[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 28th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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 333)
---------------------------------------
Vector Time (GMT): 2015/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5002098
85 A = 6780346
56 meter
Y = 24235
69 meter E =
0009007
Z = -4585610
41 I = 51
36787
XDOT = 2722
875033 Wp = 36
97323
YDOT = -6501
751044 meter/sec RA = 312
61294 deg
ZDOT = -3000
563872 TA = 202
91476
MA = 202
95497
Ha = 220
396 n
mi
Hp = 216
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16411085
47 X = -4979722
94
Y = 79513
41 feet Y = -31576
39 meter
Z = -15044653
58 Z = -4609855
26
XDOT = 8933
317039 XDOT = 2809
952422
YDOT = -21331
204211 feet/sec YDOT = -6470
815461 meter/sec
ZDOT = -9844
369660 ZDOT = -2987
124585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16309639
01 X = 4971177
97
Y = -413232
87 feet Y = -125953
38 meter
Z = -15149144
00 Z = -4617459
09
XDOT = -8586
085010 XDOT = -2617
038711
YDOT = 20323
033225 feet/sec YDOT = 6194
460527 meter/sec
ZDOT = -9785
218051 ZDOT = -2982
534462
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 15266
52140520
00016717 00000-0 10270-3 0 9006
2 25544 51
6443 313
1266 0005567 311
2859 48
7814 15
54113832 3344
Satellite: ISS
Catalog Number: 25544
Epoch time: 15266
52140520 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 313
1266 deg
Eccentricity:
0005567
Arg of perigee: 311
2859 deg
Mean anomaly: 48
7814 deg
Mean motion: 15
54113832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 334
Checksum: 284
Coasting Arc #2 (Orbit 349)
---------------------------------------
Vector Time (GMT): 2015/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4108936
82 A = 6777753
40 meter
Y = 1466122
11 meter E =
0001931
Z = 5187214
31 I = 51
33801
XDOT = -3831
275201 Wp = 341
65605
YDOT = 6535
572236 meter/sec RA = 307
59658 deg
ZDOT = 1189
556642 TA = 96
89648
MA = 96
87452
Ha = 220
438 n
mi
Hp = 215
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13480763
85 X = 4067039
42
Y = 4810111
92 feet Y = 1511837
26 meter
Z = 17018419
65 Z = 5207072
75
XDOT = -12569
800529 XDOT = -3909
851215
YDOT = 21442
166129 feet/sec YDOT = 6492
289179 meter/sec
ZDOT = 3902
744887 ZDOT = 1170
753524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13543855
91 X = -4128167
28
Y = -4303641
99 feet Y = -1311750
08 meter
Z = 17103725
06 Z = 5213215
40
XDOT = 11462
559535 XDOT = 3493
788146
YDOT = -20914
841610 feet/sec YDOT = -6374
843723 meter/sec
ZDOT = 3820
484737 ZDOT = 1164
483748
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 15267
55023716
00016717 00000-0 10270-3 0 9018
2 25544 51
6437 307
9979 0005595 316
3135 43
7574 15
54142443 3509
Satellite: ISS
Catalog Number: 25544
Epoch time: 15267
55023716 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 307
9979 deg
Eccentricity:
0005595
Arg of perigee: 316
3135 deg
Mean anomaly: 43
7574 deg
Mean motion: 15
54142443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 350
Checksum: 311
Coasting Arc #3 (Orbit 364)
---------------------------------------
Vector Time (GMT): 2015/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3093314
79 A = 6777554
07 meter
Y = -2973475
37 meter E =
0011223
Z = -5255540
55 I = 51
31903
XDOT = 4594
030084 Wp = 75
10038
YDOT = -6085
407218 meter/sec RA = 302
57439 deg
ZDOT = 743
199436 TA = 202
01424
MA = 202
06248
Ha = 220
676 n
mi
Hp = 215
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10148670
57 X = -3034305
36
Y = -9755496
63 feet Y = -3007737
60 meter
Z = -17242587
10 Z = -5270423
52
XDOT = 15072
277179 XDOT = 4658
126969
YDOT = -19965
246779 feet/sec YDOT = -6033
675262 meter/sec
ZDOT = 2438
318359 ZDOT = 765
672777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10559040
03 X = 3218395
40
Y = 9191034
66 feet Y = 2801427
37 meter
Z = -17306172
14 Z = -5274921
27
XDOT = -13267
029633 XDOT = -4043
790632
YDOT = 19991
772741 feet/sec YDOT = 6093
492331 meter/sec
ZDOT = 2536
295942 ZDOT = 773
063003
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 15268
51476242
00016717 00000-0 10270-3 0 9022
2 25544 51
6442 303
1894 0005669 320
1698 39
9038 15
54126759 3658
Satellite: ISS
Catalog Number: 25544
Epoch time: 15268
51476242 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 303
1894 deg
Eccentricity:
0005669
Arg of perigee: 320
1698 deg
Mean anomaly: 39
9038 deg
Mean motion: 15
54126759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 365
Checksum: 324
Coasting Arc #4 (Orbit 380)
---------------------------------------
Vector Time (GMT): 2015/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2007235
98 A = 6779534
19 meter
Y = 4392319
16 meter E =
0008894
Z = 4758777
43 I = 51
30837
XDOT = -5046
174322 Wp = 22
14148
YDOT = 5147
480327 meter/sec RA = 297
55350 deg
ZDOT = -2612
935430 TA = 93
79754
MA = 93
69585
Ha = 220
797 n
mi
Hp = 215
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6585419
87 X = 1934854
44
Y = 14410495
93 feet Y = 4414361
40 meter
Z = 15612786
83 Z = 4768351
73
XDOT = -16555
690033 XDOT = -5090
666983
YDOT = 16888
058815 feet/sec YDOT = 5090
801517 meter/sec
ZDOT = -8572
622801 ZDOT = -2637
557611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7507589
73 X = -2288313
35
Y = -13906885
86 feet Y = -4238818
81 meter
Z = 15653238
73 Z = 4771107
16
XDOT = 14226
262934 XDOT = 4336
164942
YDOT = -17485
333068 feet/sec YDOT = -5329
529519 meter/sec
ZDOT = -8679
672480 ZDOT = -2645
564172
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 15269
54358147
00016717 00000-0 10270-3 0 9030
2 25544 51
6428 298
0604 0005673 325
1758 34
9023 15
54177064 3812
Satellite: ISS
Catalog Number: 25544
Epoch time: 15269
54358147 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 298
0604 deg
Eccentricity:
0005673
Arg of perigee: 325
1758 deg
Mean anomaly: 34
9023 deg
Mean motion: 15
54177064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 381
Checksum: 316
Coasting Arc #5 (Orbit 395)
---------------------------------------
Vector Time (GMT): 2015/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -970793
40 A = 6783141
02 meter
Y = -5550488
13 meter E =
0004627
Z = -3775873
17 I = 51
30725
XDOT = 5198
905954 Wp = 39
91406
YDOT = -3759
399549 meter/sec RA = 292
53958 deg
ZDOT = 4195
962149 TA = 274
58829
MA = 274
64114
Ha = 220
952 n
mi
Hp = 215
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3185017
71 X = -890312
47
Y = -18210262
89 feet Y = -5560894
78 meter
Z = -12388035
34 Z = -3780392
76
XDOT = 17056
778063 XDOT = 5220
175560
YDOT = -12333
988021 feet/sec YDOT = -3701
142366 meter/sec
ZDOT = 13766
280018 ZDOT = 4221
269803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4718466
76 X = 1438188
67
Y = 17861584
95 feet Y = 5444211
09 meter
Z = -12406501
77 Z = -3781501
74
XDOT = -14497
887791 XDOT = -4418
956199
YDOT = 13453
593388 feet/sec YDOT = 4100
655265 meter/sec
ZDOT = 13876
017737 ZDOT = 4229
410206
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 15270
50809476
00016717 00000-0 10270-3 0 9045
2 25544 51
6436 293
2517 0005678 329
7762 30
3063 15
54170441 3963
Satellite: ISS
Catalog Number: 25544
Epoch time: 15270
50809476 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 293
2517 deg
Eccentricity:
0005678
Arg of perigee: 329
7762 deg
Mean anomaly: 30
3063 deg
Mean motion: 15
54170441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 396
Checksum: 312
Coasting Arc #6 (Orbit 411)
---------------------------------------
Vector Time (GMT): 2015/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -19608
25 A = 6786783
13 meter
Y = 6357528
83 meter E =
0010792
Z = 2368066
42 I = 51
30668
XDOT = -5120
558700 Wp = 83
45938
YDOT = 1985
018212 meter/sec RA = 287
53475 deg
ZDOT = -5349
300882 TA = 69
97549
MA = 69
85934
Ha = 221
121 n
mi
Hp = 215
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -64331
52 X = -102201
52
Y = 20858034
21 feet Y = 6356848
12 meter
Z = 7769246
79 Z = 2367769
57
XDOT = -16799
733267 XDOT = -5116
389918
YDOT = 6512
526942 feet/sec YDOT = 1927
779230 meter/sec
ZDOT = -17550
199745 ZDOT = -5374
165988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2105030
49 X = -641613
29
Y = -20752548
19 feet Y = -6325376
69 meter
Z = 7766821
45 Z = 2367327
18
XDOT = 14386
939968 XDOT = 4385
139302
YDOT = -8095
227062 feet/sec YDOT = -2467
425209 meter/sec
ZDOT = -17657
701310 ZDOT = -5382
067359
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 15271
53690151
00016717 00000-0 10270-3 0 9058
2 25544 51
6420 288
1217 0005715 334
2076 25
8791 15
54187671 4126
Satellite: ISS
Catalog Number: 25544
Epoch time: 15271
53690151 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 288
1217 deg
Eccentricity:
0005715
Arg of perigee: 334
2076 deg
Mean anomaly: 25
8791 deg
Mean motion: 15
54187671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 412
Checksum: 298
Coasting Arc #7 (Orbit 426)
---------------------------------------
Vector Time (GMT): 2015/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 885914
95 A = 6788839
76 meter
Y = -6682343
14 meter E =
0013954
Z = -731451
63 I = 51
30582
XDOT = 4866
547090 Wp = 18
86214
YDOT =
863456 meter/sec RA = 282
53816 deg
ZDOT = 5931
045851 TA = 333
19317
MA = 333
26522
Ha = 221
103 n
mi
Hp = 215
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2906545
12 X = 964125
86
Y = -21923697
97 feet Y = -6671999
06 meter
Z = -2399775
69 Z = -726957
06
XDOT = 15966
361843 XDOT = 4837
364533
YDOT = 2
832860 feet/sec YDOT = 55
122053 meter/sec
ZDOT = 19458
811846 ZDOT = 5954
616036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -193218
58 X = -58893
02
Y = 22116904
77 feet Y = 6741232
57 meter
Z = -2379212
19 Z = -725183
88
XDOT = -14108
396307 XDOT = -4300
239194
YDOT = 1965
027927 feet/sec YDOT = 598
940512 meter/sec
ZDOT = 19560
373542 ZDOT = 5962
001855
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 15272
50140188
00016717 00000-0 10270-3 0 9067
2 25544 51
6426 283
3131 0005627 336
9272 23
1628 15
54220567 4271
Satellite: ISS
Catalog Number: 25544
Epoch time: 15272
50140188 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 283
3131 deg
Eccentricity:
0005627
Arg of perigee: 336
9272 deg
Mean anomaly: 23
1628 deg
Mean motion: 15
54220567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 427
Checksum: 292
Coasting Arc #8 (Orbit 442)
---------------------------------------
Vector Time (GMT): 2015/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1679364
48 A = 6788710
55 meter
Y = 6498307
23 meter E =
0004702
Z = -1013211
18 I = 51
29804
XDOT = -4471
061428 Wp = 116
70776
YDOT = -2067
210154 meter/sec RA = 277
54305 deg
ZDOT = -5870
811082 TA = 74
31912
MA = 74
26725
Ha = 221
360 n
mi
Hp = 214
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5509725
98 X = -1746983
43
Y = 21319905
60 feet Y = 6479149
26 meter
Z = -3324183
67 Z = -1021534
35
XDOT = -14668
836705 XDOT = -4419
094423
YDOT = -6782
185545 feet/sec YDOT = -2116
918643 meter/sec
ZDOT = -19261
191214 ZDOT = -5892
404502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2438768
49 X = 743336
64
Y = -21879222
15 feet Y = -6668786
91 meter
Z = -3361204
91 Z = -1024495
26
XDOT = 13758
887629 XDOT = 4193
708949
YDOT = 4495
297049 feet/sec YDOT = 1370
166541 meter/sec
ZDOT = -19353
867229 ZDOT = -5899
058732
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 15273
53019586
00016717 00000-0 10270-3 0 9079
2 25544 51
6416 278
1827 0005750 341
5492 18
5452 15
54186406 4431
Satellite: ISS
Catalog Number: 25544
Epoch time: 15273
53019586 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 278
1827 deg
Eccentricity:
0005750
Arg of perigee: 341
5492 deg
Mean anomaly: 18
5452 deg
Mean motion: 15
54186406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 443
Checksum: 314
Coasting Arc #9 (Orbit 458)
---------------------------------------
Vector Time (GMT): 2015/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2364824
17 A = 6786104
37 meter
Y = -5782320
39 meter E =
0014449
Z = 2627163
45 I = 51
28629
XDOT = 3990
499730 Wp = 53
70419
YDOT = 3997
603743 meter/sec RA = 272
54448 deg
ZDOT = 5195
022288 TA = 336
08494
MA = 336
15199
Ha = 221
330 n
mi
Hp = 214
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7758609
48 X = 2416545
75
Y = -18970867
43 feet Y = -5755585
92 meter
Z = 8619302
67 Z = 2638777
69
XDOT = 13092
190715 XDOT = 3920
265104
YDOT = 13115
497843 feet/sec YDOT = 4041
835948 meter/sec
ZDOT = 17044
036377 ZDOT = 5214
236669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4619479
46 X = -1408017
34
Y = 19946610
12 feet Y = 6079726
76 meter
Z = 8670372
83 Z = 2642729
64
XDOT = -13432
434201 XDOT = -4094
205944
YDOT = -10571
630708 feet/sec YDOT = -3222
233040 meter/sec
ZDOT = 17126
123327 ZDOT = 5220
042390
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 15274
55898172
00016717 00000-0 10270-3 0 9089
2 25544 51
6415 273
0534 0005838 344
2609 15
8361 15
54219166 4592
Satellite: ISS
Catalog Number: 25544
Epoch time: 15274
55898172 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 273
0534 deg
Eccentricity:
0005838
Arg of perigee: 344
2609 deg
Mean anomaly: 15
8361 deg
Mean motion: 15
54219166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 459
Checksum: 325
Coasting Arc #10 (Orbit 473)
---------------------------------------
Vector Time (GMT): 2015/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2997223
30 A = 6782339
78 meter
Y = 4610010
22 meter E =
0009569
Z = -3981209
66 I = 51
27266
XDOT = -3403
771143 Wp = 34
70557
YDOT = -5617
602273 meter/sec RA = 267
53566 deg
ZDOT = -3939
321446 TA = 194
03529
MA = 194
06190
Ha = 221
586 n
mi
Hp = 214
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9833409
79 X = -3029211
31
Y = 15124705
45 feet Y = 4576314
10 meter
Z = -13061711
49 Z = -3995847
87
XDOT = -11167
228160 XDOT = -3321
564765
YDOT = -18430
453652 feet/sec YDOT = -5655
206175 meter/sec
ZDOT = -12924
282959 ZDOT = -3955
656378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6961771
24 X = 2121947
87
Y = -16592567
17 feet Y = -5057414
47 meter
Z = -13125601
93 Z = -4000683
47
XDOT = 12920
151830 XDOT = 3938
062278
YDOT = 15707
459168 feet/sec YDOT = 4787
633554 meter/sec
ZDOT = -12993
684712 ZDOT = -3960
475100
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 15275
52346381
00016717 00000-0 10270-3 0 9098
2 25544 51
6410 268
2439 0005894 348
8383 11
2638 15
54202923 4745
Satellite: ISS
Catalog Number: 25544
Epoch time: 15275
52346381 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 268
2439 deg
Eccentricity:
0005894
Arg of perigee: 348
8383 deg
Mean anomaly: 11
2638 deg
Mean motion: 15
54202923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 474
Checksum: 317
Coasting Arc #11 (Orbit 489)
---------------------------------------
Vector Time (GMT): 2015/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3554776
30 A = 6778805
40 meter
Y = -3058518
41 meter E =
0005356
Z = 4890013
53 I = 51
26301
XDOT = 2729
996717 Wp = 62
42200
YDOT = 6801
340586 meter/sec RA = 262
51686 deg
ZDOT = 2269
945351 TA = 5
29054
MA = 5
28489
Ha = 221
543 n
mi
Hp = 214
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11662651
91 X = 3564959
09
Y = -10034509
21 feet Y = -3018709
24 meter
Z = 16043351
46 Z = 4907307
10
XDOT = 8956
682143 XDOT = 2642
712910
YDOT = 22314
109533 feet/sec YDOT = 6831
381355 meter/sec
ZDOT = 7447
327268 ZDOT = 2282
994744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9426214
17 X = -2873110
08
Y = 12059902
61 feet Y = 3675858
32 meter
Z = 16118411
40 Z = 4912891
79
XDOT = -12135
334192 XDOT = -3698
849862
YDOT = -19510
025770 feet/sec YDOT = -5946
655855 meter/sec
ZDOT = 7502
375132 ZDOT = 2286
723940
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 15276
55223671
00016717 00000-0 10270-3 0 9100
2 25544 51
6407 263
1143 0006026 351
8016 8
3038 15
54220480 4909
Satellite: ISS
Catalog Number: 25544
Epoch time: 15276
55223671 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 263
1143 deg
Eccentricity:
0006026
Arg of perigee: 351
8016 deg
Mean anomaly: 8
3038 deg
Mean motion: 15
54220480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 490
Checksum: 273
Coasting Arc #12 (Orbit 504)
---------------------------------------
Vector Time (GMT): 2015/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4052149
91 A = 6777132
80 meter
Y = 1309821
74 meter E =
0015879
Z = -5284848
70 I = 51
26239
XDOT = -1929
518685 Wp = 64
97235
YDOT = -7402
502857 meter/sec RA = 257
49064 deg
ZDOT = -349
448092 TA = 201
64021
MA = 201
70739
Ha = 221
767 n
mi
Hp = 214
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13294455
09 X = -4040823
47
Y = 4297315
41 feet Y = 1264570
83 meter
Z = -17338742
47 Z = -5304506
01
XDOT = -6330
441879 XDOT = -1844
901190
YDOT = -24286
426697 feet/sec YDOT = -7423
606911 meter/sec
ZDOT = -1146
483240 ZDOT = -358
615262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11999956
35 X = 3657586
70
Y = -6946771
40 feet Y = -2117375
92 meter
Z = -17423686
78 Z = -5310739
73
XDOT = 10735
001782 XDOT = 3272
028543
YDOT = 21562
485817 feet/sec YDOT = 6572
245677 meter/sec
ZDOT = -1184
710461 ZDOT = -361
099749
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 15277
51670473
00016717 00000-0 10270-3 0 9114
2 25544 51
6406 258
3054 0006026 356
1289 3
9817 15
54220892 5055
Satellite: ISS
Catalog Number: 25544
Epoch time: 15277
51670473 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 258
3054 deg
Eccentricity:
0006026
Arg of perigee: 356
1289 deg
Mean anomaly: 3
9817 deg
Mean motion: 15
54220892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 505
Checksum: 303
Coasting Arc #13 (Orbit 520)
---------------------------------------
Vector Time (GMT): 2015/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4445990
26 A = 6777887
63 meter
Y = 530395
49 meter E =
0009812
Z = 5087125
07 I = 51
27268
XDOT = 982
710086 Wp = 23
89022
YDOT = 7431
225150 meter/sec RA = 252
46321 deg
ZDOT = -1623
730992 TA = 81
91130
MA = 81
80000
Ha = 221
745 n
mi
Hp = 214
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14586582
20 X = 4415017
32
Y = 1740142
70 feet Y = 579940
76 meter
Z = 16690042
89 Z = 5108647
67
XDOT = 3224
114456 XDOT = 907
426803
YDOT = 24380
659941 feet/sec YDOT = 7441
793383 meter/sec
ZDOT = -5327
201417 ZDOT = -1619
140671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14500237
56 X = -4419672
41
Y = 1561281
41 feet Y = 475878
57 meter
Z = 16782714
91 Z = 5115371
50
XDOT = -8546
773197 XDOT = -2605
056470
YDOT = -21964
397960 feet/sec YDOT = -6694
748498 meter/sec
ZDOT = -5308
689226 ZDOT = -1618
088476
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 15278
54546300
00016717 00000-0 10270-3 0 9120
2 25544 51
6403 253
1756 0006119 358
9467 1
1671 15
54242898 5211
Satellite: ISS
Catalog Number: 25544
Epoch time: 15278
54546300 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 253
1756 deg
Eccentricity:
0006119
Arg of perigee: 358
9467 deg
Mean anomaly: 1
1671 deg
Mean motion: 15
54242898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 521
Checksum: 305
Coasting Arc #14 (Orbit 535)
---------------------------------------
Vector Time (GMT): 2015/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4702867
32 A = 6780876
79 meter
Y = -2224679
39 meter E =
0009176
Z = -4354739
61 I = 51
29314
XDOT = 102
846328 Wp = 70
71637
YDOT = -6864
284717 meter/sec RA = 247
44245 deg
ZDOT = 3404
508454 TA = 233
94517
MA = 234
03022
Ha = 221
922 n
mi
Hp = 213
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15429354
73 X = -4656487
11
Y = -7298816
88 feet Y = -2277011
06 meter
Z = -14287203
46 Z = -4377472
44
XDOT = 337
422337 XDOT = 163
058891
YDOT = -22520
619150 feet/sec YDOT = -6862
797611 meter/sec
ZDOT = 11169
647158 ZDOT = 3405
155005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16647640
92 X = 5074200
95
Y = 3375666
41 feet Y = 1028903
12 meter
Z = -14384812
34 Z = -4384490
80
XDOT = 5432
099810 XDOT = 1655
704022
YDOT = 20702
008898 feet/sec YDOT = 6309
972312 meter/sec
ZDOT = 11173
595764 ZDOT = 3405
711989
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 15279
50991696
00016717 00000-0 10270-3 0 9130
2 25544 51
6403 248
3667 0006191 2
8848 357
2339 15
54233338 5367
Satellite: ISS
Catalog Number: 25544
Epoch time: 15279
50991696 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 248
3667 deg
Eccentricity:
0006191
Arg of perigee: 2
8848 deg
Mean anomaly: 357
2339 deg
Mean motion: 15
54233338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 536
Checksum: 331
Coasting Arc #15 (Orbit 551)
---------------------------------------
Vector Time (GMT): 2015/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4747648
87 A = 6784723
97 meter
Y = 3711821
80 meter E =
0014489
Z = 3111182
89 I = 51
31953
XDOT = -1344
438845 Wp = 69
24696
YDOT = 5794
616412 meter/sec RA = 242
43211 deg
ZDOT = -4838
348256 TA = 74
76375
MA = 74
60360
Ha = 221
996 n
mi
Hp = 213
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15576275
82 X = 4690676
50
Y = 12177893
05 feet Y = 3764594
94 meter
Z = 10207292
94 Z = 3134107
33
XDOT = -4410
888600 XDOT = -1385
632755
YDOT = 19011
208702 feet/sec YDOT = 5779
351135 meter/sec
ZDOT = -15873
845985 ZDOT = -4844
980016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18131030
70 X = -5526338
16
Y = -7757118
60 feet Y = -2364369
75 meter
Z = 10305489
48 Z = 3141113
19
XDOT = -1314
850263 XDOT = -400
766360
YDOT = -18155
582281 feet/sec YDOT = -5533
821479 meter/sec
ZDOT = -15903
402047 ZDOT = -4847
356944
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 15280
53866002
00016717 00000-0 10270-3 0 9148
2 25544 51
6404 243
2366 0006258 6
0608 354
0619 15
54274736 5523
Satellite: ISS
Catalog Number: 25544
Epoch time: 15280
53866002 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 243
2366 deg
Eccentricity:
0006258
Arg of perigee: 6
0608 deg
Mean anomaly: 354
0619 deg
Mean motion: 15
54274736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 552
Checksum: 295
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