[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 22nd 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
362/01:03:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
4
364/11:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 215
3
Coasting Arc #1 (Orbit 1102)
---------------------------------------
Vector Time (GMT): 2017/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6620260
22 A = 6788601
98 meter
Y = 1029854
98 meter E =
0008222
Z = -1064299
34 I = 51
65926
XDOT = -1661
988138 Wp = 20
92053
YDOT = -4615
751292 meter/sec RA = 178
37550 deg
ZDOT = 5893
245404 TA = 327
54109
MA = 327
59162
Ha = 219
767 n
mi
Hp = 215
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21720013
84 X = -6626114
50
Y = 3378789
29 feet Y = 955790
06 meter
Z = -3491795
73 Z = -1096472
36
XDOT = -5452
716987 XDOT = -1638
876284
YDOT = -15143
540983 feet/sec YDOT = -4634
208077 meter/sec
ZDOT = 19334
794633 ZDOT = 5885
227776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3516468
02 X = -1071819
45
Y = -21674628
08 feet Y = -6606426
64 meter
Z = -3634942
36 Z = -1107930
43
XDOT = 13525
539340 XDOT = 4122
584391
YDOT = -5419
647635 feet/sec YDOT = -1651
908599 meter/sec
ZDOT = 19299
788659 ZDOT = 5882
575583
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 17356
50215061
00016717 00000-0 10270-3 0 9009
2 25544 51
6361 179
5443 0002984 275
4930 84
5882 15
54198711 11032
Satellite: ISS
Catalog Number: 25544
Epoch time: 17356
50215061 = yrday
fracday
Element set: 900
Inclination: 51
6361 deg
RA of node: 179
5443 deg
Eccentricity:
0002984
Arg of perigee: 275
4930 deg
Mean anomaly: 84
5882 deg
Mean motion: 15
54198711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1103
Checksum: 305
Coasting Arc #2 (Orbit 1118)
---------------------------------------
Vector Time (GMT): 2017/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6745180
49 A = 6788821
70 meter
Y = -232464
84 meter E =
0008473
Z = -687878
60 I = 51
69296
XDOT = -439
416987 Wp = 151
72244
YDOT = 4795
683948 meter/sec RA = 173
40815 deg
ZDOT = -5966
864330 TA = 35
70179
MA = 35
64516
Ha = 219
822 n
mi
Hp = 215
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22129857
26 X = 6750620
01
Y = -762679
91 feet Y = -157005
15 meter
Z = -2256819
56 Z = -655099
71
XDOT = -1441
656780 XDOT = -464
027128
YDOT = 15733
871219 feet/sec YDOT = 4790
632924 meter/sec
ZDOT = -19576
326541 ZDOT = -5969
058280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1284436
64 X = 391496
29
Y = 22120106
45 feet Y = 6742208
45 meter
Z = -2111068
61 Z = -643453
71
XDOT = -14145
740978 XDOT = -4311
621850
YDOT = -1035
391019 feet/sec YDOT = -315
587183 meter/sec
ZDOT = -19586
733372 ZDOT = -5970
036332
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 17357
53093391
00016717 00000-0 10270-3 0 9014
2 25544 51
6360 174
4152 0002950 283
6343 76
4481 15
54242196 11193
Satellite: ISS
Catalog Number: 25544
Epoch time: 17357
53093391 = yrday
fracday
Element set: 901
Inclination: 51
6360 deg
RA of node: 174
4152 deg
Eccentricity:
0002950
Arg of perigee: 283
6343 deg
Mean anomaly: 76
4481 deg
Mean motion: 15
54242196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1119
Checksum: 301
Coasting Arc #3 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2017/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6334567
68 A = 6786842
84 meter
Y = -593768
60 meter E =
0011370
Z = 2345524
12 I = 51
71800
XDOT = 2461
740015 Wp = 65
97987
YDOT = -4856
108457 meter/sec RA = 168
43950 deg
ZDOT = 5402
974337 TA = 320
16577
MA = 320
24917
Ha = 219
906 n
mi
Hp = 215
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20782702
35 X = -6338850
51
Y = -1948059
71 feet Y = -664630
16 meter
Z = 7695289
12 Z = 2314742
58
XDOT = 8076
574852 XDOT = 2489
614589
YDOT = -15932
114359 feet/sec YDOT = -4828
424064 meter/sec
ZDOT = 17726
293755 ZDOT = 5415
000017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1096727
02 X = 334282
40
Y = -20894956
68 feet Y = -6368782
80 meter
Z = 7558511
98 Z = 2303834
45
XDOT = 14718
087647 XDOT = 4486
073115
YDOT = 7223
878978 feet/sec YDOT = 2201
838312 meter/sec
ZDOT = 17780
421439 ZDOT = 5419
472455
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 17358
55971620
00016717 00000-0 10270-3 0 9028
2 25544 51
6356 169
2853 0002902 281
3147 78
7679 15
54210455 11357
Satellite: ISS
Catalog Number: 25544
Epoch time: 17358
55971620 = yrday
fracday
Element set: 902
Inclination: 51
6356 deg
RA of node: 169
2853 deg
Eccentricity:
0002902
Arg of perigee: 281
3147 deg
Mean anomaly: 78
7679 deg
Mean motion: 15
54210455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1135
Checksum: 319
Coasting Arc #4 (Orbit 1149)
---------------------------------------
Vector Time (GMT): 2017/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5438100
59 A = 6783097
90 meter
Y = 1490885
50 meter E =
0003728
Z = -3774708
31 I = 51
73926
XDOT = -4250
876538 Wp = 56
09352
YDOT = 4755
605639 meter/sec RA = 163
46539 deg
ZDOT = -4246
771973 TA = 169
01628
MA = 169
00814
Ha = 219
930 n
mi
Hp = 215
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17841537
35 X = 5439360
50
Y = 4891356
64 feet Y = 1551705
30 meter
Z = -12384213
62 Z = -3748288
74
XDOT = -13946
445335 XDOT = -4283
110464
YDOT = 15602
380707 feet/sec YDOT = 4707
889410 meter/sec
ZDOT = -13932
978915 ZDOT = -4267
499336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3843708
88 X = -1171562
47
Y = 18175882
52 feet Y = 5540008
99 meter
Z = -12266938
03 Z = -3738962
71
XDOT = -15052
263059 XDOT = -4587
929780
YDOT = -12646
993943 feet/sec YDOT = -3854
803754 meter/sec
ZDOT = -14025
792652 ZDOT = -4275
061600
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 17359
52419531
00016717 00000-0 10270-3 0 9035
2 25544 51
6373 164
4769 0002772 288
9367 71
1485 15
54234235 11502
Satellite: ISS
Catalog Number: 25544
Epoch time: 17359
52419531 = yrday
fracday
Element set: 903
Inclination: 51
6373 deg
RA of node: 164
4769 deg
Eccentricity:
0002772
Arg of perigee: 288
9367 deg
Mean anomaly: 71
1485 deg
Mean motion: 15
54234235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1150
Checksum: 321
Coasting Arc #5 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2017/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4153013
15 A = 6779440
17 meter
Y = -2413595
37 meter E =
0004825
Z = 4781756
40 I = 51
75708
XDOT = 5646
150188 Wp = 123
23424
YDOT = -4466
667724 meter/sec RA = 158
48194 deg
ZDOT = 2644
686745 TA = 300
69911
MA = 300
74664
Ha = 220
033 n
mi
Hp = 215
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13625371
23 X = -4148942
36
Y = -7918620
00 feet Y = -2460014
67 meter
Z = 15688177
15 Z = 4761592
20
XDOT = 18524
114790 XDOT = 5682
831491
YDOT = -14654
421668 feet/sec YDOT = -4403
323633 meter/sec
ZDOT = 8676
793784 ZDOT = 2672
202783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6863921
99 X = 2092123
42
Y = -14284157
87 feet Y = -4353811
32 meter
Z = 15598833
13 Z = 4754524
34
XDOT = 14957
535994 XDOT = 4559
056971
YDOT = 16813
422572 feet/sec YDOT = 5124
731200 meter/sec
ZDOT = 8799
770766 ZDOT = 2682
170129
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 17360
55296918
00016717 00000-0 10270-3 0 9043
2 25544 51
6362 159
3469 0002848 290
0024 70
0822 15
54229424 11662
Satellite: ISS
Catalog Number: 25544
Epoch time: 17360
55296918 = yrday
fracday
Element set: 904
Inclination: 51
6362 deg
RA of node: 159
3469 deg
Eccentricity:
0002848
Arg of perigee: 290
0024 deg
Mean anomaly: 70
0822 deg
Mean motion: 15
54229424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1166
Checksum: 309
Coasting Arc #6 (Orbit 1180)
---------------------------------------
Vector Time (GMT): 2017/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2614581
05 A = 6777256
35 meter
Y = 3350734
27 meter E =
0012287
Z = -5289639
75 I = 51
78087
XDOT = -6538
413727 Wp = 78
02898
YDOT = 3919
177891 meter/sec RA = 153
49397 deg
ZDOT = -748
200863 TA = 184
82299
MA = 184
83484
Ha = 219
996 n
mi
Hp = 215
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8578021
82 X = 2602612
37
Y = 10993222
68 feet Y = 3379905
65 meter
Z = -17354461
14 Z = -5276967
85
XDOT = -21451
488605 XDOT = -6578
118690
YDOT = 12858
195181 feet/sec YDOT = 3845
838908 meter/sec
ZDOT = -2454
727240 ZDOT = -780
058669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10143109
70 X = -3091619
84
Y = 9668911
39 feet Y = 2947084
19 meter
Z = -17298560
71 Z = -5272601
31
XDOT = -14075
298195 XDOT = -4290
150890
YDOT = -19417
778605 feet/sec YDOT = -5918
538919 meter/sec
ZDOT = -2596
957161 ZDOT = -791
552543
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 17361
51744294
00016717 00000-0 10270-3 0 9056
2 25544 51
6370 154
5396 0002695 293
8689 66
2181 15
54234431 11811
Satellite: ISS
Catalog Number: 25544
Epoch time: 17361
51744294 = yrday
fracday
Element set: 905
Inclination: 51
6370 deg
RA of node: 154
5396 deg
Eccentricity:
0002695
Arg of perigee: 293
8689 deg
Mean anomaly: 66
2181 deg
Mean motion: 15
54234431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1181
Checksum: 321
Coasting Arc #7 (Orbit 1189)
---------------------------------------
Vector Time (GMT): 2017/362/01:03:30
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4012785
87 A = 6778534
23 meter
Y = -2245344
26 meter E =
0003197
Z = 4978755
97 I = 51
80191
XDOT = 5437
767176 Wp = 125
04446
YDOT = -4967
593724 meter/sec RA = 150
80146 deg
ZDOT = 2139
668794 TA = 304
14773
MA = 304
17804
Ha = 220
068 n
mi
Hp = 215
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13165307
98 X = -4011563
95
Y = -7366615
02 feet Y = -2290211
41 meter
Z = 16334501
20 Z = 4959265
93
XDOT = 17840
443491 XDOT = 5482
518533
YDOT = -16297
879672 feet/sec YDOT = -4906
534788 meter/sec
ZDOT = 7019
910742 ZDOT = 2166
192217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1934772
79 X = -589718
75
Y = 15055348
30 feet Y = 4588870
16 meter
Z = 16248120
58 Z = 4952427
15
XDOT = -20624
410304 XDOT = -6286
320261
YDOT = -10364
414660 feet/sec YDOT = -3159
073588 meter/sec
ZDOT = 7138
569456 ZDOT = 2175
835970
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 17362
09612385
00016717 00000-0 10270-3 0 9066
2 25544 51
6377 151
6576 0003150 300
6033 59
4809 15
54259969 11907
Satellite: ISS
Catalog Number: 25544
Epoch time: 17362
09612385 = yrday
fracday
Element set: 906
Inclination: 51
6377 deg
RA of node: 151
6576 deg
Eccentricity:
0003150
Arg of perigee: 300
6033 deg
Mean anomaly: 59
4809 deg
Mean motion: 15
54259969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1190
Checksum: 317
Coasting Arc #8 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2017/363/01:03:30
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2540055
73 A = 6777090
54 meter
Y = 3341786
99 meter E =
0012578
Z = -5331400
45 I = 51
82521
XDOT = -6245
605338 Wp = 79
49330
YDOT = 4429
826485 meter/sec RA = 145
81267 deg
ZDOT = -197
103727 TA = 188
62005
MA = 188
64167
Ha = 220
138 n
mi
Hp = 215
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8333516
16 X = 2528395
56
Y = 10963868
09 feet Y = 3370126
82 meter
Z = -17491471
28 Z = -5319089
70
XDOT = -20490
831162 XDOT = -6293
719228
YDOT = 14533
551459 feet/sec YDOT = 4359
714846 meter/sec
ZDOT = -646
665772 ZDOT = -227
559550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6855099
39 X = 2089434
30
Y = -12023230
42 feet Y = -3664680
63 meter
Z = -17437173
09 Z = -5314850
36
XDOT = 20434
237157 XDOT = 6228
355486
YDOT = 12794
690710 feet/sec YDOT = 3899
821728 meter/sec
ZDOT = -782
764041 ZDOT = -238
586480
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 17363
06059234
00016717 00000-0 10270-3 0 9073
2 25544 51
6380 146
8478 0003129 307
3957 52
6911 15
54226422 12057
Satellite: ISS
Catalog Number: 25544
Epoch time: 17363
06059234 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 146
8478 deg
Eccentricity:
0003129
Arg of perigee: 307
3957 deg
Mean anomaly: 52
6911 deg
Mean motion: 15
54226422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 304
Coasting Arc #9 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2017/364/01:03:30
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -980143
36 A = 6778047
62 meter
Y = -4362029
38 meter E =
0005512
Z = 5094085
32 I = 51
85499
XDOT = 6562
075632 Wp = 21
89731
YDOT = -3551
083155 meter/sec RA = 140
82667 deg
ZDOT = -1772
566651 TA = 85
22555
MA = 85
16261
Ha = 220
259 n
mi
Hp = 215
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3215693
43 X = -956037
73
Y = -14311120
01 feet Y = -4372855
71 meter
Z = 16712878
36 Z = 5089382
22
XDOT = 21529
119527 XDOT = 6609
907364
YDOT = -11650
535285 feet/sec YDOT = -3477
433928 meter/sec
ZDOT = -5815
507386 ZDOT = -1740
574222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11769937
27 X = -3587476
88
Y = 8791805
59 feet Y = 2679742
35 meter
Z = 16692569
43 Z = 5087895
16
XDOT = -18689
536129 XDOT = -5696
570612
YDOT = -14215
045480 feet/sec YDOT = -4332
745862 meter/sec
ZDOT = -5672
671245 ZDOT = -1729
030195
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 17364
08935471
00016717 00000-0 10270-3 0 9083
2 25544 51
6379 141
7192 0003125 313
1531 46
9360 15
54229644 12212
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
08935471 = yrday
fracday
Element set: 908
Inclination: 51
6379 deg
RA of node: 141
7192 deg
Eccentricity:
0003125
Arg of perigee: 313
1531 deg
Mean anomaly: 46
9360 deg
Mean motion: 15
54229644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1221
Checksum: 299
Coasting Arc #10 (Orbit 1227)
---------------------------------------
Vector Time (GMT): 2017/364/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3501072
03 A = 6777300
59 meter
Y = -2429458
41 meter E =
0000695
Z = 5269343
78 I = 51
86345
XDOT = 5218
032627 Wp = 100
18817
YDOT = -5546
799266 meter/sec RA = 138
63031 deg
ZDOT = 909
377277 TA = 341
14023
MA = 341
14281
Ha = 220
239 n
mi
Hp = 215
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11486456
79 X = -3499240
87
Y = -7970664
08 feet Y = -2468600
10 meter
Z = 17287873
30 Z = 5252340
84
XDOT = 17119
529616 XDOT = 5275
253302
YDOT = -18198
160321 feet/sec YDOT = -5488
127810 meter/sec
ZDOT = 2983
521249 ZDOT = 934
863288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7036796
76 X = 2144815
65
Y = -12188181
84 feet Y = -3714957
82 meter
Z = 17212566
73 Z = 5246390
34
XDOT = 18591
693989 XDOT = 5666
748328
YDOT = 15109
552391 feet/sec YDOT = 4605
391569 meter/sec
ZDOT = 3097
703198 ZDOT = 944
179935
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 17364
53943689
00016717 00000-0 10270-3 0 9094
2 25544 51
6375 139
4706 0002864 306
7234 53
3656 15
54246047 12283
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
53943689 = yrday
fracday
Element set: 909
Inclination: 51
6375 deg
RA of node: 139
4706 deg
Eccentricity:
0002864
Arg of perigee: 306
7234 deg
Mean anomaly: 53
3656 deg
Mean motion: 15
54246047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1228
Checksum: 331
Coasting Arc #11 (Orbit 1242)
---------------------------------------
Vector Time (GMT): 2017/365/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2148184
34 A = 6777328
26 meter
Y = 3718453
40 meter E =
0012056
Z = -5253567
68 I = 51
88900
XDOT = -5811
954285 Wp = 91
05941
YDOT = 4872
516154 meter/sec RA = 133
64637 deg
ZDOT = 1074
146377 TA = 189
19589
MA = 189
21799
Ha = 220
194 n
mi
Hp = 215
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7047848
89 X = 2131963
10
Y = 12199650
27 feet Y = 3742385
81 meter
Z = -17236114
43 Z = -5243171
44
XDOT = -19068
091486 XDOT = -5871
225773
YDOT = 15985
945387 feet/sec YDOT = 4807
191368 meter/sec
ZDOT = 3524
102287 ZDOT = 1045
770434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11459300
40 X = -3492794
76
Y = 8292306
75 feet Y = 2527495
10 meter
Z = -17190385
81 Z = -5239629
60
XDOT = -17130
055742 XDOT = -5221
240990
YDOT = -16642
942978 feet/sec YDOT = -5072
769020 meter/sec
ZDOT = 3397
130324 ZDOT = 1035
445323
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 17365
50389693
00016717 00000-0 10270-3 0 9103
2 25544 51
6388 134
6628 0002807 310
7509 49
3400 15
54259598 12438
Satellite: ISS
Catalog Number: 25544
Epoch time: 17365
50389693 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 134
6628 deg
Eccentricity:
0002807
Arg of perigee: 310
7509 deg
Mean anomaly: 49
3400 deg
Mean motion: 15
54259598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1243
Checksum: 325
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