[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 21st 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
265/22:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 215
0
278/01:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 213
2
Coasting Arc #1 (Orbit 1999)
---------------------------------------
Vector Time (GMT): 2016/265/17:02:53
678
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2245777
16 A = 6780114
53 meter
Y = 4215743
03 meter E =
0011147
Z = 4811678
02 I = 51
29624
XDOT = -4824
763656 Wp = 25
46550
YDOT = 5417
556325 meter/sec RA = 295
77279 deg
ZDOT = -2482
655678 TA = 89
11157
MA = 88
98385
Ha = 222
188 n
mi
Hp = 215
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7368035
31 X = 2175095
46
Y = 13831177
93 feet Y = 4240462
03 meter
Z = 15786345
22 Z = 4822415
51
XDOT = -15829
277088 XDOT = -4872
925774
YDOT = 17774
134926 feet/sec YDOT = 5363
333081 meter/sec
ZDOT = -8145
195794 ZDOT = -2506
210835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15187747
42 X = -4629225
41
Y = 3669253
03 feet Y = 1118388
32 meter
Z = 15832467
70 Z = 4825736
15
XDOT = -13117
007746 XDOT = -3998
063961
YDOT = -18530
132161 feet/sec YDOT = -5647
984283 meter/sec
ZDOT = -8249
022318 ZDOT = -2514
302003
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 16265
75418632
00016717 00000-0 10270-3 0 9003
2 25544 51
6412 296
2968 0006644 347
6794 12
4195 15
53901488 20001
Satellite: ISS
Catalog Number: 25544
Epoch time: 16265
75418632 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 296
2968 deg
Eccentricity:
0006644
Arg of perigee: 347
6794 deg
Mean anomaly: 12
4195 deg
Mean motion: 15
53901488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2000
Checksum: 318
Coasting Arc #2 (Orbit 2002)
---------------------------------------
Vector Time (GMT): 2016/265/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2892460
93 A = 6778955
48 meter
Y = -3450649
91 meter E =
0012078
Z = -5076708
77 I = 51
29195
XDOT = 4304
161809 Wp = 72
53163
YDOT = -6103
690400 meter/sec RA = 294
65969 deg
ZDOT = 1703
309949 TA = 213
98499
MA = 214
06242
Ha = 222
171 n
mi
Hp = 214
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9489701
21 X = -2828999
22
Y = -11321029
89 feet Y = -3482640
93 meter
Z = -16655868
67 Z = -5090605
32
XDOT = 14121
265778 XDOT = 4363
820912
YDOT = -20025
230970 feet/sec YDOT = -6055
224663 meter/sec
ZDOT = 5588
287234 ZDOT = 1724
364084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4117737
60 X = -1255086
42
Y = -14115956
92 feet Y = -4302543
67 meter
Z = -16715923
71 Z = -5095013
55
XDOT = 19845
909364 XDOT = 6049
033174
YDOT = -12490
159732 feet/sec YDOT = -3807
000686 meter/sec
ZDOT = 5681
315847 ZDOT = 1731
665070
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 16265
94712025
00016717 00000-0 10270-3 0 9018
2 25544 51
6438 295
3367 0006741 347
6262 12
4724 15
53917197 20035
Satellite: ISS
Catalog Number: 25544
Epoch time: 16265
94712025 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 295
3367 deg
Eccentricity:
0006741
Arg of perigee: 347
6262 deg
Mean anomaly: 12
4724 deg
Mean motion: 15
53917197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2003
Checksum: 307
Coasting Arc #3 (Orbit 2018)
---------------------------------------
Vector Time (GMT): 2016/266/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1997778
03 A = 6781732
26 meter
Y = 4795166
57 meter E =
0012698
Z = 4358764
59 I = 51
28871
XDOT = -4680
607415 Wp = 38
55223
YDOT = 5041
353115 meter/sec RA = 289
64279 deg
ZDOT = -3385
697919 TA = 85
98560
MA = 85
84046
Ha = 222
295 n
mi
Hp = 214
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6554389
88 X = 1922835
66
Y = 15732173
77 feet Y = 4817088
36 meter
Z = 14300408
76 Z = 4368286
97
XDOT = -15356
323539 XDOT = -4720
186874
YDOT = 16539
872424 feet/sec YDOT = 4988
789871 meter/sec
ZDOT = -11107
932804 ZDOT = -3408
531780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20457
63 X = -6235
48
Y = 17008661
75 feet Y = 5184240
10 meter
Z = 14341130
22 Z = 4371176
49
XDOT = -19192
538188 XDOT = -5849
885640
YDOT = 9469
249822 feet/sec YDOT = 2886
227346 meter/sec
ZDOT = -11208
535351 ZDOT = -3416
361575
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 16266
97610119
00016717 00000-0 10270-3 0 9024
2 25544 51
6434 290
2090 0006891 351
3131 8
7901 15
53955929 20198
Satellite: ISS
Catalog Number: 25544
Epoch time: 16266
97610119 = yrday
fracday
Element set: 902
Inclination: 51
6434 deg
RA of node: 290
2090 deg
Eccentricity:
0006891
Arg of perigee: 351
3131 deg
Mean anomaly: 8
7901 deg
Mean motion: 15
53955929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2019
Checksum: 306
Coasting Arc #4 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2016/267/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1165953
69 A = 6785448
46 meter
Y = -5839438
83 meter E =
0008344
Z = -3248456
38 I = 51
28978
XDOT = 4852
626208 Wp = 28
10222
YDOT = -3591
344296 meter/sec RA = 284
63431 deg
ZDOT = 4726
280718 TA = 294
03840
MA = 294
12570
Ha = 222
405 n
mi
Hp = 214
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3825307
37 X = -1084789
30
Y = -19158263
86 feet Y = -5852023
73 meter
Z = -10657665
28 Z = -3253922
72
XDOT = 15920
689659 XDOT = 4869
466582
YDOT = -11782
625643 feet/sec YDOT = -3536
984459 meter/sec
ZDOT = 15506
170336 ZDOT = 4749
894792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3497227
95 X = 1065955
08
Y = -19208179
90 feet Y = -5854653
23 meter
Z = -10680501
00 Z = -3255416
70
XDOT = 17628
350315 XDOT = 5373
121176
YDOT = -5447
935181 feet/sec YDOT = -1660
530643 meter/sec
ZDOT = 15609
916809 ZDOT = 4757
902643
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 16267
94076844
00016717 00000-0 10270-3 0 9034
2 25544 51
6424 285
4020 0006783 354
6585 5
4494 15
53916252 20349
Satellite: ISS
Catalog Number: 25544
Epoch time: 16267
94076844 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 285
4020 deg
Eccentricity:
0006783
Arg of perigee: 354
6585 deg
Mean anomaly: 5
4494 deg
Mean motion: 15
53916252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2034
Checksum: 317
Coasting Arc #5 (Orbit 2049)
---------------------------------------
Vector Time (GMT): 2016/268/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 345311
54 A = 6788509
17 meter
Y = 6536861
26 meter E =
0012572
Z = 1790109
28 I = 51
29372
XDOT = -4880
631607 Wp = 84
96105
YDOT = 1808
450638 meter/sec RA = 279
63454 deg
ZDOT = -5627
041749 TA = 75
28238
MA = 75
14307
Ha = 222
548 n
mi
Hp = 214
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1132911
89 X = 263493
46
Y = 21446395
21 feet Y = 6540265
44 meter
Z = 5873061
94 Z = 1791587
44
XDOT = -16012
570890 XDOT = -4873
157691
YDOT = 5933
237000 feet/sec YDOT = 1753
913457 meter/sec
ZDOT = -18461
423060 ZDOT = -5650
732620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6458739
77 X = -1968623
88
Y = 20480566
78 feet Y = 6242476
75 meter
Z = 5878373
78 Z = 1791728
33
XDOT = -15470
126466 XDOT = -4715
294547
YDOT = 483
201000 feet/sec YDOT = 147
279665 meter/sec
ZDOT = -18565
188744 ZDOT = -5658
669529
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 16268
96973933
00016717 00000-0 10270-3 0 9043
2 25544 51
6430 280
2743 0006869 358
7022 1
4111 15
53942902 20508
Satellite: ISS
Catalog Number: 25544
Epoch time: 16268
96973933 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 280
2743 deg
Eccentricity:
0006869
Arg of perigee: 358
7022 deg
Mean anomaly: 1
4111 deg
Mean motion: 15
53942902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2050
Checksum: 305
Coasting Arc #6 (Orbit 2064)
---------------------------------------
Vector Time (GMT): 2016/269/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 394938
64 A = 6789893
76 meter
Y = -6765475
54 meter E =
0017463
Z = -191606
91 I = 51
29224
XDOT = 4801
783593 Wp = 28
70310
YDOT = 117
688310 meter/sec RA = 274
63917 deg
ZDOT = 5984
189632 TA = 329
22136
MA = 329
32365
Ha = 222
622 n
mi
Hp = 214
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1295730
43 X = 471493
29
Y = -22196442
07 feet Y = -6760631
05 meter
Z = -628631
59 Z = -189501
79
XDOT = 15753
883179 XDOT = 4771
042139
YDOT = 386
116501 feet/sec YDOT = 171
213776 meter/sec
ZDOT = 19633
168084 ZDOT = 6007
440762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8613100
30 X = 2625272
97
Y = -20498496
98 feet Y = -6247941
88 meter
Z = -618272
12 Z = -188449
34
XDOT = 13111
770626 XDOT = 3996
467687
YDOT = 4938
471805 feet/sec YDOT = 1505
246206 meter/sec
ZDOT = 19734
680044 ZDOT = 6015
130478
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 16269
93439312
00016717 00000-0 10270-3 0 9050
2 25544 51
6415 275
4662 0006869 2
1592 357
9589 15
53930444 20651
Satellite: ISS
Catalog Number: 25544
Epoch time: 16269
93439312 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 275
4662 deg
Eccentricity:
0006869
Arg of perigee: 2
1592 deg
Mean anomaly: 357
9589 deg
Mean motion: 15
53930444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2065
Checksum: 335
Coasting Arc #7 (Orbit 2080)
---------------------------------------
Vector Time (GMT): 2016/270/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1133199
72 A = 6788970
34 meter
Y = 6532833
29 meter E =
0005771
Z = -1464101
98 I = 51
28639
XDOT = -4618
613386 Wp = 89
04018
YDOT = -2084
518304 meter/sec RA = 269
64602 deg
ZDOT = -5745
989146 TA = 107
00167
MA = 106
93841
Ha = 222
714 n
mi
Hp = 214
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3717846
85 X = -1199055
34
Y = 21433180
10 feet Y = 6519792
71 meter
Z = -4803484
19 Z = -1469767
47
XDOT = -15152
931056 XDOT = -4567
049024
YDOT = -6838
970813 feet/sec YDOT = -2135
879078 meter/sec
ZDOT = -18851
670427 ZDOT = -5768
299681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10281626
46 X = -3133839
75
Y = 19163578
21 feet Y = 5841058
64 meter
Z = -4829335
57 Z = -1471981
48
XDOT = -10694
837411 XDOT = -3259
786443
YDOT = -10497
052071 feet/sec YDOT = -3199
501471 meter/sec
ZDOT = -18948
743251 ZDOT = -5775
576943
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 16270
96335188
00016717 00000-0 10270-3 0 9062
2 25544 51
6403 270
3390 0006760 5
7128 354
4100 15
53933870 20819
Satellite: ISS
Catalog Number: 25544
Epoch time: 16270
96335188 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 270
3390 deg
Eccentricity:
0006760
Arg of perigee: 5
7128 deg
Mean anomaly: 354
4100 deg
Mean motion: 15
53933870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2081
Checksum: 295
Coasting Arc #8 (Orbit 2096)
---------------------------------------
Vector Time (GMT): 2016/271/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1827478
53 A = 6786057
71 meter
Y = -5821623
09 meter E =
0016320
Z = 2946848
02 I = 51
27791
XDOT = 4366
573173 Wp = 59
30525
YDOT = 3892
385504 meter/sec RA = 264
64579 deg
ZDOT = 4969
306755 TA = 334
57217
MA = 334
65238
Ha = 222
613 n
mi
Hp = 214
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5995664
46 X = 1878127
07
Y = -19099813
28 feet Y = -5800903
42 meter
Z = 9668136
55 Z = 2955849
22
XDOT = 14326
027472 XDOT = 4298
584254
YDOT = 12770
293647 feet/sec YDOT = 3940
835947 meter/sec
ZDOT = 16303
499852 ZDOT = 4990
352820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11392580
78 X = 3472458
62
Y = -16437134
79 feet Y = -5010038
69 meter
Z = 9708420
41 Z = 2959126
54
XDOT = 8531
870581 XDOT = 2600
514153
YDOT = 15620
660592 feet/sec YDOT = 4761
177348 meter/sec
ZDOT = 16394
754699 ZDOT = 4997
121232
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 16271
99230313
00016717 00000-0 10270-3 0 9071
2 25544 51
6400 265
2100 0006674 8
3570 351
7693 15
53976126 20977
Satellite: ISS
Catalog Number: 25544
Epoch time: 16271
99230313 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 265
2100 deg
Eccentricity:
0006674
Arg of perigee: 8
3570 deg
Mean anomaly: 351
7693 deg
Mean motion: 15
53976126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2097
Checksum: 302
Coasting Arc #9 (Orbit 2111)
---------------------------------------
Vector Time (GMT): 2016/272/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2538456
61 A = 6782370
57 meter
Y = 4719206
00 meter E =
0012913
Z = -4171774
01 I = 51
26853
XDOT = -3988
425228 Wp = 44
29631
YDOT = -5400
687058 meter/sec RA = 259
63664 deg
ZDOT = -3680
342158 TA = 187
65454
MA = 187
67427
Ha = 222
874 n
mi
Hp = 213
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8328269
71 X = -2570774
58
Y = 15482959
31 feet Y = 4690637
99 meter
Z = -13686922
61 Z = -4184184
39
XDOT = -13085
384607 XDOT = -3909
859383
YDOT = -17718
789559 feet/sec YDOT = -5444
849534 meter/sec
ZDOT = -12074
613380 ZDOT = -3699
525382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12293585
00 X = -3747084
71
Y = 12507674
29 feet Y = 3812339
12 meter
Z = -13741899
72 Z = -4188531
03
XDOT = -6532
623019 XDOT = -1991
143496
YDOT = -19785
677374 feet/sec YDOT = -6030
674464 meter/sec
ZDOT = -12157
494133 ZDOT = -3705
604212
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 16272
95694016
00016717 00000-0 10270-3 0 9083
2 25544 51
6390 260
4016 0006815 13
9510 346
1830 15
53971010 21127
Satellite: ISS
Catalog Number: 25544
Epoch time: 16272
95694016 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 260
4016 deg
Eccentricity:
0006815
Arg of perigee: 13
9510 deg
Mean anomaly: 346
1830 deg
Mean motion: 15
53971010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2112
Checksum: 284
Coasting Arc #10 (Orbit 2127)
---------------------------------------
Vector Time (GMT): 2016/273/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3226677
04 A = 6779315
56 meter
Y = -3288880
76 meter E =
0007810
Z = 4965816
81 I = 51
26432
XDOT = 3495
402892 Wp = 66
25211
YDOT = 6517
949345 meter/sec RA = 254
61875 deg
ZDOT = 2046
165661 TA = 3
76248
MA = 3
75661
Ha = 222
888 n
mi
Hp = 213
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10586210
76 X = 3239092
39
Y = -10790291
22 feet Y = -3252727
75 meter
Z = 16292049
91 Z = 4981521
93
XDOT = 11467
857257 XDOT = 3412
318287
YDOT = 21384
348246 feet/sec YDOT = 6556
573033 meter/sec
ZDOT = 6713
141932 ZDOT = 2062
942783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12982241
23 X = 3956987
13
Y = -7596219
59 feet Y = -2315327
73 meter
Z = 16361173
36 Z = 4986885
64
XDOT = 4740
884646 XDOT = 1445
021640
YDOT = 22713
253614 feet/sec YDOT = 6922
999701 meter/sec
ZDOT = 6785
345012 ZDOT = 2068
173160
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 16273
98588024
00016717 00000-0 10270-3 0 9099
2 25544 51
6386 255
2730 0006812 17
9085 342
2306 15
53936577 21286
Satellite: ISS
Catalog Number: 25544
Epoch time: 16273
98588024 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 255
2730 deg
Eccentricity:
0006812
Arg of perigee: 17
9085 deg
Mean anomaly: 342
2306 deg
Mean motion: 15
53936577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2128
Checksum: 329
Coasting Arc #11 (Orbit 2142)
---------------------------------------
Vector Time (GMT): 2016/274/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3896686
83 A = 6777793
24 meter
Y = 1701790
15 meter E =
0018582
Z = -5293396
65 I = 51
26902
XDOT = -2821
100846 Wp = 69
30857
YDOT = -7113
564333 meter/sec RA = 249
59505 deg
ZDOT = -204
374112 TA = 198
69602
MA = 198
76437
Ha = 222
962 n
mi
Hp = 213
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12784405
61 X = -3889713
78
Y = 5583301
01 feet Y = 1658252
99 meter
Z = -17366786
90 Z = -5312309
26
XDOT = -9255
580202 XDOT = -2740
352715
YDOT = -23338
465658 feet/sec YDOT = -7144
660316 meter/sec
ZDOT = -670
518740 ZDOT = -217
881260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13666138
52 X = -4165439
02
Y = 2228378
35 feet Y = 679209
72 meter
Z = -17449657
64 Z = -5318655
65
XDOT = -2945
191128 XDOT = -897
694256
YDOT = -23915
517106 feet/sec YDOT = -7289
449614 meter/sec
ZDOT = -728
358088 ZDOT = -222
003545
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 16274
95050345
00016717 00000-0 10270-3 0 9109
2 25544 51
6384 250
4649 0006659 22
3520 337
7922 15
53985744 21433
Satellite: ISS
Catalog Number: 25544
Epoch time: 16274
95050345 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 250
4649 deg
Eccentricity:
0006659
Arg of perigee: 22
3520 deg
Mean anomaly: 337
7922 deg
Mean motion: 15
53985744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2143
Checksum: 316
Coasting Arc #12 (Orbit 2158)
---------------------------------------
Vector Time (GMT): 2016/275/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4490134
60 A = 6778739
20 meter
Y = -28915
97 meter E =
0011379
Z = 5074384
46 I = 51
28496
XDOT = 1950
702250 Wp = 38
60562
YDOT = 7228
039859 meter/sec RA = 244
57094 deg
ZDOT = -1674
135890 TA = 67
69593
MA = 67
57533
Ha = 222
952 n
mi
Hp = 213
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14731412
74 X = 4465474
73
Y = -94868
66 feet Y = 21158
57 meter
Z = 16648242
98 Z = 5096136
80
XDOT = 6399
941765 XDOT = 1877
863823
YDOT = 23714
041531 feet/sec YDOT = 7249
446418 meter/sec
ZDOT = -5492
571817 ZDOT = -1664
837692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14239582
51 X = 4340224
75
Y = 3329481
40 feet Y = 1014825
93 meter
Z = 16743248
17 Z = 5103342
04
XDOT = 953
231057 XDOT = 290
544826
YDOT = 23522
620951 feet/sec YDOT = 7169
694866 meter/sec
ZDOT = -5453
120340 ZDOT = -1662
111080
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 16275
97942858
00016717 00000-0 10270-3 0 9112
2 25544 51
6391 245
3360 0006663 25
9467 334
2019 15
53966453 21590
Satellite: ISS
Catalog Number: 25544
Epoch time: 16275
97942858 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 245
3360 deg
Eccentricity:
0006663
Arg of perigee: 25
9467 deg
Mean anomaly: 334
2019 deg
Mean motion: 15
53966453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2159
Checksum: 336
Coasting Arc #13 (Orbit 2173)
---------------------------------------
Vector Time (GMT): 2016/276/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4958765
79 A = 6781440
24 meter
Y = -1513744
67 meter E =
0012191
Z = -4380078
22 I = 51
30951
XDOT = -882
364389 Wp = 78
28866
YDOT = -6823
480321 meter/sec RA = 239
55366 deg
ZDOT = 3367
526538 TA = 225
93995
MA = 226
04040
Ha = 223
055 n
mi
Hp = 213
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16268916
62 X = -4920193
29
Y = -4966353
91 feet Y = -1568981
83 meter
Z = -14370335
37 Z = -4404073
15
XDOT = -2894
896289 XDOT = -822
355167
YDOT = -22386
746460 feet/sec YDOT = -6833
011534 meter/sec
ZDOT = 11048
315414 ZDOT = 3363
386826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14711011
64 X = -4483916
35
Y = -8361365
11 feet Y = -2548544
08 meter
Z = -14474894
39 Z = -4411947
81
XDOT = 1355
404307 XDOT = 413
127233
YDOT = -21423
042430 feet/sec YDOT = -6529
743333 meter/sec
ZDOT = 11031
318920 ZDOT = 3362
346007
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 16276
94403813
00016717 00000-0 10270-3 0 9124
2 25544 51
6395 240
5281 0006665 31
2019 328
9528 15
54006975 21745
Satellite: ISS
Catalog Number: 25544
Epoch time: 16276
94403813 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 240
5281 deg
Eccentricity:
0006665
Arg of perigee: 31
2019 deg
Mean anomaly: 328
9528 deg
Mean motion: 15
54006975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2174
Checksum: 313
Coasting Arc #14 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2016/277/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5219866
67 A = 6785225
56 meter
Y = 2905519
77 meter E =
0017064
Z = 3208272
68 I = 51
33852
XDOT = -400
087837 Wp = 73
97768
YDOT = 6001
377586 meter/sec RA = 234
54716 deg
ZDOT = -4758
345674 TA = 68
72787
MA = 68
54574
Ha = 223
063 n
mi
Hp = 213
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17125546
81 X = 5171403
77
Y = 9532545
17 feet Y = 2963621
23 meter
Z = 10525829
01 Z = 3233511
87
XDOT = -1312
624136 XDOT = -444
052631
YDOT = 19689
559010 feet/sec YDOT = 5996
657144 meter/sec
ZDOT = -15611
370322 ZDOT = -4760
396741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14801702
72 X = 4511558
99
Y = 12756967
70 feet Y = 3888323
75 meter
Z = 10635610
90 Z = 3241734
20
XDOT = -4200
489912 XDOT = -1280
309325
YDOT = 17967
107314 feet/sec YDOT = 5476
374309 meter/sec
ZDOT = -15621
276140 ZDOT = -4761
364968
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 16277
97294810
00016717 00000-0 10270-3 0 9134
2 25544 51
6387 235
4002 0006547 33
9931 326
1639 15
54008627 21908
Satellite: ISS
Catalog Number: 25544
Epoch time: 16277
97294810 = yrday
fracday
Element set: 913
Inclination: 51
6387 deg
RA of node: 235
4002 deg
Eccentricity:
0006547
Arg of perigee: 33
9931 deg
Mean anomaly: 326
1639 deg
Mean motion: 15
54008627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 316
Coasting Arc #15 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2016/278/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1220690
49 A = 6780239
77 meter
Y = 4730438
18 meter E =
0016465
Z = -4717570
49 I = 51
32874
XDOT = -5779
780240 Wp = 57
91866
YDOT = -4213
152692 meter/sec RA = 233
86046 deg
ZDOT = -2727
544480 TA = 184
91930
MA = 184
93550
Ha = 223
068 n
mi
Hp = 213
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4004890
07 X = -1250580
40
Y = 15519810
30 feet Y = 4716619
92 meter
Z = -15477593
48 Z = -4723573
56
XDOT = -18962
533596 XDOT = -5718
988652
YDOT = -13822
679437 feet/sec YDOT = -4277
446488 meter/sec
ZDOT = -8948
636747 ZDOT = -2755
473547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7318557
26 X = 2230696
25
Y = 14230491
64 feet Y = 4337453
85 meter
Z = -15504560
09 Z = -4725789
92
XDOT = -22286
435315 XDOT = -6792
905484
YDOT = 1574
058732 feet/sec YDOT = 479
773101 meter/sec
ZDOT = -9069
962908 ZDOT = -2764
524694
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 16278
10156151
00016717 00000-0 10270-3 0 9146
2 25544 51
6430 234
7602 0006364 34
6563 325
5004 15
54009700 21925
Satellite: ISS
Catalog Number: 25544
Epoch time: 16278
10156151 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 234
7602 deg
Eccentricity:
0006364
Arg of perigee: 34
6563 deg
Mean anomaly: 325
5004 deg
Mean motion: 15
54009700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 275
Coasting Arc #16 (Orbit 2207)
---------------------------------------
Vector Time (GMT): 2016/279/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2458551
26 A = 6777812
97 meter
Y = -3538745
92 meter E =
0007658
Z = 5225306
41 I = 51
34182
XDOT = 5548
270654 Wp = 65
45210
YDOT = 5220
508162 meter/sec RA = 228
84294 deg
ZDOT = 927
042423 TA = 15
66081
MA = 15
63714
Ha = 222
944 n
mi
Hp = 213
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8066113
07 X = 2472556
94
Y = -11610058
81 feet Y = -3511173
90 meter
Z = 17143393
73 Z = 5237284
04
XDOT = 18202
987709 XDOT = 5484
977983
YDOT = 17127
651450 feet/sec YDOT = 5282
198853 meter/sec
ZDOT = 3041
477766 ZDOT = 953
840749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1935004
68 X = -589789
43
Y = -13938998
14 feet Y = -4248606
63 meter
Z = 17196269
42 Z = 5241422
92
XDOT = 23959
702267 XDOT = 7302
917251
YDOT = 561
252584 feet/sec YDOT = 171
069788 meter/sec
ZDOT = 3157
719898 ZDOT = 962
473025
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 16279
13046028
00016717 00000-0 10270-3 0 9152
2 25544 51
6437 229
6318 0006427 38
0730 322
0876 15
54071042 22088
Satellite: ISS
Catalog Number: 25544
Epoch time: 16279
13046028 = yrday
fracday
Element set: 915
Inclination: 51
6437 deg
RA of node: 229
6318 deg
Eccentricity:
0006427
Arg of perigee: 38
0730 deg
Mean anomaly: 322
0876 deg
Mean motion: 15
54071042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2208
Checksum: 294
Coasting Arc #17 (Orbit 2222)
---------------------------------------
Vector Time (GMT): 2016/280/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3689048
35 A = 6777839
23 meter
Y = 2258268
53 meter E =
0018949
Z = -5234071
64 I = 51
36350
XDOT = -4912
484476 Wp = 80
84103
YDOT = -5790
042654 meter/sec RA = 223
82546 deg
ZDOT = 970
213847 TA = 198
46249
MA = 198
53134
Ha = 223
156 n
mi
Hp = 212
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12103176
99 X = -3688601
38
Y = 7409017
48 feet Y = 2217017
14 meter
Z = -17172151
05 Z = -5251991
55
XDOT = -16117
075053 XDOT = -4852
086601
YDOT = -18996
202932 feet/sec YDOT = -5844
639557 meter/sec
ZDOT = 3183
116295 ZDOT = 946
497028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3644587
25 X = -1110870
19
Y = 13615817
57 feet Y = 4150101
19 meter
Z = -17250788
40 Z = -5258040
31
XDOT = -23779
700597 XDOT = -7248
052742
YDOT = -2487
110244 feet/sec YDOT = -758
071202 meter/sec
ZDOT = 3080
409691 ZDOT = 938
908874
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 16280
09504613
00016717 00000-0 10270-3 0 9169
2 25544 51
6435 224
8256 0006603 41
6386 318
5268 15
54062934 22239
Satellite: ISS
Catalog Number: 25544
Epoch time: 16280
09504613 = yrday
fracday
Element set: 916
Inclination: 51
6435 deg
RA of node: 224
8256 deg
Eccentricity:
0006603
Arg of perigee: 41
6386 deg
Mean anomaly: 318
5268 deg
Mean motion: 15
54062934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2223
Checksum: 302
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