[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 2nd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4736 12 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
162/10:17:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 211
5
Coasting Arc #1 (Orbit 2559)
---------------------------------------
Vector Time (GMT): 2015/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5630739
42 A = 6780635
60 meter
Y = 1106611
24 meter E =
0007873
Z = -3622036
89 I = 51
75290
XDOT = -3814
407778 Wp = 49
37751
YDOT = 4966
025714 meter/sec RA = 161
28153 deg
ZDOT = -4413
858189 TA = 173
43822
MA = 173
42791
Ha = 220
074 n
mi
Hp = 212
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18473554
51 X = 5635541
32
Y = 3630614
29 feet Y = 1169605
07 meter
Z = -11883323
14 Z = -3594671
63
XDOT = -12514
461213 XDOT = -3848
214349
YDOT = 16292
735282 feet/sec YDOT = 4923
181939 meter/sec
ZDOT = -14481
162036 ZDOT = -4432
469753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10086788
21 X = 3074453
05
Y = -15983903
63 feet Y = -4871893
82 meter
Z = -11765988
01 Z = -3586273
14
XDOT = 9536
328507 XDOT = 2906
672929
YDOT = 16734
098047 feet/sec YDOT = 5100
553085 meter/sec
ZDOT = -14561
944862 ZDOT = -4438
480794
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 15152
52459251
00016717 00000-0 10270-3 0 9004
2 25544 51
6400 162
2455 0004566 8
4510 351
6719 15
55244044 25601
Satellite: ISS
Catalog Number: 25544
Epoch time: 15152
52459251 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 162
2455 deg
Eccentricity:
0004566
Arg of perigee: 8
4510 deg
Mean anomaly: 351
6719 deg
Mean motion: 15
55244044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2560
Checksum: 279
Coasting Arc #2 (Orbit 2575)
---------------------------------------
Vector Time (GMT): 2015/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4113269
91 A = 6776227
36 meter
Y = -2354929
83 meter E =
0007374
Z = 4836105
69 I = 51
76708
XDOT = 5595
105437 Wp = 82
64706
YDOT = -4615
990091 meter/sec RA = 156
28984 deg
ZDOT = 2508
731256 TA = 342
75009
MA = 342
77514
Ha = 220
283 n
mi
Hp = 212
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13494980
03 X = -4110123
13
Y = -7726147
72 feet Y = -2400910
07 meter
Z = 15866488
50 Z = 4816131
31
XDOT = 18356
645136 XDOT = 5634
120053
YDOT = -15144
324445 feet/sec YDOT = -4553
204115 meter/sec
ZDOT = 8230
745591 ZDOT = 2536
005798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11943599
65 X = -3640409
17
Y = 10092601
68 feet Y = 3076224
99 meter
Z = 15781100
11 Z = 4810079
31
XDOT = -7156
883104 XDOT = -2181
417970
YDOT = -21535
852722 feet/sec YDOT = -6564
127910 meter/sec
ZDOT = 8348
695249 ZDOT = 2544
682312
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 15153
55268072
00016717 00000-0 10270-3 0 9018
2 25544 51
6391 157
1107 0004673 12
2291 347
8975 15
55248982 25768
Satellite: ISS
Catalog Number: 25544
Epoch time: 15153
55268072 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 157
1107 deg
Eccentricity:
0004673
Arg of perigee: 12
2291 deg
Mean anomaly: 347
8975 deg
Mean motion: 15
55248982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2576
Checksum: 320
Coasting Arc #3 (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 = 2221924
92 A = 6774120
78 meter
Y = 3565431
47 meter E =
0016813
Z = -5328099
34 I = 51
78892
XDOT = -6634
724015 Wp = 73
04903
YDOT = 3819
500132 meter/sec RA = 151
28938 deg
ZDOT = -206
660141 TA = 194
95795
MA = 195
00774
Ha = 220
234 n
mi
Hp = 212
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7289779
91 X = 2207772
45
Y = 11697609
83 feet Y = 3590200
04 meter
Z = -17480640
88 Z = -5317339
47
XDOT = -21767
467242 XDOT = -6675
937581
YDOT = 12531
168413 feet/sec YDOT = 3745
075898 meter/sec
ZDOT = -678
018835 ZDOT = -238
990307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13479909
00 X = 4108676
26
Y = -3139947
37 feet Y = -957055
96 meter
Z = -17435038
17 Z = -5314199
63
XDOT = 4443
036641 XDOT = 1354
237568
YDOT = 23691
236013 feet/sec YDOT = 7221
088737 meter/sec
ZDOT = -817
571006 ZDOT = -249
195643
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
51650751
00016717 00000-0 10270-3 0 9025
2 25544 51
6393 152
2976 0004669 15
0023 345
1268 15
55248543 25915
Satellite: ISS
Catalog Number: 25544
Epoch time: 15154
51650751 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 152
2976 deg
Eccentricity:
0004669
Arg of perigee: 15
0023 deg
Mean anomaly: 345
1268 deg
Mean motion: 15
55248543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2591
Checksum: 304
Coasting Arc #4 (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 = -168411
20 A = 6775462
57 meter
Y = -4591676
02 meter E =
0010270
Z = 4976298
44 I = 51
82087
XDOT = 6901
148149 Wp = 40
29029
YDOT = -2582
382846 meter/sec RA = 146
28861 deg
ZDOT = -2139
126492 TA = 70
53817
MA = 70
42724
Ha = 220
252 n
mi
Hp = 212
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -552530
19 X = -141226
61
Y = -15064553
89 feet Y = -4593407
95 meter
Z = 16326438
45 Z = 4975545
76
XDOT = 22641
562167 XDOT = 6939
903201
YDOT = -8472
384664 feet/sec YDOT = -2504
992726 meter/sec
ZDOT = -7018
131534 ZDOT = -2105
508032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14512585
08 X = -4423435
93
Y = -4087820
82 feet Y = -1245967
78 meter
Z = 16324008
73 Z = 4975557
86
XDOT = -1250
675937 XDOT = -381
206026
YDOT = -23139
390971 feet/sec YDOT = -7052
886368 meter/sec
ZDOT = -6873
236263 ZDOT = -2094
962413
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
54458378
00016717 00000-0 10270-3 0 9031
2 25544 51
6389 147
1626 0004747 17
7765 342
3554 15
55278000 26070
Satellite: ISS
Catalog Number: 25544
Epoch time: 15155
54458378 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 147
1626 deg
Eccentricity:
0004747
Arg of perigee: 17
7765 deg
Mean anomaly: 342
3554 deg
Mean motion: 15
55278000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2607
Checksum: 325
Coasting Arc #5 (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 = -1727187
47 A = 6779611
73 meter
Y = 5287693
38 meter E =
0008468
Z = -3880300
19 I = 51
86083
XDOT = -6380
633741 Wp = 71
30612
YDOT = 946
490268 meter/sec RA = 141
30080 deg
ZDOT = 4139
935413 TA = 242
02375
MA = 242
10947
Ha = 220
375 n
mi
Hp = 212
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5666625
54 X = -1767338
26
Y = 17348075
38 feet Y = 5268154
83 meter
Z = -12730643
67 Z = -3888787
42
XDOT = -20933
837732 XDOT = -6410
853701
YDOT = 3105
283033 feet/sec YDOT = 874
968364 meter/sec
ZDOT = 13582
465265 ZDOT = 4108
866166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14912008
12 X = 4545180
08
Y = 10475909
69 feet Y = 3193057
27 meter
Z = -12768045
38 Z = -3891700
23
XDOT = -2499
013872 XDOT = -761
699428
YDOT = 19908
671750 feet/sec YDOT = 6068
163149 meter/sec
ZDOT = 13448
789444 ZDOT = 4099
191023
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
50840050
00016717 00000-0 10270-3 0 9041
2 25544 51
6392 142
3496 0004854 21
6970 338
4388 15
55260344 26227
Satellite: ISS
Catalog Number: 25544
Epoch time: 15156
50840050 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 142
3496 deg
Eccentricity:
0004854
Arg of perigee: 21
6970 deg
Mean anomaly: 338
4388 deg
Mean motion: 15
55260344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2622
Checksum: 302
Coasting Arc #6 (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 = 3330078
51 A = 6783910
11 meter
Y = -5502710
46 meter E =
0015095
Z = 2143488
35 I = 51
90000
XDOT = 5226
808685 Wp = 90
75492
YDOT = 998
365346 meter/sec RA = 136
32882 deg
ZDOT = -5523
963939 TA = 65
55638
MA = 65
39898
Ha = 220
356 n
mi
Hp = 211
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10925454
43 X = 3380951
38
Y = -18053512
01 feet Y = -5465187
14 meter
Z = 7032442
10 Z = 2159788
16
XDOT = 17148
322457 XDOT = 5242
089588
YDOT = 3275
476858 feet/sec YDOT = 1056
901005 meter/sec
ZDOT = -18123
241271 ZDOT = -5498
535898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14285638
76 X = -4354262
69
Y = -15498754
03 feet Y = -4724020
23 meter
Z = 7103466
85 Z = 2165136
70
XDOT = 6844
887197 XDOT = 2086
321618
YDOT = -14615
052887 feet/sec YDOT = -4454
668120 meter/sec
ZDOT = -18014
135469 ZDOT = -5490
708491
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
53646522
00016717 00000-0 10270-3 0 9054
2 25544 51
6394 137
2146 0004932 23
8067 336
3314 15
55309872 26385
Satellite: ISS
Catalog Number: 25544
Epoch time: 15157
53646522 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 137
2146 deg
Eccentricity:
0004932
Arg of perigee: 23
8067 deg
Mean anomaly: 336
3314 deg
Mean motion: 15
55309872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2638
Checksum: 313
Coasting Arc #7 (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 = -4413173
96 A = 6785839
69 meter
Y = 5142508
63 meter E =
0016526
Z = -111029
29 I = 51
92885
XDOT = -3650
339363 Wp = 40
44237
YDOT = -3013
317129 meter/sec RA = 131
37071 deg
ZDOT = 6039
903351 TA = 318
36525
MA = 318
49095
Ha = 220
392 n
mi
Hp = 211
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14478917
20 X = -4469811
39
Y = 16871747
47 feet Y = 5092840
96 meter
Z = -364269
32 Z = -132604
66
XDOT = -11976
179014 XDOT = -3645
711962
YDOT = -9886
211053 feet/sec YDOT = -3054
112322 meter/sec
ZDOT = 19815
955875 ZDOT = 6022
181689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12463707
79 X = 3798938
13
Y = 18408527
85 feet Y = 5610919
29 meter
Z = -457917
52 Z = -139573
26
XDOT = -11380
174590 XDOT = -3468
677215
YDOT = 8162
777245 feet/sec YDOT = 2488
014504 meter/sec
ZDOT = 19740
319816 ZDOT = 6016
849480
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
50027132
00016717 00000-0 10270-3 0 9063
2 25544 51
6393 132
4019 0004794 29
6894 330
4530 15
55327502 26530
Satellite: ISS
Catalog Number: 25544
Epoch time: 15158
50027132 = yrday
fracday
Element set: 906
Inclination: 51
6393 deg
RA of node: 132
4019 deg
Eccentricity:
0004794
Arg of perigee: 29
6894 deg
Mean anomaly: 330
4530 deg
Mean motion: 15
55327502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2653
Checksum: 297
Coasting Arc #8 (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 = 4990417
01 A = 6784253
73 meter
Y = -4146383
33 meter E =
0007029
Z = -1985956
91 I = 51
94449
XDOT = 1842
262548 Wp = 98
66738
YDOT = 4892
692993 meter/sec RA = 126
41376 deg
ZDOT = -5603
809288 TA = 103
15327
MA = 103
07482
Ha = 220
507 n
mi
Hp = 211
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16372759
20 X = 5046058
98
Y = -13603619
84 feet Y = -4090265
95 meter
Z = -6515606
65 Z = -1961579
63
XDOT = 6044
168464 XDOT = 1814
635541
YDOT = 16052
142366 feet/sec YDOT = 4913
140350 meter/sec
ZDOT = -18385
201076 ZDOT = -5594
926658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9134001
61 X = -2784043
69
Y = -19262911
27 feet Y = -5871335
35 meter
Z = -6410078
86 Z = -1953792
04
XDOT = 15669
621841 XDOT = 4776
100737
YDOT = -1344
455734 feet/sec YDOT = -409
790108 meter/sec
ZDOT = -18347
891354 ZDOT = -5592
437285
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
52832466
00016717 00000-0 10270-3 0 9071
2 25544 51
6401 127
2668 0004988 31
0145 329
1302 15
55315983 26692
Satellite: ISS
Catalog Number: 25544
Epoch time: 15159
52832466 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 127
2668 deg
Eccentricity:
0004988
Arg of perigee: 31
0145 deg
Mean anomaly: 329
1302 deg
Mean motion: 15
55315983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2669
Checksum: 317
Coasting Arc #9 (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 = -5015718
55 A = 6779937
54 meter
Y = 2596188
53 meter E =
0014640
Z = 3736180
08 I = 51
94861
XDOT = -69
222434 Wp = 79
00414
YDOT = -6352
514560 meter/sec RA = 121
44871 deg
ZDOT = 4309
760788 TA = 325
47477
MA = 325
56976
Ha = 220
544 n
mi
Hp = 211
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16455769
51 X = -5062525
96
Y = 8517678
91 feet Y = 2539837
52 meter
Z = 12257808
67 Z = 3711701
14
XDOT = -227
107722 XDOT = -19
117189
YDOT = -20841
583201 feet/sec YDOT = -6353
008785 meter/sec
ZDOT = 14139
635130 ZDOT = 4309
545792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4487454
95 X = 1367776
27
Y = 18049544
53 feet Y = 5501501
17 meter
Z = 12152109
61 Z = 3703963
01
XDOT = -19038
197772 XDOT = -5802
842681
YDOT = -4812
293901 feet/sec YDOT = -1466
787181 meter/sec
ZDOT = 14139
851773 ZDOT = 4309
826820
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
55637041
00016717 00000-0 10270-3 0 9089
2 25544 51
6403 122
1332 0004788 34
2990 325
8472 15
55352855 26855
Satellite: ISS
Catalog Number: 25544
Epoch time: 15160
55637041 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 122
1332 deg
Eccentricity:
0004788
Arg of perigee: 34
2990 deg
Mean anomaly: 325
8472 deg
Mean motion: 15
55352855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2685
Checksum: 308
Coasting Arc #10 (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 = 4619181
69 A = 6775669
17 meter
Y = -612417
62 meter E =
0016356
Z = -4934335
82 I = 51
94997
XDOT = -1528
762409 Wp = 63
08957
YDOT = 7137
045926 meter/sec RA = 116
46783 deg
ZDOT = -2315
624647 TA = 184
32076
MA = 184
33490
Ha = 220
567 n
mi
Hp = 211
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15154795
59 X = 4649655
87
Y = -2009244
15 feet Y = -560592
19 meter
Z = -16188765
81 Z = -4911822
63
XDOT = -5015
624700 XDOT = -1597
208446
YDOT = 23415
505007 feet/sec YDOT = 7119
567751 meter/sec
ZDOT = -7597
193725 ZDOT = -2323
216902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1289025
72 X = 392895
04
Y = -15335294
84 feet Y = -4674197
87 meter
Z = -16091866
72 Z = -4904800
98
XDOT = 20698
756577 XDOT = 6308
981005
YDOT = 9751
970886 feet/sec YDOT = 2972
400726 meter/sec
ZDOT = -7631
126828 ZDOT = -2325
967457
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
52016003
00016717 00000-0 10270-3 0 9097
2 25544 51
6404 117
3189 0004970 37
3644 322
7854 15
55325946 27004
Satellite: ISS
Catalog Number: 25544
Epoch time: 15161
52016003 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 117
3189 deg
Eccentricity:
0004970
Arg of perigee: 37
3644 deg
Mean anomaly: 322
7854 deg
Mean motion: 15
55325946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2700
Checksum: 295
Coasting Arc #11 (Orbit 2714)
---------------------------------------
Vector Time (GMT): 2015/162/10:17:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4580818
90 A = 6778841
39 meter
Y = 2903421
06 meter E =
0013777
Z = 4053977
78 I = 51
97249
XDOT = -675
795690 Wp = 84
08552
YDOT = -6562
226369 meter/sec RA = 111
85910 deg
ZDOT = 3926
161984 TA = 325
38425
MA = 325
47386
Ha = 220
627 n
mi
Hp = 211
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15028933
40 X = -4632638
06
Y = 9525659
65 feet Y = 2851905
31 meter
Z = 13300452
03 Z = 4031599
21
XDOT = -2217
177462 XDOT = -621
437064
YDOT = -21529
614070 feet/sec YDOT = -6569
479910 meter/sec
ZDOT = 12881
108870 ZDOT = 3923
010622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1532607
12 X = -467138
65
Y = 17799502
88 feet Y = 5425288
48 meter
Z = 13203706
58 Z = 4024489
77
XDOT = -17250
354972 XDOT = -5257
908196
YDOT = -11055
968320 feet/sec YDOT = -3369
859144 meter/sec
ZDOT = 12868
759927 ZDOT = 3922
398026
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
48394093
00016717 00000-0 10270-3 0 9103
2 25544 51
6394 112
5057 0004818 40
8399 319
3114 15
55366515 27154
Satellite: ISS
Catalog Number: 25544
Epoch time: 15162
48394093 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 112
5057 deg
Eccentricity:
0004818
Arg of perigee: 40
8399 deg
Mean anomaly: 319
3114 deg
Mean motion: 15
55366515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2715
Checksum: 311
Coasting Arc #12 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2015/163/10:17:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4408919
13 A = 6774952
45 meter
Y = -800586
10 meter E =
0017597
Z = -5097218
58 I = 51
97040
XDOT = -759
282771 Wp = 67
86988
YDOT = 7399
238248 meter/sec RA = 106
87638 deg
ZDOT = -1817
466201 TA = 184
58400
MA = 184
60013
Ha = 220
657 n
mi
Hp = 211
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14464957
78 X = 4442304
44
Y = -2626594
82 feet Y = -751095
56 meter
Z = -16723158
08 Z = -5075719
66
XDOT = -2491
085208 XDOT = -833
137728
YDOT = 24275
716038 feet/sec YDOT = 7390
334668 meter/sec
ZDOT = -5962
815619 ZDOT = -1821
333412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6476011
74 X = 1973888
38
Y = -13314779
89 feet Y = -4058344
91 meter
Z = -16630572
11 Z = -5068998
38
XDOT = 17180
249891 XDOT = 5236
540167
YDOT = 15832
228813 feet/sec YDOT = 4825
663342 meter/sec
ZDOT = -5980
812740 ZDOT = -1822
951723
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
44771928
00016717 00000-0 10270-3 0 9117
2 25544 51
6397 107
6910 0004997 44
6183 315
5372 15
55334865 27305
Satellite: ISS
Catalog Number: 25544
Epoch time: 15163
44771928 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 107
6910 deg
Eccentricity:
0004997
Arg of perigee: 44
6183 deg
Mean anomaly: 315
5372 deg
Mean motion: 15
55334865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 326
Coasting Arc #13 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2015/164/10:17:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3929529
55 A = 6773894
73 meter
Y = -1485766
34 meter E =
0007741
Z = 5308814
10 I = 51
97587
XDOT = 2011
976577 Wp = 54
23613
YDOT = -7384
874020 meter/sec RA = 101
88672 deg
ZDOT = -572
553813 TA = 41
22682
MA = 41
16838
Ha = 220
806 n
mi
Hp = 211
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12892157
30 X = -3938411
81
Y = -4874561
48 feet Y = -1529759
15 meter
Z = 17417369
10 Z = 5289703
26
XDOT = 6600
973023 XDOT = 2097
187752
YDOT = -24228
589303 feet/sec YDOT = -7361
898275 meter/sec
ZDOT = -1878
457393 ZDOT = -562
573745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11473791
70 X = -3497211
71
Y = 7820953
14 feet Y = 2383826
52 meter
Z = 17335472
65 Z = 5283852
06
XDOT = -15424
364706 XDOT = -4701
346362
YDOT = -18526
482266 feet/sec YDOT = -5646
871795 meter/sec
ZDOT = -1834
159288 ZDOT = -559
051751
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
47574197
00016717 00000-0 10270-3 0 9121
2 25544 51
6401 102
5567 0005014 47
1383 313
0191 15
55349354 27462
Satellite: ISS
Catalog Number: 25544
Epoch time: 15164
47574197 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 102
5567 deg
Eccentricity:
0005014
Arg of perigee: 47
1383 deg
Mean anomaly: 313
0191 deg
Mean motion: 15
55349354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 297
Coasting Arc #14 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2015/165/10:17:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3265399
17 A = 6776479
38 meter
Y = 3635719
78 meter E =
0013922
Z = -4706746
50 I = 51
99073
XDOT = -3032
915416 Wp = 91
41925
YDOT = 6424
036057 meter/sec RA = 96
90012 deg
ZDOT = 2865
052666 TA = 206
88505
MA = 206
95726
Ha = 220
726 n
mi
Hp = 211
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10713251
87 X = 3247364
82
Y = 11928214
49 feet Y = 3672135
37 meter
Z = -15442081
70 Z = -4690927
02
XDOT = -9950
509896 XDOT = -3118
442594
YDOT = 21076
233784 feet/sec YDOT = 6389
641441 meter/sec
ZDOT = 9399
779088 ZDOT = 2850
112281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15940855
06 X = 4858772
62
Y = -2240604
41 feet Y = -682936
22 meter
Z = -15374745
06 Z = -4686222
29
XDOT = 11645
928145 XDOT = 3549
678899
YDOT = 18961
858575 feet/sec YDOT = 5779
574494 meter/sec
ZDOT = 9334
311968 ZDOT = 2845
098288
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
43950689
00016717 00000-0 10270-3 0 9133
2 25544 51
6407 97
7431 0005015 49
9522 310
2070 15
55348614 27619
Satellite: ISS
Catalog Number: 25544
Epoch time: 15165
43950689 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 97
7431 deg
Eccentricity:
0005015
Arg of perigee: 49
9522 deg
Mean anomaly: 310
2070 deg
Mean motion: 15
55348614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 306
Coasting Arc #15 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2015/166/10:17:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2412854
69 A = 6781048
09 meter
Y = -5391057
84 meter E =
0016860
Z = 3319778
91 I = 52
01008
XDOT = 3853
668939 Wp = 80
97048
YDOT = -4652
354519 meter/sec RA = 91
92683 deg
ZDOT = -4731
180801 TA = 60
58911
MA = 60
42091
Ha = 220
731 n
mi
Hp = 211
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7916189
92 X = -2368517
61
Y = -17687197
63 feet Y = -5417792
52 meter
Z = 10891663
08 Z = 3308164
59
XDOT = 12643
270796 XDOT = 3928
388719
YDOT = -15263
630311 feet/sec YDOT = -4608
841829 meter/sec
ZDOT = -15522
246721 ZDOT = -4712
279458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19171372
61 X = -5843434
37
Y = -3004089
46 feet Y = -915646
47 meter
Z = 10842751
77 Z = 3304870
74
XDOT = -6013
818595 XDOT = -1833
011908
YDOT = -17622
937179 feet/sec YDOT = -5371
471252 meter/sec
ZDOT = -15440
066238 ZDOT = -4706
132189
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
46751689
00016717 00000-0 10270-3 0 9147
2 25544 51
6416 92
6086 0005047 52
9743 307
1871 15
55382714 27773
Satellite: ISS
Catalog Number: 25544
Epoch time: 15166
46751689 = yrday
fracday
Element set: 914
Inclination: 51
6416 deg
RA of node: 92
6086 deg
Eccentricity:
0005047
Arg of perigee: 52
9743 deg
Mean anomaly: 307
1871 deg
Mean motion: 15
55382714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 334
Coasting Arc #16 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2015/167/10:17:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1471019
45 A = 6784817
42 meter
Y = 6459328
34 meter E =
0013350
Z = -1444231
28 I = 52
02302
XDOT = -4430
021891 Wp = 44
55579
YDOT = 2301
464549 meter/sec RA = 86
96906 deg
ZDOT = 5822
813930 TA = 299
76680
MA = 299
89953
Ha = 220
748 n
mi
Hp = 211
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4826179
28 X = 1405695
91
Y = 21192022
11 feet Y = 6475413
21 meter
Z = -4738291
61 Z = -1437243
05
XDOT = -14534
192557 XDOT = -4483
713294
YDOT = 7550
736708 feet/sec YDOT = 2251
624083 meter/sec
ZDOT = 19103
720244 ZDOT = 5801
163606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20517525
17 X = 6253741
67
Y = 7190067
10 feet Y = 2191532
45 meter
Z = -4709491
57 Z = -1435453
03
XDOT = -899
834861 XDOT = -274
269666
YDOT = 14929
252287 feet/sec YDOT = 4550
436097 meter/sec
ZDOT = 19010
157874 ZDOT = 5794
296120
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
43127045
00016717 00000-0 10270-3 0 9159
2 25544 51
6418 87
7955 0005032 56
3943 303
7690 15
55378927 27928
Satellite: ISS
Catalog Number: 25544
Epoch time: 15167
43127045 = yrday
fracday
Element set: 915
Inclination: 51
6418 deg
RA of node: 87
7955 deg
Eccentricity:
0005032
Arg of perigee: 56
3943 deg
Mean anomaly: 303
7690 deg
Mean motion: 15
55378927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2792
Checksum: 331
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