[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 14th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3492)
---------------------------------------
Vector Time (GMT): 2016/104/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3993702
20 A = 6779330
27 meter
Y = 2597445
66 meter E =
0008891
Z = 4819044
07 I = 51
76043
XDOT = -5854
544738 Wp = 54
18609
YDOT = -4248
722071 meter/sec RA = 19
81793 deg
ZDOT = -2553
432535 TA = 60
93269
MA = 60
84367
Ha = 221
341 n
mi
Hp = 214
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13102697
51 X = -4045859
61
Y = 8521803
36 feet Y = 2552494
05 meter
Z = 15810512
03 Z = 4799516
76
XDOT = -19207
823942 XDOT = -5794
195818
YDOT = -13939
376872 feet/sec YDOT = -4313
854182 meter/sec
ZDOT = -8377
403330 ZDOT = -2581
725769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4491555
93 X = -1369026
25
Y = 15060544
03 feet Y = 4590453
82 meter
Z = 15725140
51 Z = 4793022
83
XDOT = -22517
975166 XDOT = -6863
478831
YDOT = 2187
827483 feet/sec YDOT = 666
849817 meter/sec
ZDOT = -8499
509100 ZDOT = -2590
650374
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 16104
59714581
00016717 00000-0 10270-3 0 9009
2 25544 51
6440 20
1964 0001755 26
4811 333
6432 15
54212124 34934
Satellite: ISS
Catalog Number: 25544
Epoch time: 16104
59714581 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 20
1964 deg
Eccentricity:
0001755
Arg of perigee: 26
4811 deg
Mean anomaly: 333
6432 deg
Mean motion: 15
54212124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3493
Checksum: 277
Coasting Arc #2 (Orbit 3507)
---------------------------------------
Vector Time (GMT): 2016/105/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5313306
64 A = 6782963
92 meter
Y = -1732970
95 meter E =
0006788
Z = -3849507
54 I = 51
74245
XDOT = 4507
849709 Wp = 89
22621
YDOT = 4589
319441 meter/sec RA = 14
83407 deg
ZDOT = 4162
400179 TA = 224
52107
MA = 224
57563
Ha = 221
309 n
mi
Hp = 214
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17432108
39 X = 5350989
54
Y = -5685600
24 feet Y = -1673343
56 meter
Z = -12629617
92 Z = -3823605
14
XDOT = 14789
533166 XDOT = 4435
976572
YDOT = 15056
822312 feet/sec YDOT = 4639
327602 meter/sec
ZDOT = 13656
168567 ZDOT = 4184
123377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9338023
04 X = 2846229
42
Y = -15869618
49 feet Y = -4837059
72 meter
Z = -12516718
29 Z = -3815095
73
XDOT = 19832
226859 XDOT = 6044
862747
YDOT = 841
847347 feet/sec YDOT = 256
595071 meter/sec
ZDOT = 13749
651444 ZDOT = 4190
893760
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 16105
56164073
00016717 00000-0 10270-3 0 9013
2 25544 51
6445 15
3874 0001734 29
2184 330
9066 15
54196270 35089
Satellite: ISS
Catalog Number: 25544
Epoch time: 16105
56164073 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 15
3874 deg
Eccentricity:
0001734
Arg of perigee: 29
2184 deg
Mean anomaly: 330
9066 deg
Mean motion: 15
54196270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3508
Checksum: 296
Coasting Arc #3 (Orbit 3523)
---------------------------------------
Vector Time (GMT): 2016/106/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6269210
98 A = 6786718
56 meter
Y = 861586
03 meter E =
0014483
Z = 2436129
97 I = 51
72366
XDOT = -2743
321927 Wp = 99
28355
YDOT = -4762
178465 meter/sec RA = 9
85904 deg
ZDOT = -5350
680235 TA = 53
48124
MA = 53
34795
Ha = 221
387 n
mi
Hp = 214
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20568277
49 X = -6290213
19
Y = 2826725
81 feet Y = 791362
29 meter
Z = 7992552
39 Z = 2405624
60
XDOT = -9000
400022 XDOT = -2663
874834
YDOT = -15623
945096 feet/sec YDOT = -4792
412297 meter/sec
ZDOT = -17554
725180 ZDOT = -5363
813303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13285568
74 X = -4049441
35
Y = 16020051
00 feet Y = 4882911
54 meter
Z = 7859830
81 Z = 2395676
43
XDOT = -15942
849772 XDOT = -4859
380610
YDOT = -4540
592459 feet/sec YDOT = -1383
972581 meter/sec
ZDOT = -17610
843237 ZDOT = -5367
785018
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 16106
59042691
00016717 00000-0 10270-3 0 9029
2 25544 51
6445 10
2581 0001730 37
0720 323
0552 15
54190340 35240
Satellite: ISS
Catalog Number: 25544
Epoch time: 16106
59042691 = yrday
fracday
Element set: 902
Inclination: 51
6445 deg
RA of node: 10
2581 deg
Eccentricity:
0001730
Arg of perigee: 37
0720 deg
Mean anomaly: 323
0552 deg
Mean motion: 15
54190340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3524
Checksum: 263
Coasting Arc #4 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2016/107/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6736333
45 A = 6788775
75 meter
Y = -53090
96 meter E =
0012111
Z = -794028
68 I = 51
69969
XDOT = 732
379026 Wp = 38
55073
YDOT = 4780
316393 meter/sec RA = 4
88974 deg
ZDOT = 5951
787975 TA = 312
87088
MA = 312
97253
Ha = 221
272 n
mi
Hp = 214
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22100831
52 X = 6740283
52
Y = -174182
96 feet Y = 22261
21 meter
Z = -2605080
98 Z = -761295
59
XDOT = 2402
818326 XDOT = 649
958618
YDOT = 15683
452734 feet/sec YDOT = 4788
046018 meter/sec
ZDOT = 19526
863436 ZDOT = 5955
145094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15920908
78 X = 4852692
99
Y = -15353259
53 feet Y = -4679673
50 meter
Z = -2462849
21 Z = -750676
44
XDOT = 11330
639901 XDOT = 3453
579042
YDOT = 8647
372121 feet/sec YDOT = 2635
719022 meter/sec
ZDOT = 19540
499393 ZDOT = 5955
944215
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 16107
55490367
00016717 00000-0 10270-3 0 9034
2 25544 51
6448 5
4489 0001707 33
5712 326
5549 15
54235932 35399
Satellite: ISS
Catalog Number: 25544
Epoch time: 16107
55490367 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 5
4489 deg
Eccentricity:
0001707
Arg of perigee: 33
5712 deg
Mean anomaly: 326
5549 deg
Mean motion: 15
54235932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 317
Coasting Arc #5 (Orbit 3554)
---------------------------------------
Vector Time (GMT): 2016/108/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6671507
74 A = 6788683
43 meter
Y = -762104
59 meter E =
0009441
Z = -975284
87 I = 51
66699
XDOT = 1392
337018 Wp = 131
83100
YDOT = -4677
002986 meter/sec RA = 359
92234 deg
ZDOT = -5912
711275 TA = 58
72731
MA = 58
63487
Ha = 221
251 n
mi
Hp = 214
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21888148
74 X = -6657752
32
Y = -2500343
14 feet Y = -836633
01 meter
Z = -3199753
51 Z = -1007660
04
XDOT = 4568
034835 XDOT = 1473
254479
YDOT = -15344
497987 feet/sec YDOT = -4660
981078 meter/sec
ZDOT = -19398
659040 ZDOT = -5905
750635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17350879
19 X = -5288547
98
Y = 13541449
75 feet Y = 4127433
88 meter
Z = -3340258
04 Z = -1018110
65
XDOT = -6420
282078 XDOT = -1956
901977
YDOT = -12970
423483 feet/sec YDOT = -3953
385078 meter/sec
ZDOT = -19367
489007 ZDOT = -5903
210649
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 16108
58367218
00016717 00000-0 10270-3 0 9047
2 25544 51
6447
3198 0001544 37
5604 322
5656 15
54198263 35550
Satellite: ISS
Catalog Number: 25544
Epoch time: 16108
58367218 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node:
3198 deg
Eccentricity:
0001544
Arg of perigee: 37
5604 deg
Mean anomaly: 322
5656 deg
Mean motion: 15
54198263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3555
Checksum: 311
Coasting Arc #6 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2016/109/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6067830
63 A = 6786038
05 meter
Y = 1533437
79 meter E =
0014912
Z = 2603851
20 I = 51
62609
XDOT = -3385
999845 Wp = 72
47009
YDOT = 4465
245582 meter/sec RA = 354
94757 deg
ZDOT = 5240
518987 TA = 316
86858
MA = 316
98531
Ha = 221
181 n
mi
Hp = 214
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19907580
80 X = 6037583
89
Y = 5030963
87 feet Y = 1601123
45 meter
Z = 8542818
90 Z = 2633253
80
XDOT = -11108
923377 XDOT = -3461
136051
YDOT = 14649
755846 feet/sec YDOT = 4426
961491 meter/sec
ZDOT = 17193
303764 ZDOT = 5223
887586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17507285
98 X = 5336220
77
Y = -10626565
85 feet Y = -3238977
27 meter
Z = 8670245
76 Z = 2642690
91
XDOT = 1804
928018 XDOT = 550
142060
YDOT = 16995
665921 feet/sec YDOT = 5180
278973 meter/sec
ZDOT = 17120
166972 ZDOT = 5218
226893
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 16109
61243067
00016717 00000-0 10270-3 0 9058
2 25544 51
6442 355
1897 0001752 35
0099 325
1169 15
54242640 35719
Satellite: ISS
Catalog Number: 25544
Epoch time: 16109
61243067 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 355
1897 deg
Eccentricity:
0001752
Arg of perigee: 35
0099 deg
Mean anomaly: 325
1169 deg
Mean motion: 15
54242640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 301
Coasting Arc #7 (Orbit 3585)
---------------------------------------
Vector Time (GMT): 2016/110/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4978192
77 A = 6782152
57 meter
Y = -2327664
65 meter E =
0008357
Z = -3983820
31 I = 51
58051
XDOT = 5099
622135 Wp = 65
22485
YDOT = -4105
819713 meter/sec RA = 349
96193 deg
ZDOT = -3976
693893 TA = 163
29000
MA = 163
26245
Ha = 221
199 n
mi
Hp = 214
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16332653
44 X = -4932442
36
Y = -7636695
04 feet Y = -2383078
70 meter
Z = -13070276
60 Z = -4007892
02
XDOT = 16731
043749 XDOT = 5164
472693
YDOT = -13470
537117 feet/sec YDOT = -4048
430135 meter/sec
ZDOT = -13046
895975 ZDOT = -3951
763024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16728838
26 X = -5098949
90
Y = 6518321
85 feet Y = 1986784
50 meter
Z = -13174378
96 Z = -4015550
71
XDOT = 2290
760200 XDOT = 698
223709
YDOT = -20249
221742 feet/sec YDOT = -6171
962787 meter/sec
ZDOT = -12937
785199 ZDOT = -3943
436929
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 16110
57688397
00016717 00000-0 10270-3 0 9065
2 25544 51
6434 350
3809 0001618 36
4108 323
7155 15
54248538 35864
Satellite: ISS
Catalog Number: 25544
Epoch time: 16110
57688397 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 350
3809 deg
Eccentricity:
0001618
Arg of perigee: 36
4108 deg
Mean anomaly: 323
7155 deg
Mean motion: 15
54248538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3586
Checksum: 323
Coasting Arc #8 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2016/111/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3513395
42 A = 6778695
59 meter
Y = 3087675
16 meter E =
0007074
Z = 4901325
04 I = 51
53731
XDOT = -6374
076959 Wp = 107
18272
YDOT = 3600
835937 meter/sec RA = 344
96281 deg
ZDOT = 2295
905144 TA = 320
32349
MA = 320
37522
Ha = 221
209 n
mi
Hp = 214
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11526887
87 X = 3454798
28
Y = 10130167
86 feet Y = 3126637
10 meter
Z = 16080462
72 Z = 4918249
86
XDOT = -20912
325982 XDOT = -6425
021344
YDOT = 11813
766196 feet/sec YDOT = 3529
272128 meter/sec
ZDOT = 7532
497190 ZDOT = 2264
816974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15188576
06 X = 4629477
98
Y = -1564203
79 feet Y = -476769
32 meter
Z = 16153363
43 Z = 4923545
17
XDOT = -5584
274301 XDOT = -1702
086807
YDOT = 22323
048886 feet/sec YDOT = 6804
065301 meter/sec
ZDOT = 7396
751237 ZDOT = 2254
529777
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 16111
60562745
00016717 00000-0 10270-3 0 9079
2 25544 51
6432 345
2509 0001778 42
4221 317
7069 15
54243152 36025
Satellite: ISS
Catalog Number: 25544
Epoch time: 16111
60562745 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 345
2509 deg
Eccentricity:
0001778
Arg of perigee: 42
4221 deg
Mean anomaly: 317
7069 deg
Mean motion: 15
54243152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 288
Coasting Arc #9 (Orbit 3616)
---------------------------------------
Vector Time (GMT): 2016/112/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1817566
82 A = 6776906
92 meter
Y = -3827203
06 meter E =
0016077
Z = -5303105
13 I = 51
49944
XDOT = 7085
817960 Wp = 83
02767
YDOT = -2880
754903 meter/sec RA = 339
95297 deg
ZDOT = -348
552791 TA = 183
63193
MA = 183
64361
Ha = 221
202 n
mi
Hp = 213
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5963145
72 X = -1748874
35
Y = -12556440
49 feet Y = -3847144
64 meter
Z = -17398638
89 Z = -5311767
42
XDOT = 23247
434252 XDOT = 7119
197792
YDOT = -9451
295615 feet/sec YDOT = -2801
329962 meter/sec
ZDOT = -1143
545903 ZDOT = -314
049776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13278077
49 X = -4047158
02
Y = -3953716
98 feet Y = -1205092
94 meter
Z = -17435501
72 Z = -5314340
92
XDOT = 8068
065256 XDOT = 2459
146290
YDOT = -22701
614097 feet/sec YDOT = -6919
451977 meter/sec
ZDOT = -993
121608 ZDOT = -302
703466
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 16112
57006417
00016717 00000-0 10270-3 0 9086
2 25544 51
6417 340
4408 0001678 43
5343 316
5942 15
54293950 36173
Satellite: ISS
Catalog Number: 25544
Epoch time: 16112
57006417 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 340
4408 deg
Eccentricity:
0001678
Arg of perigee: 43
5343 deg
Mean anomaly: 316
5942 deg
Mean motion: 15
54293950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3617
Checksum: 303
Coasting Arc #10 (Orbit 3632)
---------------------------------------
Vector Time (GMT): 2016/113/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 38359
90 A = 6777805
98 meter
Y = 4462592
61 meter E =
0006725
Z = 5097613
53 I = 51
47278
XDOT = -7238
263276 Wp = 52
40858
YDOT = 1942
451162 meter/sec RA = 334
94084 deg
ZDOT = -1640
498319 TA = 53
48527
MA = 53
42335
Ha = 221
191 n
mi
Hp = 213
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 125852
68 X = -36307
26
Y = 14641051
88 feet Y = 4462604
42 meter
Z = 16724453
85 Z = 5097618
24
XDOT = -23747
582927 XDOT = -7251
477297
YDOT = 6372
871265 feet/sec YDOT = 1861
434097 meter/sec
ZDOT = -5382
212332 ZDOT = -1675
692876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11133225
68 X = 3393407
19
Y = 9510859
29 feet Y = 2898909
91 meter
Z = 16723589
25 Z = 5097350
00
XDOT = -9891
045842 XDOT = -3014
790773
YDOT = 21343
394071 feet/sec YDOT = 6505
466513 meter/sec
ZDOT = -5535
444025 ZDOT = -1687
203339
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 16113
59878991
00016717 00000-0 10270-3 0 9094
2 25544 51
6418 335
3111 0001597 45
8731 314
2553 15
54294791 36339
Satellite: ISS
Catalog Number: 25544
Epoch time: 16113
59878991 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 335
3111 deg
Eccentricity:
0001597
Arg of perigee: 45
8731 deg
Mean anomaly: 314
2553 deg
Mean motion: 15
54294791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3633
Checksum: 327
Coasting Arc #11 (Orbit 3647)
---------------------------------------
Vector Time (GMT): 2016/114/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1633160
60 A = 6780831
75 meter
Y = -4948614
53 meter E =
0009569
Z = -4347933
17 I = 51
45293
XDOT = 6801
603075 Wp = 101
70849
YDOT = -772
287663 meter/sec RA = 329
93068 deg
ZDOT = 3438
312378 TA = 203
29272
MA = 203
33611
Ha = 221
205 n
mi
Hp = 213
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5358138
45 X = 1709496
67
Y = -16235611
97 feet Y = -4929924
82 meter
Z = -14264872
62 Z = -4339813
88
XDOT = 22314
970720 XDOT = 6793
031303
YDOT = -2533
752175 feet/sec YDOT = -696
275379 meter/sec
ZDOT = 11280
552421 ZDOT = 3471
332734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9038861
78 X = -2755045
07
Y = -14547726
22 feet Y = -4434146
95 meter
Z = -14228632
19 Z = -4336887
09
XDOT = 11162
719507 XDOT = 3402
396906
YDOT = -18094
628506 feet/sec YDOT = -5515
242769 meter/sec
ZDOT = 11424
102063 ZDOT = 3482
066309
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 16114
56321280
00016717 00000-0 10270-3 0 9108
2 25544 51
6404 330
5003 0001617 51
3633 308
7664 15
54311741 36489
Satellite: ISS
Catalog Number: 25544
Epoch time: 16114
56321280 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 330
5003 deg
Eccentricity:
0001617
Arg of perigee: 51
3633 deg
Mean anomaly: 308
7664 deg
Mean motion: 15
54311741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3648
Checksum: 271
Coasting Arc #12 (Orbit 3663)
---------------------------------------
Vector Time (GMT): 2016/115/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3102204
16 A = 6784700
81 meter
Y = 5179890
29 meter E =
0014122
Z = 3082252
31 I = 51
43938
XDOT = -5890
043831 Wp = 90
69009
YDOT = -614
499114 meter/sec RA = 324
93034 deg
ZDOT = -4876
272272 TA = 53
75638
MA = 53
62595
Ha = 221
126 n
mi
Hp = 213
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10177835
17 X = -3174868
97
Y = 16994390
71 feet Y = 5144793
18 meter
Z = 10112376
35 Z = 3067005
63
XDOT = -19324
290784 XDOT = -5859
047293
YDOT = -2016
073209 feet/sec YDOT = -680
192338 meter/sec
ZDOT = -15998
268609 ZDOT = -4904
809881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6889789
66 X = 2100007
89
Y = 18608700
20 feet Y = 5671931
82 meter
Z = 10045141
87 Z = 3061759
24
XDOT = -12212
974508 XDOT = -3722
514630
YDOT = 13258
869015 feet/sec YDOT = 4041
303276 meter/sec
ZDOT = -16122
071516 ZDOT = -4914
007398
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 16115
59192086
00016717 00000-0 10270-3 0 9113
2 25544 51
6408 325
3701 0001566 46
6887 313
4397 15
54353236 36640
Satellite: ISS
Catalog Number: 25544
Epoch time: 16115
59192086 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 325
3701 deg
Eccentricity:
0001566
Arg of perigee: 46
6887 deg
Mean anomaly: 313
4397 deg
Mean motion: 15
54353236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3664
Checksum: 317
Coasting Arc #13 (Orbit 3678)
---------------------------------------
Vector Time (GMT): 2016/116/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4208295
06 A = 6787814
33 meter
Y = -5104739
98 meter E =
0009860
Z = -1502325
63 I = 51
42292
XDOT = 4609
387684 Wp = 40
70453
YDOT = 2116
175300 meter/sec RA = 319
93737 deg
ZDOT = 5749
890018 TA = 302
84050
MA = 302
93540
Ha = 221
220 n
mi
Hp = 213
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13806742
32 X = 4272362
55
Y = -16747834
57 feet Y = -5057321
82 meter
Z = -4928889
87 Z = -1481726
72
XDOT = 15122
663006 XDOT = 4557
450510
YDOT = 6942
832349 feet/sec YDOT = 2167
430234 meter/sec
ZDOT = 18864
468564 ZDOT = 5772
155488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4818381
75 X = -1468642
76
Y = -21184494
76 feet Y = -6457034
00 meter
Z = -4838432
68 Z = -1474754
28
XDOT = 13112
907007 XDOT = 3996
814056
YDOT = -7291
165207 feet/sec YDOT = -2222
347155 meter/sec
ZDOT = 18960
735786 ZDOT = 5779
232268
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 16116
55632990
00016717 00000-0 10270-3 0 9124
2 25544 51
6398 320
5595 0001593 59
4929 300
6381 15
54330827 36793
Satellite: ISS
Catalog Number: 25544
Epoch time: 16116
55632990 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 320
5595 deg
Eccentricity:
0001593
Arg of perigee: 59
4929 deg
Mean anomaly: 300
6381 deg
Mean motion: 15
54330827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3679
Checksum: 331
Coasting Arc #14 (Orbit 3694)
---------------------------------------
Vector Time (GMT): 2016/117/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4949125
31 A = 6788534
64 meter
Y = 4630710
15 meter E =
0011833
Z = -289478
83 I = 51
40231
XDOT = -3090
055070 Wp = 128
42939
YDOT = -3665
781290 meter/sec RA = 314
94997 deg
ZDOT = -5984
213593 TA = 54
70046
MA = 54
58985
Ha = 221
127 n
mi
Hp = 213
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16237287
75 X = -4999133
05
Y = 15192618
59 feet Y = 4575086
13 meter
Z = -949733
68 Z = -313642
31
XDOT = -10137
975953 XDOT = -3019
764544
YDOT = -12026
841502 feet/sec YDOT = -3699
943361 meter/sec
ZDOT = -19633
246695 ZDOT = -5999
053788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2505896
11 X = 763797
13
Y = 22090120
44 feet Y = 6733068
71 meter
Z = -1055571
30 Z = -321738
13
XDOT = -14015
576765 XDOT = -4271
947798
YDOT = 673
169703 feet/sec YDOT = 205
182125 meter/sec
ZDOT = -19696
966057 ZDOT = -6003
635254
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 16117
58502221
00016717 00000-0 10270-3 0 9132
2 25544 51
6401 315
4292 0001743 55
9149 304
2169 15
54386220 36957
Satellite: ISS
Catalog Number: 25544
Epoch time: 16117
58502221 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 315
4292 deg
Eccentricity:
0001743
Arg of perigee: 55
9149 deg
Mean anomaly: 304
2169 deg
Mean motion: 15
54386220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3695
Checksum: 293
Coasting Arc #15 (Orbit 3710)
---------------------------------------
Vector Time (GMT): 2016/118/13:16:58
235
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5259640
11 A = 6786895
31 meter
Y = -3775623
71 meter E =
0015580
Z = 2010854
43 I = 51
37411
XDOT = 1518
662023 Wp = 68
59257
YDOT = 5082
805815 meter/sec RA = 309
95855 deg
ZDOT = 5542
242002 TA = 313
72003
MA = 313
84896
Ha = 221
163 n
mi
Hp = 213
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17256037
11 X = 5291701
18
Y = -12387216
90 feet Y = -3716627
65 meter
Z = 6597291
43 Z = 2036482
65
XDOT = 4982
486953 XDOT = 1434
789785
YDOT = 16675
872098 feet/sec YDOT = 5099
319558 meter/sec
ZDOT = 18183
208669 ZDOT = 5549
415647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -32865
50 X = -10017
40
Y = -21206654
66 feet Y = -6463788
34 meter
Z = 6709316
76 Z = 2044999
75
XDOT = 14841
345070 XDOT = 4523
641977
YDOT = 5769
000203 feet/sec YDOT = 1758
391262 meter/sec
ZDOT = 18213
363500 ZDOT = 5551
433195
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 16118
61370831
00016717 00000-0 10270-3 0 9148
2 25544 51
6396 310
2981 0001646 68
9656 291
1673 15
54357152 37112
Satellite: ISS
Catalog Number: 25544
Epoch time: 16118
61370831 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 310
2981 deg
Eccentricity:
0001646
Arg of perigee: 68
9656 deg
Mean anomaly: 291
1673 deg
Mean motion: 15
54357152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3711
Checksum: 314
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