[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 17th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 730 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 3276)
---------------------------------------
Vector Time (GMT): 2015/198/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3150568
16 A = 6775107
45 meter
Y = 3148446
25 meter E =
0003274
Z = 5104086
87 I = 51
29025
XDOT = -3894
205136 Wp = 37
73124
YDOT = 6423
649559 meter/sec RA = 291
67226 deg
ZDOT = -1555
587797 TA = 67
34834
MA = 67
31372
Ha = 218
505 n
mi
Hp = 213
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10336509
70 X = 3090334
07
Y = 10329548
08 feet Y = 3183340
77 meter
Z = 16745691
83 Z = 5119245
37
XDOT = -12776
263568 XDOT = -3958
190191
YDOT = 21074
965745 feet/sec YDOT = 6379
744369 meter/sec
ZDOT = -5103
634505 ZDOT = -1574
659610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 950049
88 X = 289575
20
Y = -14507728
41 feet Y = -4421955
62 meter
Z = 16810247
26 Z = 5123763
37
XDOT = 23167
226506 XDOT = 7061
370639
YDOT = -4504
643308 feet/sec YDOT = -1373
015280 meter/sec
ZDOT = -5186
904884 ZDOT = -1580
968609
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 15198
59363961
00016717 00000-0 10270-3 0 9003
2 25544 51
6450 292
1866 0002001 263
5034 96
5892 15
55182320 32773
Satellite: ISS
Catalog Number: 25544
Epoch time: 15198
59363961 = yrday
fracday
Element set: 900
Inclination: 51
6450 deg
RA of node: 292
1866 deg
Eccentricity:
0002001
Arg of perigee: 263
5034 deg
Mean anomaly: 96
5892 deg
Mean motion: 15
55182320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3277
Checksum: 310
Coasting Arc #2 (Orbit 3291)
---------------------------------------
Vector Time (GMT): 2015/199/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2052366
33 A = 6778680
11 meter
Y = -4908224
91 meter E =
0006417
Z = -4207781
27 I = 51
29016
XDOT = 4530
805569 Wp = 115
82260
YDOT = -5003
616487 meter/sec RA = 286
64459 deg
ZDOT = 3628
199427 TA = 191
52327
MA = 191
53797
Ha = 218
665 n
mi
Hp = 213
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6733485
32 X = -1976889
41
Y = -16103100
09 feet Y = -4930753
53 meter
Z = -13805056
65 Z = -4217568
06
XDOT = 14864
847666 XDOT = 4568
796385
YDOT = -16416
064589 feet/sec YDOT = -4952
737858 meter/sec
ZDOT = 11903
541426 ZDOT = 3650
300732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7377843
82 X = -2248766
80
Y = 15782267
18 feet Y = 4810435
04 meter
Z = -13846180
32 Z = -4220315
76
XDOT = -20942
533861 XDOT = -6383
284321
YDOT = 732
808336 feet/sec YDOT = 223
359981 meter/sec
ZDOT = 11999
546681 ZDOT = 3657
461828
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 15199
55753251
00016717 00000-0 10270-3 0 9016
2 25544 51
6438 287
3750 0001778 267
8033 92
2916 15
55193808 32923
Satellite: ISS
Catalog Number: 25544
Epoch time: 15199
55753251 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 287
3750 deg
Eccentricity:
0001778
Arg of perigee: 267
8033 deg
Mean anomaly: 92
2916 deg
Mean motion: 15
55193808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3292
Checksum: 333
Coasting Arc #3 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2015/200/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 902620
47 A = 6783169
55 meter
Y = 6170123
98 meter E =
0011703
Z = 2655748
37 I = 51
29720
XDOT = -4838
991114 Wp = 102
67887
YDOT = 2942
605784 meter/sec RA = 281
62940 deg
ZDOT = -5175
139138 TA = 47
18265
MA = 47
08433
Ha = 218
600 n
mi
Hp = 213
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2961353
24 X = 820657
18
Y = 20243188
90 feet Y = 6179759
26 meter
Z = 8713085
21 Z = 2659934
26
XDOT = -15875
955097 XDOT = -4846
397965
YDOT = 9654
218452 feet/sec YDOT = 2888
451845 meter/sec
ZDOT = -16978
802947 ZDOT = -5198
663444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12682204
69 X = 3865535
99
Y = -16044462
58 feet Y = -4890352
19 meter
Z = 8729895
11 Z = 2660872
03
XDOT = 16685
999882 XDOT = 5085
892764
YDOT = 3865
759132 feet/sec YDOT = 1178
283384 meter/sec
ZDOT = -17080
518890 ZDOT = -5206
142158
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 15200
58566957
00016717 00000-0 10270-3 0 9028
2 25544 51
6438 282
2413 0001867 278
8120 81
2822 15
55214436 33084
Satellite: ISS
Catalog Number: 25544
Epoch time: 15200
58566957 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 282
2413 deg
Eccentricity:
0001867
Arg of perigee: 278
8120 deg
Mean anomaly: 81
2822 deg
Mean motion: 15
55214436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 306
Coasting Arc #4 (Orbit 3322)
---------------------------------------
Vector Time (GMT): 2015/201/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 202532
52 A = 6786094
92 meter
Y = -6739428
03 meter E =
0009937
Z = -719627
83 I = 51
30016
XDOT = 4839
580200 Wp = 29
99421
YDOT = -483
155176 meter/sec RA = 276
62650 deg
ZDOT = 5930
869836 TA = 322
19015
MA = 322
25991
Ha = 218
718 n
mi
Hp = 213
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 664476
76 X = 281375
00
Y = -22110984
34 feet Y = -6736722
32 meter
Z = -2360983
71 Z = -718452
74
XDOT = 15877
887796 XDOT = 4815
813784
YDOT = -1585
154776 feet/sec YDOT = -429
168919 meter/sec
ZDOT = 19458
234371 ZDOT = 5954
321463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16248929
16 X = -4952673
61
Y = 15011306
96 feet Y = 4575446
36 meter
Z = -2354647
92 Z = -717696
69
XDOT = -11075
265693 XDOT = -3375
740983
YDOT = -8943
059924 feet/sec YDOT = -2725
844665 meter/sec
ZDOT = 19559
163861 ZDOT = 5961
633145
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 15201
54953620
00016717 00000-0 10270-3 0 9033
2 25544 51
6430 277
4285 0001873 287
5773 72
5175 15
55165760 33233
Satellite: ISS
Catalog Number: 25544
Epoch time: 15201
54953620 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 277
4285 deg
Eccentricity:
0001873
Arg of perigee: 287
5773 deg
Mean anomaly: 72
5175 deg
Mean motion: 15
55165760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3323
Checksum: 310
Coasting Arc #5 (Orbit 3338)
---------------------------------------
Vector Time (GMT): 2015/202/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1274577
61 A = 6785307
61 meter
Y = 6520897
20 meter E =
0007268
Z = -1358957
96 I = 51
29569
XDOT = -4577
265955 Wp = 149
45429
YDOT = -2096
031270 meter/sec RA = 271
62717 deg
ZDOT = -5784
457781 TA = 45
42441
MA = 45
36511
Ha = 218
671 n
mi
Hp = 213
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4181685
09 X = -1340799
90
Y = 21394019
68 feet Y = 6506273
81 meter
Z = -4458523
48 Z = -1365310
17
XDOT = -15017
276754 XDOT = -4525
389078
YDOT = -6876
743013 feet/sec YDOT = -2146
927024 meter/sec
ZDOT = -18977
879860 ZDOT = -5806
567022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17961843
54 X = 5474769
91
Y = -12341289
36 feet Y = -3761625
00 meter
Z = -4487065
12 Z = -1367657
45
XDOT = 4897
726470 XDOT = 1492
827028
YDOT = 14039
238802 feet/sec YDOT = 4279
159987 meter/sec
ZDOT = -19072
551763 ZDOT = -5813
313777
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 15202
57764717
00016717 00000-0 10270-3 0 9045
2 25544 51
6432 272
2944 0001728 291
1547 68
9421 15
55238485 33394
Satellite: ISS
Catalog Number: 25544
Epoch time: 15202
57764717 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 272
2944 deg
Eccentricity:
0001728
Arg of perigee: 291
1547 deg
Mean anomaly: 68
9421 deg
Mean motion: 15
55238485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3339
Checksum: 323
Coasting Arc #6 (Orbit 3354)
---------------------------------------
Vector Time (GMT): 2015/203/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2250050
80 A = 6781686
50 meter
Y = -5528121
77 meter E =
0011388
Z = 3208501
27 I = 51
28292
XDOT = 4080
220395 Wp = 82
48946
YDOT = 4428
269040 meter/sec RA = 266
61999 deg
ZDOT = 4755
298931 TA = 314
87283
MA = 314
96525
Ha = 218
684 n
mi
Hp = 213
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7382056
42 X = 2296114
82
Y = -18136882
45 feet Y = -5502702
76 meter
Z = 10526578
96 Z = 3219543
19
XDOT = 13386
549852 XDOT = 4007
299953
YDOT = 14528
441733 feet/sec YDOT = 4473
488882 meter/sec
ZDOT = 15601
374444 ZDOT = 4774
942659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17794982
97 X = -5423910
81
Y = 8109019
39 feet Y = 2471629
11 meter
Z = 10575089
24 Z = 3223287
20
XDOT = 967
379500 XDOT = 294
857272
YDOT = -18387
822914 feet/sec YDOT = -5604
608424 meter/sec
ZDOT = 15685
015691 ZDOT = 4780
792783
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 15203
60574440
00016717 00000-0 10270-3 0 9053
2 25544 51
6425 267
1602 0001670 298
0760 62
0225 15
55240616 33553
Satellite: ISS
Catalog Number: 25544
Epoch time: 15203
60574440 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 267
1602 deg
Eccentricity:
0001670
Arg of perigee: 298
0760 deg
Mean anomaly: 62
0225 deg
Mean motion: 15
55240616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3355
Checksum: 280
Coasting Arc #7 (Orbit 3369)
---------------------------------------
Vector Time (GMT): 2015/204/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3147821
10 A = 6777028
70 meter
Y = 3878204
64 meter E =
0009262
Z = -4589548
08 I = 51
27123
XDOT = -3331
698324 Wp = 61
80844
YDOT = -6225
224435 meter/sec RA = 261
59806 deg
ZDOT = -2975
565631 TA = 178
33794
MA = 178
33486
Ha = 218
717 n
mi
Hp = 213
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10327497
04 X = -3168660
03
Y = 12723768
49 feet Y = 3842887
27 meter
Z = -15057572
45 Z = -4604889
96
XDOT = -10930
768778 XDOT = -3247
384678
YDOT = -20423
964681 feet/sec YDOT = -6262
010150 meter/sec
ZDOT = -9762
354432 ZDOT = -2991
545661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16140587
94 X = 4919651
20
Y = -2453598
75 feet Y = -747856
90 meter
Z = -15124260
05 Z = -4609874
46
XDOT = -5984
393252 XDOT = -1824
043063
YDOT = 21219
276348 feet/sec YDOT = 6467
635431 meter/sec
ZDOT = -9829
919487 ZDOT = -2996
159460
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 15204
56957329
00016717 00000-0 10270-3 0 9061
2 25544 51
6433 262
3469 0001707 301
4360 58
6626 15
55261857 33709
Satellite: ISS
Catalog Number: 25544
Epoch time: 15204
56957329 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 262
3469 deg
Eccentricity:
0001707
Arg of perigee: 301
4360 deg
Mean anomaly: 58
6626 deg
Mean motion: 15
55261857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3370
Checksum: 314
Coasting Arc #8 (Orbit 3385)
---------------------------------------
Vector Time (GMT): 2015/205/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3895404
91 A = 6774137
29 meter
Y = -1792768
32 meter E =
0001517
Z = 5242886
65 I = 51
26661
XDOT = 2346
755004 Wp = 105
25529
YDOT = 7266
524255 meter/sec RA = 256
56341 deg
ZDOT = 740
552625 TA = 337
63321
MA = 337
63983
Ha = 218
593 n
mi
Hp = 213
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12780199
83 X = 3889694
74
Y = -5881785
83 feet Y = -1749239
49 meter
Z = 17201071
67 Z = 5261795
71
XDOT = 7699
327441 XDOT = 2261
727261
YDOT = 23840
302674 feet/sec YDOT = 7292
291761 meter/sec
ZDOT = 2429
634598 ZDOT = 751
746408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13381331
51 X = -4078629
85
Y = -4006687
60 feet Y = -1221238
38 meter
Z = 17282713
91 Z = 5267771
20
XDOT = 9776
140976 XDOT = 2979
767769
YDOT = -21959
760533 feet/sec YDOT = -6693
335011 meter/sec
ZDOT = 2476
439227 ZDOT = 754
818677
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 15205
59764399
00016717 00000-0 10270-3 0 9079
2 25544 51
6425 257
2128 0001702 309
8400 50
2603 15
55295777 33865
Satellite: ISS
Catalog Number: 25544
Epoch time: 15205
59764399 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 257
2128 deg
Eccentricity:
0001702
Arg of perigee: 309
8400 deg
Mean anomaly: 50
2603 deg
Mean motion: 15
55295777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3386
Checksum: 318
Coasting Arc #9 (Orbit 3400)
---------------------------------------
Vector Time (GMT): 2015/206/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4455628
86 A = 6774833
47 meter
Y = -445416
75 meter E =
0012020
Z = -5094770
95 I = 51
27830
XDOT = -1107
181249 Wp = 97
74743
YDOT = -7406
311889 meter/sec RA = 251
52512 deg
ZDOT = 1617
487161 TA = 187
94331
MA = 187
96236
Ha = 218
746 n
mi
Hp = 213
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14618204
91 X = -4425568
60
Y = -1461341
03 feet Y = -495074
16 meter
Z = -16715127
79 Z = -5116342
42
XDOT = -3632
484412 XDOT = -1032
136901
YDOT = -24298
923520 feet/sec YDOT = -7418
273605 meter/sec
ZDOT = 5306
716406 ZDOT = 1612
290597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10069938
70 X = 3069317
32
Y = 10550668
99 feet Y = 3215843
91 meter
Z = -16807815
08 Z = -5123022
04
XDOT = -12252
097798 XDOT = -3734
439409
YDOT = 20105
471042 feet/sec YDOT = 6128
147574 meter/sec
ZDOT = 5285
715190 ZDOT = 1611
085990
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 15206
56144911
00016717 00000-0 10270-3 0 9080
2 25544 51
6436 252
3996 0001829 313
8036 46
2966 15
55289742 34016
Satellite: ISS
Catalog Number: 25544
Epoch time: 15206
56144911 = yrday
fracday
Element set: 908
Inclination: 51
6436 deg
RA of node: 252
3996 deg
Eccentricity:
0001829
Arg of perigee: 313
8036 deg
Mean anomaly: 46
2966 deg
Mean motion: 15
55289742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3401
Checksum: 320
Coasting Arc #10 (Orbit 3416)
---------------------------------------
Vector Time (GMT): 2015/207/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4721283
23 A = 6778431
69 meter
Y = 2566281
73 meter E =
0009746
Z = 4126716
63 I = 51
30055
XDOT = -357
779824 Wp = 65
92141
YDOT = 6689
143831 meter/sec RA = 246
49540 deg
ZDOT = -3739
538789 TA = 62
77897
MA = 62
67968
Ha = 218
651 n
mi
Hp = 213
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15489774
36 X = 4672189
64
Y = 8419559
50 feet Y = 2618803
44 meter
Z = 13539096
56 Z = 4149532
49
XDOT = -1173
818321 XDOT = -414
387694
YDOT = 21946
009943 feet/sec YDOT = 6684
826644 meter/sec
ZDOT = -12268
828049 ZDOT = -3741
413841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6502613
37 X = -1981996
55
Y = -16305949
89 feet Y = -4970053
53 meter
Z = 13636760
80 Z = 4156484
69
XDOT = 13641
419845 XDOT = 4157
904769
YDOT = -15738
003230 feet/sec YDOT = -4796
943385 meter/sec
ZDOT = -12278
099446 ZDOT = -3742
364711
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 15207
58949418
00016717 00000-0 10270-3 0 9099
2 25544 51
6422 247
2653 0001822 321
7499 38
3525 15
55352724 34179
Satellite: ISS
Catalog Number: 25544
Epoch time: 15207
58949418 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 247
2653 deg
Eccentricity:
0001822
Arg of perigee: 321
7499 deg
Mean anomaly: 38
3525 deg
Mean motion: 15
55352724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3417
Checksum: 322
Coasting Arc #11 (Orbit 3431)
---------------------------------------
Vector Time (GMT): 2015/208/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4621161
33 A = 6782929
25 meter
Y = -4272407
22 meter E =
0005626
Z = -2524920
62 I = 51
33013
XDOT = 1956
945816 Wp = 33
53321
YDOT = -5221
300720 meter/sec RA = 241
48197 deg
ZDOT = 5263
526393 TA = 297
98360
MA = 298
04052
Ha = 218
728 n
mi
Hp = 212
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15161290
45 X = -4560777
78
Y = -14017084
06 feet Y = -4323746
25 meter
Z = -8283860
29 Z = -2547222
79
XDOT = 6420
425907 XDOT = 1989
618210
YDOT = -17130
251705 feet/sec YDOT = -5199
234606 meter/sec
ZDOT = 17268
787377 ZDOT = 5273
111710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3059157
37 X = 932431
17
Y = 20381345
71 feet Y = 6212234
17 meter
Z = -8379022
50 Z = -2553926
06
XDOT = -14132
822337 XDOT = -4307
684248
YDOT = 9224
385477 feet/sec YDOT = 2811
592693 meter/sec
ZDOT = 17310
950984 ZDOT = 5276
377860
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 15208
55327577
00016717 00000-0 10270-3 0 9105
2 25544 51
6429 242
4523 0001714 326
7088 33
3957 15
55376869 34325
Satellite: ISS
Catalog Number: 25544
Epoch time: 15208
55327577 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 242
4523 deg
Eccentricity:
0001714
Arg of perigee: 326
7088 deg
Mean anomaly: 33
3957 deg
Mean motion: 15
55376869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3432
Checksum: 324
Coasting Arc #12 (Orbit 3447)
---------------------------------------
Vector Time (GMT): 2015/209/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4053108
37 A = 6785629
39 meter
Y = 5413915
34 meter E =
0011330
Z = 487165
10 I = 51
35330
XDOT = -3583
108392 Wp = 126
29108
YDOT = 3227
332357 meter/sec RA = 236
48184 deg
ZDOT = -5964
563099 TA = 48
43064
MA = 48
33356
Ha = 218
845 n
mi
Hp = 212
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13297599
64 X = 3989900
99
Y = 17762189
43 feet Y = 5458886
40 meter
Z = 1598310
70 Z = 506701
00
XDOT = -11755
604959 XDOT = -3589
957654
YDOT = 10588
360750 feet/sec YDOT = 3187
225894 meter/sec
ZDOT = -19568
776571 ZDOT = -5981
985288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 318894
66 X = 97199
09
Y = -22179886
57 feet Y = -6760429
43 meter
Z = 1681387
72 Z = 512486
98
XDOT = 14057
266545 XDOT = 4284
654843
YDOT = -1308
439723 feet/sec YDOT = -398
812428 meter/sec
ZDOT = -19644
294634 ZDOT = -5987
581004
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 15209
58129631
00016717 00000-0 10270-3 0 9111
2 25544 51
6413 237
3173 0001807 331
7758 28
3297 15
55363829 34485
Satellite: ISS
Catalog Number: 25544
Epoch time: 15209
58129631 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 237
3173 deg
Eccentricity:
0001807
Arg of perigee: 331
7758 deg
Mean anomaly: 28
3297 deg
Mean motion: 15
55363829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3448
Checksum: 320
Coasting Arc #13 (Orbit 3463)
---------------------------------------
Vector Time (GMT): 2015/210/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3017712
23 A = 6784557
55 meter
Y = -5851956
28 meter E =
0014028
Z = 1605056
74 I = 51
36796
XDOT = 5023
680311 Wp = 55
46023
YDOT = -1016
678892 meter/sec RA = 231
48644 deg
ZDOT = 5710
570209 TA = 322
18864
MA = 322
28710
Ha = 218
778 n
mi
Hp = 212
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9900630
68 X = -2959846
60
Y = -19199331
63 feet Y = -5885378
90 meter
Z = 5265934
17 Z = 1590537
61
XDOT = 16481
890783 XDOT = 5006
936350
YDOT = -3335
560669 feet/sec YDOT = -960
594873 meter/sec
ZDOT = 18735
466564 ZDOT = 5734
933114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3485226
09 X = -1062296
91
Y = 21333853
07 feet Y = 6502558
42 meter
Z = 5204497
83 Z = 1586330
94
XDOT = -13563
303237 XDOT = -4134
094827
YDOT = -6834
543922 feet/sec YDOT = -2083
168987 meter/sec
ZDOT = 18840
459951 ZDOT = 5742
572193
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 15210
60930226
00016717 00000-0 10270-3 0 9127
2 25544 51
6409 232
1832 0001883 332
3414 27
7639 15
55404777 34644
Satellite: ISS
Catalog Number: 25544
Epoch time: 15210
60930226 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 232
1832 deg
Eccentricity:
0001883
Arg of perigee: 332
3414 deg
Mean anomaly: 27
7639 deg
Mean motion: 15
55404777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3464
Checksum: 295
Coasting Arc #14 (Orbit 3478)
---------------------------------------
Vector Time (GMT): 2015/211/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1515039
81 A = 6780565
69 meter
Y = 5626240
89 meter E =
0004708
Z = -3473558
75 I = 51
37392
XDOT = -6078
709975 Wp = 65
21770
YDOT = -1153
522456 meter/sec RA = 226
48191 deg
ZDOT = -4522
608169 TA = 155
73612
MA = 155
71394
Ha = 218
879 n
mi
Hp = 212
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4970603
05 X = 1468886
13
Y = 18458795
57 feet Y = 5642925
22 meter
Z = -11396190
11 Z = -3466310
87
XDOT = -19943
274196 XDOT = -6043
390548
YDOT = -3784
522494 feet/sec YDOT = -1221
300810 meter/sec
ZDOT = -14837
953309 ZDOT = -4552
051040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6660011
20 X = 2029971
41
Y = -17937833
97 feet Y = -5467451
79 meter
Z = -11365981
75 Z = -3464351
24
XDOT = 12613
742669 XDOT = 3844
668765
YDOT = 14159
172741 feet/sec YDOT = 4315
715851 meter/sec
ZDOT = -14964
438285 ZDOT = -4561
160789
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 15211
57304764
00016717 00000-0 10270-3 0 9137
2 25544 51
6398 227
3685 0001934 338
2565 21
8506 15
55391976 34792
Satellite: ISS
Catalog Number: 25544
Epoch time: 15211
57304764 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 227
3685 deg
Eccentricity:
0001934
Arg of perigee: 338
2565 deg
Mean anomaly: 21
8506 deg
Mean motion: 15
55391976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3479
Checksum: 333
Coasting Arc #15 (Orbit 3494)
---------------------------------------
Vector Time (GMT): 2015/212/13:09:20
031
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 303309
28 A = 6775927
65 meter
Y = -4807351
50 meter E =
0006194
Z = 4761082
19 I = 51
38066
XDOT = 6557
585480 Wp = 105
52992
YDOT = 3007
331467 meter/sec RA = 221
46355 deg
ZDOT = 2614
330341 TA = 318
59357
MA = 318
64050
Ha = 218
838 n
mi
Hp = 212
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 995109
19 X = 333916
68
Y = -15772150
60 feet Y = -4803788
76 meter
Z = 15620348
40 Z = 4762629
71
XDOT = 21514
388057 XDOT = 6510
770260
YDOT = 9866
573056 feet/sec YDOT = 3080
400823 meter/sec
ZDOT = 8577
199280 ZDOT = 2646
071503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9706617
48 X = -2958577
01
Y = 12461889
08 feet Y = 3798383
79 meter
Z = 15627832
81 Z = 4763363
44
XDOT = -11128
905325 XDOT = -3392
090343
YDOT = -19613
613750 feet/sec YDOT = -5978
229471 meter/sec
ZDOT = 8713
273545 ZDOT = 2655
805776
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 15212
60102860
00016717 00000-0 10270-3 0 9146
2 25544 51
6392 222
2332 0002073 341
1191 18
9885 15
55419467 34953
Satellite: ISS
Catalog Number: 25544
Epoch time: 15212
60102860 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 222
2332 deg
Eccentricity:
0002073
Arg of perigee: 341
1191 deg
Mean anomaly: 18
9885 deg
Mean motion: 15
55419467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3495
Checksum: 293
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