[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 18th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24322 131 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
352/04:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (Orbit 3332)
---------------------------------------
Vector Time (GMT): 2016/351/11:19:27
151
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5420859
51 A = 6783777
06 meter
Y = -1496499
04 meter E =
0005850
Z = -3793097
69 I = 51
36049
XDOT = -1178
140607 Wp = 37
04521
YDOT = -6315
039510 meter/sec RA = 228
06221 deg
ZDOT = 4183
166643 TA = 277
23764
MA = 277
30413
Ha = 221
825 n
mi
Hp = 215
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17784972
16 X = -5385297
31
Y = -4909773
74 feet Y = -1556919
51 meter
Z = -12444546
22 Z = -3819344
43
XDOT = -3865
290704 XDOT = -1127
756503
YDOT = -20718
633564 feet/sec YDOT = -6327
932979 meter/sec
ZDOT = 13724
300010 ZDOT = 4177
565314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9453079
55 X = 2881298
65
Y = -15753786
46 feet Y = -4801754
11 meter
Z = -12559273
17 Z = -3828066
46
XDOT = 19872
969712 XDOT = 6057
281168
YDOT = 1022
795805 feet/sec YDOT = 311
748161 meter/sec
ZDOT = 13700
844765 ZDOT = 4176
017484
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 16351
48006449
00016717 00000-0 10270-3 0 9008
2 25544 51
6419 229
0989 0006695 338
1743 21
9123 15
53900348 33330
Satellite: ISS
Catalog Number: 25544
Epoch time: 16351
48006449 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 229
0989 deg
Eccentricity:
0006695
Arg of perigee: 338
1743 deg
Mean anomaly: 21
9123 deg
Mean motion: 15
53900348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3333
Checksum: 312
Coasting Arc #2 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2016/352/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2623894
95 A = 6778101
08 meter
Y = -3340996
45 meter E =
0005355
Z = 5280806
95 I = 51
35358
XDOT = 5695
234633 Wp = 6
15780
YDOT = 5119
645082 meter/sec RA = 224
43347 deg
ZDOT = 414
410472 TA = 79
90520
MA = 79
84478
Ha = 221
940 n
mi
Hp = 215
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8608579
23 X = 2635408
19
Y = -10961274
46 feet Y = -3311590
38 meter
Z = 17325482
11 Z = 5293580
72
XDOT = 18685
152995 XDOT = 5635
549159
YDOT = 16796
735834 feet/sec YDOT = 5182
999266 meter/sec
ZDOT = 1359
614411 ZDOT = 441
931694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11934441
64 X = -3637617
81
Y = 7061453
27 feet Y = 2152330
96 meter
Z = 17382016
14 Z = 5298038
52
XDOT = -10664
245856 XDOT = -3250
462137
YDOT = -21623
091971 feet/sec YDOT = -6590
718433 meter/sec
ZDOT = 1479
321917 ZDOT = 450
897320
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 16352
25180261
00016717 00000-0 10270-3 0 9010
2 25544 51
6381 225
2512 0006536 342
4057 17
6868 15
53892295 33450
Satellite: ISS
Catalog Number: 25544
Epoch time: 16352
25180261 = yrday
fracday
Element set: 901
Inclination: 51
6381 deg
RA of node: 225
2512 deg
Eccentricity:
0006536
Arg of perigee: 342
4057 deg
Mean anomaly: 17
6868 deg
Mean motion: 15
53892295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 304
Coasting Arc #3 (Orbit 3359)
---------------------------------------
Vector Time (GMT): 2016/353/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3856564
81 A = 6778687
72 meter
Y = 2156296
65 meter E =
0012671
Z = -5150477
04 I = 51
37932
XDOT = -5025
418484 Wp = 72
42769
YDOT = -5602
918220 meter/sec RA = 219
41759 deg
ZDOT = 1423
858556 TA = 211
29819
MA = 211
37368
Ha = 222
148 n
mi
Hp = 215
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12652771
68 X = -3855371
92
Y = 7074464
09 feet Y = 2113176
96 meter
Z = -16897890
55 Z = -5169208
03
XDOT = -16487
593450 XDOT = -4969
308130
YDOT = -18382
277625 feet/sec YDOT = -5658
802188 meter/sec
ZDOT = 4671
451955 ZDOT = 1399
582512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14230094
61 X = 4337332
84
Y = -2202773
64 feet Y = -671405
41 meter
Z = -16980329
03 Z = -5175604
29
XDOT = 8825
547303 XDOT = 2690
026818
YDOT = 21983
433351 feet/sec YDOT = 6700
550485 meter/sec
ZDOT = 4566
020878 ZDOT = 1391
723164
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 16353
21647054
00016717 00000-0 10270-3 0 9026
2 25544 51
6381 220
4442 0006641 346
2769 13
8202 15
53889654 33600
Satellite: ISS
Catalog Number: 25544
Epoch time: 16353
21647054 = yrday
fracday
Element set: 902
Inclination: 51
6381 deg
RA of node: 220
4442 deg
Eccentricity:
0006641
Arg of perigee: 346
2769 deg
Mean anomaly: 13
8202 deg
Mean motion: 15
53889654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3360
Checksum: 300
Coasting Arc #4 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2016/354/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4976303
00 A = 6781204
13 meter
Y = -950414
44 meter E =
0012082
Z = 4506883
72 I = 51
41319
XDOT = 3963
581463 Wp = 34
70321
YDOT = 5759
149375 meter/sec RA = 214
40728 deg
ZDOT = -3148
001537 TA = 87
05145
MA = 86
91319
Ha = 222
173 n
mi
Hp = 214
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16326453
42 X = 4964668
65
Y = -3118157
62 feet Y = -894831
34 meter
Z = 14786363
92 Z = 4531028
82
XDOT = 13003
876191 XDOT = 3914
178079
YDOT = 18894
847031 feet/sec YDOT = 5803
196727 meter/sec
ZDOT = -10328
089033 ZDOT = -3128
867355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16333752
29 X = -4978527
70
Y = -2517833
77 feet Y = -767435
73 meter
Z = 14892333
45 Z = 4539183
24
XDOT = -6145
878159 XDOT = -1873
263663
YDOT = -20996
143576 feet/sec YDOT = -6399
624562 meter/sec
ZDOT = -10245
195399 ZDOT = -3122
735558
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 16354
24544663
00016717 00000-0 10270-3 0 9033
2 25544 51
6376 215
3163 0006700 349
2297 10
8711 15
53918978 33763
Satellite: ISS
Catalog Number: 25544
Epoch time: 16354
24544663 = yrday
fracday
Element set: 903
Inclination: 51
6376 deg
RA of node: 215
3163 deg
Eccentricity:
0006700
Arg of perigee: 349
2297 deg
Mean anomaly: 10
8711 deg
Mean motion: 15
53918978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 320
Coasting Arc #5 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2016/355/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5836599
31 A = 6784819
83 meter
Y = -130426
14 meter E =
0007661
Z = -3454270
15 I = 51
45314
XDOT = -2563
081241 Wp = 33
87811
YDOT = -5609
587136 meter/sec RA = 209
40764 deg
ZDOT = 4553
697343 TA = 285
49755
MA = 285
58213
Ha = 222
315 n
mi
Hp = 214
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19148947
88 X = -5817927
84
Y = -427907
28 feet Y = -195590
39 meter
Z = -11332907
33 Z = -3482577
33
XDOT = -8409
059191 XDOT = -2522
282632
YDOT = -18404
157271 feet/sec YDOT = -5638
021290 meter/sec
ZDOT = 14939
951912 ZDOT = 4541
345510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17936377
10 X = 5467007
74
Y = 6505749
19 feet Y = 1982952
35 meter
Z = -11456949
94 Z = -3492078
34
XDOT = 2649
358325 XDOT = 807
524417
YDOT = 18848
495585 feet/sec YDOT = 5745
021454 meter/sec
ZDOT = 14886
741862 ZDOT = 4537
478919
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 16355
21010816
00016717 00000-0 10270-3 0 9040
2 25544 51
6384 210
5092 0006747 353
0232 7
0826 15
53899902 33910
Satellite: ISS
Catalog Number: 25544
Epoch time: 16355
21010816 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 210
5092 deg
Eccentricity:
0006747
Arg of perigee: 353
0232 deg
Mean anomaly: 7
0826 deg
Mean motion: 15
53899902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 294
Coasting Arc #6 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2016/356/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6376632
23 A = 6788078
47 meter
Y = 1117621
84 meter E =
0012769
Z = 2034258
62 I = 51
49373
XDOT = 860
239989 Wp = 81
81618
YDOT = 5229
560445 meter/sec RA = 204
41893 deg
ZDOT = -5538
023976 TA = 75
65915
MA = 75
51742
Ha = 222
484 n
mi
Hp = 214
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20920709
43 X = 6353779
27
Y = 3666738
31 feet Y = 1188801
77 meter
Z = 6674076
83 Z = 2065179
08
XDOT = 2822
309676 XDOT = 828
598961
YDOT = 17157
350540 feet/sec YDOT = 5239
003513 meter/sec
ZDOT = -18169
370000 ZDOT = -5533
921827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18780096
88 X = -5724173
53
Y = -9828735
42 feet Y = -2995798
56 meter
Z = 6809425
49 Z = 2075512
89
XDOT = 1686
846003 XDOT = 514
150662
YDOT = -15869
586151 feet/sec YDOT = -4837
049859 meter/sec
ZDOT = -18152
246254 ZDOT = -5532
804658
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
23907564
00016717 00000-0 10270-3 0 9059
2 25544 51
6392 205
3809 0006843 356
7773 3
3335 15
53931387 34070
Satellite: ISS
Catalog Number: 25544
Epoch time: 16356
23907564 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 205
3809 deg
Eccentricity:
0006843
Arg of perigee: 356
7773 deg
Mean anomaly: 3
3335 deg
Mean motion: 15
53931387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 323
Coasting Arc #7 (Orbit 3421)
---------------------------------------
Vector Time (GMT): 2016/357/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6489668
52 A = 6789792
25 meter
Y = -1910517
89 meter E =
0016792
Z = -450881
80 I = 51
52856
XDOT = 974
811866 Wp = 26
53983
YDOT = -4700
159649 meter/sec RA = 199
43994 deg
ZDOT = 5986
041971 TA = 328
58758
MA = 328
68776
Ha = 222
538 n
mi
Hp = 214
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21291563
39 X = -6465632
11
Y = -6268103
32 feet Y = -1982955
31 meter
Z = -1479271
01 Z = -482348
60
XDOT = 3198
201661 XDOT = 998
220277
YDOT = -15420
471290 feet/sec YDOT = -4689
128008 meter/sec
ZDOT = 19639
245312 ZDOT = 5990
834014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18587556
60 X = 5665487
25
Y = 12111829
14 feet Y = 3691685
52 meter
Z = -1616900
68 Z = -492831
33
XDOT = -6483
004807 XDOT = -1976
019865
YDOT = 12533
512479 feet/sec YDOT = 3820
214604 meter/sec
ZDOT = 19661
019131 ZDOT = 5992
678631
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
20372977
00016717 00000-0 10270-3 0 9062
2 25544 51
6385 200
5743 0006815
4465 359
6693 15
53934779 34225
Satellite: ISS
Catalog Number: 25544
Epoch time: 16357
20372977 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 200
5743 deg
Eccentricity:
0006815
Arg of perigee:
4465 deg
Mean anomaly: 359
6693 deg
Mean motion: 15
53934779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3422
Checksum: 331
Coasting Arc #8 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2016/358/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6160011
35 A = 6789276
10 meter
Y = 2584839
53 meter E =
0006103
Z = -1214809
34 I = 51
55874
XDOT = -2848
740190 Wp = 94
35071
YDOT = 4054
974834 meter/sec RA = 194
46439 deg
ZDOT = -5843
047287 TA = 98
85373
MA = 98
78461
Ha = 222
680 n
mi
Hp = 214
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20210011
01 X = 6136550
20
Y = 8480444
65 feet Y = 2653593
80 meter
Z = -3985594
96 Z = -1184942
43
XDOT = -9346
260466 XDOT = -2865
489258
YDOT = 13303
723209 feet/sec YDOT = 4023
024945 meter/sec
ZDOT = -19170
102649 ZDOT = -5856
926223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17187883
66 X = -5238866
94
Y = -13636807
60 feet Y = -4156498
96 meter
Z = -3855072
89 Z = -1175026
22
XDOT = 11481
076645 XDOT = 3499
432161
YDOT = -9058
855780 feet/sec YDOT = -2761
139242 meter/sec
ZDOT = -19231
611007 ZDOT = -5861
795035
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
23269104
00016717 00000-0 10270-3 0 9074
2 25544 51
6396 195
4463 0006884 3
3740 356
7458 15
53943175 34386
Satellite: ISS
Catalog Number: 25544
Epoch time: 16358
23269104 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 195
4463 deg
Eccentricity:
0006884
Arg of perigee: 3
3740 deg
Mean anomaly: 356
7458 deg
Mean motion: 15
53943175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 334
Coasting Arc #9 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2016/359/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5372995
78 A = 6786757
62 meter
Y = -3095329
44 meter E =
0017019
Z = 2732823
76 I = 51
58185
XDOT = 4575
184814 Wp = 56
34118
YDOT = -3379
501352 meter/sec RA = 189
48678 deg
ZDOT = 5153
615455 TA = 334
63833
MA = 334
72176
Ha = 222
817 n
mi
Hp = 214
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17627938
91 X = -5351258
56
Y = -10155280
32 feet Y = -3155292
52 meter
Z = 8965957
21 Z = 2706775
70
XDOT = 15010
448866 XDOT = 4587
601190
YDOT = -11087
602861 feet/sec YDOT = -3328
269449 meter/sec
ZDOT = 16908
187188 ZDOT = 5175
870509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14528708
91 X = 4428350
48
Y = 14311417
94 feet Y = 4362120
19 meter
Z = 8852246
68 Z = 2698164
79
XDOT = -16182
868468 XDOT = -4932
538309
YDOT = 5880
938402 feet/sec YDOT = 1792
510025 meter/sec
ZDOT = 17006
320057 ZDOT = 5183
526353
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
26164740
00016717 00000-0 10270-3 0 9089
2 25544 51
6396 190
3187 0006873 7
3138 352
8114 15
53951504 34545
Satellite: ISS
Catalog Number: 25544
Epoch time: 16359
26164740 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 190
3187 deg
Eccentricity:
0006873
Arg of perigee: 7
3138 deg
Mean anomaly: 352
8114 deg
Mean motion: 15
53951504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 318
Coasting Arc #10 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2016/360/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4193458
45 A = 6783083
14 meter
Y = 3522661
18 meter E =
0011963
Z = -4015631
35 I = 51
60148
XDOT = -6004
816149 Wp = 41
92553
YDOT = 2657
503590 meter/sec RA = 184
50264 deg
ZDOT = -3937
565710 TA = 187
05572
MA = 187
07257
Ha = 222
899 n
mi
Hp = 214
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13758065
78 X = 4173261
68
Y = 11557287
32 feet Y = 3569442
62 meter
Z = -13174643
54 Z = -3995309
38
XDOT = -19700
840384 XDOT = -6014
959756
YDOT = 8718
843799 feet/sec YDOT = 2590
297273 meter/sec
ZDOT = -12918
522670 ZDOT = -3966
760040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10707482
57 X = -3263640
69
Y = -14509663
42 feet Y = -4422545
41 meter
Z = -13086098
77 Z = -3988642
90
XDOT = 20066
373755 XDOT = 6116
230720
YDOT = -3035
487486 feet/sec YDOT = -925
216586 meter/sec
ZDOT = -13046
982517 ZDOT = -3976
720271
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
22629116
00016717 00000-0 10270-3 0 9091
2 25544 51
6394 185
5113 0007058 11
3362 348
7948 15
53963109 34697
Satellite: ISS
Catalog Number: 25544
Epoch time: 16360
22629116 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 185
5113 deg
Eccentricity:
0007058
Arg of perigee: 11
3362 deg
Mean anomaly: 348
7948 deg
Mean motion: 15
53963109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 322
Coasting Arc #11 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2016/361/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2686783
64 A = 6779666
53 meter
Y = -3846713
29 meter E =
0008146
Z = 4886002
75 I = 51
62258
XDOT = 7044
386633 Wp = 67
76283
YDOT = -1926
541812 meter/sec RA = 179
51185 deg
ZDOT = 2356
789024 TA = 359
17243
MA = 359
17378
Ha = 222
907 n
mi
Hp = 213
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8814906
96 X = -2667303
08
Y = -12620450
43 feet Y = -3876650
21 meter
Z = 16030192
76 Z = 4872998
03
XDOT = 23111
504702 XDOT = 7053
957918
YDOT = -6320
675236 feet/sec YDOT = -1847
713433 meter/sec
ZDOT = 7732
247453 ZDOT = 2391
031922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5917812
33 X = 1803749
20
Y = 14274565
00 feet Y = 4350887
41 meter
Z = 15973782
43 Z = 4868808
88
XDOT = -22845
764686 XDOT = -6963
389076
YDOT = 649
619565 feet/sec YDOT = 198
004043 meter/sec
ZDOT = 7882
749975 ZDOT = 2402
662192
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
25524018
00016717 00000-0 10270-3 0 9102
2 25544 51
6393 180
3841 0006858 13
5198 346
6137 15
53986100 34856
Satellite: ISS
Catalog Number: 25544
Epoch time: 16361
25524018 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 180
3841 deg
Eccentricity:
0006858
Arg of perigee: 13
5198 deg
Mean anomaly: 346
6137 deg
Mean motion: 15
53986100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 312
Coasting Arc #12 (Orbit 3499)
---------------------------------------
Vector Time (GMT): 2016/362/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1011459
97 A = 6777938
49 meter
Y = 4117796
91 meter E =
0018551
Z = -5303011
51 I = 51
64974
XDOT = -7548
781438 Wp = 65
32089
YDOT = 1152
899490 meter/sec RA = 174
51482 deg
ZDOT = -538
494824 TA = 199
49742
MA = 199
56846
Ha = 223
041 n
mi
Hp = 213
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3318438
24 X = 991098
18
Y = 13509832
39 feet Y = 4128994
41 meter
Z = -17398331
71 Z = -5298147
16
XDOT = -24766
343300 XDOT = -7558
496650
YDOT = 3782
478641 feet/sec YDOT = 1068
429673 meter/sec
ZDOT = -1766
715302 ZDOT = -575
188261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -608909
90 X = -185595
74
Y = -13923916
73 feet Y = -4244009
82 meter
Z = -17377667
33 Z = -5296713
00
XDOT = 23990
546599 XDOT = 7312
318603
YDOT = 1381
847818 feet/sec YDOT = 421
187215 meter/sec
ZDOT = -1927
864398 ZDOT = -587
613068
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
21987814
00016717 00000-0 10270-3 0 9117
2 25544 51
6400 175
5760 0007048 17
8084 342
3314 15
53969788 35005
Satellite: ISS
Catalog Number: 25544
Epoch time: 16362
21987814 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 175
5760 deg
Eccentricity:
0007048
Arg of perigee: 17
8084 deg
Mean anomaly: 342
3314 deg
Mean motion: 15
53969788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3500
Checksum: 316
Coasting Arc #13 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2016/363/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 751407
03 A = 6778297
54 meter
Y = -4302149
73 meter E =
0010879
Z = 5180380
91 I = 51
68319
XDOT = 7545
977175 Wp = 33
94689
YDOT = -314
579714 meter/sec RA = 169
51921 deg
ZDOT = -1345
593253 TA = 69
02940
MA = 68
91302
Ha = 223
049 n
mi
Hp = 213
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2465246
15 X = 774295
05
Y = -14114664
47 feet Y = -4293619
55 meter
Z = 16996000
36 Z = 5184086
18
XDOT = 24757
142964 XDOT = 7555
470320
YDOT = -1032
085677 feet/sec YDOT = -230
142306 meter/sec
ZDOT = -4414
676026 ZDOT = -1308
914014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4949003
58 X = -1508456
29
Y = 13425040
31 feet Y = 4091952
29 meter
Z = 17012962
01 Z = 5185550
82
XDOT = -23563
102738 XDOT = -7182
033715
YDOT = -3253
447965 feet/sec YDOT = -991
650940 meter/sec
ZDOT = -4253
700829 ZDOT = -1296
528013
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
24881897
00016717 00000-0 10270-3 0 9126
2 25544 51
6398 170
4486 0007119 20
7748 339
3692 15
53994516 35168
Satellite: ISS
Catalog Number: 25544
Epoch time: 16363
24881897 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 170
4486 deg
Eccentricity:
0007119
Arg of perigee: 20
7748 deg
Mean anomaly: 339
3692 deg
Mean motion: 15
53994516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 348
Coasting Arc #14 (Orbit 3530)
---------------------------------------
Vector Time (GMT): 2016/364/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2380016
07 A = 6780828
25 meter
Y = 4408004
80 meter E =
0012849
Z = -4579307
54 I = 51
72381
XDOT = -6989
501297 Wp = 77
05560
YDOT = -586
075015 meter/sec RA = 164
52928 deg
ZDOT = 3078
607039 TA = 223
68839
MA = 223
79017
Ha = 223
172 n
mi
Hp = 213
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7808451
67 X = -2406886
56
Y = 14461958
00 feet Y = 4381240
09 meter
Z = -15023974
88 Z = -4590933
75
XDOT = -22931
434700 XDOT = -6997
382568
YDOT = -1922
818290 feet/sec YDOT = -664
280703 meter/sec
ZDOT = 10100
416793 ZDOT = 3044
634944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10054448
41 X = 3064595
88
Y = -12941052
84 feet Y = -3944432
90 meter
Z = -15075715
12 Z = -4595077
97
XDOT = 21392
456622 XDOT = 6520
420778
YDOT = 5066
153661 feet/sec YDOT = 1544
163636 meter/sec
ZDOT = 9951
442695 ZDOT = 3033
199733
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
21345003
00016717 00000-0 10270-3 0 9139
2 25544 51
6404 165
6409 0007112 24
9193 335
2301 15
53977892 35317
Satellite: ISS
Catalog Number: 25544
Epoch time: 16364
21345003 = yrday
fracday
Element set: 913
Inclination: 51
6404 deg
RA of node: 165
6409 deg
Eccentricity:
0007112
Arg of perigee: 24
9193 deg
Mean anomaly: 335
2301 deg
Mean motion: 15
53977892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3531
Checksum: 290
Coasting Arc #15 (Orbit 3546)
---------------------------------------
Vector Time (GMT): 2016/365/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3836758
60 A = 6784555
88 meter
Y = -4366648
44 meter E =
0016895
Z = 3491786
49 I = 51
76739
XDOT = 5969
762716 Wp = 67
42738
YDOT = 1593
673625 meter/sec RA = 159
55065 deg
ZDOT = -4542
716916 TA = 71
61077
MA = 71
42712
Ha = 223
219 n
mi
Hp = 213
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12587790
69 X = 3868341
08
Y = -14326274
42 feet Y = -4323566
98 meter
Z = 11455992
42 Z = 3510500
52
XDOT = 19585
835684 XDOT = 5973
564413
YDOT = 5228
588008 feet/sec YDOT = 1660
453225 meter/sec
ZDOT = -14903
926890 ZDOT = -4513
708318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14555647
15 X = -4436561
25
Y = 12244290
55 feet Y = 3732059
76 meter
Z = 11538841
38 Z = 3517038
85
XDOT = -17759
128751 XDOT = -5412
982443
YDOT = -7112
752969 feet/sec YDOT = -2167
967105 meter/sec
ZDOT = -14776
878562 ZDOT = -4503
992586
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
24238562
00016717 00000-0 10270-3 0 9145
2 25544 51
6407 160
5133 0007060 28
6405 331
5135 15
53967571 35471
Satellite: ISS
Catalog Number: 25544
Epoch time: 16365
24238562 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 160
5133 deg
Eccentricity:
0007060
Arg of perigee: 28
6405 deg
Mean anomaly: 331
5135 deg
Mean motion: 15
53967571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3547
Checksum: 300
Coasting Arc #16 (Orbit 3561)
---------------------------------------
Vector Time (GMT): 2016/366/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4919500
61 A = 6787771
72 meter
Y = 4169688
55 meter E =
0013414
Z = -2103359
61 I = 51
80987
XDOT = -4595
890994 Wp = 36
74920
YDOT = -2641
793217 meter/sec RA = 154
58266 deg
ZDOT = 5540
855048 TA = 300
01437
MA = 300
14740
Ha = 223
250 n
mi
Hp = 213
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16140093
87 X = -4955544
47
Y = 13680080
53 feet Y = 4114474
03 meter
Z = -6900786
11 Z = -2127344
09
XDOT = -15078
382526 XDOT = -4592
922835
YDOT = -8667
300580 feet/sec YDOT = -2693
171443 meter/sec
ZDOT = 18178
658293 ZDOT = 5518
536717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17803783
35 X = 5426593
16
Y = -11366566
74 feet Y = -3464529
54 meter
Z = -7006749
69 Z = -2135657
31
XDOT = 13049
451378 XDOT = 3977
472780
YDOT = 9351
068796 feet/sec YDOT = 2850
205769 meter/sec
ZDOT = 18081
129805 ZDOT = 5511
128365
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
20700713
00016717 00000-0 10270-3 0 9155
2 25544 51
6422 155
7054 0007138 31
5019 328
6560 15
53997315 35621
Satellite: ISS
Catalog Number: 25544
Epoch time: 16366
20700713 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 155
7054 deg
Eccentricity:
0007138
Arg of perigee: 31
5019 deg
Mean anomaly: 328
6560 deg
Mean motion: 15
53997315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3562
Checksum: 300
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