[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 24th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1552 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 ET - UTC (sec) : 68 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 3411)
---------------------------------------
Vector Time (GMT): 2016/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5240598
68 A = 6788422
27 meter
Y = -3857804
43 meter E =
0017473
Z = 1894565
79 I = 51
50436
XDOT = 4269
475164 Wp = 45
16862
YDOT = -3035
531224 meter/sec RA = 202
97007 deg
ZDOT = 5609
126785 TA = 335
75726
MA = 335
83938
Ha = 222
495 n
mi
Hp = 214
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17193565
21 X = -5206273
17
Y = -12656838
69 feet Y = -3916216
48 meter
Z = 6215767
03 Z = 1869191
61
XDOT = 14007
464448 XDOT = 4275
855336
YDOT = -9959
091943 feet/sec YDOT = -2987
751617 meter/sec
ZDOT = 18402
646933 ZDOT = 5629
882121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12767154
76 X = 3891428
77
Y = -17151577
88 feet Y = -5227800
94 meter
Z = 6105173
69 Z = 1860856
94
XDOT = 8616
901347 XDOT = 2626
431531
YDOT = 13020
621728 feet/sec YDOT = 3968
685503 meter/sec
ZDOT = 18494
122062 ZDOT = 5637
008404
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 16356
56065695
00016717 00000-0 10270-3 0 9000
2 25544 51
6402 203
7787 0006855 356
1102 3
9996 15
53937329 34129
Satellite: ISS
Catalog Number: 25544
Epoch time: 16356
56065695 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 203
7787 deg
Eccentricity:
0006855
Arg of perigee: 356
1102 deg
Mean anomaly: 3
9996 deg
Mean motion: 15
53937329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3412
Checksum: 323
Coasting Arc #2 (Orbit 3426)
---------------------------------------
Vector Time (GMT): 2016/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213679
20 A = 6785327
25 meter
Y = 4153207
48 meter E =
0007956
Z = -3333112
81 I = 51
52260
XDOT = -5713
472648 Wp = 35
98945
YDOT = 2047
915527 meter/sec RA = 197
98598 deg
ZDOT = -4670
490698 TA = 182
83820
MA = 182
84272
Ha = 222
628 n
mi
Hp = 214
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13824406
84 X = 4183114
59
Y = 13626008
80 feet Y = 4200156
92 meter
Z = -10935409
48 Z = -3312717
91
XDOT = -18744
989003 XDOT = -5713
261146
YDOT = 6718
882961 feet/sec YDOT = 1984
025017 meter/sec
ZDOT = -15323
132212 ZDOT = -4698
244659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13474809
61 X = -4107121
97
Y = 14040818
96 feet Y = 4279641
62 meter
Z = -10846678
28 Z = -3306067
54
XDOT = -5893
682419 XDOT = -1796
394401
YDOT = -17589
197276 feet/sec YDOT = -5361
187330 meter/sec
ZDOT = -15445
135475 ZDOT = -4707
677293
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 16357
52532308
00016717 00000-0 10270-3 0 9018
2 25544 51
6388 198
9720 0006891 359
8290
2859 15
53913695 34276
Satellite: ISS
Catalog Number: 25544
Epoch time: 16357
52532308 = yrday
fracday
Element set: 901
Inclination: 51
6388 deg
RA of node: 198
9720 deg
Eccentricity:
0006891
Arg of perigee: 359
8290 deg
Mean anomaly:
2859 deg
Mean motion: 15
53913695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3427
Checksum: 338
Coasting Arc #3 (Orbit 3442)
---------------------------------------
Vector Time (GMT): 2016/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2839899
07 A = 6781736
32 meter
Y = -4266883
05 meter E =
0009876
Z = 4430761
83 I = 51
54172
XDOT = 6835
640304 Wp = 68
12457
YDOT = -1116
049212 meter/sec RA = 192
99327 deg
ZDOT = 3304
229936 TA = 348
50645
MA = 348
52898
Ha = 222
818 n
mi
Hp = 214
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9317254
17 X = -2813497
34
Y = -13998960
13 feet Y = -4298493
32 meter
Z = 14536620
18 Z = 4417030
22
XDOT = 22426
641416 XDOT = 6831
561698
YDOT = -3661
578781 feet/sec YDOT = -1039
631465 meter/sec
ZDOT = 10840
649397 ZDOT = 3337
425783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13729090
13 X = 4184626
67
Y = -9799020
27 feet Y = -2986741
38 meter
Z = 14477110
28 Z = 4412623
21
XDOT = 3569
455193 XDOT = 1087
969943
YDOT = 21243
586896 feet/sec YDOT = 6475
045286 meter/sec
ZDOT = 10986
373893 ZDOT = 3348
646763
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 16358
55429836
00016717 00000-0 10270-3 0 9024
2 25544 51
6391 193
8433 0006957 3
2809 356
8388 15
53894450 34436
Satellite: ISS
Catalog Number: 25544
Epoch time: 16358
55429836 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 193
8433 deg
Eccentricity:
0006957
Arg of perigee: 3
2809 deg
Mean anomaly: 356
8388 deg
Mean motion: 15
53894450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3443
Checksum: 344
Coasting Arc #4 (Orbit 3457)
---------------------------------------
Vector Time (GMT): 2016/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1240722
17 A = 6778872
90 meter
Y = 4279958
46 meter E =
0017113
Z = -5122969
28 I = 51
56287
XDOT = -7481
243669 Wp = 55
79168
YDOT = 237
804203 meter/sec RA = 187
99394 deg
ZDOT = -1607
640918 TA = 198
62633
MA = 198
68904
Ha = 222
834 n
mi
Hp = 214
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4070610
79 X = 1217655
53
Y = 14041858
46 feet Y = 4293704
41 meter
Z = -16807642
01 Z = -5116997
91
XDOT = -24544
762695 XDOT = -7475
537609
YDOT = 780
197515 feet/sec YDOT = 154
175914 meter/sec
ZDOT = -5274
412460 ZDOT = -1643
969054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13837315
76 X = -4217613
84
Y = 4809206
30 feet Y = 1465846
08 meter
Z = -16782154
76 Z = -5115200
77
XDOT = -1534
636634 XDOT = -467
757246
YDOT = -23440
781617 feet/sec YDOT = -7144
750237 meter/sec
ZDOT = -5433
747204 ZDOT = -1656
206148
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 16359
51895847
00016717 00000-0 10270-3 0 9031
2 25544 51
6378 189
0353 0006890 8
0428 352
0834 15
53922701 34586
Satellite: ISS
Catalog Number: 25544
Epoch time: 16359
51895847 = yrday
fracday
Element set: 903
Inclination: 51
6378 deg
RA of node: 189
0353 deg
Eccentricity:
0006890
Arg of perigee: 8
0428 deg
Mean anomaly: 352
0834 deg
Mean motion: 15
53922701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3458
Checksum: 331
Coasting Arc #5 (Orbit 3473)
---------------------------------------
Vector Time (GMT): 2016/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 501906
26 A = 6778051
65 meter
Y = -4185285
20 meter E =
0008072
Z = 5304763
34 I = 51
59154
XDOT = 7644
253300 Wp = 28
72878
YDOT = 595
300020 meter/sec RA = 182
99241 deg
ZDOT = -246
497249 TA = 63
66277
MA = 63
57989
Ha = 222
922 n
mi
Hp = 214
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1646674
10 X = 522901
66
Y = -13731250
67 feet Y = -4179555
57 meter
Z = 17404079
21 Z = 5307252
15
XDOT = 25079
571194 XDOT = 7638
225741
YDOT = 1953
084055 feet/sec YDOT = 680
749517 meter/sec
ZDOT = -808
718009 ZDOT = -209
377991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13798525
91 X = 4205790
70
Y = 675026
87 feet Y = 205748
19 meter
Z = 17415676
13 Z = 5308298
08
XDOT = -336
774421 XDOT = -102
648844
YDOT = 24151
043204 feet/sec YDOT = 7361
237969 meter/sec
ZDOT = -646
027827 ZDOT = -196
909282
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 16360
54792934
00016717 00000-0 10270-3 0 9040
2 25544 51
6372 183
9073 0006851 11
8635 348
2677 15
53890624 34749
Satellite: ISS
Catalog Number: 25544
Epoch time: 16360
54792934 = yrday
fracday
Element set: 904
Inclination: 51
6372 deg
RA of node: 183
9073 deg
Eccentricity:
0006851
Arg of perigee: 11
8635 deg
Mean anomaly: 348
2677 deg
Mean motion: 15
53890624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3474
Checksum: 333
Coasting Arc #6 (Orbit 3488)
---------------------------------------
Vector Time (GMT): 2016/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2186949
80 A = 6779279
49 meter
Y = 4037223
83 meter E =
0014549
Z = -4998971
41 I = 51
62801
XDOT = -7245
115009 Wp = 77
71812
YDOT = -1380
449887 meter/sec RA = 177
99303 deg
ZDOT = 2062
827334 TA = 212
33127
MA = 212
42052
Ha = 222
947 n
mi
Hp = 213
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7175032
17 X = -2207649
75
Y = 13245485
00 feet Y = 4012652
60 meter
Z = -16400824
84 Z = -5009644
96
XDOT = -23770
062365 XDOT = -7239
160295
YDOT = -4529
035061 feet/sec YDOT = -1461
436524 meter/sec
ZDOT = 6767
806215 ZDOT = 2027
646789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13763843
79 X = -4195219
59
Y = -5993416
50 feet Y = -1826793
35 meter
Z = -16448300
15 Z = -5013441
89
XDOT = 2184
406011 XDOT = 665
806952
YDOT = -23094
412996 feet/sec YDOT = -7039
177081 meter/sec
ZDOT = 6613
724220 ZDOT = 2015
863142
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 16361
51258670
00016717 00000-0 10270-3 0 9053
2 25544 51
6368 179
0990 0006759 15
9573 344
1791 15
53927976 34890
Satellite: ISS
Catalog Number: 25544
Epoch time: 16361
51258670 = yrday
fracday
Element set: 905
Inclination: 51
6368 deg
RA of node: 179
0990 deg
Eccentricity:
0006759
Arg of perigee: 15
9573 deg
Mean anomaly: 344
1791 deg
Mean motion: 15
53927976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3489
Checksum: 357
Coasting Arc #7 (Orbit 3504)
---------------------------------------
Vector Time (GMT): 2016/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3754652
41 A = 6782442
30 meter
Y = -3791883
66 meter E =
0015051
Z = 4182050
44 I = 51
67121
XDOT = 6349
657023 Wp = 53
22334
YDOT = 2175
633370 meter/sec RA = 173
00212 deg
ZDOT = -3710
014948 TA = 74
93353
MA = 74
76704
Ha = 222
988 n
mi
Hp = 213
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12318413
41 X = 3776460
67
Y = -12440563
18 feet Y = -3749775
09 meter
Z = 13720637
92 Z = 4200342
11
XDOT = 20832
208080 XDOT = 6342
878178
YDOT = 7137
904758 feet/sec YDOT = 2246
601971 meter/sec
ZDOT = -12171
965054 ZDOT = -3679
186295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13562576
42 X = 4133873
29
Y = 10970046
09 feet Y = 3343670
05 meter
Z = 13801501
21 Z = 4206697
57
XDOT = -4283
199419 XDOT = -1305
519183
YDOT = 20513
503489 feet/sec YDOT = 6252
515863 meter/sec
ZDOT = -12037
081021 ZDOT = -3668
902295
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 16362
54155206
00016717 00000-0 10270-3 0 9069
2 25544 51
6372 173
9704 0006770 18
9690 341
1714 15
53916536 35058
Satellite: ISS
Catalog Number: 25544
Epoch time: 16362
54155206 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 173
9704 deg
Eccentricity:
0006770
Arg of perigee: 18
9690 deg
Mean anomaly: 341
1714 deg
Mean motion: 15
53916536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3505
Checksum: 311
Coasting Arc #8 (Orbit 3519)
---------------------------------------
Vector Time (GMT): 2016/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4993804
10 A = 6785994
61 meter
Y = 3478666
48 meter E =
0010423
Z = -2998324
73 I = 51
71525
XDOT = -5030
875309 Wp = 43
41690
YDOT = -2948
105500 meter/sec RA = 168
02309 deg
ZDOT = 4976
337725 TA = 282
31809
MA = 282
43475
Ha = 223
087 n
mi
Hp = 213
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16383871
71 X = -5017767
84
Y = 11412947
77 feet Y = 3422688
73 meter
Z = -9837023
39 Z = -3022641
03
XDOT = -16505
496421 XDOT = -5021
707637
YDOT = -9672
262140 feet/sec YDOT = -3004
313390 meter/sec
ZDOT = 16326
567338 ZDOT = 4951
921146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13193854
96 X = -4021486
99
Y = -14916001
22 feet Y = -4546397
17 meter
Z = -9944282
63 Z = -3031017
35
XDOT = 6631
315009 XDOT = 2021
224815
YDOT = -16641
067983 feet/sec YDOT = -5072
197521 meter/sec
ZDOT = 16219
922484 ZDOT = 4943
832373
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 16363
50620607
00016717 00000-0 10270-3 0 9079
2 25544 51
6371 169
1627 0006777 24
6760 335
4716 15
53934112 35202
Satellite: ISS
Catalog Number: 25544
Epoch time: 16363
50620607 = yrday
fracday
Element set: 907
Inclination: 51
6371 deg
RA of node: 169
1627 deg
Eccentricity:
0006777
Arg of perigee: 24
6760 deg
Mean anomaly: 335
4716 deg
Mean motion: 15
53934112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3520
Checksum: 305
Coasting Arc #9 (Orbit 3535)
---------------------------------------
Vector Time (GMT): 2016/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5896772
27 A = 6788854
30 meter
Y = -3014541
66 meter E =
0015295
Z = 1478233
34 I = 51
75602
XDOT = 3372
556382 Wp = 91
99558
YDOT = 3736
619550 meter/sec RA = 163
05556 deg
ZDOT = -5782
178563 TA = 71
90061
MA = 71
73407
Ha = 223
146 n
mi
Hp = 213
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19346365
70 X = 5922862
85
Y = -9890228
55 feet Y = -2948454
26 meter
Z = 4849846
91 Z = 1506941
11
XDOT = 11064
817526 XDOT = 3358
608887
YDOT = 12259
250492 feet/sec YDOT = 3774
256351 meter/sec
ZDOT = -18970
402111 ZDOT = -5765
829211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12330995
98 X = 3758487
57
Y = 17855035
47 feet Y = 5442214
81 meter
Z = 4976318
72 Z = 1516781
95
XDOT = -9386
914468 XDOT = -2861
131530
YDOT = 11795
690585 feet/sec YDOT = 3595
326490 meter/sec
ZDOT = -18899
271442 ZDOT = -5760
497935
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 16364
53516715
00016717 00000-0 10270-3 0 9088
2 25544 51
6368 164
0346 0006817 26
4695 333
6805 15
53956959 35361
Satellite: ISS
Catalog Number: 25544
Epoch time: 16364
53516715 = yrday
fracday
Element set: 908
Inclination: 51
6368 deg
RA of node: 164
0346 deg
Eccentricity:
0006817
Arg of perigee: 26
4695 deg
Mean anomaly: 333
6805 deg
Mean motion: 15
53956959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3536
Checksum: 343
Coasting Arc #10 (Orbit 3551)
---------------------------------------
Vector Time (GMT): 2016/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6328769
45 A = 6789851
43 meter
Y = 2428328
47 meter E =
0018918
Z = 137276
83 I = 51
79210
XDOT = -1577
772820 Wp = 41
74420
YDOT = -4478
905785 meter/sec RA = 158
09498 deg
ZDOT = 6027
046629 TA = 319
73232
MA = 319
87229
Ha = 223
239 n
mi
Hp = 213
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20763679
30 X = -6356120
10
Y = 7966956
92 feet Y = 2357402
97 meter
Z = 450383
32 Z = 106467
51
XDOT = -5176
420013 XDOT = -1556
847634
YDOT = -14694
572786 feet/sec YDOT = -4496
433073 meter/sec
ZDOT = 19773
775029 ZDOT = 6019
432717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10949247
27 X = -3337330
57
Y = -19360282
37 feet Y = -5901014
07 meter
Z = 314764
21 Z = 95940
13
XDOT = 12335
361658 XDOT = 3759
818233
YDOT = -6620
017589 feet/sec YDOT = -2017
781361 meter/sec
ZDOT = 19741
095238 ZDOT = 6017
085828
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 16365
56412791
00016717 00000-0 10270-3 0 9092
2 25544 51
6391 158
9065 0006765 32
1623 327
9941 15
53949724 35521
Satellite: ISS
Catalog Number: 25544
Epoch time: 16365
56412791 = yrday
fracday
Element set: 909
Inclination: 51
6391 deg
RA of node: 158
9065 deg
Eccentricity:
0006765
Arg of perigee: 32
1623 deg
Mean anomaly: 327
9941 deg
Mean motion: 15
53949724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3552
Checksum: 337
Coasting Arc #11 (Orbit 3566)
---------------------------------------
Vector Time (GMT): 2016/366/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6342737
63 A = 6788502
48 meter
Y = -1633363
81 meter E =
0008683
Z = -1791605
84 I = 51
81705
XDOT = -272
284888 Wp = 91
90372
YDOT = 5139
910662 meter/sec RA = 153
13631 deg
ZDOT = -5673
911496 TA = 107
70940
MA = 107
61460
Ha = 223
367 n
mi
Hp = 213
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20809506
65 X = 6369233
61
Y = -5358805
14 feet Y = -1562286
75 meter
Z = -5877971
91 Z = -1760730
73
XDOT = -893
323122 XDOT = -302
179526
YDOT = 16863
223956 feet/sec YDOT = 5136
699105 meter/sec
ZDOT = -18615
195197 ZDOT = -5675
306351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8722025
78 X = 2658473
46
Y = 19678836
59 feet Y = 5998109
39 meter
Z = -5742174
69 Z = -1750214
84
XDOT = -15323
204794 XDOT = -4670
512821
YDOT = 1381
225682 feet/sec YDOT = 420
997588 meter/sec
ZDOT = -18622
164675 ZDOT = -5676
035793
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 16366
52877522
00016717 00000-0 10270-3 0 9108
2 25544 51
6387 154
0990 0006959 35
4266 324
7348 15
53964025 35677
Satellite: ISS
Catalog Number: 25544
Epoch time: 16366
52877522 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 154
0990 deg
Eccentricity:
0006959
Arg of perigee: 35
4266 deg
Mean anomaly: 324
7348 deg
Mean motion: 15
53964025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3567
Checksum: 339
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