[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 12th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16684 06 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 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 1563)
---------------------------------------
Vector Time (GMT): 2015/345/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3890752
37 A = 6780416
80 meter
Y = -3698474
38 meter E =
0003505
Z = 4142472
60 I = 51
27587
XDOT = 2091
786466 Wp = 146
35836
YDOT = 6370
319127 meter/sec RA = 278
22518 deg
ZDOT = 3718
475479 TA = 265
18456
MA = 265
22458
Ha = 217
663 n
mi
Hp = 217
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12764935
58 X = 3911697
70
Y = -12134102
30 feet Y = -3654848
71 meter
Z = 13590789
38 Z = 4161423
79
XDOT = 6862
816491 XDOT = 2002
333427
YDOT = 20899
997136 feet/sec YDOT = 6393
210338 meter/sec
ZDOT = 12199
722700 ZDOT = 3728
420404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12518413
67 X = 3815612
49
Y = 12297039
54 feet Y = 3748137
65 meter
Z = 13673394
33 Z = 4167650
59
XDOT = -19785
025126 XDOT = -6030
475658
YDOT = 6513
750802 feet/sec YDOT = 1985
391245 meter/sec
ZDOT = 12241
426139 ZDOT = 3731
186687
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 15345
59032597
00016717 00000-0 10270-3 0 9005
2 25544 51
6429 278
7244 0008049 267
9201 92
1030 15
54659985 15649
Satellite: ISS
Catalog Number: 25544
Epoch time: 15345
59032597 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 278
7244 deg
Eccentricity:
0008049
Arg of perigee: 267
9201 deg
Mean anomaly: 92
1030 deg
Mean motion: 15
54659985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 328
Coasting Arc #2 (Orbit 1578)
---------------------------------------
Vector Time (GMT): 2015/346/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4148250
71 A = 6776798
73 meter
Y = 1851981
25 meter E =
0005840
Z = -5033716
52 I = 51
26109
XDOT = -1061
456055 Wp = 54
46628
YDOT = -7366
414233 meter/sec RA = 273
20054 deg
ZDOT = -1833
647342 TA = 197
66355
MA = 197
68386
Ha = 217
340 n
mi
Hp = 216
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13609746
43 X = -4144199
71
Y = 6076053
96 feet Y = 1805615
92 meter
Z = -16514817
96 Z = -5053857
97
XDOT = -3482
467371 XDOT = -970
096909
YDOT = -24168
025700 feet/sec YDOT = -7377
773132 meter/sec
ZDOT = -6015
903352 ZDOT = -1838
582547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6716462
06 X = -2047177
64
Y = -13196167
87 feet Y = -4022191
97 meter
Z = -16602202
66 Z = -5060351
37
XDOT = 23012
873309 XDOT = 7014
323785
YDOT = -4111
699069 feet/sec YDOT = -1253
245876 meter/sec
ZDOT = -6035
779695 ZDOT = -1839
705651
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 15346
55451882
00016717 00000-0 10270-3 0 9015
2 25544 51
6435 273
9138 0007998 271
9945 88
0292 15
54703313 15792
Satellite: ISS
Catalog Number: 25544
Epoch time: 15346
55451882 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 273
9138 deg
Eccentricity:
0007998
Arg of perigee: 271
9945 deg
Mean anomaly: 88
0292 deg
Mean motion: 15
54703313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1579
Checksum: 341
Coasting Arc #3 (Orbit 1594)
---------------------------------------
Vector Time (GMT): 2015/347/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4246217
42 A = 6775574
14 meter
Y = 198856
38 meter E =
0005849
Z = 5281221
54 I = 51
25618
XDOT = 8
655024 Wp = 283
42259
YDOT = 7659
944599 meter/sec RA = 268
16847 deg
ZDOT = -294
323574 TA = 169
40527
MA = 169
39294
Ha = 218
026 n
mi
Hp = 217
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13931159
53 X = 4218023
98
Y = 652415
94 feet Y = 246182
24 meter
Z = 17326842
32 Z = 5301780
38
XDOT = 28
395749 XDOT = -75
571283
YDOT = 25131
051833 feet/sec YDOT = 7659
570476 meter/sec
ZDOT = -965
628524 ZDOT = -294
485370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 248872
99 X = 75856
49
Y = 13833150
25 feet Y = 4216344
20 meter
Z = 17415634
75 Z = 5308285
47
XDOT = -24066
442996 XDOT = -7335
451825
YDOT = 1655
792747 feet/sec YDOT = 504
685629 meter/sec
ZDOT = -967
817200 ZDOT = -294
990683
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 15347
58297109
00016717 00000-0 10270-3 0 9020
2 25544 51
6431 268
7827 0008189 275
5297 84
4922 15
54748776 15958
Satellite: ISS
Catalog Number: 25544
Epoch time: 15347
58297109 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 268
7827 deg
Eccentricity:
0008189
Arg of perigee: 275
5297 deg
Mean anomaly: 84
4922 deg
Mean motion: 15
54748776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 362
Coasting Arc #4 (Orbit 1609)
---------------------------------------
Vector Time (GMT): 2015/348/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4184296
66 A = 6777459
08 meter
Y = -2229608
86 meter E =
0004029
Z = -4846744
77 I = 51
26475
XDOT = 1066
234623 Wp = 123
38249
YDOT = -7204
375959 meter/sec RA = 263
13673 deg
ZDOT = 2392
933284 TA = 170
21041
MA = 170
20256
Ha = 218
058 n
mi
Hp = 216
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13728007
41 X = -4135510
05
Y = -7314989
71 feet Y = -2276127
23 meter
Z = -15901393
59 Z = -4866952
90
XDOT = 3498
145089 XDOT = 1135
092543
YDOT = -23636
404064 feet/sec YDOT = -7192
067819 meter/sec
ZDOT = 7850
830985 ZDOT = 2398
279452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6168986
35 X = 1880307
04
Y = -14182378
53 feet Y = -4322788
98 meter
Z = -15988287
16 Z = -4873229
93
XDOT = 22805
168099 XDOT = 6951
015237
YDOT = 1038
865294 feet/sec YDOT = 316
646142 meter/sec
ZDOT = 7875
318441 ZDOT = 2400
397061
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 15348
54712973
00016717 00000-0 10270-3 0 9039
2 25544 51
6434 263
9717 0008098 279
4059 80
6178 15
54746168 16106
Satellite: ISS
Catalog Number: 25544
Epoch time: 15348
54712973 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 263
9717 deg
Eccentricity:
0008098
Arg of perigee: 279
4059 deg
Mean anomaly: 80
6178 deg
Mean motion: 15
54746168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1610
Checksum: 339
Coasting Arc #5 (Orbit 1625)
---------------------------------------
Vector Time (GMT): 2015/349/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3938723
42 A = 6781354
43 meter
Y = 4029623
02 meter E =
0004814
Z = 3772651
76 I = 51
28207
XDOT = -2162
165899 Wp = 47
67783
YDOT = 6044
318171 meter/sec RA = 258
11508 deg
ZDOT = -4192
054040 TA = 86
83901
MA = 86
78393
Ha = 218
475 n
mi
Hp = 216
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12922320
93 X = 3875044
43
Y = 13220547
95 feet Y = 4073312
10 meter
Z = 12377466
42 Z = 3791630
83
XDOT = -7093
720141 XDOT = -2209
230939
YDOT = 19830
440194 feet/sec YDOT = 6019
876553 meter/sec
ZDOT = -13753
458138 ZDOT = -4202
671240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11877958
07 X = -3620401
62
Y = 14094871
39 feet Y = 4296116
80 meter
Z = 12458717
99 Z = 3797417
24
XDOT = -19400
069421 XDOT = -5913
141159
YDOT = -4131
135071 feet/sec YDOT = -1259
169970 meter/sec
ZDOT = -13800
489169 ZDOT = -4206
389099
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 15349
57554648
00016717 00000-0 10270-3 0 9047
2 25544 51
6428 258
8402 0008055 283
2361 76
7893 15
54767847 16269
Satellite: ISS
Catalog Number: 25544
Epoch time: 15349
57554648 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 258
8402 deg
Eccentricity:
0008055
Arg of perigee: 283
2361 deg
Mean anomaly: 76
7893 deg
Mean motion: 15
54767847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1626
Checksum: 350
Coasting Arc #6 (Orbit 1640)
---------------------------------------
Vector Time (GMT): 2015/350/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3477035
92 A = 6785253
50 meter
Y = -5389616
10 meter E =
0007709
Z = -2197980
14 I = 51
30345
XDOT = 3247
886834 Wp = 331
76423
YDOT = -4316
592556 meter/sec RA = 253
10553 deg
ZDOT = 5445
534757 TA = 3
69305
MA = 3
68736
Ha = 218
529 n
mi
Hp = 216
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11407598
16 X = -3405832
59
Y = -17682467
51 feet Y = -5428100
37 meter
Z = -7211220
94 Z = -2214698
16
XDOT = 10655
796700 XDOT = 3269
462441
YDOT = -14162
049068 feet/sec YDOT = -4280
152210 meter/sec
ZDOT = 17865
927681 ZDOT = 5461
364424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16237522
90 X = 4949196
98
Y = -13345908
92 feet Y = -4067833
04 meter
Z = -7282460
15 Z = -2219693
85
XDOT = 14319
861229 XDOT = 4364
693703
YDOT = 7633
746098 feet/sec YDOT = 2326
765811 meter/sec
ZDOT = 17935
150740 ZDOT = 5466
633946
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 15350
53966905
00016717 00000-0 10270-3 0 9059
2 25544 51
6432 254
0284 0008154 286
7014 73
3244 15
54810953 16410
Satellite: ISS
Catalog Number: 25544
Epoch time: 15350
53966905 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 254
0284 deg
Eccentricity:
0008154
Arg of perigee: 286
7014 deg
Mean anomaly: 73
3244 deg
Mean motion: 15
54810953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1641
Checksum: 303
Coasting Arc #7 (Orbit 1656)
---------------------------------------
Vector Time (GMT): 2015/351/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2760673
01 A = 6787350
68 meter
Y = 6188106
52 meter E =
0005984
Z = 317565
79 I = 51
32020
XDOT = -4266
597618 Wp = 161
81978
YDOT = 2211
349105 meter/sec RA = 248
10736 deg
ZDOT = -5975
037590 TA = 14
74218
MA = 14
72474
Ha = 218
795 n
mi
Hp = 216
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9057326
14 X = 2689728
29
Y = 20302186
75 feet Y = 6218581
50 meter
Z = 1041882
50 Z = 330804
47
XDOT = -13998
023680 XDOT = -4261
984016
YDOT = 7255
082367 feet/sec YDOT = 2163
663235 meter/sec
ZDOT = -19603
141698 ZDOT = -5995
752492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18910092
36 X = -5763796
15
Y = 11683422
94 feet Y = 3561107
31 meter
Z = 1097951
72 Z = 334655
68
XDOT = -8190
701940 XDOT = -2496
525951
YDOT = -11399
028799 feet/sec YDOT = -3474
423978 meter/sec
ZDOT = -19693
083241 ZDOT = -6002
451772
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 15351
56805019
00016717 00000-0 10270-3 0 9062
2 25544 51
6430 248
8964 0008126 289
5604 70
4671 15
54792415 16570
Satellite: ISS
Catalog Number: 25544
Epoch time: 15351
56805019 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 248
8964 deg
Eccentricity:
0008126
Arg of perigee: 289
5604 deg
Mean anomaly: 70
4671 deg
Mean motion: 15
54792415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1657
Checksum: 326
Coasting Arc #8 (Orbit 1672)
---------------------------------------
Vector Time (GMT): 2015/352/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1770937
06 A = 6786156
48 meter
Y = -6342138
46 meter E =
0010914
Z = 1610512
52 I = 51
32941
XDOT = 5129
123632 Wp = 26
73428
YDOT = 18
093749 meter/sec RA = 243
11046 deg
ZDOT = 5705
773600 TA = 350
98153
MA = 351
00112
Ha = 218
979 n
mi
Hp = 216
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5810160
97 X = -1707709
34
Y = -20807540
89 feet Y = -6361588
78 meter
Z = 5283833
74 Z = 1602063
04
XDOT = 16827
833437 XDOT = 5100
823650
YDOT = 59
362694 feet/sec YDOT = 75
292579 meter/sec
ZDOT = 18719
729660 ZDOT = 5730
621093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19688596
70 X = 6001084
28
Y = -8913095
02 feet Y = -2716711
36 meter
Z = 5248478
27 Z = 1599736
18
XDOT = 1807
709741 XDOT = 550
989929
YDOT = 15090
235062 feet/sec YDOT = 4599
503647 meter/sec
ZDOT = 18827
125208 ZDOT = 5738
507763
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 15352
59641162
00016717 00000-0 10270-3 0 9074
2 25544 51
6430 243
7633 0008291 294
8634 65
1657 15
54847537 16731
Satellite: ISS
Catalog Number: 25544
Epoch time: 15352
59641162 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 243
7633 deg
Eccentricity:
0008291
Arg of perigee: 294
8634 deg
Mean anomaly: 65
1657 deg
Mean motion: 15
54847537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 329
Coasting Arc #9 (Orbit 1687)
---------------------------------------
Vector Time (GMT): 2015/353/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 523925
37 A = 6782509
53 meter
Y = 5886124
73 meter E =
0004487
Z = -3330267
74 I = 51
33252
XDOT = -5708
586671 Wp = 321
87595
YDOT = -2127
796391 meter/sec RA = 238
10772 deg
ZDOT = -4652
059662 TA = 257
08582
MA = 257
13594
Ha = 219
141 n
mi
Hp = 216
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1718915
24 X = 474243
54
Y = 19311432
85 feet Y = 5891705
94 meter
Z = -10926075
25 Z = -3327843
08
XDOT = -18728
958893 XDOT = -5661
770872
YDOT = -6980
959289 feet/sec YDOT = -2191
371661 meter/sec
ZDOT = -15262
662932 ZDOT = -4679
677253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18736940
14 X = -5711019
35
Y = 5001866
52 feet Y = 1524568
91 meter
Z = -10916667
73 Z = -3327400
33
XDOT = 4123
904779 XDOT = 1256
966177
YDOT = -18171
591545 feet/sec YDOT = -5538
701103 meter/sec
ZDOT = -15381
654968 ZDOT = -4688
328434
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 15353
56048475
00016717 00000-0 10270-3 0 9081
2 25544 51
6429 238
9520 0008416 297
2410 62
7885 15
54859477 16886
Satellite: ISS
Catalog Number: 25544
Epoch time: 15353
56048475 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 238
9520 deg
Eccentricity:
0008416
Arg of perigee: 297
2410 deg
Mean anomaly: 62
7885 deg
Mean motion: 15
54859477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1688
Checksum: 351
Coasting Arc #10 (Orbit 1703)
---------------------------------------
Vector Time (GMT): 2015/354/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 930982
94 A = 6778122
90 meter
Y = -4889370
80 meter E =
0001146
Z = 4600085
22 I = 51
33581
XDOT = 5897
611737 Wp = 34
66727
YDOT = 3907
914875 meter/sec RA = 233
09187 deg
ZDOT = 2960
652326 TA = 25
70551
MA = 25
69982
Ha = 219
266 n
mi
Hp = 215
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3054405
97 X = 963242
32
Y = -16041242
78 feet Y = -4878779
76 meter
Z = 15092143
11 Z = 4604685
91
XDOT = 19349
119873 XDOT = 5839
092361
YDOT = 12821
243029 feet/sec YDOT = 3973
538534 meter/sec
ZDOT = 9713
426265 ZDOT = 2989
159914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16310131
23 X = 4971328
00
Y = -54640
34 feet Y = -16654
37 meter
Z = 15112917
76 Z = 4606417
33
XDOT = -9044
813033 XDOT = -2756
859013
YDOT = 20132
953489 feet/sec YDOT = 6136
524224 meter/sec
ZDOT = 9835
954619 ZDOT = 2997
998968
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 15354
58881386
00016717 00000-0 10270-3 0 9091
2 25544 51
6429 233
8189 0008312 302
4936 57
5413 15
54883842 17049
Satellite: ISS
Catalog Number: 25544
Epoch time: 15354
58881386 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 233
8189 deg
Eccentricity:
0008312
Arg of perigee: 302
4936 deg
Mean anomaly: 57
5413 deg
Mean motion: 15
54883842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1704
Checksum: 334
Coasting Arc #11 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2015/355/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2467026
35 A = 6775233
57 meter
Y = 3525903
90 meter E =
0010008
Z = -5240469
97 I = 51
34580
XDOT = -5578
533050 Wp = 48
61330
YDOT = -5184
552351 meter/sec RA = 228
06564 deg
ZDOT = -856
678831 TA = 213
12572
MA = 213
18843
Ha = 219
373 n
mi
Hp = 215
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8093918
48 X = -2480814
17
Y = 11567926
20 feet Y = 3498239
22 meter
Z = -17193142
93 Z = -5252487
63
XDOT = -18302
273787 XDOT = -5515
982061
YDOT = -17009
686192 feet/sec YDOT = -5246
585397 meter/sec
ZDOT = -2810
626085 ZDOT = -883
626773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12937804
28 X = -3943442
74
Y = -5489118
30 feet Y = -1673083
26 meter
Z = -17245735
63 Z = -5256500
22
XDOT = 12576
364736 XDOT = 3833
275972
YDOT = -20393
067262 feet/sec YDOT = -6215
806901 meter/sec
ZDOT = -2926
195865 ZDOT = -891
904500
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 15355
55285472
00016717 00000-0 10270-3 0 9105
2 25544 51
6420 229
0068 0008468 305
5839 54
4524 15
54947745 17199
Satellite: ISS
Catalog Number: 25544
Epoch time: 15355
55285472 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 229
0068 deg
Eccentricity:
0008468
Arg of perigee: 305
5839 deg
Mean anomaly: 54
4524 deg
Mean motion: 15
54947745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1719
Checksum: 328
Coasting Arc #12 (Orbit 1734)
---------------------------------------
Vector Time (GMT): 2015/356/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3957691
94 A = 6775527
16 meter
Y = -1936963
30 meter E =
0008379
Z = 5151303
91 I = 51
36921
XDOT = 4697
140036 Wp = 339
10002
YDOT = 5898
826287 meter/sec RA = 223
03724 deg
ZDOT = -1383
734164 TA = 124
29856
MA = 124
21922
Ha = 219
464 n
mi
Hp = 215
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12984553
60 X = 3954034
20
Y = -6354866
46 feet Y = -1892726
64 meter
Z = 16900603
40 Z = 5170520
64
XDOT = 15410
564423 XDOT = 4637
550496
YDOT = 19353
104616 feet/sec YDOT = 5951
019736 meter/sec
ZDOT = -4539
810248 ZDOT = -1361
060551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9011188
13 X = 2746610
14
Y = 11178290
27 feet Y = 3407142
87 meter
Z = 16984041
63 Z = 5176735
89
XDOT = -14699
818758 XDOT = -4480
504757
YDOT = 18635
003706 feet/sec YDOT = 5679
949130 meter/sec
ZDOT = -4442
833916 ZDOT = -1354
175778
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 15356
58114992
00016717 00000-0 10270-3 0 9118
2 25544 51
6421 223
8743 0008492 308
8713 51
1682 15
54965182 17358
Satellite: ISS
Catalog Number: 25544
Epoch time: 15356
58114992 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 223
8743 deg
Eccentricity:
0008492
Arg of perigee: 308
8713 deg
Mean anomaly: 51
1682 deg
Mean motion: 15
54965182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1735
Checksum: 320
Coasting Arc #13 (Orbit 1749)
---------------------------------------
Vector Time (GMT): 2015/357/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5191265
77 A = 6778692
26 meter
Y = 344752
54 meter E =
0003319
Z = -4345616
16 I = 51
40247
XDOT = -3268
131423 Wp = 38
30396
YDOT = -6029
596436 meter/sec RA = 218
01510 deg
ZDOT = 3429
718644 TA = 266
58709
MA = 266
62505
Ha = 219
552 n
mi
Hp = 215
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17031711
84 X = -5173625
67
Y = 1131077
88 feet Y = 286799
43 meter
Z = -14257270
87 Z = -4370791
46
XDOT = -10722
215956 XDOT = -3217
124397
YDOT = -19782
140538 feet/sec YDOT = -6065
857973 meter/sec
ZDOT = 11252
357756 ZDOT = 3413
965996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5080359
94 X = -1548493
71
Y = -16199707
77 feet Y = -4937670
93 meter
Z = -14366200
92 Z = -4378818
04
XDOT = 15507
911374 XDOT = 4726
811387
YDOT = -14771
311273 feet/sec YDOT = -4502
295676 meter/sec
ZDOT = 11185
317313 ZDOT = 3409
284717
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 15357
54516177
00016717 00000-0 10270-3 0 9127
2 25544 51
6405 219
0612 0008522 312
3924 47
6508 15
54986902 17507
Satellite: ISS
Catalog Number: 25544
Epoch time: 15357
54516177 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 219
0612 deg
Eccentricity:
0008522
Arg of perigee: 312
3924 deg
Mean anomaly: 47
6508 deg
Mean motion: 15
54986902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1750
Checksum: 308
Coasting Arc #14 (Orbit 1765)
---------------------------------------
Vector Time (GMT): 2015/358/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6019218
37 A = 6782975
79 meter
Y = 1144710
14 meter E =
0008406
Z = 2909633
30 I = 51
44308
XDOT = 1355
784863 Wp = 57
75293
YDOT = 5642
150963 meter/sec RA = 213
00893 deg
ZDOT = -5009
459679 TA = 88
97880
MA = 88
88249
Ha = 219
798 n
mi
Hp = 214
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19748091
77 X = 5991836
73
Y = 3755610
70 feet Y = 1211867
61 meter
Z = 9546041
00 Z = 2938807
00
XDOT = 4448
113067 XDOT = 1316
926165
YDOT = 18510
993974 feet/sec YDOT = 5657
095508 meter/sec
ZDOT = -16435
235167 ZDOT = -5002
967345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1320898
66 X = 402609
91
Y = 19998150
05 feet Y = 6095436
13 meter
Z = 9672014
31 Z = 2948029
96
XDOT = -15308
534092 XDOT = -4666
041191
YDOT = 8970
400124 feet/sec YDOT = 2734
177958 meter/sec
ZDOT = -16408
162458 ZDOT = -5001
207917
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 15358
57342354
00016717 00000-0 10270-3 0 9136
2 25544 51
6405 213
9285 0008734 316
5125 43
5339 15
55046759 17662
Satellite: ISS
Catalog Number: 25544
Epoch time: 15358
57342354 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 213
9285 deg
Eccentricity:
0008734
Arg of perigee: 316
5125 deg
Mean anomaly: 43
5339 deg
Mean motion: 15
55046759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1766
Checksum: 322
Coasting Arc #15 (Orbit 1780)
---------------------------------------
Vector Time (GMT): 2015/359/12:50:46
594
Vector Time (MET): N/A
Weight (LBS) : 906357
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6259280
47 A = 6786243
82 meter
Y = -2369113
45 meter E =
0013997
Z = -1065983
92 I = 51
47902
XDOT = 839
346180 Wp = 1
50042
YDOT = -4857
286101 meter/sec RA = 208
01561 deg
ZDOT = 5882
109802 TA = 346
90144
MA = 346
93775
Ha = 219
906 n
mi
Hp = 214
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20535697
09 X = -6227145
16
Y = -7772681
92 feet Y = -2438929
06 meter
Z = -3497322
58 Z = -1096312
24
XDOT = 2753
760433 XDOT = 865
026325
YDOT = -15935
978022 feet/sec YDOT = -4847
757036 meter/sec
ZDOT = 19298
260505 ZDOT = 5886
248990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1982676
11 X = 604319
68
Y = -21846433
04 feet Y = -6658792
79 meter
Z = -3628093
63 Z = -1105842
94
XDOT = 14462
353606 XDOT = 4408
125379
YDOT = -1887
378094 feet/sec YDOT = -575
272843 meter/sec
ZDOT = 19317
027966 ZDOT = 5887
830124
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 15359
53740620
00016717 00000-0 10270-3 0 9142
2 25544 51
6386 209
1149 0008617 319
6675 40
3838 15
55012382 17811
Satellite: ISS
Catalog Number: 25544
Epoch time: 15359
53740620 = yrday
fracday
Element set: 914
Inclination: 51
6386 deg
RA of node: 209
1149 deg
Eccentricity:
0008617
Arg of perigee: 319
6675 deg
Mean anomaly: 40
3838 deg
Mean motion: 15
55012382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1781
Checksum: 317
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