[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 2nd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2015/001/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4634250
17 A = 6784482
74 meter
Y = -2232791
82 meter E =
0007401
Z = 4415887
26 I = 51
52143
XDOT = 5306
789338 Wp = 116
12623
YDOT = 4425
389764 meter/sec RA = 197
29951 deg
ZDOT = -3330
463833 TA = 7
56446
MA = 7
55330
Ha = 223
567 n
mi
Hp = 216
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15204232
85 X = 4637422
49
Y = -7325432
48 feet Y = -2180951
21 meter
Z = 14487819
10 Z = 4438407
24
XDOT = 17410
726173 XDOT = 5273
087428
YDOT = 14518
995289 feet/sec YDOT = 4484
545532 meter/sec
ZDOT = -10926
718611 ZDOT = -3304
765851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9718134
82 X = -2962087
49
Y = -13696061
32 feet Y = -4174559
49 meter
Z = 14584351
89 Z = 4445310
45
XDOT = 10434
867396 XDOT = 3180
547582
YDOT = -18927
459852 feet/sec YDOT = -5769
089763 meter/sec
ZDOT = -10817
738850 ZDOT = -3297
246801
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 15001
19974287
00016717 00000-0 10270-3 0 9001
2 25544 51
6430 198
2180 0006738 196
7826 163
3104 15
52912883 2030
Satellite: ISS
Catalog Number: 25544
Epoch time: 15001
19974287 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 198
2180 deg
Eccentricity:
0006738
Arg of perigee: 196
7826 deg
Mean anomaly: 163
3104 deg
Mean motion: 15
52912883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 203
Checksum: 305
Coasting Arc #2 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2015/002/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5526488
25 A = 6787373
13 meter
Y = 1691895
25 meter E =
0007532
Z = -3567820
77 I = 51
56170
XDOT = -4265
696159 Wp = 157
23425
YDOT = -4545
104955 meter/sec RA = 192
31519 deg
ZDOT = 4448
510767 TA = 160
65078
MA = 160
62216
Ha = 223
518 n
mi
Hp = 216
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18131523
12 X = -5527665
47
Y = 5550837
44 feet Y = 1630088
19 meter
Z = -11705448
72 Z = -3594670
20
XDOT = -13995
066139 XDOT = -4236
163973
YDOT = -14911
761662 feet/sec YDOT = -4592
641992 meter/sec
ZDOT = 14594
851598 ZDOT = 4427
860108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8743557
15 X = 2665036
22
Y = 16745446
73 feet Y = 5104012
16 meter
Z = -11820392
50 Z = -3602855
63
XDOT = -10876
348775 XDOT = -3315
111107
YDOT = 15927
990377 feet/sec YDOT = 4854
851467 meter/sec
ZDOT = 14507
430616 ZDOT = 4421
864852
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 15002
16503319
00016717 00000-0 10270-3 0 9014
2 25544 51
6433 193
4150 0006645 200
6161 159
4724 15
52914548 2181
Satellite: ISS
Catalog Number: 25544
Epoch time: 15002
16503319 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 193
4150 deg
Eccentricity:
0006645
Arg of perigee: 200
6161 deg
Mean anomaly: 159
4724 deg
Mean motion: 15
52914548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 218
Checksum: 279
Coasting Arc #3 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2015/003/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6199577
26 A = 6790023
03 meter
Y = -1183142
78 meter E =
0014026
Z = 2479607
54 I = 51
60055
XDOT = 3015
382014 Wp = 132
06351
YDOT = 4636
865960 meter/sec RA = 187
33796 deg
ZDOT = -5316
546458 TA = 20
12337
MA = 20
06813
Ha = 223
172 n
mi
Hp = 217
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20339820
40 X = 6200301
66
Y = -3881702
05 feet Y = -1113811
27 meter
Z = 8135195
34 Z = 2509725
54
XDOT = 9892
985609 XDOT = 2989
133178
YDOT = 15212
814828 feet/sec YDOT = 4670
439644 meter/sec
ZDOT = -17442
737722 ZDOT = -5301
961639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7838536
93 X = -2389186
06
Y = -19110741
47 feet Y = -5824954
00 meter
Z = 8264030
93 Z = 2518876
63
XDOT = 11524
181553 XDOT = 3512
570537
YDOT = -12257
063453 feet/sec YDOT = -3735
952941 meter/sec
ZDOT = -17381
226197 ZDOT = -5297
797745
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 15003
19465744
00016717 00000-0 10270-3 0 9028
2 25544 51
6419 188
2906 0006534 205
1386 154
9449 15
52966382 2347
Satellite: ISS
Catalog Number: 25544
Epoch time: 15003
19465744 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 188
2906 deg
Eccentricity:
0006534
Arg of perigee: 205
1386 deg
Mean anomaly: 154
9449 deg
Mean motion: 15
52966382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 234
Checksum: 319
Coasting Arc #4 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2015/004/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6638398
97 A = 6791868
50 meter
Y = 711518
82 meter E =
0002657
Z = -1244833
16 I = 51
63833
XDOT = -1596
341927 Wp = 64
08428
YDOT = -4693
289856 meter/sec RA = 182
36881 deg
ZDOT = 5841
176805 TA = 282
39718
MA = 282
42691
Ha = 223
118 n
mi
Hp = 217
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21779524
18 X = -6639815
05
Y = 2334379
34 feet Y = 637276
14 meter
Z = -4084098
30 Z = -1277084
48
XDOT = -5237
342281 XDOT = -1572
115962
YDOT = -15397
932600 feet/sec YDOT = -4711
006283 meter/sec
ZDOT = 19163
965895 ZDOT = 5833
480513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6971676
35 X = 2124966
95
Y = 20737584
53 feet Y = 6320815
76 meter
Z = -4221987
20 Z = -1286861
70
XDOT = -12365
521425 XDOT = -3769
010930
YDOT = 8045
182373 feet/sec YDOT = 2452
171587 meter/sec
ZDOT = 19131
879348 ZDOT = 5831
396825
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 15004
15991338
00016717 00000-0 10270-3 0 9039
2 25544 51
6418 183
4874 0006632 207
7298 152
3501 15
53012348 2498
Satellite: ISS
Catalog Number: 25544
Epoch time: 15004
15991338 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 183
4874 deg
Eccentricity:
0006632
Arg of perigee: 207
7298 deg
Mean anomaly: 152
3501 deg
Mean motion: 15
53012348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 301
Coasting Arc #5 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2015/005/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6778632
16 A = 6792604
60 meter
Y = -230573
92 meter E =
0014691
Z = -97097
05 I = 51
67159
XDOT = 79
572940 Wp = 160
67727
YDOT = 4757
809051 meter/sec RA = 177
40339 deg
ZDOT = -6016
675015 TA = 20
36826
MA = 20
30973
Ha = 222
890 n
mi
Hp = 217
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22239606
84 X = 6781178
35
Y = -756476
10 feet Y = -154756
61 meter
Z = -318559
88 Z = -64161
84
XDOT = 261
066075 XDOT = 55
590630
YDOT = 15609
609748 feet/sec YDOT = 4758
565331 meter/sec
ZDOT = -19739
747425 ZDOT = -6016
346294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5906520
44 X = -1800307
43
Y = -21455890
78 feet Y = -6539755
51 meter
Z = -177808
92 Z = -54196
16
XDOT = 13525
820915 XDOT = 4122
670215
YDOT = -3573
225865 feet/sec YDOT = -1089
119244 meter/sec
ZDOT = -19739
142502 ZDOT = -6016
490635
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 15005
18950136
00016717 00000-0 10270-3 0 9045
2 25544 51
6413 178
3624 0006411 213
4559 146
6189 15
53003445 2652
Satellite: ISS
Catalog Number: 25544
Epoch time: 15005
18950136 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 178
3624 deg
Eccentricity:
0006411
Arg of perigee: 213
4559 deg
Mean anomaly: 146
6189 deg
Mean motion: 15
53003445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 291
Coasting Arc #6 (Orbit 280)
---------------------------------------
Vector Time (GMT): 2015/006/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6633733
61 A = 6791576
50 meter
Y = -252556
79 meter E =
0008161
Z = 1421989
68 I = 51
70017
XDOT = 1430
936281 Wp = 79
30836
YDOT = -4806
586687 meter/sec RA = 172
44097 deg
ZDOT = 5794
990968 TA = 296
17104
MA = 296
25495
Ha = 222
666 n
mi
Hp = 217
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21764217
89 X = -6637323
85
Y = -828598
41 feet Y = -326759
70 meter
Z = 4665320
47 Z = 1389755
87
XDOT = 4694
672838 XDOT = 1456
428703
YDOT = -15769
641360 feet/sec YDOT = -4790
442943 meter/sec
ZDOT = 19012
437560 ZDOT = 5802
003652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4628424
66 X = 1410743
83
Y = 21312232
42 feet Y = 6495968
44 meter
Z = 4527626
92 Z = 1380020
69
XDOT = -14856
236523 XDOT = -4528
180892
YDOT = -838
468849 feet/sec YDOT = -255
565305 meter/sec
ZDOT = 19043
208972 ZDOT = 5804
370095
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 15006
21906765
00016717 00000-0 10270-3 0 9050
2 25544 51
6413 173
2386 0006611 217
4385 142
6307 15
53078607 2812
Satellite: ISS
Catalog Number: 25544
Epoch time: 15006
21906765 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 173
2386 deg
Eccentricity:
0006611
Arg of perigee: 217
4385 deg
Mean anomaly: 142
6307 deg
Mean motion: 15
53078607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 281
Checksum: 296
Coasting Arc #7 (Orbit 295)
---------------------------------------
Vector Time (GMT): 2015/007/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6179598
59 A = 6789472
73 meter
Y = 797927
90 meter E =
0007569
Z = -2685410
99 I = 51
72434
XDOT = -2881
648247 Wp = 181
88642
YDOT = 4842
619197 meter/sec RA = 167
47620 deg
ZDOT = -5199
232981 TA = 28
38951
MA = 28
34829
Ha = 222
522 n
mi
Hp = 217
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20274273
59 X = 6183261
26
Y = 2617873
69 feet Y = 867052
83 meter
Z = -8810403
50 Z = -2655383
11
XDOT = -9454
226532 XDOT = -2910
329761
YDOT = 15887
858258 feet/sec YDOT = 4810
234689 meter/sec
ZDOT = -17057
850989 ZDOT = -5213
300665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2880742
78 X = -878050
40
Y = -20293920
34 feet Y = -6185586
92 meter
Z = -8682209
41 Z = -2646337
43
XDOT = 16319
184480 XDOT = 4974
087430
YDOT = 4997
363181 feet/sec YDOT = 1523
196297 meter/sec
ZDOT = -17118
781275 ZDOT = -5217
804533
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 15007
18427270
00016717 00000-0 10270-3 0 9067
2 25544 51
6416 168
4338 0006275 222
4462 137
6205 15
53058601 2965
Satellite: ISS
Catalog Number: 25544
Epoch time: 15007
18427270 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 168
4338 deg
Eccentricity:
0006275
Arg of perigee: 222
4462 deg
Mean anomaly: 137
6205 deg
Mean motion: 15
53058601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 296
Checksum: 296
Coasting Arc #8 (Orbit 311)
---------------------------------------
Vector Time (GMT): 2015/008/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5475714
06 A = 6786381
71 meter
Y = -1383977
93 meter E =
0008841
Z = 3761403
30 I = 51
74543
XDOT = 4155
276342 Wp = 129
32588
YDOT = -4830
713177 meter/sec RA = 162
50912 deg
ZDOT = 4259
511740 TA = 275
57490
MA = 275
67573
Ha = 222
207 n
mi
Hp = 217
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17964941
15 X = -5478102
39
Y = -4540610
00 feet Y = -1445224
44 meter
Z = 12340562
02 Z = 3734797
82
XDOT = 13632
796398 XDOT = 4188
294831
YDOT = -15848
796514 feet/sec YDOT = -4784
061750 meter/sec
ZDOT = 13974
776049 ZDOT = 4279
776994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 739492
73 X = 225397
39
Y = 18590251
53 feet Y = 5666308
67 meter
Z = 12227077
31 Z = 3726813
16
XDOT = -17671
218728 XDOT = -5386
187468
YDOT = -8572
474658 feet/sec YDOT = -2612
890276 meter/sec
ZDOT = 14062
200085 ZDOT = 4286
158586
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 15008
21380196
00016717 00000-0 10270-3 0 9078
2 25544 51
6420 163
3101 0006456 227
4039 132
6569 15
53121106 3126
Satellite: ISS
Catalog Number: 25544
Epoch time: 15008
21380196 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 163
3101 deg
Eccentricity:
0006456
Arg of perigee: 227
4039 deg
Mean anomaly: 132
6569 deg
Mean motion: 15
53121106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 312
Checksum: 268
Coasting Arc #9 (Orbit 326)
---------------------------------------
Vector Time (GMT): 2015/009/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4533669
24 A = 6783393
68 meter
Y = 2056931
98 meter E =
0004603
Z = -4611262
85 I = 51
76560
XDOT = -5215
817450 Wp = 95
50426
YDOT = 4731
790813 meter/sec RA = 157
53581 deg
ZDOT = -3020
378948 TA = 144
39120
MA = 144
36048
Ha = 222
044 n
mi
Hp = 218
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14874242
93 X = 4532730
72
Y = 6748464
51 feet Y = 2107625
30 meter
Z = -15128815
12 Z = -4589241
65
XDOT = -17112
261975 XDOT = -5253
670101
YDOT = 15524
248074 feet/sec YDOT = 4673
252594 meter/sec
ZDOT = -9909
379750 ZDOT = -3045
807877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1965811
03 X = 599179
20
Y = -16301825
26 feet Y = -4968796
34 meter
Z = -15035025
87 Z = -4582675
89
XDOT = 18719
793027 XDOT = 5705
792915
YDOT = 11488
496978 feet/sec YDOT = 3501
693879 meter/sec
ZDOT = -10018
869644 ZDOT = -3053
751468
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 15009
17897057
00016717 00000-0 10270-3 0 9084
2 25544 51
6424 158
5053 0006201 231
5354 128
5242 15
53112615 3279
Satellite: ISS
Catalog Number: 25544
Epoch time: 15009
17897057 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 158
5053 deg
Eccentricity:
0006201
Arg of perigee: 231
5354 deg
Mean anomaly: 128
5242 deg
Mean motion: 15
53112615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 327
Checksum: 287
Coasting Arc #10 (Orbit 342)
---------------------------------------
Vector Time (GMT): 2015/010/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3448066
22 A = 6781034
44 meter
Y = -2771038
29 meter E =
0006400
Z = 5142037
86 I = 51
78744
XDOT = 5991
008094 Wp = 190
93593
YDOT = -4512
233461 meter/sec RA = 152
56016 deg
ZDOT = 1579
908958 TA = 243
82218
MA = 243
88801
Ha = 221
737 n
mi
Hp = 218
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11312553
23 X = -3441801
39
Y = -9091332
96 feet Y = -2809561
86 meter
Z = 16870202
96 Z = 5125303
17
XDOT = 19655
538367 XDOT = 6033
345156
YDOT = -14803
915553 feet/sec YDOT = -4445
001421 meter/sec
ZDOT = 5183
428339 ZDOT = 1609
114569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5027482
89 X = -1532376
78
Y = 13701963
09 feet Y = 4176358
35 meter
Z = 16799123
98 Z = 5120372
99
XDOT = -19234
297645 XDOT = -5862
613922
YDOT = -13589
937364 feet/sec YDOT = -4142
212908 meter/sec
ZDOT = 5309
039178 ZDOT = 1618
195142
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 15010
20846215
00016717 00000-0 10270-3 0 9091
2 25544 51
6429 153
3817 0006272 237
0319 123
0230 15
53162650 3434
Satellite: ISS
Catalog Number: 25544
Epoch time: 15010
20846215 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 153
3817 deg
Eccentricity:
0006272
Arg of perigee: 237
0319 deg
Mean anomaly: 123
0230 deg
Mean motion: 15
53162650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 343
Checksum: 269
Coasting Arc #11 (Orbit 357)
---------------------------------------
Vector Time (GMT): 2015/011/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2257382
11 A = 6780149
83 meter
Y = 3536713
23 meter E =
0009911
Z = -5334163
61 I = 51
81233
XDOT = -6462
013303 Wp = 107
32668
YDOT = 4113
459987 meter/sec RA = 147
58094 deg
ZDOT = -10
223414 TA = 162
59303
MA = 162
55903
Ha = 221
469 n
mi
Hp = 218
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7406109
27 X = 2243577
14
Y = 11603389
85 feet Y = 3561879
60 meter
Z = -17500536
78 Z = -5323231
27
XDOT = -21200
831047 XDOT = -6507
481046
YDOT = 13495
603631 feet/sec YDOT = 4040
943329 meter/sec
ZDOT = -33
541385 ZDOT = -41
724768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8454507
71 X = 2576933
95
Y = -10937253
63 feet Y = -3333674
91 meter
Z = -17454388
58 Z = -5320097
64
XDOT = 18962
055927 XDOT = 5779
634647
YDOT = 14912
068927 feet/sec YDOT = 4545
198609 meter/sec
ZDOT = -168
914704 ZDOT = -51
485202
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 15011
17359332
00016717 00000-0 10270-3 0 9109
2 25544 51
6431 148
5768 0006162 241
0455 119
0079 15
53168609 3584
Satellite: ISS
Catalog Number: 25544
Epoch time: 15011
17359332 = yrday
fracday
Element set: 910
Inclination: 51
6431 deg
RA of node: 148
5768 deg
Eccentricity:
0006162
Arg of perigee: 241
0455 deg
Mean anomaly: 119
0079 deg
Mean motion: 15
53168609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 358
Checksum: 297
Coasting Arc #12 (Orbit 373)
---------------------------------------
Vector Time (GMT): 2015/012/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1058692
83 A = 6780821
35 meter
Y = -4284058
80 meter E =
0001678
Z = 5149837
06 I = 51
84146
XDOT = 6628
133854 Wp = 276
89424
YDOT = -3518
912173 meter/sec RA = 142
60481 deg
ZDOT = -1564
963299 TA = 188
15261
MA = 188
15534
Ha = 221
253 n
mi
Hp = 218
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3473401
68 X = -1035724
64
Y = -14055311
01 feet Y = -4295769
40 meter
Z = 16895790
87 Z = 5144749
92
XDOT = 21745
845977 XDOT = 6674
592502
YDOT = -11544
987445 feet/sec YDOT = -3444
532297 meter/sec
ZDOT = -5134
394026 ZDOT = -1532
652466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11932616
17 X = -3637061
41
Y = 8242521
88 feet Y = 2512320
67 meter
Z = 16874760
45 Z = 5143426
99
XDOT = -17795
064271 XDOT = -5423
935590
YDOT = -15535
862359 feet/sec YDOT = -4735
330847 meter/sec
ZDOT = -4995
644406 ZDOT = -1522
672415
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 15012
20304679
00016717 00000-0 10270-3 0 9119
2 25544 51
6435 143
4528 0006109 245
5717 114
4798 15
53199488 3741
Satellite: ISS
Catalog Number: 25544
Epoch time: 15012
20304679 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 143
4528 deg
Eccentricity:
0006109
Arg of perigee: 245
5717 deg
Mean anomaly: 114
4798 deg
Mean motion: 15
53199488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 314
Coasting Arc #13 (Orbit 388)
---------------------------------------
Vector Time (GMT): 2015/013/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -97564
31 A = 6782956
14 meter
Y = 4982990
85 meter E =
0006750
Z = -4607045
66 I = 51
87329
XDOT = -6495
212527 Wp = 145
81507
YDOT = 2690
413715 meter/sec RA = 137
63217 deg
ZDOT = 3044
230912 TA = 154
54152
MA = 154
50825
Ha = 220
902 n
mi
Hp = 218
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -320092
88 X = -130898
80
Y = 16348395
16 feet Y = 4981713
47 meter
Z = -15114979
19 Z = -4607600
53
XDOT = -21309
752385 XDOT = -6539
602313
YDOT = 8826
816649 feet/sec YDOT = 2617
531803 meter/sec
ZDOT = 9987
634225 ZDOT = 3012
570732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15309062
04 X = 4666202
11
Y = -5736534
63 feet Y = -1748495
76 meter
Z = -15118196
64 Z = -4608026
34
XDOT = 15578
253718 XDOT = 4748
251733
YDOT = 15581
641805 feet/sec YDOT = 4749
284422 meter/sec
ZDOT = 9851
791536 ZDOT = 3002
826060
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 15013
16814007
00016717 00000-0 10270-3 0 9127
2 25544 51
6434 138
6479 0006119 250
1910 109
8583 15
53230862 3897
Satellite: ISS
Catalog Number: 25544
Epoch time: 15013
16814007 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 138
6479 deg
Eccentricity:
0006119
Arg of perigee: 250
1910 deg
Mean anomaly: 109
8583 deg
Mean motion: 15
53230862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 389
Checksum: 298
Coasting Arc #14 (Orbit 404)
---------------------------------------
Vector Time (GMT): 2015/014/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1145848
36 A = 6785920
15 meter
Y = -5551600
05 meter E =
0005753
Z = 3724995
09 I = 51
90679
XDOT = 6118
111976 Wp = 94
59171
YDOT = -1639
945610 meter/sec RA = 132
66799 deg
ZDOT = -4320
829612 TA = 41
15818
MA = 41
11481
Ha = 220
644 n
mi
Hp = 218
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3759345
01 X = 1189747
89
Y = -18213910
92 feet Y = -5538541
03 meter
Z = 12221112
50 Z = 3730667
93
XDOT = 20072
545853 XDOT = 6156
984461
YDOT = -5380
398984 feet/sec YDOT = -1571
311488 meter/sec
ZDOT = -14175
950171 ZDOT = -4291
014664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18246930
35 X = -5561664
37
Y = 3508839
12 feet Y = 1069494
16 meter
Z = 12246321
79 Z = 3732678
88
XDOT = -12377
904128 XDOT = -3772
785178
YDOT = -15278
153466 feet/sec YDOT = -4656
781177 meter/sec
ZDOT = -14048
162685 ZDOT = -4281
879986
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 15014
19755369
00016717 00000-0 10270-3 0 9137
2 25544 51
6440 133
5232 0006078 254
7070 105
3411 15
53270668 4054
Satellite: ISS
Catalog Number: 25544
Epoch time: 15014
19755369 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 133
5232 deg
Eccentricity:
0006078
Arg of perigee: 254
7070 deg
Mean anomaly: 105
3411 deg
Mean motion: 15
53270668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 405
Checksum: 285
Coasting Arc #15 (Orbit 419)
---------------------------------------
Vector Time (GMT): 2015/015/00:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2044221
57 A = 6788944
79 meter
Y = 5938268
01 meter E =
0002805
Z = -2573502
35 I = 51
93749
XDOT = -5534
166570 Wp = 316
31912
YDOT = 387
416824 meter/sec RA = 127
71147 deg
ZDOT = 5288
473209 TA = 14
89150
MA = 14
88324
Ha = 220
374 n
mi
Hp = 218
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6706763
67 X = -2097971
64
Y = 19482506
59 feet Y = 5915107
73 meter
Z = -8443249
18 Z = -2583563
15
XDOT = -18156
714469 XDOT = -5563
776839
YDOT = 1271
052571 feet/sec YDOT = 325
364464 meter/sec
ZDOT = 17350
633887 ZDOT = 5261
517419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20524579
50 X = 6255891
83
Y = -1595152
34 feet Y = -486202
43 meter
Z = -8487303
68 Z = -2586930
16
XDOT = 8277
495452 XDOT = 2522
980614
YDOT = 14776
475106 feet/sec YDOT = 4503
869612 meter/sec
ZDOT = 17235
276663 ZDOT = 5253
312327
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 15015
16261041
00016717 00000-0 10270-3 0 9145
2 25544 51
6437 128
7181 0006085 259
2987 100
7480 15
53285449 4209
Satellite: ISS
Catalog Number: 25544
Epoch time: 15015
16261041 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 128
7181 deg
Eccentricity:
0006085
Arg of perigee: 259
2987 deg
Mean anomaly: 100
7480 deg
Mean motion: 15
53285449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 420
Checksum: 298
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