[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 28th 2016
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) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 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 2299)
---------------------------------------
Vector Time (GMT): 2016/027/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4521058
54 A = 6788596
48 meter
Y = -4991415
74 meter E =
0011654
Z = -845770
23 I = 51
91307
XDOT = 4027
677066 Wp = 107
34807
YDOT = -2650
749261 meter/sec RA = 42
18221 deg
ZDOT = -5957
123790 TA = 81
76118
MA = 81
62903
Ha = 222
842 n
mi
Hp = 212
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14832869
23 X = -4460798
98
Y = -16376035
89 feet Y = -5041636
32 meter
Z = -2774836
70 Z = -867585
41
XDOT = 13214
163602 XDOT = 4085
955650
YDOT = -8696
683928 feet/sec YDOT = -2605
383509 meter/sec
ZDOT = -19544
369389 ZDOT = -5937
417051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19397100
22 X = -5912236
15
Y = 10555223
75 feet Y = 3217232
20 meter
Z = -2868455
04 Z = -874305
10
XDOT = -4553
375013 XDOT = -1387
868704
YDOT = -13594
407270 feet/sec YDOT = -4143
575336 meter/sec
ZDOT = -19458
356173 ZDOT = -5930
906962
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 16027
89356426
00016717 00000-0 10270-3 0 9006
2 25544 51
6437 42
6561 0006367 47
9724 312
1970 15
54266964 23003
Satellite: ISS
Catalog Number: 25544
Epoch time: 16027
89356426 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 42
6561 deg
Eccentricity:
0006367
Arg of perigee: 47
9724 deg
Mean anomaly: 312
1970 deg
Mean motion: 15
54266964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2300
Checksum: 313
Coasting Arc #2 (Orbit 2315)
---------------------------------------
Vector Time (GMT): 2016/028/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3572485
42 A = 6786114
10 meter
Y = 5183380
13 meter E =
0019814
Z = 2505889
98 I = 51
88077
XDOT = -5408
220979 Wp = 67
07799
YDOT = 1139
908277 meter/sec RA = 37
22461 deg
ZDOT = 5326
414885 TA = 320
96249
MA = 321
10532
Ha = 222
876 n
mi
Hp = 212
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11720752
68 X = 3502085
73
Y = 17005840
32 feet Y = 5222936
52 meter
Z = 8221423
81 Z = 2523072
70
XDOT = -17743
507150 XDOT = -5446
438782
YDOT = 3739
856551 feet/sec YDOT = 1079
216532 meter/sec
ZDOT = 17475
114451 ZDOT = 5300
050644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19141583
22 X = 5834354
57
Y = -7678596
64 feet Y = -2340436
26 meter
Z = 8294902
26 Z = 2528286
21
XDOT = -801
945273 XDOT = -244
432919
YDOT = 16845
651212 feet/sec YDOT = 5134
554489 meter/sec
ZDOT = 17360
533583 ZDOT = 5291
490636
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 16028
92227879
00016717 00000-0 10270-3 0 9011
2 25544 51
6437 37
5258 0006586 50
0830 310
0901 15
54302988 23160
Satellite: ISS
Catalog Number: 25544
Epoch time: 16028
92227879 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 37
5258 deg
Eccentricity:
0006586
Arg of perigee: 50
0830 deg
Mean anomaly: 310
0901 deg
Mean motion: 15
54302988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2316
Checksum: 305
Coasting Arc #3 (Orbit 2330)
---------------------------------------
Vector Time (GMT): 2016/029/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2230931
67 A = 6782180
04 meter
Y = -5064427
17 meter E =
0012859
Z = -3935289
36 I = 51
84161
XDOT = 6477
832814 Wp = 63
04655
YDOT = 306
000249 meter/sec RA = 32
25658 deg
ZDOT = -4070
675164 TA = 164
43149
MA = 164
39190
Ha = 222
834 n
mi
Hp = 212
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7319329
63 X = -2155018
51
Y = -16615574
71 feet Y = -5088950
66 meter
Z = -12911054
33 Z = -3945941
90
XDOT = 21252
732331 XDOT = 6493
702923
YDOT = 1003
937824 feet/sec YDOT = 378
528212 meter/sec
ZDOT = -13355
233477 ZDOT = -4039
169364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17733046
67 X = -5405032
62
Y = 3744393
38 feet Y = 1141291
10 meter
Z = -12956226
58 Z = -3949057
86
XDOT = 5549
217760 XDOT = 1691
401573
YDOT = -19406
596388 feet/sec YDOT = -5915
130579 meter/sec
ZDOT = -13218
652437 ZDOT = -4029
045263
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 16029
88668872
00016717 00000-0 10270-3 0 9020
2 25544 51
6435 32
7164 0006382 53
2039 306
9699 15
54318001 23319
Satellite: ISS
Catalog Number: 25544
Epoch time: 16029
88668872 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 32
7164 deg
Eccentricity:
0006382
Arg of perigee: 53
2039 deg
Mean anomaly: 306
9699 deg
Mean motion: 15
54318001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2331
Checksum: 313
Coasting Arc #4 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2016/030/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 619289
84 A = 6778574
49 meter
Y = 4645930
60 meter E =
0011308
Z = 4887230
60 I = 51
80222
XDOT = -7127
020990 Wp = 89
35620
YDOT = -1563
466220 meter/sec RA = 27
27547 deg
ZDOT = 2384
749359 TA = 337
33382
MA = 337
38372
Ha = 222
948 n
mi
Hp = 212
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2031790
83 X = 543552
08
Y = 15242554
47 feet Y = 4652432
64 meter
Z = 16034221
14 Z = 4890054
77
XDOT = -23382
614798 XDOT = -7120
592188
YDOT = -5129
482349 feet/sec YDOT = -1643
129245 meter/sec
ZDOT = 7823
980835 ZDOT = 2350
144145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15338341
28 X = 4675126
42
Y = 914559
24 feet Y = 278757
66 meter
Z = 16045521
38 Z = 4890674
92
XDOT = -9294
078185 XDOT = -2832
835031
YDOT = 20966
692232 feet/sec YDOT = 6390
647792 meter/sec
ZDOT = 7674
222647 ZDOT = 2339
103063
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 16030
91538448
00016717 00000-0 10270-3 0 9032
2 25544 51
6436 27
5862 0006582 57
5674 302
6115 15
54327288 23471
Satellite: ISS
Catalog Number: 25544
Epoch time: 16030
91538448 = yrday
fracday
Element set: 903
Inclination: 51
6436 deg
RA of node: 27
5862 deg
Eccentricity:
0006582
Arg of perigee: 57
5674 deg
Mean anomaly: 302
6115 deg
Mean motion: 15
54327288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 317
Coasting Arc #5 (Orbit 2361)
---------------------------------------
Vector Time (GMT): 2016/031/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1158319
85 A = 6776688
79 meter
Y = -4056320
26 meter E =
0020790
Z = -5321429
29 I = 51
76637
XDOT = 7188
269277 Wp = 78
63982
YDOT = 2595
584651 meter/sec RA = 22
28355 deg
ZDOT = -411
209047 TA = 187
42268
MA = 187
45350
Ha = 222
850 n
mi
Hp = 212
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3800261
97 X = 1229441
49
Y = -13308137
34 feet Y = -4042969
68 meter
Z = -17458757
53 Z = -5315629
64
XDOT = 23583
560620 XDOT = 7160
708020
YDOT = 8515
697674 feet/sec YDOT = 2675
814522 meter/sec
ZDOT = -1349
111045 ZDOT = -376
357612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12466887
75 X = -3799907
39
Y = -6085372
91 feet Y = -1854821
66 meter
Z = -17432775
77 Z = -5313510
06
XDOT = 11901
431773 XDOT = 3627
556404
YDOT = -20923
938239 feet/sec YDOT = -6377
616375 meter/sec
ZDOT = -1198
505858 ZDOT = -365
304586
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 16031
87977526
00016717 00000-0 10270-3 0 9043
2 25544 51
6426 22
7760 0006473 60
3785 299
8012 15
54374899 23628
Satellite: ISS
Catalog Number: 25544
Epoch time: 16031
87977526 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 22
7760 deg
Eccentricity:
0006473
Arg of perigee: 60
3785 deg
Mean anomaly: 299
8012 deg
Mean motion: 15
54374899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2362
Checksum: 335
Coasting Arc #6 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2016/032/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2939027
84 A = 6777499
14 meter
Y = 3315452
84 meter E =
0011438
Z = 5121653
19 I = 51
73950
XDOT = -6681
318964 Wp = 59
61605
YDOT = -3414
037515 meter/sec RA = 17
28899 deg
ZDOT = -1615
647178 TA = 45
98183
MA = 45
88763
Ha = 222
935 n
mi
Hp = 212
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9642479
79 X = -3000762
16
Y = 10877469
95 feet Y = 3282241
63 meter
Z = 16803324
11 Z = 5107226
24
XDOT = -21920
337807 XDOT = -6634
797743
YDOT = -11200
910483 feet/sec YDOT = -3488
492374 meter/sec
ZDOT = -5300
679717 ZDOT = -1647
989964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9288402
89 X = 2831105
20
Y = 11275802
38 feet Y = 3436864
57 meter
Z = 16740081
31 Z = 5102376
78
XDOT = -13544
186085 XDOT = -4128
267919
YDOT = 19274
330331 feet/sec YDOT = 5874
815885 meter/sec
ZDOT = -5440
228939 ZDOT = -1658
181781
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 16032
90844949
00016717 00000-0 10270-3 0 9051
2 25544 51
6429 17
6461 0006399 64
2569 295
9244 15
54388656 23789
Satellite: ISS
Catalog Number: 25544
Epoch time: 16032
90844949 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 17
6461 deg
Eccentricity:
0006399
Arg of perigee: 64
2569 deg
Mean anomaly: 295
9244 deg
Mean motion: 15
54388656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 354
Coasting Arc #7 (Orbit 2392)
---------------------------------------
Vector Time (GMT): 2016/033/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4528887
54 A = 6780568
40 meter
Y = -2543542
08 meter E =
0014078
Z = -4370875
18 I = 51
71759
XDOT = 5555
420748 Wp = 92
13346
YDOT = 3991
705411 meter/sec RA = 12
29680 deg
ZDOT = 3442
434865 TA = 212
75836
MA = 212
84573
Ha = 222
877 n
mi
Hp = 212
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14858554
92 X = 4578225
06
Y = -8344954
34 feet Y = -2492621
26 meter
Z = -14340141
68 Z = -4348755
35
XDOT = 18226
446024 XDOT = 5493
649935
YDOT = 13096
146362 feet/sec YDOT = 4053
484468 meter/sec
ZDOT = 11294
077642 ZDOT = 3469
271341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6277120
19 X = -1913266
24
Y = -15930139
42 feet Y = -4855506
50 meter
Z = -14243700
38 Z = -4341479
88
XDOT = 14240
377125 XDOT = 4340
466948
YDOT = -15786
242795 feet/sec YDOT = -4811
646804 meter/sec
ZDOT = 11409
623426 ZDOT = 3477
653220
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 16033
87282248
00016717 00000-0 10270-3 0 9067
2 25544 51
6416 12
8354 0006416 68
1438 292
0397 15
54397704 23939
Satellite: ISS
Catalog Number: 25544
Epoch time: 16033
87282248 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 12
8354 deg
Eccentricity:
0006416
Arg of perigee: 68
1438 deg
Mean anomaly: 292
0397 deg
Mean motion: 15
54397704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2393
Checksum: 320
Coasting Arc #8 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2016/034/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5795886
19 A = 6784487
01 meter
Y = 1702817
13 meter E =
0018994
Z = 3072908
50 I = 51
70012
XDOT = -3913
175336 Wp = 87
39393
YDOT = -4411
186620 meter/sec RA = 7
31408 deg
ZDOT = -4909
299009 TA = 57
31429
MA = 57
13124
Ha = 222
828 n
mi
Hp = 211
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19015374
63 X = -5829423
42
Y = 5586670
36 feet Y = 1637816
18 meter
Z = 10081720
79 Z = 3044672
43
XDOT = -12838
501758 XDOT = -3839
710570
YDOT = -14472
397047 feet/sec YDOT = -4454
535585 meter/sec
ZDOT = -16106
624046 ZDOT = -4928
129546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3329832
14 X = 1014932
84
Y = 19600211
43 feet Y = 5974144
44 meter
Z = 9958934
77 Z = 3035483
32
XDOT = -14427
959915 XDOT = -4397
642182
YDOT = 10721
593763 feet/sec YDOT = 3267
941779 meter/sec
ZDOT = -16187
363526 ZDOT = -4933
908403
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 16034
90147477
00016717 00000-0 10270-3 0 9077
2 25544 51
6420 7
7049 0006344 70
3125 289
8711 15
54450337 24090
Satellite: ISS
Catalog Number: 25544
Epoch time: 16034
90147477 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 7
7049 deg
Eccentricity:
0006344
Arg of perigee: 70
3125 deg
Mean anomaly: 289
8711 deg
Mean motion: 15
54450337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2409
Checksum: 301
Coasting Arc #9 (Orbit 2423)
---------------------------------------
Vector Time (GMT): 2016/035/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6562999
98 A = 6787625
96 meter
Y = -893287
93 meter E =
0014088
Z = -1468061
26 I = 51
67708
XDOT = 1916
727657 Wp = 53
43180
YDOT = 4653
643151 meter/sec RA = 2
33870 deg
ZDOT = 5783
830573 TA = 290
55703
MA = 290
70813
Ha = 222
893 n
mi
Hp = 211
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21532152
18 X = 6579632
27
Y = -2930734
68 feet Y = -819803
12 meter
Z = -4816473
93 Z = -1436139
96
XDOT = 6288
476565 XDOT = 1836
452108
YDOT = 15267
858108 feet/sec YDOT = 4674
628414 meter/sec
ZDOT = 18975
822089 ZDOT = 5792
946438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -776766
08 X = -236758
30
Y = -21747075
33 feet Y = -6628508
56 meter
Z = -4677879
17 Z = -1425817
57
XDOT = 14220
396604 XDOT = 4334
376885
YDOT = -4564
051225 feet/sec YDOT = -1391
122813 meter/sec
ZDOT = 19014
386688 ZDOT = 5795
585063
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 16035
86582902
00016717 00000-0 10270-3 0 9080
2 25544 51
6406 2
8941 0006378 75
8762 284
3099 15
54415918 24247
Satellite: ISS
Catalog Number: 25544
Epoch time: 16035
86582902 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 2
8941 deg
Eccentricity:
0006378
Arg of perigee: 75
8762 deg
Mean anomaly: 284
3099 deg
Mean motion: 15
54415918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2424
Checksum: 331
Coasting Arc #10 (Orbit 2439)
---------------------------------------
Vector Time (GMT): 2016/036/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6774097
79 A = 6788278
28 meter
Y = 18289
66 meter E =
0015576
Z = -370016
73 I = 51
64805
XDOT = 303
763930 Wp = 116
47316
YDOT = -4765
478884 meter/sec RA = 357
36830 deg
ZDOT = -5998
928278 TA = 67
51488
MA = 67
35004
Ha = 222
797 n
mi
Hp = 211
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22224730
27 X = -6772001
50
Y = 60005
46 feet Y = -57451
06 meter
Z = -1213965
65 Z = -402917
86
XDOT = 996
600821 XDOT = 386
169753
YDOT = -15634
773241 feet/sec YDOT = -4761
621255 meter/sec
ZDOT = -19681
523223 ZDOT = -5997
252533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1764550
48 X = -537834
99
Y = 22146373
95 feet Y = 6750214
78 meter
Z = -1356624
95 Z = -413499
29
XDOT = -13876
644377 XDOT = -4229
601206
YDOT = -2274
411060 feet/sec YDOT = -693
240491 meter/sec
ZDOT = -19673
274571 ZDOT = -5996
414089
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 16036
89446093
00016717 00000-0 10270-3 0 9095
2 25544 51
6408 357
7633 0006467 78
7660 281
4219 15
54464216 24402
Satellite: ISS
Catalog Number: 25544
Epoch time: 16036
89446093 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 357
7633 deg
Eccentricity:
0006467
Arg of perigee: 78
7660 deg
Mean anomaly: 281
4219 deg
Mean motion: 15
54464216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2440
Checksum: 331
Coasting Arc #11 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2016/037/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6387417
66 A = 6786408
52 meter
Y = 832418
33 meter E =
0020205
Z = 2108571
46 I = 51
60919
XDOT = -2451
288068 Wp = 74
39794
YDOT = 4737
274547 meter/sec RA = 352
39264 deg
ZDOT = 5516
734703 TA = 308
98768
MA = 309
16747
Ha = 222
781 n
mi
Hp = 211
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20956094
67 X = 6367392
33
Y = 2731031
25 feet Y = 903734
73 meter
Z = 6917885
38 Z = 2139550
57
XDOT = -8042
283688 XDOT = -2530
876564
YDOT = 15542
239327 feet/sec YDOT = 4709
417706 meter/sec
ZDOT = 18099
523304 ZDOT = 5504
633848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4084225
99 X = 1244872
08
Y = -20689647
23 feet Y = -6306204
47 meter
Z = 7052032
99 Z = 2149459
66
XDOT = 13472
431458 XDOT = 4106
397108
YDOT = 8852
935933 feet/sec YDOT = 2698
374872 meter/sec
ZDOT = 18046
083658 ZDOT = 5500
446299
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 16037
92308259
00016717 00000-0 10270-3 0 9103
2 25544 51
6401 352
6316 0006435 84
8476 275
3411 15
54461112 24560
Satellite: ISS
Catalog Number: 25544
Epoch time: 16037
92308259 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 352
6316 deg
Eccentricity:
0006435
Arg of perigee: 84
8476 deg
Mean anomaly: 275
3411 deg
Mean motion: 15
54461112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 297
Coasting Arc #12 (Orbit 2470)
---------------------------------------
Vector Time (GMT): 2016/038/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5442597
14 A = 6782515
29 meter
Y = -1758068
22 meter E =
0012227
Z = -3657328
99 I = 51
56530
XDOT = 4382
334098 Wp = 83
41481
YDOT = -4523
022810 meter/sec RA = 347
40724 deg
ZDOT = -4358
472910 TA = 140
03726
MA = 139
94720
Ha = 222
828 n
mi
Hp = 211
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17856289
83 X = -5404768
20
Y = -5767940
34 feet Y = -1818719
56 meter
Z = -11999110
85 Z = -3683675
15
XDOT = 14377
736543 XDOT = 4453
757007
YDOT = -14839
313680 feet/sec YDOT = -4473
617454 meter/sec
ZDOT = -14299
451806 ZDOT = -4337
011528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6611966
73 X = -2015327
46
Y = 17482920
48 feet Y = 5328794
16 meter
Z = -12112979
43 Z = -3692036
13
XDOT = -12857
432720 XDOT = -3918
945493
YDOT = -14679
678148 feet/sec YDOT = -4474
365900 meter/sec
ZDOT = -14205
479485 ZDOT = -4329
830147
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 16038
88740536
00016717 00000-0 10270-3 0 9118
2 25544 51
6404 347
8215 0006606 87
7625 272
4284 15
54486124 24718
Satellite: ISS
Catalog Number: 25544
Epoch time: 16038
88740536 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 347
8215 deg
Eccentricity:
0006606
Arg of perigee: 87
7625 deg
Mean anomaly: 272
4284 deg
Mean motion: 15
54486124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2471
Checksum: 320
Coasting Arc #13 (Orbit 2486)
---------------------------------------
Vector Time (GMT): 2016/039/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4055883
45 A = 6778673
18 meter
Y = 2656173
59 meter E =
0013719
Z = 4727805
28 I = 51
52112
XDOT = -5876
747748 Wp = 105
71734
YDOT = 4125
858214 meter/sec RA = 342
40739 deg
ZDOT = 2713
346864 TA = 317
38683
MA = 317
49319
Ha = 222
695 n
mi
Hp = 211
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13306704
25 X = 4002914
97
Y = 8714480
29 feet Y = 2701233
28 meter
Z = 15511172
16 Z = 4747378
43
XDOT = -19280
668464 XDOT = -5935
627280
YDOT = 13536
280230 feet/sec YDOT = 4059
811467 meter/sec
ZDOT = 8902
056642 ZDOT = 2684
656579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9115864
31 X = 2778515
44
Y = -12934011
14 feet Y = -3942286
59 meter
Z = 15595492
30 Z = 4753506
05
XDOT = 11996
001144 XDOT = 3656
381149
YDOT = 19077
774965 feet/sec YDOT = 5814
905809 meter/sec
ZDOT = 8776
835000 ZDOT = 2675
179308
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 16039
91600519
00016717 00000-0 10270-3 0 9120
2 25544 51
6402 342
6901 0006468 92
3402 267
8491 15
54487876 24872
Satellite: ISS
Catalog Number: 25544
Epoch time: 16039
91600519 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 342
6901 deg
Eccentricity:
0006468
Arg of perigee: 92
3402 deg
Mean anomaly: 267
8491 deg
Mean motion: 15
54487876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2487
Checksum: 326
Coasting Arc #14 (Orbit 2501)
---------------------------------------
Vector Time (GMT): 2016/040/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2363172
34 A = 6776396
56 meter
Y = -3563944
24 meter E =
0021247
Z = -5275212
93 I = 51
48419
XDOT = 6795
301792 Wp = 88
08553
YDOT = -3447
200659 meter/sec RA = 337
39677 deg
ZDOT = -717
011855 TA = 175
04809
MA = 175
02705
Ha = 222
842 n
mi
Hp = 211
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7753190
09 X = -2297519
69
Y = -11692730
44 feet Y = -3590004
12 meter
Z = -17307129
05 Z = -5286532
63
XDOT = 22294
297218 XDOT = 6836
827057
YDOT = -11309
713449 feet/sec YDOT = -3370
978963 meter/sec
ZDOT = -2352
401100 ZDOT = -683
901643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11795631
37 X = -3595308
44
Y = 7484572
20 feet Y = 2281297
61 meter
Z = -17355485
51 Z = -5289951
98
XDOT = -10464
290421 XDOT = -3189
515720
YDOT = -21598
285276 feet/sec YDOT = -6583
157352 meter/sec
ZDOT = -2208
168083 ZDOT = -673
049632
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 16040
88030784
00016717 00000-0 10270-3 0 9130
2 25544 51
6410 337
8806 0006704 96
7621 263
4295 15
54511630 25023
Satellite: ISS
Catalog Number: 25544
Epoch time: 16040
88030784 = yrday
fracday
Element set: 913
Inclination: 51
6410 deg
RA of node: 337
8806 deg
Eccentricity:
0006704
Arg of perigee: 96
7621 deg
Mean anomaly: 263
4295 deg
Mean motion: 15
54511630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2502
Checksum: 297
Coasting Arc #15 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2016/041/20:42:47
442
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 543162
42 A = 6776973
42 meter
Y = 4352880
74 meter E =
0010366
Z = 5157121
39 I = 51
45588
XDOT = -7127
427346 Wp = 82
13698
YDOT = 2505
851854 meter/sec RA = 332
38000 deg
ZDOT = -1360
652539 TA = 20
98241
MA = 20
93990
Ha = 222
868 n
mi
Hp = 211
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1782028
95 X = 469396
50
Y = 14281104
79 feet Y = 4358542
77 meter
Z = 16919689
61 Z = 5159580
32
XDOT = -23383
947985 XDOT = -7148
309349
YDOT = 8221
298732 feet/sec YDOT = 2426
031351 meter/sec
ZDOT = -4464
083134 ZDOT = -1395
326035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14276176
17 X = 4351378
50
Y = -1727709
97 feet Y = -526606
00 meter
Z = 16929479
91 Z = 5160105
48
XDOT = 8183
739425 XDOT = 2494
403777
YDOT = 22282
301905 feet/sec YDOT = 6791
645621 meter/sec
ZDOT = -4614
890451 ZDOT = -1406
618609
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 16041
90888704
00016717 00000-0 10270-3 0 9148
2 25544 51
6403 332
7489 0006719 100
7051 259
4859 15
54479938 25187
Satellite: ISS
Catalog Number: 25544
Epoch time: 16041
90888704 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 332
7489 deg
Eccentricity:
0006719
Arg of perigee: 100
7051 deg
Mean anomaly: 259
4859 deg
Mean motion: 15
54479938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2518
Checksum: 339
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list