[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 21st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 905 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 737)
---------------------------------------
Vector Time (GMT): 2015/292/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6691078
49 A = 6788277
64 meter
Y = -857410
02 meter E =
0019863
Z = 666790
13 I = 51
63781
XDOT = 1204
094978 Wp = 51
81116
YDOT = -4670
566876 meter/sec RA = 182
81494 deg
ZDOT = 5968
372477 TA = 315
39561
MA = 315
55527
Ha = 222
743 n
mi
Hp = 212
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21952357
24 X = -6684232
49
Y = -2813025
00 feet Y = -932195
76 meter
Z = 2187631
65 Z = 634302
31
XDOT = 3950
442842 XDOT = 1227
240308
YDOT = -15323
382140 feet/sec YDOT = -4656
972152 meter/sec
ZDOT = 19581
274531 ZDOT = 5974
278307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22094828
27 X = 6734503
66
Y = 1493586
68 feet Y = 455245
22 meter
Z = 2047582
19 Z = 624103
05
XDOT = -2792
797313 XDOT = -851
244621
YDOT = 13911
840369 feet/sec YDOT = 4240
328944 meter/sec
ZDOT = 19607
504965 ZDOT = 5976
367513
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 15292
49834216
00016717 00000-0 10270-3 0 9003
2 25544 51
6424 183
6263 0006731 50
8952 309
2798 15
54435892 7381
Satellite: ISS
Catalog Number: 25544
Epoch time: 15292
49834216 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 183
6263 deg
Eccentricity:
0006731
Arg of perigee: 50
8952 deg
Mean anomaly: 309
2798 deg
Mean motion: 15
54435892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 738
Checksum: 328
Coasting Arc #2 (Orbit 752)
---------------------------------------
Vector Time (GMT): 2015/293/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6103453
31 A = 6785888
71 meter
Y = 1699705
14 meter E =
0009461
Z = -2438575
71 I = 51
66287
XDOT = -3340
871831 Wp = 90
24996
YDOT = 4355
167431 meter/sec RA = 177
84095 deg
ZDOT = -5344
190074 TA = 117
00506
MA = 116
90844
Ha = 222
723 n
mi
Hp = 212
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20024453
12 X = 6095839
02
Y = 5576460
43 feet Y = 1767915
26 meter
Z = -8000576
46 Z = -2408944
51
XDOT = -10960
865586 XDOT = -3363
363645
YDOT = 14288
607058 feet/sec YDOT = 4317
681528 meter/sec
ZDOT = -17533
432001 ZDOT = -5360
474485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20444861
45 X = -6231593
77
Y = -4013580
73 feet Y = -1223339
41 meter
Z = -7872970
68 Z = -2399681
46
XDOT = 9423
756740 XDOT = 2872
361054
YDOT = -13588
990310 feet/sec YDOT = -4141
924247 meter/sec
ZDOT = -17604
405370 ZDOT = -5365
822757
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 15293
46266517
00016717 00000-0 10270-3 0 9015
2 25544 51
6433 178
8162 0006641 54
5202 305
6569 15
54470527 7531
Satellite: ISS
Catalog Number: 25544
Epoch time: 15293
46266517 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 178
8162 deg
Eccentricity:
0006641
Arg of perigee: 54
5202 deg
Mean anomaly: 305
6569 deg
Mean motion: 15
54470527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 753
Checksum: 310
Coasting Arc #3 (Orbit 768)
---------------------------------------
Vector Time (GMT): 2015/294/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4971570
45 A = 6781968
15 meter
Y = -2468179
90 meter E =
0017003
Z = 3880946
25 I = 51
68160
XDOT = 5164
970818 Wp = 83
91710
YDOT = -3920
148837 meter/sec RA = 172
85959 deg
ZDOT = 4109
630041 TA = 322
99945
MA = 323
11658
Ha = 222
826 n
mi
Hp = 211
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16310926
68 X = -4962453
57
Y = -8097703
09 feet Y = -2523724
04 meter
Z = 12732763
30 Z = 3856817
36
XDOT = 16945
442315 XDOT = 5188
459726
YDOT = -12861
380698 feet/sec YDOT = -3862
259110 meter/sec
ZDOT = 13483
038192 ZDOT = 4134
778079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17081303
79 X = 5206381
39
Y = 6517629
13 feet Y = 1986573
36 meter
Z = 12629012
52 Z = 3849323
01
XDOT = -15098
283078 XDOT = -4601
956682
YDOT = 13144
397235 feet/sec YDOT = 4006
412277 meter/sec
ZDOT = 13592
207811 ZDOT = 4142
904941
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 15294
49125988
00016717 00000-0 10270-3 0 9026
2 25544 51
6432 173
6856 0006704 58
1742 302
0063 15
54494353 7692
Satellite: ISS
Catalog Number: 25544
Epoch time: 15294
49125988 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 173
6856 deg
Eccentricity:
0006704
Arg of perigee: 58
1742 deg
Mean anomaly: 302
0063 deg
Mean motion: 15
54494353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 769
Checksum: 322
Coasting Arc #4 (Orbit 783)
---------------------------------------
Vector Time (GMT): 2015/295/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3408375
38 A = 6778032
92 meter
Y = 3229732
41 meter E =
0018472
Z = -4905437
54 I = 51
70129
XDOT = -6498
695853 Wp = 68
94401
YDOT = 3293
341442 meter/sec RA = 167
86839 deg
ZDOT = -2347
731424 TA = 178
05392
MA = 178
04672
Ha = 222
652 n
mi
Hp = 211
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11182333
94 X = 3395835
46
Y = 10596234
95 feet Y = 3267776
59 meter
Z = -16093955
19 Z = -4888910
86
XDOT = -21321
180619 XDOT = -6523
635270
YDOT = 10804
925991 feet/sec YDOT = 3220
529097 meter/sec
ZDOT = -7702
530918 ZDOT = -2379
362031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12393484
49 X = -3777534
07
Y = -9273674
10 feet Y = -2826615
87 meter
Z = -16023129
91 Z = -4883850
00
XDOT = 19261
379633 XDOT = 5870
868512
YDOT = -12199
684652 feet/sec YDOT = -3718
463882 meter/sec
ZDOT = -7839
596321 ZDOT = -2389
508959
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 15295
45554998
00016717 00000-0 10270-3 0 9031
2 25544 51
6440 168
8756 0006657 60
9044 299
2775 15
54547195 7846
Satellite: ISS
Catalog Number: 25544
Epoch time: 15295
45554998 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 168
8756 deg
Eccentricity:
0006657
Arg of perigee: 60
9044 deg
Mean anomaly: 299
2775 deg
Mean motion: 15
54547195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 784
Checksum: 361
Coasting Arc #5 (Orbit 799)
---------------------------------------
Vector Time (GMT): 2015/296/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1566630
92 A = 6776064
15 meter
Y = -3899688
42 meter E =
0008622
Z = 5308050
02 I = 51
72605
XDOT = 7253
611836 Wp = 76
25569
YDOT = -2492
548400 meter/sec RA = 162
87047 deg
ZDOT = 311
216912 TA = 10
79329
MA = 10
77480
Ha = 222
629 n
mi
Hp = 211
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5139865
21 X = -1548692
06
Y = -12794253
34 feet Y = -3917106
69 meter
Z = 17414862
27 Z = 5300483
49
XDOT = 23797
939096 XDOT = 7279
433218
YDOT = -8177
652230 feet/sec YDOT = -2411
289320 meter/sec
ZDOT = 1021
052860 ZDOT = 346
516958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6849184
14 X = 2087631
32
Y = 12013110
98 feet Y = 3661596
23 meter
Z = 17382819
16 Z = 5298283
28
XDOT = -21668
898074 XDOT = -6604
680133
YDOT = 10663
329722 feet/sec YDOT = 3250
182899 meter/sec
ZDOT = 1173
846392 ZDOT = 357
788380
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 15296
48410882
00016717 00000-0 10270-3 0 9049
2 25544 51
6439 163
7447 0006521 64
4610 295
7217 15
54580924 8001
Satellite: ISS
Catalog Number: 25544
Epoch time: 15296
48410882 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 163
7447 deg
Eccentricity:
0006521
Arg of perigee: 64
4610 deg
Mean anomaly: 295
7217 deg
Mean motion: 15
54580924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 800
Checksum: 314
Coasting Arc #6 (Orbit 814)
---------------------------------------
Vector Time (GMT): 2015/297/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -336770
58 A = 6776994
43 meter
Y = 4472814
30 meter E =
0019009
Z = -5096736
55 I = 51
75964
XDOT = -7302
447974 Wp = 91
80133
YDOT = 1462
499419 meter/sec RA = 157
87311 deg
ZDOT = 1771
105667 TA = 195
30159
MA = 195
35916
Ha = 222
581 n
mi
Hp = 211
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1104890
36 X = -362003
22
Y = 14674587
61 feet Y = 4468906
67 meter
Z = -16721576
60 Z = -5098434
32
XDOT = -23958
162645 XDOT = -7326
862766
YDOT = 4798
226441 feet/sec YDOT = 1380
702311 meter/sec
ZDOT = 5810
714131 ZDOT = 1735
571774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1145460
54 X = -349136
37
Y = -14662300
87 feet Y = -4469069
30 meter
Z = -16729622
88 Z = -5099189
05
XDOT = 21973
219925 XDOT = 6697
437433
YDOT = -8152
116905 feet/sec YDOT = -2484
765233 meter/sec
ZDOT = 5657
061082 ZDOT = 1724
272218
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 15297
44836780
00016717 00000-0 10270-3 0 9056
2 25544 51
6441 158
9344 0006522 67
1244 293
0597 15
54590802 8154
Satellite: ISS
Catalog Number: 25544
Epoch time: 15297
44836780 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 158
9344 deg
Eccentricity:
0006522
Arg of perigee: 67
1244 deg
Mean anomaly: 293
0597 deg
Mean motion: 15
54590802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 815
Checksum: 324
Coasting Arc #7 (Orbit 830)
---------------------------------------
Vector Time (GMT): 2015/298/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2159784
42 A = 6780213
53 meter
Y = -4837673
42 meter E =
0016550
Z = 4220905
47 I = 51
79985
XDOT = 6737
997327 Wp = 72
58378
YDOT = -207
091145 meter/sec RA = 152
88421 deg
ZDOT = -3668
428080 TA = 54
95630
MA = 54
80114
Ha = 222
477 n
mi
Hp = 211
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7085906
90 X = 2193215
95
Y = -15871631
96 feet Y = -4813333
89 meter
Z = 13848115
05 Z = 4231479
23
XDOT = 22106
290443 XDOT = 6757
632493
YDOT = -679
432890 feet/sec YDOT = -131
633033 meter/sec
ZDOT = -12035
525196 ZDOT = -3635
647828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4327766
87 X = -1319103
34
Y = 16795861
98 feet Y = 5119378
73 meter
Z = 13894550
10 Z = 4235058
87
XDOT = -20553
173896 XDOT = -6264
607403
YDOT = 4588
584527 feet/sec YDOT = 1398
600564 meter/sec
ZDOT = -11893
950455 ZDOT = -3625
276099
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 15298
47689220
00016717 00000-0 10270-3 0 9066
2 25544 51
6438 153
8034 0006516 69
6680 290
5173 15
54642437 8316
Satellite: ISS
Catalog Number: 25544
Epoch time: 15298
47689220 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 153
8034 deg
Eccentricity:
0006516
Arg of perigee: 69
6680 deg
Mean anomaly: 290
5173 deg
Mean motion: 15
54642437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 831
Checksum: 326
Coasting Arc #8 (Orbit 845)
---------------------------------------
Vector Time (GMT): 2015/299/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3659723
74 A = 6784340
61 meter
Y = 4947353
89 meter E =
0010994
Z = -2859739
46 I = 51
84092
XDOT = -5598
865979 Wp = 69
46508
YDOT = -1210
444905 meter/sec RA = 147
90848 deg
ZDOT = 5090
591609 TA = 258
12577
MA = 258
24908
Ha = 222
490 n
mi
Hp = 211
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12006967
65 X = -3700882
37
Y = 16231476
02 feet Y = 4906198
03 meter
Z = -9382347
33 Z = -2877618
59
XDOT = -18368
982871 XDOT = -5609
643159
YDOT = -3971
275934 feet/sec YDOT = -1273
114867 meter/sec
ZDOT = 16701
416041 ZDOT = 5063
366688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8842904
61 X = 2695317
32
Y = -18109699
49 feet Y = -5519836
40 meter
Z = -9460356
74 Z = -2883516
73
XDOT = 17567
137592 XDOT = 5354
463538
YDOT = -52
133723 feet/sec YDOT = -15
890359 meter/sec
ZDOT = 16584
049155 ZDOT = 5054
818182
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 15299
44111860
00016717 00000-0 10270-3 0 9075
2 25544 51
6432 148
9926 0006410 72
8743 287
3112 15
54629899 8464
Satellite: ISS
Catalog Number: 25544
Epoch time: 15299
44111860 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 148
9926 deg
Eccentricity:
0006410
Arg of perigee: 72
8743 deg
Mean anomaly: 287
3112 deg
Mean motion: 15
54629899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 846
Checksum: 333
Coasting Arc #9 (Orbit 861)
---------------------------------------
Vector Time (GMT): 2015/300/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4789207
48 A = 6787347
64 meter
Y = -4677342
12 meter E =
0018792
Z = 1079339
01 I = 51
87694
XDOT = 4041
872797 Wp = 109
21342
YDOT = 2757
368620 meter/sec RA = 142
94596 deg
ZDOT = -5907
699524 TA = 59
11290
MA = 58
92824
Ha = 222
552 n
mi
Hp = 211
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15712622
97 X = 4835911
55
Y = -15345610
63 feet Y = -4623524
82 meter
Z = 3541138
47 Z = 1102718
50
XDOT = 13260
737522 XDOT = 4039
437004
YDOT = 9046
484974 feet/sec YDOT = 2802
553417 meter/sec
ZDOT = -19382
216286 ZDOT = -5888
070492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12373948
64 X = -3771579
55
Y = 18125363
96 feet Y = 5524610
94 meter
Z = 3642873
05 Z = 1110347
71
XDOT = -13577
056058 XDOT = -4138
286686
YDOT = -5340
581100 feet/sec YDOT = -1627
809119 meter/sec
ZDOT = -19297
899158 ZDOT = -5881
999663
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 15300
46961010
00016717 00000-0 10270-3 0 9081
2 25544 51
6428 143
8610 0006462 78
0864 282
1013 15
54631664 8626
Satellite: ISS
Catalog Number: 25544
Epoch time: 15300
46961010 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 143
8610 deg
Eccentricity:
0006462
Arg of perigee: 78
0864 deg
Mean anomaly: 282
1013 deg
Mean motion: 15
54631664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 862
Checksum: 291
Coasting Arc #10 (Orbit 877)
---------------------------------------
Vector Time (GMT): 2015/301/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5395605
28 A = 6787415
05 meter
Y = 4028757
61 meter E =
0019124
Z = 787848
00 I = 51
90191
XDOT = -2282
278850 Wp = 62
03774
YDOT = -4243
899340 meter/sec RA = 137
98893 deg
ZDOT = 5969
995071 TA = 306
45399
MA = 306
63010
Ha = 222
392 n
mi
Hp = 211
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17702117
05 X = -5444081
99
Y = 13217708
71 feet Y = 3968149
39 meter
Z = 2584803
15 Z = 761518
50
XDOT = -7487
791501 XDOT = -2263
653718
YDOT = -13923
554265 feet/sec YDOT = -4269
316820 meter/sec
ZDOT = 19586
598001 ZDOT = 5958
953368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14495579
30 X = 4418252
57
Y = -16689194
29 feet Y = -5086866
42 meter
Z = 2470415
63 Z = 752982
68
XDOT = 9186
944791 XDOT = 2800
180772
YDOT = 10923
312133 feet/sec YDOT = 3329
425538 meter/sec
ZDOT = 19539
614532 ZDOT = 5955
674509
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 15301
49808056
00016717 00000-0 10270-3 0 9096
2 25544 51
6420 138
7285 0006299 80
3345 279
8519 15
54706248 8789
Satellite: ISS
Catalog Number: 25544
Epoch time: 15301
49808056 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 138
7285 deg
Eccentricity:
0006299
Arg of perigee: 80
3345 deg
Mean anomaly: 279
8519 deg
Mean motion: 15
54706248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 878
Checksum: 339
Coasting Arc #11 (Orbit 892)
---------------------------------------
Vector Time (GMT): 2015/302/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5536955
72 A = 6784843
83 meter
Y = -2919985
83 meter E =
0010488
Z = -2622155
09 I = 51
91554
XDOT = 449
727928 Wp = 103
85224
YDOT = 5556
153495 meter/sec RA = 133
03066 deg
ZDOT = -5257
631617 TA = 105
54548
MA = 105
42967
Ha = 222
408 n
mi
Hp = 211
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18165865
21 X = 5581933
97
Y = -9580006
00 feet Y = -2857816
54 meter
Z = -8602871
04 Z = -2595147
59
XDOT = 1475
485328 XDOT = 413
104511
YDOT = 18228
850049 feet/sec YDOT = 5560
977704 meter/sec
ZDOT = -17249
447561 ZDOT = -5255
536007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15530988
80 X = -4733845
39
Y = 13511679
97 feet Y = 4118360
06 meter
Z = -8485720
67 Z = -2586447
66
XDOT = -4746
863669 XDOT = -1446
844046
YDOT = -16242
455791 feet/sec YDOT = -4950
700525 meter/sec
ZDOT = -17241
331823 ZDOT = -5255
157940
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 15302
46225821
00016717 00000-0 10270-3 0 9109
2 25544 51
6413 133
9173 0006205 83
6111 276
5749 15
54693965 8935
Satellite: ISS
Catalog Number: 25544
Epoch time: 15302
46225821 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 133
9173 deg
Eccentricity:
0006205
Arg of perigee: 83
6111 deg
Mean anomaly: 276
5749 deg
Mean motion: 15
54693965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 893
Checksum: 308
Coasting Arc #12 (Orbit 908)
---------------------------------------
Vector Time (GMT): 2015/303/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5206314
18 A = 6780681
57 meter
Y = 1471226
69 meter E =
0016836
Z = 4074387
03 I = 51
92267
XDOT = 1219
871302 Wp = 96
25735
YDOT = -6503
088593 meter/sec RA = 128
06205 deg
ZDOT = 3891
437084 TA = 313
58060
MA = 313
72023
Ha = 222
492 n
mi
Hp = 211
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17081083
27 X = -5242171
14
Y = 4826859
21 feet Y = 1412805
83 meter
Z = 13367411
53 Z = 4049008
08
XDOT = 4002
202435 XDOT = 1273
596188
YDOT = -21335
592497 feet/sec YDOT = -6489
146725 meter/sec
ZDOT = 12767
182035 ZDOT = 3897
493727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15446151
41 X = 4707986
95
Y = -8910899
31 feet Y = -2716042
11 meter
Z = 13257524
16 Z = 4040893
37
XDOT = 810
080758 XDOT = 246
912615
YDOT = 20516
124115 feet/sec YDOT = 6253
314630 meter/sec
ZDOT = 12794
455897 ZDOT = 3899
750157
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 15303
49069682
00016717 00000-0 10270-3 0 9115
2 25544 51
6411 128
7845 0006267 85
7196 274
4673 15
54715830 9092
Satellite: ISS
Catalog Number: 25544
Epoch time: 15303
49069682 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 128
7845 deg
Eccentricity:
0006267
Arg of perigee: 85
7196 deg
Mean anomaly: 274
4673 deg
Mean motion: 15
54715830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 909
Checksum: 331
Coasting Arc #13 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2015/304/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4531971
52 A = 6776844
83 meter
Y = 286395
98 meter E =
0018857
Z = -5047362
39 I = 51
92828
XDOT = -2642
942958 Wp = 80
18998
YDOT = 6904
808679 meter/sec RA = 123
08212 deg
ZDOT = -1984
455670 TA = 170
60161
MA = 170
56627
Ha = 222
277 n
mi
Hp = 211
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14868672
97 X = 4552950
80
Y = 939619
36 feet Y = 337192
71 meter
Z = -16559587
91 Z = -5025295
59
XDOT = -8671
072696 XDOT = -2710
317857
YDOT = 22653
571780 feet/sec YDOT = 6874
876806 meter/sec
ZDOT = -6510
681333 ZDOT = -1997
458555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14693292
75 X = -4478515
63
Y = 3035505
38 feet Y = 925222
04 meter
Z = -16464298
56 Z = -5018318
20
XDOT = 2585
224171 XDOT = 787
976327
YDOT = -23053
920896 feet/sec YDOT = -7026
835089 meter/sec
ZDOT = -6568
050658 ZDOT = -2001
941841
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 15304
45483999
00016717 00000-0 10270-3 0 9124
2 25544 51
6402 123
9725 0006200 89
9181 270
2682 15
54761144 9243
Satellite: ISS
Catalog Number: 25544
Epoch time: 15304
45483999 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 123
9725 deg
Eccentricity:
0006200
Arg of perigee: 89
9181 deg
Mean anomaly: 270
2682 deg
Mean motion: 15
54761144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 924
Checksum: 311
Coasting Arc #14 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2015/305/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3589746
04 A = 6775483
12 meter
Y = -2133745
79 meter E =
0008619
Z = 5328126
43 I = 51
94109
XDOT = 3732
063784 Wp = 90
82370
YDOT = -6706
247846 meter/sec RA = 118
09604 deg
ZDOT = -171
100070 TA =
79907
MA =
79770
Ha = 222
402 n
mi
Hp = 211
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11777382
03 X = -3591501
62
Y = -7000478
32 feet Y = -2173898
42 meter
Z = 17480729
77 Z = 5310683
65
XDOT = 12244
303752 XDOT = 3807
608458
YDOT = -22002
125478 feet/sec YDOT = -6664
091055 meter/sec
ZDOT = -561
351937 ZDOT = -152
786538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13371993
42 X = 4075783
60
Y = 3394053
63 feet Y = 1034507
55 meter
Z = 17405732
65 Z = 5305267
31
XDOT = -5357
001991 XDOT = -1632
814207
YDOT = 23574
639788 feet/sec YDOT = 7185
550207 meter/sec
ZDOT = -481
052909 ZDOT = -146
624927
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 15305
48324350
00016717 00000-0 10270-3 0 9134
2 25544 51
6408 118
8405 0006214 93
7268 266
4596 15
54768874 9407
Satellite: ISS
Catalog Number: 25544
Epoch time: 15305
48324350 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 118
8405 deg
Eccentricity:
0006214
Arg of perigee: 93
7268 deg
Mean anomaly: 266
4596 deg
Mean motion: 15
54768874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 940
Checksum: 325
Coasting Arc #15 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2015/306/10:26:45
850
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2531936
59 A = 6777072
46 meter
Y = 3911087
30 meter E =
0018339
Z = -4938417
89 I = 51
96015
XDOT = -4439
535532 Wp = 103
63550
YDOT = 5791
493668 meter/sec RA = 113
11002 deg
ZDOT = 2313
536294 TA = 188
91275
MA = 188
94535
Ha = 222
184 n
mi
Hp = 211
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8306878
59 X = 2512002
98
Y = 12831651
26 feet Y = 3939289
50 meter
Z = -16202158
43 Z = -4926166
60
XDOT = -14565
405288 XDOT = -4515
205908
YDOT = 19000
963478 feet/sec YDOT = 5741
424821 meter/sec
ZDOT = 7590
342173 ZDOT = 2291
785650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11833020
49 X = -3606704
65
Y = -9763486
56 feet Y = -2975910
70 meter
Z = -16149904
03 Z = -4922490
75
XDOT = 7617
953179 XDOT = 2321
952129
YDOT = -21614
519634 feet/sec YDOT = -6588
105585 meter/sec
ZDOT = 7495
333615 ZDOT = 2284
577686
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 15306
44735399
00016717 00000-0 10270-3 0 9141
2 25544 51
6398 114
0277 0006230 97
2807 262
9054 15
54820740 9553
Satellite: ISS
Catalog Number: 25544
Epoch time: 15306
44735399 = yrday
fracday
Element set: 914
Inclination: 51
6398 deg
RA of node: 114
0277 deg
Eccentricity:
0006230
Arg of perigee: 97
2807 deg
Mean anomaly: 262
9054 deg
Mean motion: 15
54820740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 318
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