[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 3rd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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 225)
---------------------------------------
Vector Time (GMT): 2015/002/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3245932
06 A = 6784882
11 meter
Y = 4071070
19 meter E =
0006090
Z = -4352850
64 I = 51
56587
XDOT = -6648
349793 Wp = 121
42249
YDOT = 1620
733601 meter/sec RA = 189
87247 deg
ZDOT = -3448
547584 TA = 113
54369
MA = 113
47970
Ha = 223
427 n
mi
Hp = 217
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10649383
40 X = 3221311
72
Y = 13356529
50 feet Y = 4107231
04 meter
Z = -14281006
02 Z = -4337141
93
XDOT = -21812
171237 XDOT = -6649
227310
YDOT = 5317
367458 feet/sec YDOT = 1546
382840 meter/sec
ZDOT = -11314
132492 ZDOT = -3480
846033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11066305
79 X = -3373010
00
Y = 13085689
85 feet Y = 3988518
26 meter
Z = -14214604
38 Z = -4332611
41
XDOT = -8403
851850 XDOT = -2561
494044
YDOT = -19523
429265 feet/sec YDOT = -5950
741240 meter/sec
ZDOT = -11452
344127 ZDOT = -3490
674490
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
52246161
00016717 00000-0 10270-3 0 9002
2 25544 51
6406 190
8516 0006769 204
9577 155
1248 15
52925311 2266
Satellite: ISS
Catalog Number: 25544
Epoch time: 15002
52246161 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 190
8516 deg
Eccentricity:
0006769
Arg of perigee: 204
9577 deg
Mean anomaly: 155
1248 deg
Mean motion: 15
52925311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 226
Checksum: 292
Coasting Arc #2 (Orbit 241)
---------------------------------------
Vector Time (GMT): 2015/003/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2083501
86 A = 6782511
34 meter
Y = -4127924
36 meter E =
0009542
Z = 4963350
99 I = 51
58862
XDOT = 7278
757456 Wp = 167
68821
YDOT = -1084
086581 meter/sec RA = 184
88496 deg
ZDOT = 2143
958818 TA = 261
34375
MA = 261
45186
Ha = 223
311 n
mi
Hp = 217
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6835636
03 X = -2061297
65
Y = -13543058
92 feet Y = -4151099
74 meter
Z = 16283959
95 Z = 4953283
30
XDOT = 23880
437848 XDOT = 7279
924463
YDOT = -3556
714503 feet/sec YDOT = -1002
684466 meter/sec
ZDOT = 7033
985622 ZDOT = 2179
320286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11809605
10 X = 3599567
63
Y = -9594252
43 feet Y = -2924328
14 meter
Z = 16241652
14 Z = 4950455
57
XDOT = 7718
969584 XDOT = 2352
741929
YDOT = 21719
850904 feet/sec YDOT = 6620
210556 meter/sec
ZDOT = 7185
211312 ZDOT = 2190
052408
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
55209224
00016717 00000-0 10270-3 0 9016
2 25544 51
6403 185
7269 0006743 209
3530 150
7244 15
52905245 2420
Satellite: ISS
Catalog Number: 25544
Epoch time: 15003
55209224 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 185
7269 deg
Eccentricity:
0006743
Arg of perigee: 209
3530 deg
Mean anomaly: 150
7244 deg
Mean motion: 15
52905245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 242
Checksum: 280
Coasting Arc #3 (Orbit 256)
---------------------------------------
Vector Time (GMT): 2015/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 776363
45 A = 6780945
90 meter
Y = 4186380
05 meter E =
0011827
Z = -5286606
88 I = 51
61547
XDOT = -7608
252360 Wp = 112
11056
YDOT = 555
137356 meter/sec RA = 179
89550 deg
ZDOT = -683
279562 TA = 151
38685
MA = 151
32189
Ha = 223
108 n
mi
Hp = 217
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2547124
17 X = 755172
88
Y = 13734842
69 feet Y = 4194943
86 meter
Z = -17344510
77 Z = -5282886
56
XDOT = -24961
457874 XDOT = -7610
575477
YDOT = 1821
316784 feet/sec YDOT = 470
044012 meter/sec
ZDOT = -2241
730845 ZDOT = -720
244368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12788912
69 X = -3898060
59
Y = 5666050
30 feet Y = 1727012
13 meter
Z = -17329321
54 Z = -5281977
21
XDOT = -6950
722291 XDOT = -2118
580154
YDOT = -22972
044830 feet/sec YDOT = -7001
879264 meter/sec
ZDOT = -2399
740374 ZDOT = -731
440866
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
51735860
00016717 00000-0 10270-3 0 9024
2 25544 51
6404 180
9229 0006787 211
3885 148
6862 15
52955899 2576
Satellite: ISS
Catalog Number: 25544
Epoch time: 15004
51735860 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 180
9229 deg
Eccentricity:
0006787
Arg of perigee: 211
3885 deg
Mean anomaly: 148
6862 deg
Mean motion: 15
52955899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 257
Checksum: 334
Coasting Arc #4 (Orbit 272)
---------------------------------------
Vector Time (GMT): 2015/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 539378
66 A = 6781050
51 meter
Y = -4234194
96 meter E =
0004172
Z = 5269568
38 I = 51
64691
XDOT = 7623
288638 Wp = 195
31293
YDOT = -34
409922 meter/sec RA = 174
90656 deg
ZDOT = -812
028065 TA = 262
42582
MA = 262
47320
Ha = 223
033 n
mi
Hp = 217
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1769615
02 X = 561088
97
Y = -13891715
76 feet Y = -4228042
34 meter
Z = 17288610
16 Z = 5272240
93
XDOT = 25010
789494 XDOT = 7627
051333
YDOT = -112
893446 feet/sec YDOT = 50
859748 meter/sec
ZDOT = -2664
134071 ZDOT = -774
986795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13881230
29 X = 4230998
99
Y = -1732969
32 feet Y = -528209
05 meter
Z = 17300740
12 Z = 5273265
59
XDOT = 6009
252971 XDOT = 1831
620306
YDOT = 23251
415170 feet/sec YDOT = 7087
031344 meter/sec
ZDOT = -2505
861480 ZDOT = -763
786579
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
54696634
00016717 00000-0 10270-3 0 9034
2 25544 51
6402 175
7983 0006737 215
0833 144
9876 15
52923364 2736
Satellite: ISS
Catalog Number: 25544
Epoch time: 15005
54696634 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 175
7983 deg
Eccentricity:
0006737
Arg of perigee: 215
0833 deg
Mean anomaly: 144
9876 deg
Mean motion: 15
52923364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 273
Checksum: 324
Coasting Arc #5 (Orbit 287)
---------------------------------------
Vector Time (GMT): 2015/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1850285
03 A = 6782332
32 meter
Y = 4285602
66 meter E =
0011570
Z = -4929987
78 I = 51
68425
XDOT = -7294
107220 Wp = 139
45978
YDOT = -527
882887 meter/sec RA = 169
92138 deg
ZDOT = 2273
099836 TA = 152
79886
MA = 152
73821
Ha = 222
774 n
mi
Hp = 217
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6070488
94 X = -1874122
36
Y = 14060376
17 feet Y = 4264778
63 meter
Z = -16174500
61 Z = -4939033
61
XDOT = -23930
797965 XDOT = -7298
703939
YDOT = -1731
899236 feet/sec YDOT = -609
476193 meter/sec
ZDOT = 7457
676626 ZDOT = 2237
655674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15121412
49 X = -4609006
53
Y = -2147707
10 feet Y = -654621
13 meter
Z = -16213874
37 Z = -4941988
91
XDOT = -4656
294312 XDOT = -1419
238506
YDOT = -22512
374191 feet/sec YDOT = -6861
771654 meter/sec
ZDOT = 7306
300498 ZDOT = 2226
960392
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
51221036
00016717 00000-0 10270-3 0 9043
2 25544 51
6413 170
9942 0006755 218
4845 141
5826 15
52985754 2885
Satellite: ISS
Catalog Number: 25544
Epoch time: 15006
51221036 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 170
9942 deg
Eccentricity:
0006755
Arg of perigee: 218
4845 deg
Mean anomaly: 141
5826 deg
Mean motion: 15
52985754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 288
Checksum: 312
Coasting Arc #6 (Orbit 303)
---------------------------------------
Vector Time (GMT): 2015/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3037734
95 A = 6784871
75 meter
Y = -4305434
28 meter E =
0005282
Z = 4268787
12 I = 51
72330
XDOT = 6675
919008 Wp = 113
51542
YDOT = 1142
917774 meter/sec RA = 164
94286 deg
ZDOT = -3596
491490 TA = 13
17606
MA = 13
16227
Ha = 222
596 n
mi
Hp = 217
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9966322
01 X = 3064917
65
Y = -14125440
55 feet Y = -4271312
59 meter
Z = 14005207
08 Z = 4283609
45
XDOT = 21902
621418 XDOT = 6680
112655
YDOT = 3749
730231 feet/sec YDOT = 1217
595876 meter/sec
ZDOT = -11799
512763 ZDOT = -3564
051330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16290138
81 X = 4965234
31
Y = 5629237
67 feet Y = 1715791
64 meter
Z = 14069276
14 Z = 4288315
37
XDOT = 2827
288418 XDOT = 861
757510
YDOT = 20974
970035 feet/sec YDOT = 6393
170867 meter/sec
ZDOT = -11661
058029 ZDOT = -3554
290487
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
54179375
00016717 00000-0 10270-3 0 9056
2 25544 51
6411 165
8699 0006745 222
5926 137
4704 15
52980717 3042
Satellite: ISS
Catalog Number: 25544
Epoch time: 15007
54179375 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 165
8699 deg
Eccentricity:
0006745
Arg of perigee: 222
5926 deg
Mean anomaly: 137
4704 deg
Mean motion: 15
52980717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 304
Checksum: 322
Coasting Arc #7 (Orbit 318)
---------------------------------------
Vector Time (GMT): 2015/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4074838
49 A = 6787752
22 meter
Y = 4284667
46 meter E =
0004456
Z = -3338042
78 I = 51
76519
XDOT = -5772
147448 Wp = 180
86017
YDOT = -1830
711518 meter/sec RA = 159
97265 deg
ZDOT = 4691
910273 TA = 140
39407
MA = 140
36151
Ha = 222
416 n
mi
Hp = 217
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13368892
67 X = -4106233
03
Y = 14057307
94 feet Y = 4238924
55 meter
Z = -10951583
93 Z = -3357913
41
XDOT = -18937
491626 XDOT = -5774
038263
YDOT = -6006
271385 feet/sec YDOT = -1895
270163 meter/sec
ZDOT = 15393
406408 ZDOT = 4663
865991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17313730
77 X = -5277225
14
Y = -8642138
84 feet Y = -2634123
92 meter
Z = -11037234
79 Z = -3364149
16
XDOT = -414
167550 XDOT = -126
238269
YDOT = -18695
519007 feet/sec YDOT = -5698
394193 meter/sec
ZDOT = 15273
839440 ZDOT = 4655
466261
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
50701633
00016717 00000-0 10270-3 0 9062
2 25544 51
6428 161
0661 0006682 225
9355 134
1248 15
53024470 3199
Satellite: ISS
Catalog Number: 25544
Epoch time: 15008
50701633 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 161
0661 deg
Eccentricity:
0006682
Arg of perigee: 225
9355 deg
Mean anomaly: 134
1248 deg
Mean motion: 15
53024470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 319
Checksum: 285
Coasting Arc #8 (Orbit 334)
---------------------------------------
Vector Time (GMT): 2015/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4886792
83 A = 6790461
49 meter
Y = -4168870
84 meter E =
0011844
Z = 2178571
57 I = 51
80299
XDOT = 4672
049949 Wp = 138
10459
YDOT = 2597
583652 meter/sec RA = 155
01065 deg
ZDOT = -5500
651294 TA = 17
77240
MA = 17
73101
Ha = 222
192 n
mi
Hp = 218
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16032784
88 X = 4922464
36
Y = -13677397
78 feet Y = -4114024
15 meter
Z = 7147544
52 Z = 2202396
94
XDOT = 15328
247865 XDOT = 4669
375727
YDOT = 8522
256076 feet/sec YDOT = 2649
814721 meter/sec
ZDOT = -18046
756214 ZDOT = -5477
962074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17923593
43 X = 5463111
28
Y = 11017702
43 feet Y = 3358195
70 meter
Z = 7250091
41 Z = 2209827
86
XDOT = -2566
198566 XDOT = -782
177323
YDOT = 16004
996297 feet/sec YDOT = 4878
322871 meter/sec
ZDOT = -17950
196601 ZDOT = -5471
219924
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
53657550
00016717 00000-0 10270-3 0 9075
2 25544 51
6423 155
9419 0006701 230
3818 129
6743 15
53028609 3358
Satellite: ISS
Catalog Number: 25544
Epoch time: 15009
53657550 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 155
9419 deg
Eccentricity:
0006701
Arg of perigee: 230
3818 deg
Mean anomaly: 129
6743 deg
Mean motion: 15
53028609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 335
Checksum: 307
Coasting Arc #9 (Orbit 349)
---------------------------------------
Vector Time (GMT): 2015/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5456829
89 A = 6792079
54 meter
Y = 3942703
10 meter E =
0003982
Z = -881323
39 I = 51
83839
XDOT = -3426
444775 Wp = 13
90473
YDOT = -3415
930866 meter/sec RA = 150
05571 deg
ZDOT = 5943
054840 TA = 336
59284
MA = 336
61097
Ha = 222
001 n
mi
Hp = 218
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17902985
21 X = -5496231
46
Y = 12935377
62 feet Y = 3881460
98 meter
Z = -2891480
92 Z = -907927
01
XDOT = -11241
616716 XDOT = -3416
861244
YDOT = -11207
122265 feet/sec YDOT = -3454
194088 meter/sec
ZDOT = 19498
211416 ZDOT = 5926
433223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18021899
62 X = -5493075
00
Y = -12742737
56 feet Y = -3883986
41 meter
Z = -3005879
11 Z = -916191
95
XDOT = 6000
755445 XDOT = 1829
030260
YDOT = -13062
642507 feet/sec YDOT = -3981
493436 meter/sec
ZDOT = 19427
720765 ZDOT = 5921
569289
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
50177570
00016717 00000-0 10270-3 0 9084
2 25544 51
6439 151
1383 0006601 234
1158 125
9382 15
53059131 3500
Satellite: ISS
Catalog Number: 25544
Epoch time: 15010
50177570 = yrday
fracday
Element set: 908
Inclination: 51
6439 deg
RA of node: 151
1383 deg
Eccentricity:
0006601
Arg of perigee: 234
1158 deg
Mean anomaly: 125
9382 deg
Mean motion: 15
53059131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 350
Checksum: 278
Coasting Arc #10 (Orbit 365)
---------------------------------------
Vector Time (GMT): 2015/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5761999
02 A = 6792266
35 meter
Y = -3547642
16 meter E =
0011833
Z = -492389
32 I = 51
86550
XDOT = 2119
176819 Wp = 171
61886
YDOT = 4271
535825 meter/sec RA = 145
10456 deg
ZDOT = -6006
885134 TA = 13
67534
MA = 13
64331
Ha = 221
782 n
mi
Hp = 218
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18904196
24 X = 5803633
16
Y = -11639245
95 feet Y = -3482974
95 meter
Z = -1615450
51 Z = -464297
73
XDOT = 6952
679854 XDOT = 2100
433004
YDOT = 14014
225148 feet/sec YDOT = 4295
129078 meter/sec
ZDOT = -19707
628392 ZDOT = -5996
636149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17369232
61 X = 5294142
10
Y = 13839286
89 feet Y = 4218214
64 meter
Z = -1494743
85 Z = -455597
93
XDOT = -9768
405956 XDOT = -2977
410135
YDOT = 10147
401300 feet/sec YDOT = 3092
927916 meter/sec
ZDOT = -19664
524436 ZDOT = -5993
747048
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
53131022
00016717 00000-0 10270-3 0 9091
2 25544 51
6433 146
0141 0006574 238
9098 121
1410 15
53089183 3660
Satellite: ISS
Catalog Number: 25544
Epoch time: 15011
53131022 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 146
0141 deg
Eccentricity:
0006574
Arg of perigee: 238
9098 deg
Mean anomaly: 121
1410 deg
Mean motion: 15
53089183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 366
Checksum: 275
Coasting Arc #11 (Orbit 381)
---------------------------------------
Vector Time (GMT): 2015/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5815209
77 A = 6790913
58 meter
Y = 2985930
88 meter E =
0007410
Z = 1827339
13 I = 51
88771
XDOT = -830
939403 Wp = 68
97139
YDOT = -5095
343154 meter/sec RA = 140
15402 deg
ZDOT = 5665
718772 TA = 311
03749
MA = 311
10152
Ha = 221
536 n
mi
Hp = 218
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19078772
22 X = -5857043
44
Y = 9796361
17 feet Y = 2920667
51 meter
Z = 5995207
12 Z = 1798988
50
XDOT = -2726
179144 XDOT = -801
422147
YDOT = -16717
005100 feet/sec YDOT = -5104
470256 meter/sec
ZDOT = 18588
316180 ZDOT = 5661
753907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15954609
93 X = -4862965
11
Y = -14382749
28 feet Y = -4383861
98 meter
Z = 5873473
83 Z = 1790234
82
XDOT = 13562
552070 XDOT = 4133
865871
YDOT = -7438
696038 feet/sec YDOT = -2267
314553 meter/sec
ZDOT = 18572
222815 ZDOT = 5660
813514
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
56083172
00016717 00000-0 10270-3 0 9109
2 25544 51
6445 140
8900 0006555 242
2026 117
8462 15
53117498 3824
Satellite: ISS
Catalog Number: 25544
Epoch time: 15012
56083172 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 140
8900 deg
Eccentricity:
0006555
Arg of perigee: 242
2026 deg
Mean anomaly: 117
8462 deg
Mean motion: 15
53117498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 382
Checksum: 287
Coasting Arc #12 (Orbit 396)
---------------------------------------
Vector Time (GMT): 2015/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5636402
30 A = 6788414
36 meter
Y = -2216764
92 meter E =
0004450
Z = -3059302
61 I = 51
90271
XDOT = -384
254238 Wp = 203
29550
YDOT = 5845
359881 meter/sec RA = 135
20087 deg
ZDOT = -4945
007936 TA = 11
65808
MA = 11
64778
Ha = 221
448 n
mi
Hp = 218
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18492133
52 X = 5675632
69
Y = -7272850
79 feet Y = -2153515
62 meter
Z = -10037082
06 Z = -3031826
86
XDOT = -1260
676635 XDOT = -425
568921
YDOT = 19177
689898 feet/sec YDOT = 5840
831953 meter/sec
ZDOT = -16223
779319 ZDOT = -4946
974848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13648719
13 X = 4160129
59
Y = 14523022
41 feet Y = 4426617
23 meter
Z = -9919206
78 Z = -3023374
23
XDOT = -17174
048228 XDOT = -5234
649900
YDOT = 5056
369392 feet/sec YDOT = 1541
181391 meter/sec
ZDOT = -16233
185262 ZDOT = -4947
874868
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
52599802
00016717 00000-0 10270-3 0 9119
2 25544 51
6444 136
0863 0006539 246
6800 113
3664 15
53111441 3971
Satellite: ISS
Catalog Number: 25544
Epoch time: 15013
52599802 = yrday
fracday
Element set: 911
Inclination: 51
6444 deg
RA of node: 136
0863 deg
Eccentricity:
0006539
Arg of perigee: 246
6800 deg
Mean anomaly: 113
3664 deg
Mean motion: 15
53111441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 397
Checksum: 294
Coasting Arc #13 (Orbit 412)
---------------------------------------
Vector Time (GMT): 2015/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5269076
69 A = 6785201
11 meter
Y = 1277313
26 meter E =
0006167
Z = 4079215
32 I = 51
91491
XDOT = 1456
827841 Wp = 135
53903
YDOT = -6441
262566 meter/sec RA = 130
24252 deg
ZDOT = 3890
862708 TA = 274
26552
MA = 274
33599
Ha = 221
034 n
mi
Hp = 218
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17286997
02 X = -5302783
58
Y = 4190660
31 feet Y = 1218202
47 meter
Z = 13383252
36 Z = 4053537
35
XDOT = 4779
618902 XDOT = 1509
846943
YDOT = -21132
751201 feet/sec YDOT = -6424
675008 meter/sec
ZDOT = 12765
297597 ZDOT = 3898
068325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10596651
73 X = -3229859
45
Y = -14389097
47 feet Y = -4385796
91 meter
Z = 13273213
23 Z = 4045675
39
XDOT = 20251
818382 XDOT = 6172
754243
YDOT = -3085
460495 feet/sec YDOT = -940
448359 meter/sec
ZDOT = 12797
220341 ZDOT = 3900
592760
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
55549413
00016717 00000-0 10270-3 0 9127
2 25544 51
6451 130
9618 0006521 250
9826 109
0620 15
53165406 4130
Satellite: ISS
Catalog Number: 25544
Epoch time: 15014
55549413 = yrday
fracday
Element set: 912
Inclination: 51
6451 deg
RA of node: 130
9618 deg
Eccentricity:
0006521
Arg of perigee: 250
9826 deg
Mean anomaly: 109
0620 deg
Mean motion: 15
53165406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 413
Checksum: 281
Coasting Arc #14 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2015/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4757318
97 A = 6782425
76 meter
Y = -164658
33 meter E =
0004933
Z = -4836058
44 I = 51
92520
XDOT = -2368
038191 Wp = 67
14559
YDOT = 6822
054151 meter/sec RA = 125
27928 deg
ZDOT = -2561
970973 TA = 177
72133
MA = 177
71908
Ha = 220
893 n
mi
Hp = 218
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15608001
88 X = 4782298
38
Y = -540217
63 feet Y = -111319
06 meter
Z = -15866333
46 Z = -4812887
67
XDOT = -7769
154171 XDOT = -2431
702925
YDOT = 22382
067424 feet/sec YDOT = 6795
217332 meter/sec
ZDOT = -8405
416579 ZDOT = -2573
628815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6831613
43 X = 2082275
77
Y = 14155091
23 feet Y = 4314471
81 meter
Z = -15767198
40 Z = -4805842
07
XDOT = -22559
858313 XDOT = -6876
244814
YDOT = 1469
188352 feet/sec YDOT = 447
808610 meter/sec
ZDOT = -8456
462247 ZDOT = -2577
529693
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
52063763
00016717 00000-0 10270-3 0 9135
2 25544 51
6453 126
1582 0006523 255
5568 104
4860 15
53141048 4282
Satellite: ISS
Catalog Number: 25544
Epoch time: 15015
52063763 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 126
1582 deg
Eccentricity:
0006523
Arg of perigee: 255
5568 deg
Mean anomaly: 104
4860 deg
Mean motion: 15
53141048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 428
Checksum: 291
Coasting Arc #15 (Orbit 443)
---------------------------------------
Vector Time (GMT): 2015/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4155278
66 A = 6780427
62 meter
Y = -1049380
35 meter E =
0004516
Z = 5257448
50 I = 51
93720
XDOT = 3092
877823 Wp = 225
11067
YDOT = -6932
357015 meter/sec RA = 120
31121 deg
ZDOT = 1058
250120 TA = 214
77453
MA = 214
80405
Ha = 220
540 n
mi
Hp = 218
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13632804
01 X = -4168774
05
Y = -3442848
92 feet Y = -1095923
11 meter
Z = 17248846
79 Z = 5237230
19
XDOT = 10147
236952 XDOT = 3165
026630
YDOT = -22743
953460 feet/sec YDOT = -6897
367092 meter/sec
ZDOT = 3471
949214 ZDOT = 1073
449555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2633708
95 X = -802754
49
Y = -13919049
86 feet Y = -4242526
40 meter
Z = 17162543
44 Z = 5231143
24
XDOT = 23878
296093 XDOT = 7278
104649
YDOT = -145
133574 feet/sec YDOT = -44
236713 meter/sec
ZDOT = 3538
180925 ZDOT = 1078
437546
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 15016
55010951
00016717 00000-0 10270-3 0 9141
2 25544 51
6458 121
0335 0006450 259
9769 100
0656 15
53204220 4442
Satellite: ISS
Catalog Number: 25544
Epoch time: 15016
55010951 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 121
0335 deg
Eccentricity:
0006450
Arg of perigee: 259
9769 deg
Mean anomaly: 100
0656 deg
Mean motion: 15
53204220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 444
Checksum: 277
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