[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 20th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16915 4846 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 3379)
---------------------------------------
Vector Time (GMT): 2016/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6088304
07 A = 6789182
47 meter
Y = -2664185
81 meter E =
0014158
Z = -1347680
72 I = 51
45040
XDOT = 882
638408 Wp = 16
64833
YDOT = -4938
559346 meter/sec RA = 212
93313 deg
ZDOT = 5803
869730 TA = 328
62984
MA = 328
71422
Ha = 222
259 n
mi
Hp = 215
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19974750
87 X = -6051513
57
Y = -8740767
09 feet Y = -2732063
55 meter
Z = -4421524
67 Z = -1377166
67
XDOT = 2895
795303 XDOT = 909
604612
YDOT = -16202
622527 feet/sec YDOT = -4928
538570 meter/sec
ZDOT = 19041
567357 ZDOT = 5808
222606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9548517
81 X = 2910388
23
Y = -19571972
55 feet Y = -5965537
23 meter
Z = -4550303
33 Z = -1386932
45
XDOT = 14646
913456 XDOT = 4464
379221
YDOT = 2735
190591 feet/sec YDOT = 833
686092 meter/sec
ZDOT = 19061
463040 ZDOT = 5809
933935
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
50270128
00016717 00000-0 10270-3 0 9001
2 25544 51
6405 214
0357 0006887 349
0887 11
0115 15
53898308 33806
Satellite: ISS
Catalog Number: 25544
Epoch time: 16354
50270128 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 214
0357 deg
Eccentricity:
0006887
Arg of perigee: 349
0887 deg
Mean anomaly: 11
0115 deg
Mean motion: 15
53898308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3380
Checksum: 301
Coasting Arc #2 (Orbit 3395)
---------------------------------------
Vector Time (GMT): 2016/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5874598
18 A = 6790002
12 meter
Y = 3389578
39 meter E =
0007206
Z = -302223
62 I = 51
48129
XDOT = -2613
700079 Wp = 104
19167
YDOT = 4007
024742 meter/sec RA = 207
95184 deg
ZDOT = -5986
023734 TA = 79
07003
MA = 78
98895
Ha = 222
421 n
mi
Hp = 214
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19273616
07 X = 5837726
49
Y = 11120664
01 feet Y = 3455065
95 meter
Z = -991547
31 Z = -273775
92
XDOT = -8575
131494 XDOT = -2629
236083
YDOT = 13146
406634 feet/sec YDOT = 3977
709945 meter/sec
ZDOT = -19639
185479 ZDOT = -5998
757934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11573422
21 X = -3527579
09
Y = 19011262
16 feet Y = 5794632
71 meter
Z = -867421
38 Z = -264390
04
XDOT = -11554
813891 XDOT = -3521
907274
YDOT = -7911
995145 feet/sec YDOT = -2411
576120 meter/sec
ZDOT = -19695
657867 ZDOT = -6003
236518
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
53168127
00016717 00000-0 10270-3 0 9011
2 25544 51
6412 208
9078 0006763 352
1561 7
9485 15
53884875 33968
Satellite: ISS
Catalog Number: 25544
Epoch time: 16355
53168127 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 208
9078 deg
Eccentricity:
0006763
Arg of perigee: 352
1561 deg
Mean anomaly: 7
9485 deg
Mean motion: 15
53884875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3396
Checksum: 333
Coasting Arc #3 (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 = -5240412
75 A = 6788419
78 meter
Y = -3857966
92 meter E =
0017446
Z = 1894799
83 I = 51
50430
XDOT = 4269
754363 Wp = 45
17080
YDOT = -3035
308540 meter/sec RA = 202
97036 deg
ZDOT = 5609
010945 TA = 335
75776
MA = 335
83975
Ha = 222
484 n
mi
Hp = 214
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17192955
22 X = -5206086
57
Y = -12657371
79 feet Y = -3916376
88 meter
Z = 6216534
88 Z = 1869426
56
XDOT = 14008
380456 XDOT = 4276
132587
YDOT = -9958
361352 feet/sec YDOT = -2987
525822 meter/sec
ZDOT = 18402
266880 ZDOT = 5629
767632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12767683
87 X = 3891590
04
Y = -17150969
46 feet Y = -5227615
49 meter
Z = 6105945
53 Z = 1861092
20
XDOT = 8616
209249 XDOT = 2626
220579
YDOT = 13021
496870 feet/sec YDOT = 3968
952246 meter/sec
ZDOT = 18493
747897 ZDOT = 5636
894359
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
56065642
00016717 00000-0 10270-3 0 9024
2 25544 51
6401 203
7789 0006837 355
9418 4
1678 15
53938053 34122
Satellite: ISS
Catalog Number: 25544
Epoch time: 16356
56065642 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 203
7789 deg
Eccentricity:
0006837
Arg of perigee: 355
9418 deg
Mean anomaly: 4
1678 deg
Mean motion: 15
53938053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3412
Checksum: 320
Coasting Arc #4 (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 = 4213193
84 A = 6785324
14 meter
Y = 4153381
48 meter E =
0007932
Z = -3333468
93 I = 51
52254
XDOT = -5713
925925 Wp = 35
94417
YDOT = 2047
478030 meter/sec RA = 197
98626 deg
ZDOT = -4670
161973 TA = 182
88859
MA = 182
89318
Ha = 222
617 n
mi
Hp = 214
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13822814
45 X = 4182629
05
Y = 13626579
66 feet Y = 4200325
49 meter
Z = -10936577
85 Z = -3313076
39
XDOT = -18746
476131 XDOT = -5713
711093
YDOT = 6717
447604 feet/sec YDOT = 1983
582470 meter/sec
ZDOT = -15322
053718 ZDOT = -4697
918128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13475397
37 X = -4107301
12
Y = 14039240
42 feet Y = 4279160
48 meter
Z = -10847857
02 Z = -3306426
82
XDOT = -5892
378418 XDOT = -1795
996942
YDOT = -17590
663862 feet/sec YDOT = -5361
634345 meter/sec
ZDOT = -15444
066527 ZDOT = -4707
351477
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
52532210
00016717 00000-0 10270-3 0 9032
2 25544 51
6388 198
9722 0006873 359
6619
4528 15
53914412 34274
Satellite: ISS
Catalog Number: 25544
Epoch time: 16357
52532210 = yrday
fracday
Element set: 903
Inclination: 51
6388 deg
RA of node: 198
9722 deg
Eccentricity:
0006873
Arg of perigee: 359
6619 deg
Mean anomaly:
4528 deg
Mean motion: 15
53914412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3427
Checksum: 320
Coasting Arc #5 (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 = -2839064
45 A = 6781732
78 meter
Y = -4267045
23 meter E =
0009848
Z = 4431164
58 I = 51
54165
XDOT = 6836
065675 Wp = 68
16544
YDOT = -1115
361422 meter/sec RA = 192
99354 deg
ZDOT = 3303
536076 TA = 348
47337
MA = 348
49591
Ha = 222
807 n
mi
Hp = 214
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9314515
90 X = -2812662
92
Y = -13999492
21 feet Y = -4298646
17 meter
Z = 14537941
52 Z = 4417437
02
XDOT = 22428
036991 XDOT = 6831
982717
YDOT = -3659
322251 feet/sec YDOT = -1038
938942 meter/sec
ZDOT = 10838
372952 ZDOT = 3336
733979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13729698
18 X = 4184812
01
Y = -9796306
57 feet Y = -2985914
24 meter
Z = 14478449
42 Z = 4413031
38
XDOT = 3567
437061 XDOT = 1087
354816
YDOT = 21245
015399 feet/sec YDOT = 6475
480693 meter/sec
ZDOT = 10984
106349 ZDOT = 3347
955615
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
55429689
00016717 00000-0 10270-3 0 9042
2 25544 51
6390 193
8435 0006940 3
1153 357
0042 15
53895154 34432
Satellite: ISS
Catalog Number: 25544
Epoch time: 16358
55429689 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 193
8435 deg
Eccentricity:
0006940
Arg of perigee: 3
1153 deg
Mean anomaly: 357
0042 deg
Mean motion: 15
53895154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3443
Checksum: 318
Coasting Arc #6 (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 = 1239484
96 A = 6778869
62 meter
Y = 4279996
09 meter E =
0017087
Z = -5123210
88 I = 51
56280
XDOT = -7481
519308 Wp = 55
79851
YDOT = 236
894504 meter/sec RA = 187
99419 deg
ZDOT = -1606
590642 TA = 198
62999
MA = 198
69261
Ha = 222
823 n
mi
Hp = 214
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4066551
71 X = 1216419
17
Y = 14041981
94 feet Y = 4293728
21 meter
Z = -16808434
64 Z = -5117245
52
XDOT = -24545
667021 XDOT = -7475
808156
YDOT = 777
212940 feet/sec YDOT = 153
263162 meter/sec
ZDOT = -5270
966674 ZDOT = -1642
920105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13837622
03 X = -4217707
20
Y = 4805162
15 feet Y = 1464613
42 meter
Z = -16782973
74 Z = -5115450
40
XDOT = -1531
992155 XDOT = -466
951209
YDOT = -23441
819735 feet/sec YDOT = -7145
066655 meter/sec
ZDOT = -5430
307086 ZDOT = -1655
157600
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
51895655
00016717 00000-0 10270-3 0 9050
2 25544 51
6377 189
0355 0006872 7
8782 352
2477 15
53923426 34587
Satellite: ISS
Catalog Number: 25544
Epoch time: 16359
51895655 = yrday
fracday
Element set: 905
Inclination: 51
6377 deg
RA of node: 189
0355 deg
Eccentricity:
0006872
Arg of perigee: 7
8782 deg
Mean anomaly: 352
2477 deg
Mean motion: 15
53923426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3458
Checksum: 351
Coasting Arc #7 (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 = 503444
32 A = 6778049
76 meter
Y = -4185178
54 meter E =
0008052
Z = 5304720
01 I = 51
59147
XDOT = 7644
106212 Wp = 28
62350
YDOT = 596
401863 meter/sec RA = 182
99264 deg
ZDOT = -247
854860 TA = 63
78095
MA = 63
69819
Ha = 222
911 n
mi
Hp = 214
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1651720
21 X = 524438
62
Y = -13730900
71 feet Y = -4179431
71 meter
Z = 17403937
04 Z = 5307216
28
XDOT = 25079
088621 XDOT = 7638
072937
YDOT = 1956
699025 feet/sec YDOT = 681
849683 meter/sec
ZDOT = -813
172112 ZDOT = -210
736330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13798491
16 X = 4205780
11
Y = 680085
80 feet Y = 207290
15 meter
Z = 17415566
69 Z = 5308264
73
XDOT = -340
041320 XDOT = -103
644594
YDOT = 24150
818235 feet/sec YDOT = 7361
169398 meter/sec
ZDOT = -650
485304 ZDOT = -198
267921
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
54792694
00016717 00000-0 10270-3 0 9065
2 25544 51
6371 183
9075 0006834 11
6977 348
4333 15
53891349 34744
Satellite: ISS
Catalog Number: 25544
Epoch time: 16360
54792694 = yrday
fracday
Element set: 906
Inclination: 51
6371 deg
RA of node: 183
9075 deg
Eccentricity:
0006834
Arg of perigee: 11
6977 deg
Mean anomaly: 348
4333 deg
Mean motion: 15
53891349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3474
Checksum: 343
Coasting Arc #8 (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 = -2188737
00 A = 6779279
47 meter
Y = 4036872
86 meter E =
0014519
Z = -4998450
85 I = 51
62796
XDOT = -7244
446904 Wp = 77
74529
YDOT = -1381
734661 meter/sec RA = 177
99325 deg
ZDOT = 2064
380265 TA = 212
31995
MA = 212
40898
Ha = 222
936 n
mi
Hp = 213
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7180895
68 X = -2209435
42
Y = 13244333
53 feet Y = 4012281
65 meter
Z = -16399116
96 Z = -5009133
07
XDOT = -23767
870421 XDOT = -7238
485417
YDOT = -4533
250201 feet/sec YDOT = -1462
713790 meter/sec
ZDOT = 6772
901132 ZDOT = 2029
202982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13763163
00 X = -4195012
08
Y = -5999363
90 feet Y = -1828606
12 meter
Z = -16446630
27 Z = -5012932
91
XDOT = 2188
345231 XDOT = 667
007626
YDOT = -23092
645628 feet/sec YDOT = -7038
638388 meter/sec
ZDOT = 6618
833654 ZDOT = 2017
420498
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
51258384
00016717 00000-0 10270-3 0 9077
2 25544 51
6367 179
0992 0006741 15
7908 344
3454 15
53928703 34899
Satellite: ISS
Catalog Number: 25544
Epoch time: 16361
51258384 = yrday
fracday
Element set: 907
Inclination: 51
6367 deg
RA of node: 179
0992 deg
Eccentricity:
0006741
Arg of perigee: 15
7908 deg
Mean anomaly: 344
3454 deg
Mean motion: 15
53928703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3489
Checksum: 340
Coasting Arc #9 (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 = 3756435
81 A = 6782443
81 meter
Y = -3791271
59 meter E =
0015027
Z = 4181019
73 I = 51
67116
XDOT = 6348
298038 Wp = 53
21729
YDOT = 2177
017091 meter/sec RA = 173
00234 deg
ZDOT = -3711
507252 TA = 74
95761
MA = 74
79136
Ha = 222
977 n
mi
Hp = 213
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12324264
46 X = 3778242
10
Y = -12438555
09 feet Y = -3749143
09 meter
Z = 13717256
34 Z = 4199320
06
XDOT = 20827
749467 XDOT = 6341
511069
YDOT = 7142
444523 feet/sec YDOT = 2247
970449 meter/sec
ZDOT = -12176
861062 ZDOT = -3680
685219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13561145
43 X = 4133437
13
Y = 10976085
49 feet Y = 3345510
86 meter
Z = 13798157
51 Z = 4205678
41
XDOT = -4287
704771 XDOT = -1306
892414
YDOT = 20509
640379 feet/sec YDOT = 6251
338388 meter/sec
ZDOT = -12042
006302 ZDOT = -3670
403521
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
54154872
00016717 00000-0 10270-3 0 9089
2 25544 51
6371 173
9706 0006753 18
7998 341
3403 15
53917274 35056
Satellite: ISS
Catalog Number: 25544
Epoch time: 16362
54154872 = yrday
fracday
Element set: 908
Inclination: 51
6371 deg
RA of node: 173
9706 deg
Eccentricity:
0006753
Arg of perigee: 18
7998 deg
Mean anomaly: 341
3403 deg
Mean motion: 15
53917274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3505
Checksum: 329
Coasting Arc #10 (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 = -4995456
92 A = 6785996
68 meter
Y = 3477682
09 meter E =
0010402
Z = -2996691
60 I = 51
71521
XDOT = -5028
798845 Wp = 43
31792
YDOT = -2949
574935 meter/sec RA = 168
02330 deg
ZDOT = 4977
583819 TA = 282
43825
MA = 282
55463
Ha = 223
076 n
mi
Hp = 213
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16389294
36 X = -5019417
47
Y = 11409718
14 feet Y = 3421685
87 meter
Z = -9831665
36 Z = -3021015
92
XDOT = -16498
683876 XDOT = -5019
620949
YDOT = -9677
083121 feet/sec YDOT = -3005
759547 meter/sec
ZDOT = 16330
655574 ZDOT = 4953
177352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13191267
37 X = -4020698
30
Y = -14921790
37 feet Y = -4548161
70 meter
Z = -9938959
64 Z = -3029394
90
XDOT = 6636
453867 XDOT = 2022
791139
YDOT = -16635
063040 feet/sec YDOT = -5070
367214 meter/sec
ZDOT = 16224
055327 ZDOT = 4945
092064
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
50620228
00016717 00000-0 10270-3 0 9090
2 25544 51
6371 169
1629 0006759 24
5133 335
6340 15
53934833 35202
Satellite: ISS
Catalog Number: 25544
Epoch time: 16363
50620228 = yrday
fracday
Element set: 909
Inclination: 51
6371 deg
RA of node: 169
1629 deg
Eccentricity:
0006759
Arg of perigee: 24
5133 deg
Mean anomaly: 335
6340 deg
Mean motion: 15
53934833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3520
Checksum: 306
Coasting Arc #11 (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 = 5897989
32 A = 6788854
72 meter
Y = -3013181
32 meter E =
0015266
Z = 1476160
36 I = 51
75597
XDOT = 3369
828686 Wp = 92
04394
YDOT = 3738
026487 meter/sec RA = 163
05577 deg
ZDOT = -5782
856415 TA = 71
87543
MA = 71
70923
Ha = 223
136 n
mi
Hp = 213
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19350358
66 X = 5924074
67
Y = -9885765
47 feet Y = -2947080
33 meter
Z = 4843045
80 Z = 1504874
03
XDOT = 11055
868391 XDOT = 3355
868954
YDOT = 12263
866426 feet/sec YDOT = 3775
632716 meter/sec
ZDOT = -18972
626033 ZDOT = -5766
520342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12327099
88 X = 3757300
04
Y = 17859621
50 feet Y = 5443612
63 meter
Z = 4969543
27 Z = 1514716
79
XDOT = -9392
324687 XDOT = -2862
780565
YDOT = 11787
720643 feet/sec YDOT = 3592
897252 meter/sec
ZDOT = -18901
553871 ZDOT = -5761
193620
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
53516287
00016717 00000-0 10270-3 0 9105
2 25544 51
6367 164
0348 0006800 26
3018 333
8479 15
53957722 35360
Satellite: ISS
Catalog Number: 25544
Epoch time: 16364
53516287 = yrday
fracday
Element set: 910
Inclination: 51
6367 deg
RA of node: 164
0348 deg
Eccentricity:
0006800
Arg of perigee: 26
3018 deg
Mean anomaly: 333
8479 deg
Mean motion: 15
53957722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3536
Checksum: 319
Coasting Arc #12 (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 = -6329423
16 A = 6789849
07 meter
Y = 2426478
52 meter E =
0018900
Z = 139735
74 I = 51
79204
XDOT = -1574
469750 Wp = 41
71178
YDOT = -4480
176858 meter/sec RA = 158
09518 deg
ZDOT = 6026
966686 TA = 319
79119
MA = 319
93086
Ha = 223
229 n
mi
Hp = 213
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20765824
00 X = -6356765
01
Y = 7960887
54 feet Y = 2355545
77 meter
Z = 458450
58 Z = 108923
26
XDOT = -5165
583170 XDOT = -1553
530208
YDOT = -14698
742974 feet/sec YDOT = -4497
667129 meter/sec
ZDOT = 19773
512748 ZDOT = 6019
368854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10943570
10 X = -3335600
17
Y = -19363352
39 feet Y = -5901949
81 meter
Z = 322817
93 Z = 98394
91
XDOT = 12340
864369 XDOT = 3761
495460
YDOT = -6610
328802 feet/sec YDOT = -2014
828219 meter/sec
ZDOT = 19740
903740 ZDOT = 6017
027460
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
56412315
00016717 00000-0 10270-3 0 9117
2 25544 51
6390 158
9067 0006746 31
9993 328
1568 15
53950465 35520
Satellite: ISS
Catalog Number: 25544
Epoch time: 16365
56412315 = yrday
fracday
Element set: 911
Inclination: 51
6390 deg
RA of node: 158
9067 deg
Eccentricity:
0006746
Arg of perigee: 31
9993 deg
Mean anomaly: 328
1568 deg
Mean motion: 15
53950465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3552
Checksum: 331
Coasting Arc #13 (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 = 6342613
96 A = 6788496
77 meter
Y = -1631077
53 meter E =
0008653
Z = -1794096
06 I = 51
81697
XDOT = -275
871007 Wp = 91
88825
YDOT = 5140
841132 meter/sec RA = 153
13650 deg
ZDOT = -5672
902407 TA = 107
75330
MA = 107
65885
Ha = 223
357 n
mi
Hp = 213
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20809100
92 X = 6369096
49
Y = -5351304
24 feet Y = -1560001
94 meter
Z = -5886141
92 Z = -1763221
58
XDOT = -905
088606 XDOT = -305
780685
YDOT = 16866
276679 feet/sec YDOT = 5137
589388 meter/sec
ZDOT = -18611
884538 ZDOT = -5674
314719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8714570
09 X = 2656200
96
Y = 19679724
91 feet Y = 5998380
15 meter
Z = -5750347
86 Z = -1752706
03
XDOT = -15328
093942 XDOT = -4672
003033
YDOT = 1370
647002 feet/sec YDOT = 417
773206 meter/sec
ZDOT = -18618
930796 ZDOT = -5675
050107
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
52877001
00016717 00000-0 10270-3 0 9122
2 25544 51
6387 154
0991 0006940 35
2680 324
8931 15
53964719 35675
Satellite: ISS
Catalog Number: 25544
Epoch time: 16366
52877001 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 154
0991 deg
Eccentricity:
0006940
Arg of perigee: 35
2680 deg
Mean anomaly: 324
8931 deg
Mean motion: 15
53964719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3567
Checksum: 331
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