[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 4th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 568 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 2590)
---------------------------------------
Vector Time (GMT): 2015/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2218353
39 A = 6774098
60 meter
Y = 3567424
53 meter E =
0016852
Z = -5328273
56 I = 51
78965
XDOT = -6636
231758 Wp = 73
33474
YDOT = 3817
008142 meter/sec RA = 151
29035 deg
ZDOT = -203
133863 TA = 194
70620
MA = 194
75528
Ha = 220
227 n
mi
Hp = 212
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7278062
31 X = 2204179
75
Y = 11704148
71 feet Y = 3592153
03 meter
Z = -17481212
48 Z = -5317531
09
XDOT = -21772
413904 XDOT = -6677
434475
YDOT = 12522
992591 feet/sec YDOT = 3742
567108 meter/sec
ZDOT = -666
449681 ZDOT = -235
471328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13482229
17 X = 4109383
45
Y = -3126734
32 feet Y = -953028
62 meter
Z = -17435684
87 Z = -5314396
75
XDOT = 4434
628753 XDOT = 1351
674844
YDOT = 23693
117392 feet/sec YDOT = 7221
662181 meter/sec
ZDOT = -806
032769 ZDOT = -245
678788
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 15154
51650162
00016717 00000-0 10270-3 0 9009
2 25544 51
6400 152
2987 0004625 15
9152 344
2145 15
55255899 25916
Satellite: ISS
Catalog Number: 25544
Epoch time: 15154
51650162 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 152
2987 deg
Eccentricity:
0004625
Arg of perigee: 15
9152 deg
Mean anomaly: 344
2145 deg
Mean motion: 15
55255899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2591
Checksum: 299
Coasting Arc #2 (Orbit 2606)
---------------------------------------
Vector Time (GMT): 2015/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -161200
42 A = 6775437
81 meter
Y = -4594217
85 meter E =
0010266
Z = 4974085
04 I = 51
82162
XDOT = 6901
468285 Wp = 40
82776
YDOT = -2576
241713 meter/sec RA = 146
28958 deg
ZDOT = -2145
753413 TA = 70
06743
MA = 69
95687
Ha = 220
236 n
mi
Hp = 212
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -528872
78 X = -133977
19
Y = -15072893
21 feet Y = -4595868
93 meter
Z = 16319176
64 Z = 4973367
48
XDOT = 22642
612482 XDOT = 6940
186833
YDOT = -8452
236592 feet/sec YDOT = -2498
848217 meter/sec
ZDOT = -7039
873403 ZDOT = -2112
133486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14513093
11 X = -4423590
78
Y = -4112943
21 feet Y = -1253625
09 meter
Z = 16316898
27 Z = 4973390
59
XDOT = -1233
000854 XDOT = -375
818660
YDOT = -23134
181812 feet/sec YDOT = -7051
298616 meter/sec
ZDOT = -6894
972905 ZDOT = -2101
587741
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 15155
54457158
00016717 00000-0 10270-3 0 9014
2 25544 51
6396 147
1637 0004697 18
6771 341
4554 15
55289571 26076
Satellite: ISS
Catalog Number: 25544
Epoch time: 15155
54457158 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 147
1637 deg
Eccentricity:
0004697
Arg of perigee: 18
6771 deg
Mean anomaly: 341
4554 deg
Mean motion: 15
55289571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2607
Checksum: 334
Coasting Arc #3 (Orbit 2621)
---------------------------------------
Vector Time (GMT): 2015/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1738745
30 A = 6779590
20 meter
Y = 5289317
98 meter E =
0008474
Z = -3872926
61 I = 51
86164
XDOT = -6376
625740 Wp = 71
70475
YDOT = 934
329957 meter/sec RA = 141
30178 deg
ZDOT = 4148
829668 TA = 241
74112
MA = 241
82668
Ha = 220
350 n
mi
Hp = 211
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5704544
96 X = -1778949
22
Y = 17353405
45 feet Y = 5269649
89 meter
Z = -12706452
14 Z = -3881470
11
XDOT = -20920
688122 XDOT = -6406
753223
YDOT = 3065
386997 feet/sec YDOT = 862
853388 meter/sec
ZDOT = 13611
645892 ZDOT = 4117
780115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14905816
84 X = 4543292
97
Y = 10513851
95 feet Y = 3204622
07 meter
Z = -12744095
94 Z = -3884400
44
XDOT = -2530
505696 XDOT = -771
298136
YDOT = 19884
918228 feet/sec YDOT = 6060
923076 meter/sec
ZDOT = 13478
056837 ZDOT = 4108
111724
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 15156
50837985
00016717 00000-0 10270-3 0 9022
2 25544 51
6399 142
3508 0004800 22
5996 337
5368 15
55276032 26226
Satellite: ISS
Catalog Number: 25544
Epoch time: 15156
50837985 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 142
3508 deg
Eccentricity:
0004800
Arg of perigee: 22
5996 deg
Mean anomaly: 337
5368 deg
Mean motion: 15
55276032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2622
Checksum: 322
Coasting Arc #4 (Orbit 2637)
---------------------------------------
Vector Time (GMT): 2015/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3344607
95 A = 6783880
26 meter
Y = -5499733
34 meter E =
0015129
Z = 2128154
34 I = 51
90083
XDOT = 5214
978144 Wp = 91
27172
YDOT = 1017
936548 meter/sec RA = 136
32987 deg
ZDOT = -5531
692673 TA = 65
21923
MA = 65
06190
Ha = 220
321 n
mi
Hp = 211
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10973123
20 X = 3395520
94
Y = -18043744
55 feet Y = -5462047
32 meter
Z = 6982133
67 Z = 2144524
83
XDOT = 17109
508347 XDOT = 5230
078620
YDOT = 3339
686837 feet/sec YDOT = 1076
338902 meter/sec
ZDOT = -18148
598007 ZDOT = -5506
322537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14262833
99 X = -4347311
80
Y = -15542090
80 feet Y = -4737229
27 meter
Z = 7053461
64 Z = 2149895
11
XDOT = 6892
548877 XDOT = 2100
848898
YDOT = -14561
636472 feet/sec YDOT = -4438
386797 meter/sec
ZDOT = -18039
744529 ZDOT = -5498
514132
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 15157
53643279
00016717 00000-0 10270-3 0 9038
2 25544 51
6401 137
2158 0004871 24
6889 335
4497 15
55329753 26382
Satellite: ISS
Catalog Number: 25544
Epoch time: 15157
53643279 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 137
2158 deg
Eccentricity:
0004871
Arg of perigee: 24
6889 deg
Mean anomaly: 335
4497 deg
Mean motion: 15
55329753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2638
Checksum: 334
Coasting Arc #5 (Orbit 2652)
---------------------------------------
Vector Time (GMT): 2015/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4427759
09 A = 6785771
23 meter
Y = 5130368
97 meter E =
0016522
Z = -86978
14 I = 51
92959
XDOT = -3627
620654 Wp = 40
91136
YDOT = -3039
566321 meter/sec RA = 131
37180 deg
ZDOT = 6040
444947 TA = 318
15459
MA = 318
28078
Ha = 220
348 n
mi
Hp = 211
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14526768
67 X = -4484376
52
Y = 16831919
18 feet Y = 5080538
31 meter
Z = -285361
37 Z = -108624
33
XDOT = -11901
642566 XDOT = -3622
704047
YDOT = -9972
330450 feet/sec YDOT = -3080
105841 meter/sec
ZDOT = 19817
732765 ZDOT = 6022
834348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12412558
75 X = 3783347
91
Y = 18444686
23 feet Y = 5621940
36 meter
Z = -379311
74 Z = -115614
22
XDOT = -11440
990794 XDOT = -3487
213994
YDOT = 8071
934290 feet/sec YDOT = 2460
325572 meter/sec
ZDOT = 19742
578733 ZDOT = 6017
537998
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 15158
50022523
00016717 00000-0 10270-3 0 9040
2 25544 51
6401 132
4030 0004729 30
6399 329
5030 15
55351980 26534
Satellite: ISS
Catalog Number: 25544
Epoch time: 15158
50022523 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 132
4030 deg
Eccentricity:
0004729
Arg of perigee: 30
6399 deg
Mean anomaly: 329
5030 deg
Mean motion: 15
55351980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2653
Checksum: 278
Coasting Arc #6 (Orbit 2668)
---------------------------------------
Vector Time (GMT): 2015/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5000323
35 A = 6784120
42 meter
Y = -4119453
73 meter E =
0007026
Z = -2016466
68 I = 51
94506
XDOT = 1807
379641 Wp = 98
74145
YDOT = 4921
515119 meter/sec RA = 126
41473 deg
ZDOT = -5589
981713 TA = 103
43227
MA = 103
35395
Ha = 220
453 n
mi
Hp = 211
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16405260
35 X = 5055811
67
Y = -13515268
15 feet Y = -4063226
43 meter
Z = -6615704
35 Z = -1992041
66
XDOT = 5929
723230 XDOT = 1779
365762
YDOT = 16146
703145 feet/sec YDOT = 4941
570228 meter/sec
ZDOT = -18339
835015 ZDOT = -5581
269474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9040214
60 X = -2755457
41
Y = -19273227
95 feet Y = -5874479
88 meter
Z = -6509976
09 Z = -1984240
71
XDOT = 15732
204373 XDOT = 4795
175893
YDOT = -1216
778883 feet/sec YDOT = -370
874204 meter/sec
ZDOT = -18303
262877 ZDOT = -5578
834525
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 15159
52826120
00016717 00000-0 10270-3 0 9059
2 25544 51
6409 127
2680 0004915 31
9140 328
2310 15
55344378 26697
Satellite: ISS
Catalog Number: 25544
Epoch time: 15159
52826120 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 127
2680 deg
Eccentricity:
0004915
Arg of perigee: 31
9140 deg
Mean anomaly: 328
2310 deg
Mean motion: 15
55344378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2669
Checksum: 300
Coasting Arc #7 (Orbit 2684)
---------------------------------------
Vector Time (GMT): 2015/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5016013
40 A = 6779744
96 meter
Y = 2550776
73 meter E =
0014526
Z = 3766763
80 I = 51
94903
XDOT = -23
187915 Wp = 79
79428
YDOT = -6376
027203 meter/sec RA = 121
44931 deg
ZDOT = 4275
396876 TA = 325
14751
MA = 325
24255
Ha = 220
480 n
mi
Hp = 211
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16456736
89 X = -5062461
55
Y = 8368690
07 feet Y = 2494424
43 meter
Z = 12358148
94 Z = 3742284
29
XDOT = -76
075836 XDOT = 27
343759
YDOT = -20918
724419 feet/sec YDOT = -6376
004253 meter/sec
ZDOT = 14026
892638 ZDOT = 4275
406542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4342100
80 X = 1323472
32
Y = 18016839
34 feet Y = 5491532
63 meter
Z = 12252455
61 Z = 3734548
47
XDOT = -19080
761699 XDOT = -5815
816166
YDOT = -4967
117686 feet/sec YDOT = -1513
977471 meter/sec
ZDOT = 14028
079300 ZDOT = 4275
758571
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 15160
55628664
00016717 00000-0 10270-3 0 9068
2 25544 51
6410 122
1343 0004708 35
2216 324
9248 15
55385729 26856
Satellite: ISS
Catalog Number: 25544
Epoch time: 15160
55628664 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 122
1343 deg
Eccentricity:
0004708
Arg of perigee: 35
2216 deg
Mean anomaly: 324
9248 deg
Mean motion: 15
55385729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2685
Checksum: 308
Coasting Arc #8 (Orbit 2699)
---------------------------------------
Vector Time (GMT): 2015/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4604896
57 A = 6775475
56 meter
Y = -547415
53 meter E =
0016433
Z = -4955090
75 I = 51
95042
XDOT = -1582
230251 Wp = 63
79651
YDOT = 7143
792906 meter/sec RA = 116
46787 deg
ZDOT = -2258
356553 TA = 184
20237
MA = 184
21618
Ha = 220
493 n
mi
Hp = 211
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15107928
37 X = 4634745
75
Y = -1795982
71 feet Y = -495753
34 meter
Z = -16256859
41 Z = -4932648
47
XDOT = -5191
044132 XDOT = -1651
025949
YDOT = 23437
640767 feet/sec YDOT = 7125
714860 meter/sec
ZDOT = -7409
306276 ZDOT = -2266
209394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1487474
29 X = 453382
16
Y = -15244454
75 feet Y = -4646509
81 meter
Z = -16160276
94 Z = -4925652
41
XDOT = 20689
363610 XDOT = 6306
118028
YDOT = 9914
772473 feet/sec YDOT = 3022
022650 meter/sec
ZDOT = -7444
360909 ZDOT = -2269
041205
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 15161
52005454
00016717 00000-0 10270-3 0 9073
2 25544 51
6411 117
3199 0004883 38
2723 321
8776 15
55362617 27003
Satellite: ISS
Catalog Number: 25544
Epoch time: 15161
52005454 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 117
3199 deg
Eccentricity:
0004883
Arg of perigee: 38
2723 deg
Mean anomaly: 321
8776 deg
Mean motion: 15
55362617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2700
Checksum: 300
Coasting Arc #9 (Orbit 2715)
---------------------------------------
Vector Time (GMT): 2015/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3835119
06 A = 6773679
94 meter
Y = -1645040
00 meter E =
0006811
Z = 5330823
70 I = 51
95847
XDOT = 2890
346194 Wp = 55
37958
YDOT = -7109
453057 meter/sec RA = 111
47778 deg
ZDOT = -110
653706 TA = 35
69206
MA = 35
64654
Ha = 220
620 n
mi
Hp = 211
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12582411
61 X = -3842334
16
Y = -5397112
85 feet Y = -1687967
55 meter
Z = 17489579
06 Z = 5312175
62
XDOT = 9482
763105 XDOT = 2970
168500
YDOT = -23324
977221 feet/sec YDOT = -7076
684994 meter/sec
ZDOT = -363
037092 ZDOT = -96
419488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7783436
26 X = -2372391
37
Y = 11386465
75 feet Y = 3470594
76 meter
Z = 17409704
26 Z = 5306477
86
XDOT = -20177
515955 XDOT = -6150
106863
YDOT = -13313
701783 feet/sec YDOT = -4058
016304 meter/sec
ZDOT = -300
536985 ZDOT = -91
603673
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 15162
54806286
00016717 00000-0 10270-3 0 9089
2 25544 51
6415 112
1858 0004882 40
9079 319
2440 15
55388088 27161
Satellite: ISS
Catalog Number: 25544
Epoch time: 15162
54806286 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 112
1858 deg
Eccentricity:
0004882
Arg of perigee: 40
9079 deg
Mean anomaly: 319
2440 deg
Mean motion: 15
55388088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2716
Checksum: 324
Coasting Arc #10 (Orbit 2730)
---------------------------------------
Vector Time (GMT): 2015/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2876450
81 A = 6775649
24 meter
Y = 3731926
61 meter E =
0014668
Z = -4881750
74 I = 51
97598
XDOT = -3829
389041 Wp = 90
26046
YDOT = 6160
874062 meter/sec RA = 106
48789 deg
ZDOT = 2459
699113 TA = 203
76258
MA = 203
83038
Ha = 220
552 n
mi
Hp = 211
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9437174
56 X = 2858219
69
Y = 12243853
71 feet Y = 3763991
47 meter
Z = -16016242
58 Z = -4867821
29
XDOT = -12563
612338 XDOT = -3909
945223
YDOT = 20212
841410 feet/sec YDOT = 6117
600688 meter/sec
ZDOT = 8069
878981 ZDOT = 2440
901378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13755809
04 X = 4192770
59
Y = -7186290
65 feet Y = -2190381
39 meter
Z = -15957041
96 Z = -4863706
39
XDOT = 17096
762449 XDOT = 5211
093194
YDOT = 15035
210912 feet/sec YDOT = 4582
732286 meter/sec
ZDOT = 7987
913610 ZDOT = 2434
716068
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 15163
51181228
00016717 00000-0 10270-3 0 9090
2 25544 51
6416 107
3716 0004892 44
1037 316
0505 15
55387760 27312
Satellite: ISS
Catalog Number: 25544
Epoch time: 15163
51181228 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 107
3716 deg
Eccentricity:
0004892
Arg of perigee: 44
1037 deg
Mean anomaly: 316
0505 deg
Mean motion: 15
55387760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2731
Checksum: 296
Coasting Arc #11 (Orbit 2746)
---------------------------------------
Vector Time (GMT): 2015/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1772964
00 A = 6780072
61 meter
Y = -5448475
25 meter E =
0016100
Z = 3615272
09 I = 52
00000
XDOT = 4440
257475 Wp = 75
48935
YDOT = -4406
791681 meter/sec RA = 101
51077 deg
ZDOT = -4443
403367 TA = 61
88688
MA = 61
72424
Ha = 220
570 n
mi
Hp = 211
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5816811
03 X = -1729467
91
Y = -17875574
97 feet Y = -5468058
89 meter
Z = 11861128
90 Z = 3606764
32
XDOT = 14567
773869 XDOT = 4510
789888
YDOT = -14457
977957 feet/sec YDOT = -4356
742957 meter/sec
ZDOT = -14578
095035 ZDOT = -4421
662384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18594538
39 X = -5667615
30
Y = 2908078
39 feet Y = 886382
29 meter
Z = 11825568
57 Z = 3604433
30
XDOT = -11671
774500 XDOT = -3557
556868
YDOT = -15459
787047 feet/sec YDOT = -4712
143092 meter/sec
ZDOT = -14483
783049 ZDOT = -4414
657073
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 15164
53980229
00016717 00000-0 10270-3 0 9103
2 25544 51
6425 102
2370 0004911 47
5947 312
5621 15
55415243 27476
Satellite: ISS
Catalog Number: 25544
Epoch time: 15164
53980229 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 102
2370 deg
Eccentricity:
0004911
Arg of perigee: 47
5947 deg
Mean anomaly: 312
5621 deg
Mean motion: 15
55415243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2747
Checksum: 293
Coasting Arc #12 (Orbit 2761)
---------------------------------------
Vector Time (GMT): 2015/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 671036
82 A = 6784227
62 meter
Y = 6501603
53 meter E =
0012211
Z = -1803752
39 I = 52
01939
XDOT = -4709
841755 Wp = 43
29941
YDOT = 2056
736961 meter/sec RA = 96
54970 deg
ZDOT = 5692
671326 TA = 296
97610
MA = 297
10075
Ha = 220
593 n
mi
Hp = 211
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2201564
37 X = 607046
50
Y = 21330720
25 feet Y = 6508749
95 meter
Z = -5917822
79 Z = -1800647
19
XDOT = -15452
236730 XDOT = -4760
143754
YDOT = 6747
824674 feet/sec YDOT = 2003
786449 meter/sec
ZDOT = 18676
743197 ZDOT = 5669
669693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21428915
12 X = 6531533
33
Y = 889592
83 feet Y = 271147
89 meter
Z = -5905705
72 Z = -1800059
10
XDOT = 4476
013181 XDOT = 1364
288817
YDOT = 14824
753579 feet/sec YDOT = 4518
584891 meter/sec
ZDOT = 18577
439550 ZDOT = 5662
403575
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 15165
50353443
00016717 00000-0 10270-3 0 9114
2 25544 51
6426 97
4234 0004909 50
3294 309
8292 15
55409286 27625
Satellite: ISS
Catalog Number: 25544
Epoch time: 15165
50353443 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 97
4234 deg
Eccentricity:
0004909
Arg of perigee: 50
3294 deg
Mean anomaly: 309
8292 deg
Mean motion: 15
55409286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2762
Checksum: 313
Coasting Arc #13 (Orbit 2777)
---------------------------------------
Vector Time (GMT): 2015/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 464080
08 A = 6785507
38 meter
Y = -6757147
71 meter E =
0012968
Z = -352790
86 I = 52
02788
XDOT = 4692
393788 Wp = 115
46074
YDOT = 627
939865 meter/sec RA = 91
59894 deg
ZDOT = -6032
126084 TA = 68
32268
MA = 68
18463
Ha = 220
593 n
mi
Hp = 211
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1522572
43 X = 541319
36
Y = -22169119
77 feet Y = -6751526
14 meter
Z = -1157450
34 Z = -350349
78
XDOT = 15394
992742 XDOT = 4714
325255
YDOT = 2060
170160 feet/sec YDOT = 680
536754 meter/sec
ZDOT = -19790
439909 ZDOT = -6009
277839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21788733
74 X = -6641206
05
Y = -4366503
49 feet Y = -1330910
26 meter
Z = -1145652
09 Z = -349194
76
XDOT = 3717
606125 XDOT = 1133
126347
YDOT = -13538
449899 feet/sec YDOT = -4126
519529 meter/sec
ZDOT = -19692
300355 ZDOT = -6002
213148
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 15166
53150646
00016717 00000-0 10270-3 0 9129
2 25544 51
6439 92
2886 0004883 55
0067 305
1545 15
55425228 27787
Satellite: ISS
Catalog Number: 25544
Epoch time: 15166
53150646 = yrday
fracday
Element set: 912
Inclination: 51
6439 deg
RA of node: 92
2886 deg
Eccentricity:
0004883
Arg of perigee: 55
0067 deg
Mean anomaly: 305
1545 deg
Mean motion: 15
55425228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2778
Checksum: 320
Coasting Arc #14 (Orbit 2793)
---------------------------------------
Vector Time (GMT): 2015/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1522164
27 A = 6783080
04 meter
Y = 6146120
04 meter E =
0018575
Z = 2406847
19 I = 52
01984
XDOT = -4409
709432 Wp = 69
58805
YDOT = -3216
476693 meter/sec RA = 86
64640 deg
ZDOT = 5397
527046 TA = 317
20572
MA = 317
35017
Ha = 220
641 n
mi
Hp = 211
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4993977
28 X = -1602470
12
Y = 20164435
83 feet Y = 6128648
83 meter
Z = 7896480
27 Z = 2399258
64
XDOT = -14467
550630 XDOT = -4399
633508
YDOT = -10552
745055 feet/sec YDOT = -3265
733406 meter/sec
ZDOT = 17708
422068 ZDOT = 5376
129473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19477406
88 X = 5936713
62
Y = 7260032
89 feet Y = 2212858
02 meter
Z = 7862647
49 Z = 2396534
96
XDOT = -11580
828510 XDOT = -3529
836530
YDOT = 11892
889893 feet/sec YDOT = 3624
952839 meter/sec
ZDOT = 17617
019128 ZDOT = 5369
667430
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 15167
55946889
00016717 00000-0 10270-3 0 9135
2 25544 51
6439 87
1543 0004934 57
8019 302
3612 15
55441469 27941
Satellite: ISS
Catalog Number: 25544
Epoch time: 15167
55946889 = yrday
fracday
Element set: 913
Inclination: 51
6439 deg
RA of node: 87
1543 deg
Eccentricity:
0004934
Arg of perigee: 57
8019 deg
Mean anomaly: 302
3612 deg
Mean motion: 15
55441469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2794
Checksum: 340
Coasting Arc #15 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2015/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2554005
88 A = 6778287
86 meter
Y = -4753446
85 meter E =
0012298
Z = -4115249
51 I = 52
00242
XDOT = 3833
501773 Wp = 67
00265
YDOT = 5394
445338 meter/sec RA = 81
68069 deg
ZDOT = -3856
340950 TA = 163
30792
MA = 163
26741
Ha = 220
579 n
mi
Hp = 210
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8379284
37 X = 2626960
55
Y = -15595298
07 feet Y = -4724477
76 meter
Z = -13501474
76 Z = -4102666
16
XDOT = 12577
105556 XDOT = 3791
627513
YDOT = 17698
311475 feet/sec YDOT = 5437
080500 meter/sec
ZDOT = -12652
037236 ZDOT = -3837
819472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14728456
09 X = -4489233
42
Y = -9898583
48 feet Y = -3017088
24 meter
Z = -13446418
68 Z = -4098468
41
XDOT = 18090
431733 XDOT = 5513
963592
YDOT = -9857
406744 feet/sec YDOT = -3004
537576 meter/sec
ZDOT = -12573
431831 ZDOT = -3832
382022
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 15168
52317436
00016717 00000-0 10270-3 0 9144
2 25544 51
6448 82
3406 0004947 61
0909 299
0740 15
55479044 28096
Satellite: ISS
Catalog Number: 25544
Epoch time: 15168
52317436 = yrday
fracday
Element set: 914
Inclination: 51
6448 deg
RA of node: 82
3406 deg
Eccentricity:
0004947
Arg of perigee: 61
0909 deg
Mean anomaly: 299
0740 deg
Mean motion: 15
55479044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2809
Checksum: 324
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