[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 27th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 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 1344)
---------------------------------------
Vector Time (GMT): 2015/331/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5033539
81 A = 6782093
08 meter
Y = -2197562
38 meter E =
0005388
Z = -3976943
15 I = 51
57244
XDOT = 4993
892198 Wp = 155
94703
YDOT = -4239
756663 meter/sec RA = 348
52256 deg
ZDOT = -3984
603646 TA = 72
52604
MA = 72
46715
Ha = 221
311 n
mi
Hp = 215
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16514238
24 X = -4989273
25
Y = -7209850
32 feet Y = -2253602
93 meter
Z = -13047713
76 Z = -4001288
11
XDOT = 16384
160754 XDOT = 5060
287022
YDOT = -13909
962806 feet/sec YDOT = -4183
540126 meter/sec
ZDOT = -13072
846607 ZDOT = -3960
182992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14313746
69 X = 4362829
99
Y = -10820118
65 feet Y = -3297972
16 meter
Z = -13152434
32 Z = -4008861
98
XDOT = 3314
114626 XDOT = 1010
142138
YDOT = 20119
000449 feet/sec YDOT = 6132
271337 meter/sec
ZDOT = -12966
432443 ZDOT = -3952
168609
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 15331
51108185
00016717 00000-0 10270-3 0 9009
2 25544 51
6438 348
9392 0008373 212
5375 147
5263 15
54271498 13450
Satellite: ISS
Catalog Number: 25544
Epoch time: 15331
51108185 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 348
9392 deg
Eccentricity:
0008373
Arg of perigee: 212
5375 deg
Mean anomaly: 147
5263 deg
Mean motion: 15
54271498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 313
Coasting Arc #2 (Orbit 1360)
---------------------------------------
Vector Time (GMT): 2015/332/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3601195
62 A = 6778585
64 meter
Y = 2996804
88 meter E =
0010201
Z = 4901887
21 I = 51
52844
XDOT = -6272
329333 Wp = 175
31787
YDOT = 3760
229181 meter/sec RA = 343
52255 deg
ZDOT = 2298
856355 TA = 252
10502
MA = 252
21629
Ha = 221
158 n
mi
Hp = 215
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11814946
26 X = 3543605
20
Y = 9832037
01 feet Y = 3036753
44 meter
Z = 16082307
11 Z = 4919241
64
XDOT = -20578
508310 XDOT = -6325
078051
YDOT = 12336
709911 feet/sec YDOT = 3689
792743 meter/sec
ZDOT = 7542
179641 ZDOT = 2268
258464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14203916
72 X = -4329353
82
Y = 5666901
85 feet Y = 1727271
68 meter
Z = 16156654
42 Z = 4924548
27
XDOT = -699
437533 XDOT = -213
188560
YDOT = -22972
980646 feet/sec YDOT = -7002
164501 meter/sec
ZDOT = 7409
178841 ZDOT = 2258
317711
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 15332
53981436
00016717 00000-0 10270-3 0 9011
2 25544 51
6425 343
8089 0008262 215
8803 144
1795 15
54287604 13619
Satellite: ISS
Catalog Number: 25544
Epoch time: 15332
53981436 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 343
8089 deg
Eccentricity:
0008262
Arg of perigee: 215
8803 deg
Mean anomaly: 144
1795 deg
Mean motion: 15
54287604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1361
Checksum: 314
Coasting Arc #3 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2015/333/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1894629
09 A = 6776866
73 meter
Y = -3785816
13 meter E =
0011077
Z = -5299818
00 I = 51
49323
XDOT = 7020
497212 Wp = 121
00147
YDOT = -3051
179561 meter/sec RA = 338
51297 deg
ZDOT = -336
314738 TA = 145
81880
MA = 145
74744
Ha = 220
998 n
mi
Hp = 215
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6215974
72 X = -1826409
67
Y = -12420656
59 feet Y = -3806621
32 meter
Z = -17387854
33 Z = -5308856
36
XDOT = 23033
127336 XDOT = 7055
728168
YDOT = -10010
431631 feet/sec YDOT = -2972
474718 meter/sec
ZDOT = -1103
394811 ZDOT = -302
124952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13838780
74 X = 4218060
37
Y = 259857
61 feet Y = 79204
60 meter
Z = -17426105
47 Z = -5311476
95
XDOT = -1629
147363 XDOT = -496
564116
YDOT = 24057
229583 feet/sec YDOT = 7332
643577 meter/sec
ZDOT = -955
028283 ZDOT = -291
092621
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 15333
50423347
00016717 00000-0 10270-3 0 9022
2 25544 51
6433 339
0000 0008327 220
2820 139
7717 15
54304513 13768
Satellite: ISS
Catalog Number: 25544
Epoch time: 15333
50423347 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 339
0000 deg
Eccentricity:
0008327
Arg of perigee: 220
2820 deg
Mean anomaly: 139
7717 deg
Mean motion: 15
54304513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 274
Coasting Arc #4 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2015/334/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 136085
36 A = 6777655
55 meter
Y = 4467066
14 meter E =
0003301
Z = 5095921
53 I = 51
46588
XDOT = -7184
536694 Wp = 205
53573
YDOT = 2106
595840 meter/sec RA = 333
49953 deg
ZDOT = -1658
094091 TA = 260
49210
MA = 260
52941
Ha = 220
735 n
mi
Hp = 215
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 446474
29 X = 61369
25
Y = 14655728
80 feet Y = 4468169
90 meter
Z = 16718902
65 Z = 5096401
37
XDOT = -23571
314612 XDOT = -7199
504762
YDOT = 6911
403674 feet/sec YDOT = 2026
170007 meter/sec
ZDOT = -5439
941243 ZDOT = -1693
031553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13294738
08 X = -4052236
17
Y = -6180758
02 feet Y = -1883895
04 meter
Z = 16720035
92 Z = 5096266
95
XDOT = 3765
293899 XDOT = 1147
661580
YDOT = -23195
168670 feet/sec YDOT = -7069
887411 meter/sec
ZDOT = -5591
333970 ZDOT = -1704
238594
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 15334
53292939
00016717 00000-0 10270-3 0 9038
2 25544 51
6423 333
8696 0008221 223
9605 136
0895 15
54351767 13922
Satellite: ISS
Catalog Number: 25544
Epoch time: 15334
53292939 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 333
8696 deg
Eccentricity:
0008221
Arg of perigee: 223
9605 deg
Mean anomaly: 136
0895 deg
Mean motion: 15
54351767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 324
Coasting Arc #5 (Orbit 1406)
---------------------------------------
Vector Time (GMT): 2015/335/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1565712
05 A = 6780820
12 meter
Y = -4995068
61 meter E =
0008611
Z = -4317016
31 I = 51
44850
XDOT = 6766
656049 Wp = 167
07707
YDOT = -893
875311 meter/sec RA = 328
49036 deg
ZDOT = 3481
550166 TA = 138
47797
MA = 138
41253
Ha = 220
576 n
mi
Hp = 216
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5136850
55 X = 1642422
27
Y = -16388020
36 feet Y = -4977130
70 meter
Z = -14163439
35 Z = -4309224
23
XDOT = 22200
315123 XDOT = 6759
236550
YDOT = -2932
661781 feet/sec YDOT = -818
247713 meter/sec
ZDOT = 11422
408680 ZDOT = 3514
403315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12588481
29 X = 3836969
10
Y = 11724615
82 feet Y = 3573662
90 meter
Z = -14128728
94 Z = -4306436
58
XDOT = -5941
401058 XDOT = -1810
939042
YDOT = 20342
248047 feet/sec YDOT = 6200
317205 meter/sec
ZDOT = 11564
536248 ZDOT = 3524
870648
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 15335
49731498
00016717 00000-0 10270-3 0 9043
2 25544 51
6425 329
0605 0008170 228
1290 131
9166 15
54353741 14077
Satellite: ISS
Catalog Number: 25544
Epoch time: 15335
49731498 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 329
0605 deg
Eccentricity:
0008170
Arg of perigee: 228
1290 deg
Mean anomaly: 131
9166 deg
Mean motion: 15
54353741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1407
Checksum: 304
Coasting Arc #6 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2015/336/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3024754
51 A = 6784607
58 meter
Y = 5251396
49 meter E =
0009238
Z = 3036631
97 I = 51
43433
XDOT = -5865
738429 Wp = 134
10285
YDOT = -534
306041 meter/sec RA = 323
48923 deg
ZDOT = -4915
793736 TA = 10
94124
MA = 10
92117
Ha = 220
271 n
mi
Hp = 216
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9923735
29 X = -3098002
99
Y = 17228991
09 feet Y = 5217162
05 meter
Z = 9962703
33 Z = 3021760
47
XDOT = -19244
548652 XDOT = -5835
448558
YDOT = -1752
972577 feet/sec YDOT = -599
731115 meter/sec
ZDOT = -16127
932204 ZDOT = -4944
214906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11596498
40 X = -3534612
71
Y = -16190663
05 feet Y = -4934914
10 meter
Z = 9897361
70 Z = 3016715
85
XDOT = 8292
079038 XDOT = 2527
425691
YDOT = -15879
232065 feet/sec YDOT = -4839
989933 meter/sec
ZDOT = -16250
609566 ZDOT = -4953
185796
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 15336
52597428
00016717 00000-0 10270-3 0 9052
2 25544 51
6417 323
9299 0008126 232
5517 127
4897 15
54423881 14234
Satellite: ISS
Catalog Number: 25544
Epoch time: 15336
52597428 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 323
9299 deg
Eccentricity:
0008126
Arg of perigee: 232
5517 deg
Mean anomaly: 127
4897 deg
Mean motion: 15
54423881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 330
Coasting Arc #7 (Orbit 1437)
---------------------------------------
Vector Time (GMT): 2015/337/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4160758
25 A = 6787576
38 meter
Y = -5174255
48 meter E =
0002509
Z = -1401470
46 I = 51
41914
XDOT = 4571
920114 Wp = 328
91021
YDOT = 2110
447994 meter/sec RA = 318
49760 deg
ZDOT = 5779
009638 TA = 15
77091
MA = 15
76310
Ha = 220
101 n
mi
Hp = 216
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13650781
66 X = 4225116
66
Y = -16975903
80 feet Y = -5127367
26 meter
Z = -4598000
19 Z = -1381101
96
XDOT = 14999
737908 XDOT = 4519
908352
YDOT = 6924
041975 feet/sec YDOT = 2161
283301 meter/sec
ZDOT = 18960
005374 ZDOT = 5801
092970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10179550
14 X = 3102726
88
Y = 19279860
31 feet Y = 5876501
42 meter
Z = -4508935
65 Z = -1374323
59
XDOT = -10840
768792 XDOT = -3304
266328
YDOT = 10182
125846 feet/sec YDOT = 3103
511958 meter/sec
ZDOT = 19054
972780 ZDOT = 5807
955703
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 15337
49032623
00016717 00000-0 10270-3 0 9061
2 25544 51
6413 319
1207 0008084 234
4024 125
6376 15
54454511 14385
Satellite: ISS
Catalog Number: 25544
Epoch time: 15337
49032623 = yrday
fracday
Element set: 906
Inclination: 51
6413 deg
RA of node: 319
1207 deg
Eccentricity:
0008084
Arg of perigee: 234
4024 deg
Mean anomaly: 125
6376 deg
Mean motion: 15
54454511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1438
Checksum: 290
Coasting Arc #8 (Orbit 1453)
---------------------------------------
Vector Time (GMT): 2015/338/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4891508
86 A = 6788284
25 meter
Y = 4676784
32 meter E =
0012366
Z = -410646
65 I = 51
39823
XDOT = -3052
703403 Wp = 177
26127
YDOT = -3716
035225 meter/sec RA = 313
50893 deg
ZDOT = -5977
896921 TA = 7
18372
MA = 7
16601
Ha = 219
778 n
mi
Hp = 216
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16048257
41 X = -4941447
47
Y = 15343780
56 feet Y = 4621805
02 meter
Z = -1347265
90 Z = -434530
05
XDOT = -10015
431111 XDOT = -2981
884289
YDOT = -12191
716617 feet/sec YDOT = -3749
776496 meter/sec
ZDOT = -19612
522706 ZDOT = -5992
554528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8103334
76 X = -2469896
43
Y = -20664527
28 feet Y = -6298547
92 meter
Z = -1451403
14 Z = -442387
68
XDOT = 13528
861410 XDOT = 4123
596958
YDOT = -3927
449855 feet/sec YDOT = -1197
086716 meter/sec
ZDOT = -19675
080220 ZDOT = -5996
964451
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 15338
51894958
00016717 00000-0 10270-3 0 9073
2 25544 51
6412 313
9895 0008035 239
8860 120
1497 15
54460498 14545
Satellite: ISS
Catalog Number: 25544
Epoch time: 15338
51894958 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 313
9895 deg
Eccentricity:
0008035
Arg of perigee: 239
8860 deg
Mean anomaly: 120
1497 deg
Mean motion: 15
54460498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1454
Checksum: 342
Coasting Arc #9 (Orbit 1469)
---------------------------------------
Vector Time (GMT): 2015/339/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5212508
76 A = 6786100
64 meter
Y = -3758068
14 meter E =
0005860
Z = 2174819
99 I = 51
37003
XDOT = 1452
665000 Wp = 83
00505
YDOT = 5181
657617 meter/sec RA = 308
51760 deg
ZDOT = 5460
193811 TA = 301
22306
MA = 301
28047
Ha = 219
636 n
mi
Hp = 216
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17101406
71 X = 5243580
43
Y = -12329619
87 feet Y = -3699604
73 meter
Z = 7135236
19 Z = 2200217
01
XDOT = 4765
961286 XDOT = 1368
090620
YDOT = 17000
189032 feet/sec YDOT = 5197
429285 meter/sec
ZDOT = 17914
021690 ZDOT = 5467
045326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5279810
59 X = 1609286
27
Y = 20371854
06 feet Y = 6209341
12 meter
Z = 7245715
66 Z = 2208494
13
XDOT = -16043
466244 XDOT = -4890
048511
YDOT = -2237
434080 feet/sec YDOT = -681
969908 meter/sec
ZDOT = 17942
560713 ZDOT = 5468
892505
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 15339
54755187
00016717 00000-0 10270-3 0 9088
2 25544 51
6409 308
8592 0008245 242
7896 117
2417 15
54527912 14705
Satellite: ISS
Catalog Number: 25544
Epoch time: 15339
54755187 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 308
8592 deg
Eccentricity:
0008245
Arg of perigee: 242
7896 deg
Mean anomaly: 117
2417 deg
Mean motion: 15
54527912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1470
Checksum: 337
Coasting Arc #10 (Orbit 1484)
---------------------------------------
Vector Time (GMT): 2015/340/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5146168
50 A = 6782312
53 meter
Y = 2418366
43 meter E =
0002566
Z = -3693863
27 I = 51
33833
XDOT = 92
446574 Wp = 222
27893
YDOT = -6355
336163 meter/sec RA = 303
51467 deg
ZDOT = -4289
745604 TA = 1
96113
MA = 1
96012
Ha = 219
215 n
mi
Hp = 216
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16883754
91 X = -5154885
16
Y = 7934273
06 feet Y = 2360769
94 meter
Z = -12118973
99 Z = -3718883
78
XDOT = 303
302408 XDOT = 184
344866
YDOT = -20850
840429 feet/sec YDOT = -6353
788415 meter/sec
ZDOT = -14073
968517 ZDOT = -4289
073467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1594683
58 X = -486059
55
Y = -18515600
18 feet Y = -5643554
94 meter
Z = -12227548
14 Z = -3726956
67
XDOT = 18064
126341 XDOT = 5505
945709
YDOT = 7735
496043 feet/sec YDOT = 2357
779194 meter/sec
ZDOT = -14069
773351 ZDOT = -4288
466917
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 15340
51185278
00016717 00000-0 10270-3 0 9096
2 25544 51
6411 304
0484 0008020 247
6052 112
4251 15
54514395 14855
Satellite: ISS
Catalog Number: 25544
Epoch time: 15340
51185278 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 304
0484 deg
Eccentricity:
0008020
Arg of perigee: 247
6052 deg
Mean anomaly: 112
4251 deg
Mean motion: 15
54514395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1485
Checksum: 285
Coasting Arc #11 (Orbit 1500)
---------------------------------------
Vector Time (GMT): 2015/341/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4761476
31 A = 6778301
54 meter
Y = -769604
02 meter E =
0006324
Z = 4766220
42 I = 51
30877
XDOT = -1465
488612 Wp = 191
82000
YDOT = 7061
094209 meter/sec RA = 298
49958 deg
ZDOT = 2598
721684 TA = 232
40789
MA = 232
46532
Ha = 219
090 n
mi
Hp = 217
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15621641
44 X = 4746575
49
Y = -2524947
56 feet Y = -716441
55 meter
Z = 15637206
11 Z = 4789314
85
XDOT = -4808
033503 XDOT = -1556
962370
YDOT = 23166
319584 feet/sec YDOT = 7044
194587 meter/sec
ZDOT = 8525
989776 ZDOT = 2591
380615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2764905
15 X = -842743
09
Y = 15480036
07 feet Y = 4718314
99 meter
Z = 15737122
97 Z = 4796675
08
XDOT = -19116
085231 XDOT = -5826
582778
YDOT = -12066
357525 feet/sec YDOT = -3677
825774 meter/sec
ZDOT = 8492
850270 ZDOT = 2588
620762
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 15341
54041892
00016717 00000-0 10270-3 0 9105
2 25544 51
6413 298
9179 0008217 251
6895 108
3364 15
54566226 15015
Satellite: ISS
Catalog Number: 25544
Epoch time: 15341
54041892 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 298
9179 deg
Eccentricity:
0008217
Arg of perigee: 251
6895 deg
Mean anomaly: 108
3364 deg
Mean motion: 15
54566226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1501
Checksum: 314
Coasting Arc #12 (Orbit 1515)
---------------------------------------
Vector Time (GMT): 2015/342/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4132990
12 A = 6776195
24 meter
Y = -1079248
51 meter E =
0006914
Z = -5266147
27 I = 51
28749
XDOT = 2612
215976 Wp = 97
49290
YDOT = -7182
250663 meter/sec RA = 293
47223 deg
ZDOT = -579
730485 TA = 166
95330
MA = 166
93541
Ha = 218
757 n
mi
Hp = 217
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13559678
86 X = -4095033
18
Y = -3540841
58 feet Y = -1125253
82 meter
Z = -17277386
06 Z = -5286132
69
XDOT = 8570
262389 XDOT = 2695
151669
YDOT = -23563
814511 feet/sec YDOT = -7152
575387 meter/sec
ZDOT = -1902
002905 ZDOT = -566
839612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7601537
15 X = 2316948
52
Y = -11646287
55 feet Y = -3549788
44 meter
Z = -17363500
17 Z = -5292394
85
XDOT = 18807
670434 XDOT = 5732
577948
YDOT = 15018
800927 feet/sec YDOT = 4577
730523 meter/sec
ZDOT = -1844
872020 ZDOT = -562
316992
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 15342
50468425
00016717 00000-0 10270-3 0 9118
2 25544 51
6416 294
1068 0008088 255
4414 104
5842 15
54561235 15168
Satellite: ISS
Catalog Number: 25544
Epoch time: 15342
50468425 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 294
1068 deg
Eccentricity:
0008088
Arg of perigee: 255
4414 deg
Mean anomaly: 104
5842 deg
Mean motion: 15
54561235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1516
Checksum: 300
Coasting Arc #13 (Orbit 1531)
---------------------------------------
Vector Time (GMT): 2015/343/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3348673
90 A = 6776791
71 meter
Y = 2926856
70 meter E =
0004205
Z = 5116971
23 I = 51
27846
XDOT = -3498
308765 Wp = 287
03827
YDOT = 6651
043778 meter/sec RA = 288
44302 deg
ZDOT = -1514
773810 TA = 177
63335
MA = 177
63136
Ha = 218
542 n
mi
Hp = 217
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10986462
93 X = 3290839
52
Y = 9602548
24 feet Y = 2963980
04 meter
Z = 16787963
34 Z = 5133098
39
XDOT = -11477
390960 XDOT = -3565
064058
YDOT = 21821
009771 feet/sec YDOT = 6611
550239 meter/sec
ZDOT = -4969
730347 ZDOT = -1531
929809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12416556
40 X = -3784566
39
Y = 7511074
30 feet Y = 2289375
45 meter
Z = 16857043
14 Z = 5138026
75
XDOT = -16854
713550 XDOT = -5137
316690
YDOT = -16538
390392 feet/sec YDOT = -5040
901392 meter/sec
ZDOT = -5045
173346 ZDOT = -1537
768836
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 15343
53321499
00016717 00000-0 10270-3 0 9122
2 25544 51
6422 288
9763 0008078 259
3664 100
6580 15
54589238 15324
Satellite: ISS
Catalog Number: 25544
Epoch time: 15343
53321499 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 288
9763 deg
Eccentricity:
0008078
Arg of perigee: 259
3664 deg
Mean anomaly: 100
6580 deg
Mean motion: 15
54589238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1532
Checksum: 330
Coasting Arc #14 (Orbit 1546)
---------------------------------------
Vector Time (GMT): 2015/344/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2473731
07 A = 6779903
80 meter
Y = -4594628
47 meter E =
0004008
Z = -4331158
28 I = 51
28001
XDOT = 4134
238685 Wp = 178
78141
YDOT = -5466
359581 meter/sec RA = 283
41783 deg
ZDOT = 3433
745720 TA = 126
27499
MA = 126
23796
Ha = 218
252 n
mi
Hp = 217
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8115915
59 X = -2401129
57
Y = -15074240
39 feet Y = -4621885
04 meter
Z = -14209836
89 Z = -4342999
39
XDOT = 13563
775212 XDOT = 4178
377549
YDOT = -17934
250593 feet/sec YDOT = -5419
881302 meter/sec
ZDOT = 11265
569946 ZDOT = 3453
936010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16728222
81 X = 5098762
31
Y = -3440510
00 feet Y = -1048667
45 meter
Z = -14260074
55 Z = -4346470
72
XDOT = 13142
081093 XDOT = 4005
706317
YDOT = 16786
941983 feet/sec YDOT = 5116
659916 meter/sec
ZDOT = 11353
880360 ZDOT = 3460
662734
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 15344
49744453
00016717 00000-0 10270-3 0 9138
2 25544 51
6423 284
1656 0008140 263
2688 96
7538 15
54614674 15471
Satellite: ISS
Catalog Number: 25544
Epoch time: 15344
49744453 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 284
1656 deg
Eccentricity:
0008140
Arg of perigee: 263
2688 deg
Mean anomaly: 96
7538 deg
Mean motion: 15
54614674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1547
Checksum: 333
Coasting Arc #15 (Orbit 1562)
---------------------------------------
Vector Time (GMT): 2015/345/11:42:12
734
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1558603
64 A = 6783955
31 meter
Y = 5880110
18 meter E =
0005327
Z = 2996060
93 I = 51
28826
XDOT = -4544
766594 Wp = 111
67953
YDOT = 3719
825152 meter/sec RA = 278
40449 deg
ZDOT = -4931
166840 TA = 33
83235
MA = 33
79837
Ha = 217
500 n
mi
Hp = 217
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5113529
02 X = 1478181
11
Y = 19291700
07 feet Y = 5897089
55 meter
Z = 9829596
22 Z = 3003437
62
XDOT = -14910
651555 XDOT = -4562
070857
YDOT = 12204
150761 feet/sec YDOT = 3668
906300 meter/sec
ZDOT = -16178
368898 ZDOT = -4953
286285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19941046
61 X = -6078031
01
Y = -260685
80 feet Y = -79457
03 meter
Z = 9860300
98 Z = 3005419
74
XDOT = -7845
694549 XDOT = -2391
367699
YDOT = -16064
058227 feet/sec YDOT = -4896
324948 meter/sec
ZDOT = -16274
665457 ZDOT = -4960
518031
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 15345
52593850
00016717 00000-0 10270-3 0 9147
2 25544 51
6431 279
0348 0008108 267
2352 92
7873 15
54658858 15635
Satellite: ISS
Catalog Number: 25544
Epoch time: 15345
52593850 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 279
0348 deg
Eccentricity:
0008108
Arg of perigee: 267
2352 deg
Mean anomaly: 92
7873 deg
Mean motion: 15
54658858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1563
Checksum: 336
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