = 3012425
79 meter E =
0012210
Z = -1159643
22 I = 51
53431
XDOT = -3077
785102 Wp = 109
93101
YDOT = 3866
485741 meter/sec RA = 198
85358 deg
ZDOT = -5857
607878 TA = 82
67239
MA = 82
53364
Ha = 223
231 n
mi
Hp = 212
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19589679
45 X = 5942437
90
Y = 9883286
71 feet Y = 3079037
34 meter
Z = -3804603
72 Z = -1130707
17
XDOT = -10097
720152 XDOT = -3092
338413
YDOT = 12685
320671 feet/sec YDOT = 3831
985978 meter/sec
ZDOT = -19217
873616 ZDOT = -5872
594807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20435393
50 X = 6228707
94
Y = -8048148
03 feet Y = -2453075
52 meter
Z = -3678574
76 Z = -1121229
59
XDOT = 2231
764120 XDOT = 680
241704
YDOT = 14396
671316 feet/sec YDOT = 4388
105417 meter/sec
ZDOT = -19283
967930 ZDOT = -5877
753425
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 16285
11059283
00016717 00000-0 10270-3 0 9165
2 25544 51
6415 199
8250 0006591 59
8669 300
3136 15
54170167 23011
Satellite: ISS
Catalog Number: 25544
Epoch time: 16285
11059283 = yrday
fracday
Element set: 916
Inclination: 51
6415 deg
RA of node: 199
8250 deg
Eccentricity:
0006591
Arg of perigee: 59
8669 deg
Mean anomaly: 300
3136 deg
Mean motion: 15
54170167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 310
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