[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 21st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13282 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 905 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 769)
---------------------------------------
Vector Time (GMT): 2015/294/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 518192
23 A = 6776236
81 meter
Y = 4179701
64 meter E =
0020721
Z = -5326034
75 I = 51
66551
XDOT = -7589
540250 Wp = 80
57066
YDOT = 990
300104 meter/sec RA = 172
31618 deg
ZDOT = 42
190377 TA = 189
81170
MA = 189
85223
Ha = 222
641 n
mi
Hp = 211
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1700105
73 X = 497287
45
Y = 13712931
88 feet Y = 4185379
14 meter
Z = -17473867
28 Z = -5323568
51
XDOT = -24900
066436 XDOT = -7600
254900
YDOT = 3249
016088 feet/sec YDOT = 905
368953 meter/sec
ZDOT = 138
419872 ZDOT = 5
295347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10677566
14 X = -3254522
16
Y = -8790508
16 feet Y = -2679346
89 meter
Z = -17463889
76 Z = -5322993
60
XDOT = 15351
034405 XDOT = 4678
995287
YDOT = -18582
229828 feet/sec YDOT = -5663
863652 meter/sec
ZDOT = -20
986301 ZDOT = -6
396624
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 15294
55554533
00016717 00000-0 10270-3 0 9003
2 25544 51
6427 173
3666 0006572 57
4252 302
7534 15
54514765 7705
Satellite: ISS
Catalog Number: 25544
Epoch time: 15294
55554533 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 173
3666 deg
Eccentricity:
0006572
Arg of perigee: 57
4252 deg
Mean anomaly: 302
7534 deg
Mean motion: 15
54514765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 770
Checksum: 312
Coasting Arc #2 (Orbit 785)
---------------------------------------
Vector Time (GMT): 2015/295/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1447029
62 A = 6777506
58 meter
Y = -4356125
24 meter E =
0012498
Z = 4979268
80 I = 51
70215
XDOT = 7381
690871 Wp = 59
11026
YDOT = 39
109030 meter/sec RA = 167
31595 deg
ZDOT = -2100
803260 TA = 51
35842
MA = 51
24662
Ha = 222
530 n
mi
Hp = 211
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4747472
50 X = 1471445
63
Y = -14291749
49 feet Y = -4339806
66 meter
Z = 16336183
72 Z = 4986357
94
XDOT = 24218
145902 XDOT = 7390
909950
YDOT = 128
310466 feet/sec YDOT = 121
707334 meter/sec
ZDOT = -6892
399147 ZDOT = -2064
921647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6585782
86 X = 2007346
62
Y = 13505425
83 feet Y = 4116453
79 meter
Z = 16367481
00 Z = 4988808
21
XDOT = -16557
752503 XDOT = -5046
802963
YDOT = 16279
944800 feet/sec YDOT = 4962
127175 meter/sec
ZDOT = -6737
513394 ZDOT = -2053
594082
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 15295
58412407
00016717 00000-0 10270-3 0 9011
2 25544 51
6431 168
2360 0006466 60
6897 299
4901 15
54554074 7861
Satellite: ISS
Catalog Number: 25544
Epoch time: 15295
58412407 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 168
2360 deg
Eccentricity:
0006466
Arg of perigee: 60
6897 deg
Mean anomaly: 299
4901 deg
Mean motion: 15
54554074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 786
Checksum: 326
Coasting Arc #3 (Orbit 800)
---------------------------------------
Vector Time (GMT): 2015/296/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3209408
75 A = 6780999
81 meter
Y = 4386874
72 meter E =
0012756
Z = -4065015
37 I = 51
74375
XDOT = -6494
423034 Wp = 88
45324
YDOT = -1153
049538 meter/sec RA = 162
32451 deg
ZDOT = 3894
021788 TA = 221
84475
MA = 221
94233
Ha = 222
560 n
mi
Hp = 211
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10529556
28 X = -3238478
75
Y = 14392633
59 feet Y = 4350822
04 meter
Z = -13336664
61 Z = -4080677
31
XDOT = -21307
162186 XDOT = -6499
962616
YDOT = -3782
970925 feet/sec YDOT = -1225
705042 meter/sec
ZDOT = 12775
662035 ZDOT = 3862
459399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2785212
30 X = -848932
71
Y = -17562322
24 feet Y = -5352995
82 meter
Z = -13404980
80 Z = -4085838
15
XDOT = 16521
569676 XDOT = 5035
774437
YDOT = -12240
568346 feet/sec YDOT = -3730
925232 meter/sec
ZDOT = 12639
585236 ZDOT = 3852
545580
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 15296
54840069
00016717 00000-0 10270-3 0 9028
2 25544 51
6420 163
4251 0006444 64
3133 295
8685 15
54561063 8018
Satellite: ISS
Catalog Number: 25544
Epoch time: 15296
54840069 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 163
4251 deg
Eccentricity:
0006444
Arg of perigee: 64
3133 deg
Mean anomaly: 295
8685 deg
Mean motion: 15
54561063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 801
Checksum: 300
Coasting Arc #4 (Orbit 816)
---------------------------------------
Vector Time (GMT): 2015/297/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4667166
33 A = 6784956
56 meter
Y = -4169143
53 meter E =
0019171
Z = 2603983
28 I = 51
78779
XDOT = 5064
968746 Wp = 91
57528
YDOT = 2368
075987 meter/sec RA = 157
34772 deg
ZDOT = -5253
754923 TA = 59
15429
MA = 58
96582
Ha = 222
467 n
mi
Hp = 211
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15312225
51 X = 4700790
46
Y = -13678292
41 feet Y = -4116763
90 meter
Z = 8543252
24 Z = 2626737
97
XDOT = 16617
351530 XDOT = 5063
633091
YDOT = 7769
278172 feet/sec YDOT = 2424
707760 meter/sec
ZDOT = -17236
728749 ZDOT = -5229
153399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -771929
30 X = -235284
05
Y = 20475942
00 feet Y = 6241067
12 meter
Z = 8642165
03 Z = 2634131
90
XDOT = -15718
082705 XDOT = -4790
871609
YDOT = 6682
729190 feet/sec YDOT = 2036
895857 meter/sec
ZDOT = -17130
889027 ZDOT = -5221
494975
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 15297
57694230
00016717 00000-0 10270-3 0 9030
2 25544 51
6422 158
2941 0006448 66
4797 293
7033 15
54621468 8178
Satellite: ISS
Catalog Number: 25544
Epoch time: 15297
57694230 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 158
2941 deg
Eccentricity:
0006448
Arg of perigee: 66
4797 deg
Mean anomaly: 293
7033 deg
Mean motion: 15
54621468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 817
Checksum: 332
Coasting Arc #5 (Orbit 831)
---------------------------------------
Vector Time (GMT): 2015/298/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5613314
11 A = 6787620
35 meter
Y = 3706680
89 meter E =
0015789
Z = -867575
46 I = 51
82370
XDOT = -3265
049350 Wp = 51
79690
YDOT = -3571
331095 meter/sec RA = 152
38190 deg
ZDOT = 5949
742770 TA = 298
83838
MA = 298
99678
Ha = 222
516 n
mi
Hp = 211
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18416384
86 X = -5650131
47
Y = 12161026
54 feet Y = 3643703
15 meter
Z = -2846376
19 Z = -894934
25
XDOT = -10712
104167 XDOT = -3253
773407
YDOT = -11716
965535 feet/sec YDOT = -3607
779327 meter/sec
ZDOT = 19520
153444 ZDOT = 5933
909253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3671761
43 X = 1119152
88
Y = -21745849
43 feet Y = -6628134
91 meter
Z = -2965106
36 Z = -903764
42
XDOT = 14372
728013 XDOT = 4380
807498
YDOT = -189
980828 feet/sec YDOT = -57
906156 meter/sec
ZDOT = 19452
360820 ZDOT = 5929
079578
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 15298
54118448
00016717 00000-0 10270-3 0 9041
2 25544 51
6405 153
4829 0006374 70
9290 289
2553 15
54596117 8323
Satellite: ISS
Catalog Number: 25544
Epoch time: 15298
54118448 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 153
4829 deg
Eccentricity:
0006374
Arg of perigee: 70
9290 deg
Mean anomaly: 289
2553 deg
Mean motion: 15
54596117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 832
Checksum: 328
Coasting Arc #6 (Orbit 847)
---------------------------------------
Vector Time (GMT): 2015/299/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6048846
15 A = 6787416
30 meter
Y = -2890556
81 meter E =
0013593
Z = -1045351
38 I = 51
85057
XDOT = 1243
674861 Wp = 116
21908
YDOT = 4717
418444 meter/sec RA = 147
42297 deg
ZDOT = -5913
288379 TA = 75
07905
MA = 74
92857
Ha = 222
532 n
mi
Hp = 211
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19845295
76 X = 6085797
54
Y = -9483454
10 feet Y = -2822708
12 meter
Z = -3429630
51 Z = -1015876
49
XDOT = 4080
298100 XDOT = 1219
556360
YDOT = 15477
094634 feet/sec YDOT = 4731
190600 meter/sec
ZDOT = -19400
552424 ZDOT = -5907
305746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6268741
70 X = -1910712
47
Y = 21102949
89 feet Y = 6432179
13 meter
Z = -3301880
42 Z = -1006413
15
XDOT = -12766
813235 XDOT = -3891
324674
YDOT = -6789
205098 feet/sec YDOT = -2069
349714 meter/sec
ZDOT = -19375
484536 ZDOT = -5905
647687
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 15299
56969015
00016717 00000-0 10270-3 0 9059
2 25544 51
6399 148
3513 0006389 74
8422 285
3437 15
54637149 8480
Satellite: ISS
Catalog Number: 25544
Epoch time: 15299
56969015 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 148
3513 deg
Eccentricity:
0006389
Arg of perigee: 74
8422 deg
Mean anomaly: 285
3437 deg
Mean motion: 15
54637149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 848
Checksum: 353
Coasting Arc #7 (Orbit 863)
---------------------------------------
Vector Time (GMT): 2015/300/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5913632
03 A = 6784531
10 meter
Y = 1793080
00 meter E =
0019744
Z = 2778870
81 I = 51
86651
XDOT = 718
866359 Wp = 79
50318
YDOT = -5648
067533 meter/sec RA = 142
45945 deg
ZDOT = 5146
787255 TA = 311
92399
MA = 312
09216
Ha = 222
480 n
mi
Hp = 211
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19401679
89 X = -5946742
26
Y = 5882808
41 feet Y = 1726764
95 meter
Z = 9117030
22 Z = 2750062
18
XDOT = 2358
485429 XDOT = 756
969143
YDOT = -18530
405291 feet/sec YDOT = -5639
815251 meter/sec
ZDOT = 16885
784957 ZDOT = 5150
372452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8351090
91 X = 2545412
51
Y = -18535109
72 feet Y = -5649501
44 meter
Z = 8992321
49 Z = 2740859
59
XDOT = 11137
210294 XDOT = 3394
621698
YDOT = 13262
345763 feet/sec YDOT = 4042
362989 meter/sec
ZDOT = 16902
196690 ZDOT = 5151
789551
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 15300
59817575
00016717 00000-0 10270-3 0 9069
2 25544 51
6388 143
2185 0006265 79
5792 280
6067 15
54683704 8645
Satellite: ISS
Catalog Number: 25544
Epoch time: 15300
59817575 = yrday
fracday
Element set: 906
Inclination: 51
6388 deg
RA of node: 143
2185 deg
Eccentricity:
0006265
Arg of perigee: 79
5792 deg
Mean anomaly: 280
6067 deg
Mean motion: 15
54683704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 864
Checksum: 338
Coasting Arc #8 (Orbit 878)
---------------------------------------
Vector Time (GMT): 2015/301/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5305263
63 A = 6780245
64 meter
Y = -370917
12 meter E =
0014216
Z = -4219937
18 I = 51
87648
XDOT = -2498
332817 Wp = 76
10786
YDOT = 6224
205133 meter/sec RA = 137
48712 deg
ZDOT = -3695
072115 TA = 156
08964
MA = 156
02355
Ha = 222
471 n
mi
Hp = 211
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17405720
56 X = 5329516
45
Y = -1216919
67 feet Y = -311454
77 meter
Z = -13844938
27 Z = -4194105
60
XDOT = -8196
629976 XDOT = -2549
797936
YDOT = 20420
620514 feet/sec YDOT = 6195
979175 meter/sec
ZDOT = -12122
940011 ZDOT = -3707
334202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10334257
23 X = -3149881
60
Y = 14167628
07 feet Y = 4318293
04 meter
Z = -13733308
40 Z = -4185912
40
XDOT = -9359
488169 XDOT = -2852
771994
YDOT = -18607
923772 feet/sec YDOT = -5671
695166 meter/sec
ZDOT = -12176
937301 ZDOT = -3711
530489
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 15301
56236545
00016717 00000-0 10270-3 0 9070
2 25544 51
6382 138
4068 0006469 82
4443 277
7444 15
54702111 8793
Satellite: ISS
Catalog Number: 25544
Epoch time: 15301
56236545 = yrday
fracday
Element set: 907
Inclination: 51
6382 deg
RA of node: 138
4068 deg
Eccentricity:
0006469
Arg of perigee: 82
4443 deg
Mean anomaly: 277
7444 deg
Mean motion: 15
54702111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 879
Checksum: 317
Coasting Arc #9 (Orbit 894)
---------------------------------------
Vector Time (GMT): 2015/302/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4302179
61 A = 6776812
57 meter
Y = -1210261
97 meter E =
0011213
Z = 5085621
00 I = 51
88760
XDOT = 3915
207955 Wp = 103
80760
YDOT = -6354
895677 meter/sec RA = 132
50359 deg
ZDOT = 1793
831862 TA = 328
88226
MA = 328
94862
Ha = 222
614 n
mi
Hp = 211
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14114762
49 X = -4313031
09
Y = -3970675
75 feet Y = -1258432
30 meter
Z = 16685108
27 Z = 5064694
99
XDOT = 12845
170456 XDOT = 3977
264970
YDOT = -20849
395265 feet/sec YDOT = -6310
766203 meter/sec
ZDOT = 5885
275139 ZDOT = 1813
002600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12050017
19 X = 3672845
24
Y = -8531780
21 feet Y = -2600486
61 meter
Z = 16594922
00 Z = 5058132
23
XDOT = 7477
959748 XDOT = 2279
282131
YDOT = 22210
031921 feet/sec YDOT = 6769
617730 meter/sec
ZDOT = 5969
156005 ZDOT = 1819
398750
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 15302
59081590
00016717 00000-0 10270-3 0 9083
2 25544 51
6380 133
2739 0006425 85
8831 274
3056 15
54687906 8953
Satellite: ISS
Catalog Number: 25544
Epoch time: 15302
59081590 = yrday
fracday
Element set: 908
Inclination: 51
6380 deg
RA of node: 133
2739 deg
Eccentricity:
0006425
Arg of perigee: 85
8831 deg
Mean anomaly: 274
3056 deg
Mean motion: 15
54687906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 895
Checksum: 330
Coasting Arc #10 (Orbit 909)
---------------------------------------
Vector Time (GMT): 2015/303/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3066724
15 A = 6775597
41 meter
Y = 2872097
87 meter E =
0021307
Z = -5333926
67 I = 51
90539
XDOT = -4878
931669 Wp = 92
26036
YDOT = 5885
736497 meter/sec RA = 127
51447 deg
ZDOT = 364
536427 TA = 181
20673
MA = 181
21188
Ha = 222
399 n
mi
Hp = 211
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10061430
95 X = 3060290
52
Y = 9422893
28 feet Y = 2906355
94 meter
Z = -17499759
42 Z = -5319044
46
XDOT = -16006
993664 XDOT = -4946
155614
YDOT = 19310
159111 feet/sec YDOT = 5830
801201 meter/sec
ZDOT = 1195
985654 ZDOT = 340
671615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13691868
52 X = -4173281
52
Y = 2187459
10 feet Y = 666737
53 meter
Z = -17435958
52 Z = -5314480
16
XDOT = -5146
385928 XDOT = -1568
618431
YDOT = -23520
784208 feet/sec YDOT = -7169
135027 meter/sec
ZDOT = 1091
883776 ZDOT = 332
806175
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 15303
55496889
00016717 00000-0 10270-3 0 9092
2 25544 51
6384 128
4622 0006489 90
6279 269
5618 15
54747755 9101
Satellite: ISS
Catalog Number: 25544
Epoch time: 15303
55496889 = yrday
fracday
Element set: 909
Inclination: 51
6384 deg
RA of node: 128
4622 deg
Eccentricity:
0006489
Arg of perigee: 90
6279 deg
Mean anomaly: 269
5618 deg
Mean motion: 15
54747755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 910
Checksum: 357
Coasting Arc #11 (Orbit 925)
---------------------------------------
Vector Time (GMT): 2015/304/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1702978
68 A = 6777531
64 meter
Y = -4401376
31 meter E =
0012887
Z = 4854831
10 I = 51
93057
XDOT = 5405
774320 Wp = 76
37722
YDOT = -4848
269189 meter/sec RA = 122
52782 deg
ZDOT = -2490
701493 TA = 38
00647
MA = 37
91560
Ha = 222
442 n
mi
Hp = 211
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5587200
41 X = -1677218
24
Y = -14440211
00 feet Y = -4420276
04 meter
Z = 15927923
56 Z = 4846620
84
XDOT = 17735
480051 XDOT = 5471
686193
YDOT = -15906
394976 feet/sec YDOT = -4787
449753 meter/sec
ZDOT = -8171
592825 ZDOT = -2464
280648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14945186
86 X = 4555292
96
Y = 4181206
15 feet Y = 1274431
64 meter
Z = 15893210
99 Z = 4844250
71
XDOT = 2248
371354 XDOT = 685
303589
YDOT = 22693
569457 feet/sec YDOT = 6916
999970 meter/sec
ZDOT = -8056
604160 ZDOT = -2455
652948
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 15304
58338107
00016717 00000-0 10270-3 0 9106
2 25544 51
6383 123
3295 0006439 94
2132 265
9757 15
54751275 9266
Satellite: ISS
Catalog Number: 25544
Epoch time: 15304
58338107 = yrday
fracday
Element set: 910
Inclination: 51
6383 deg
RA of node: 123
3295 deg
Eccentricity:
0006439
Arg of perigee: 94
2132 deg
Mean anomaly: 265
9757 deg
Mean motion: 15
54751275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 926
Checksum: 316
Coasting Arc #12 (Orbit 940)
---------------------------------------
Vector Time (GMT): 2015/305/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 390357
21 A = 6781337
27 meter
Y = 5630705
33 meter E =
0012441
Z = -3771382
34 I = 51
96149
XDOT = -5465
076301 Wp = 100
38483
YDOT = 3238
101460 meter/sec RA = 117
55226 deg
ZDOT = 4278
635602 TA = 214
75298
MA = 214
83431
Ha = 222
309 n
mi
Hp = 211
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1280699
51 X = 345684
52
Y = 18473442
68 feet Y = 5634820
71 meter
Z = -12373301
64 Z = -3769594
64
XDOT = -17930
040356 XDOT = -5521
663685
YDOT = 10623
692454 feet/sec YDOT = 3176
671053 meter/sec
ZDOT = 14037
518380 ZDOT = 4251
949414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15718247
25 X = -4790921
76
Y = -9798561
15 feet Y = -2986601
44 meter
Z = -12366558
60 Z = -3769327
06
XDOT = 1335
348741 XDOT = 407
014296
YDOT = -19671
755493 feet/sec YDOT = -5995
951074 meter/sec
ZDOT = 13921
644040 ZDOT = 4243
317103
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 15305
54749916
00016717 00000-0 10270-3 0 9118
2 25544 51
6395 118
5179 0006514 97
8144 262
3748 15
54807004 9412
Satellite: ISS
Catalog Number: 25544
Epoch time: 15305
54749916 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 118
5179 deg
Eccentricity:
0006514
Arg of perigee: 97
8144 deg
Mean anomaly: 262
3748 deg
Mean motion: 15
54807004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 941
Checksum: 324
Coasting Arc #13 (Orbit 956)
---------------------------------------
Vector Time (GMT): 2015/306/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 846050
53 A = 6785345
45 meter
Y = -6375668
76 meter E =
0020226
Z = 2134082
98 I = 51
98845
XDOT = 5179
696892 Wp = 107
16463
YDOT = -1179
162125 meter/sec RA = 112
59045 deg
ZDOT = -5538
969136 TA = 49
27502
MA = 49
09954
Ha = 222
215 n
mi
Hp = 211
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2775756
33 X = 906915
22
Y = -20917548
42 feet Y = -6365867
29 meter
Z = 7001584
58 Z = 2138341
01
XDOT = 16993
756206 XDOT = 5219
404185
YDOT = -3868
642143 feet/sec YDOT = -1121
017485 meter/sec
ZDOT = -18172
470919 ZDOT = -5513
710370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15527087
34 X = 4732656
22
Y = 14278811
96 feet Y = 4352181
88 meter
Z = 7021106
01 Z = 2140033
11
XDOT = -5648
303271 XDOT = -1721
602837
YDOT = 15084
004552 feet/sec YDOT = 4597
604588 meter/sec
ZDOT = -18063
111823 ZDOT = -5505
636484
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 15306
57587235
00016717 00000-0 10270-3 0 9127
2 25544 51
6390 113
3851 0006368 101
0141 259
1729 15
54832305 9571
Satellite: ISS
Catalog Number: 25544
Epoch time: 15306
57587235 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 113
3851 deg
Eccentricity:
0006368
Arg of perigee: 101
0141 deg
Mean anomaly: 259
1729 deg
Mean motion: 15
54832305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 957
Checksum: 302
Coasting Arc #14 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2015/307/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1862273
02 A = 6787138
81 meter
Y = 6517326
20 meter E =
0015754
Z = -256333
13 I = 52
00766
XDOT = -4601
414493 Wp = 64
65559
YDOT = -1088
989195 meter/sec RA = 107
63951 deg
ZDOT = 6036
662549 TA = 292
59593
MA = 292
76252
Ha = 222
181 n
mi
Hp = 211
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6109819
62 X = -1933767
76
Y = 21382303
81 feet Y = 6496101
27 meter
Z = -840987
96 Z = -265553
73
XDOT = -15096
504242 XDOT = -4618
219357
YDOT = -3572
799195 feet/sec YDOT = -1140
538954 meter/sec
ZDOT = 19805
323325 ZDOT = 6014
268734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14260330
60 X = -4346548
77
Y = -17061803
39 feet Y = -5200437
67 meter
Z = -881991
69 Z = -268831
07
XDOT = 10261
694695 XDOT = 3127
764543
YDOT = -9547
894775 feet/sec YDOT = -2910
198327 meter/sec
ZDOT = 19708
738142 ZDOT = 6007
223386
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 15307
53995497
00016717 00000-0 10270-3 0 9138
2 25544 51
6405 108
5739 0006500 104
6115 255
5759 15
54870554 9725
Satellite: ISS
Catalog Number: 25544
Epoch time: 15307
53995497 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 108
5739 deg
Eccentricity:
0006500
Arg of perigee: 104
6115 deg
Mean anomaly: 255
5759 deg
Mean motion: 15
54870554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 972
Checksum: 327
Coasting Arc #15 (Orbit 987)
---------------------------------------
Vector Time (GMT): 2015/308/12:56:47
147
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2724899
46 A = 6785815
72 meter
Y = -5967278
47 meter E =
0013412
Z = -1725431
18 I = 52
01196
XDOT = 3817
859152 Wp = 126
04124
YDOT = 3386
731633 meter/sec RA = 102
68996 deg
ZDOT = -5721
984308 TA = 72
78806
MA = 72
64129
Ha = 222
105 n
mi
Hp = 211
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8939958
85 X = 2799806
10
Y = -19577685
28 feet Y = -5936388
11 meter
Z = -5660863
45 Z = -1712011
72
XDOT = 12525
784620 XDOT = 3807
499742
YDOT = 11111
324256 feet/sec YDOT = 3429
367225 meter/sec
ZDOT = -18772
914397 ZDOT = -5703
463004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11469951
06 X = 3496041
08
Y = 18229483
51 feet Y = 5556346
58 meter
Z = -5601799
13 Z = -1707428
37
XDOT = -14890
421961 XDOT = -4538
600614
YDOT = 3663
966923 feet/sec YDOT = 1116
777118 meter/sec
ZDOT = -18693
473098 ZDOT = -5697
770600
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 15308
56828913
00016717 00000-0 10270-3 0 9141
2 25544 51
6400 103
4408 0006412 106
8667 253
3190 15
54910146 9889
Satellite: ISS
Catalog Number: 25544
Epoch time: 15308
56828913 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 103
4408 deg
Eccentricity:
0006412
Arg of perigee: 106
8667 deg
Mean anomaly: 253
3190 deg
Mean motion: 15
54910146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 988
Checksum: 304
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