[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 15th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
271/15:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 214
8
Coasting Arc #1 (Orbit 187)
---------------------------------------
Vector Time (GMT): 2015/257/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2090939
04 A = 6778859
04 meter
Y = 3995347
67 meter E =
0002951
Z = 5063118
40 I = 51
63159
XDOT = -7293
488673 Wp = 201
27311
YDOT = 1494
827274 meter/sec RA = 359
63920 deg
ZDOT = 1830
090654 TA = 230
98822
MA = 231
01450
Ha = 219
186 n
mi
Hp = 216
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6860036
24 X = 2021512
01
Y = 13108096
02 feet Y = 4018342
45 meter
Z = 16611280
83 Z = 5073106
55
XDOT = -23928
768611 XDOT = -7318
552004
YDOT = 4904
288958 feet/sec YDOT = 1413
126802 meter/sec
ZDOT = 6004
234429 ZDOT = 1794
599288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11044588
30 X = 3366390
51
Y = 9772035
95 feet Y = 2978516
56 meter
Z = 16653567
54 Z = 5076007
39
XDOT = -19848
782120 XDOT = -6049
908790
YDOT = 12449
261918 feet/sec YDOT = 3794
535033 meter/sec
ZDOT = 5850
919727 ZDOT = 1783
360333
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 15257
13284446
00016717 00000-0 10270-3 0 9009
2 25544 51
6462 359
9210 0005521 273
5036 86
5485 15
53971537 1883
Satellite: ISS
Catalog Number: 25544
Epoch time: 15257
13284446 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 359
9210 deg
Eccentricity:
0005521
Arg of perigee: 273
5036 deg
Mean anomaly: 86
5485 deg
Mean motion: 15
53971537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 188
Checksum: 316
Coasting Arc #2 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2015/258/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -357638
76 A = 6777685
70 meter
Y = -4199103
12 meter E =
0009375
Z = -5316251
31 I = 51
59642
XDOT = 7630
441766 Wp = 85
54230
YDOT = -690
101497 meter/sec RA = 354
63938 deg
ZDOT = 32
525962 TA = 184
76362
MA = 184
77255
Ha = 219
251 n
mi
Hp = 216
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1173355
51 X = -284832
39
Y = -13776585
05 feet Y = -4202696
15 meter
Z = -17441769
38 Z = -5317811
21
XDOT = 25034
257763 XDOT = 7637
433537
YDOT = -2264
112523 feet/sec YDOT = -604
733772 meter/sec
ZDOT = 106
712473 ZDOT = 69
610303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6195029
70 X = -1888245
05
Y = -12352592
62 feet Y = -3765070
23 meter
Z = -17447677
22 Z = -5318052
02
XDOT = 21415
699973 XDOT = 6527
505352
YDOT = -11113
539511 feet/sec YDOT = -3387
406843 meter/sec
ZDOT = 266
724831 ZDOT = 81
297729
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 15258
09746729
00016717 00000-0 10270-3 0 9013
2 25544 51
6464 355
1134 0005585 278
4570 81
5949 15
54014376 2033
Satellite: ISS
Catalog Number: 25544
Epoch time: 15258
09746729 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 355
1134 deg
Eccentricity:
0005585
Arg of perigee: 278
4570 deg
Mean anomaly: 81
5949 deg
Mean motion: 15
54014376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 203
Checksum: 320
Coasting Arc #3 (Orbit 218)
---------------------------------------
Vector Time (GMT): 2015/259/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1396647
07 A = 6778798
68 meter
Y = 4318480
34 meter E =
0004580
Z = 5037112
07 I = 51
56890
XDOT = -7424
534785 Wp = 349
66646
YDOT = -177
091742 meter/sec RA = 349
63746 deg
ZDOT = -1902
643097 TA = 118
82676
MA = 118
78077
Ha = 219
354 n
mi
Hp = 216
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4582175
43 X = -1469302
09
Y = 14168242
59 feet Y = 4302456
57 meter
Z = 16525958
24 Z = 5030150
33
XDOT = -24358
709924 XDOT = -7412
760319
YDOT = -581
009651 feet/sec YDOT = -260
052208 meter/sec
ZDOT = -6242
267379 ZDOT = -1938
681592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1276798
87 X = 389168
30
Y = 14870237
21 feet Y = 4532448
30 meter
Z = 16495107
02 Z = 5027708
62
XDOT = -21494
628575 XDOT = -6551
562790
YDOT = 8957
340926 feet/sec YDOT = 2730
197514 meter/sec
ZDOT = -6397
589325 ZDOT = -1949
985226
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 15259
12637878
00016717 00000-0 10270-3 0 9023
2 25544 51
6463 349
9854 0005728 283
0989 76
9524 15
54063656 2196
Satellite: ISS
Catalog Number: 25544
Epoch time: 15259
12637878 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 349
9854 deg
Eccentricity:
0005728
Arg of perigee: 283
0989 deg
Mean anomaly: 76
9524 deg
Mean motion: 15
54063656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 219
Checksum: 353
Coasting Arc #4 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2015/260/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3011984
89 A = 6781915
91 meter
Y = -4335530
52 meter E =
0002407
Z = -4259965
49 I = 51
54769
XDOT = 6680
884397 Wp = 116
63262
YDOT = 1117
989221 meter/sec RA = 344
63858 deg
ZDOT = 3586
374537 TA = 190
05565
MA = 190
06047
Ha = 219
533 n
mi
Hp = 216
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9881840
19 X = 3080935
46
Y = -14224181
51 feet Y = -4301463
55 meter
Z = -13976264
72 Z = -4245165
71
XDOT = 21918
912065 XDOT = 6650
464837
YDOT = 3667
943638 feet/sec YDOT = 1192
529647 meter/sec
ZDOT = 11766
320658 ZDOT = 3618
755178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3263820
47 X = 994812
48
Y = -17062479
40 feet Y = -5200643
72 meter
Z = -13911626
55 Z = -4240263
77
XDOT = 20183
726965 XDOT = 6151
999979
YDOT = -5844
859850 feet/sec YDOT = -1781
513282 meter/sec
ZDOT = 11905
680743 ZDOT = 3628
851490
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 15260
09096758
00016717 00000-0 10270-3 0 9038
2 25544 51
6459 345
1772 0005748 287
1622 72
8901 15
54056992 2345
Satellite: ISS
Catalog Number: 25544
Epoch time: 15260
09096758 = yrday
fracday
Element set: 903
Inclination: 51
6459 deg
RA of node: 345
1772 deg
Eccentricity:
0005748
Arg of perigee: 287
1622 deg
Mean anomaly: 72
8901 deg
Mean motion: 15
54056992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 234
Checksum: 327
Coasting Arc #5 (Orbit 249)
---------------------------------------
Vector Time (GMT): 2015/261/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4378396
29 A = 6785589
07 meter
Y = 4197450
29 meter E =
0007800
Z = 3036333
64 I = 51
52981
XDOT = -5474
521952 Wp = 85
13144
YDOT = -2141
187130 meter/sec RA = 339
64758 deg
ZDOT = -4922
708024 TA = 59
99608
MA = 59
91870
Ha = 219
687 n
mi
Hp = 216
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14364817
21 X = -4439757
28
Y = 13771162
37 feet Y = 4148145
44 meter
Z = 9961724
55 Z = 3014914
53
XDOT = -17961
030027 XDOT = -5426
258915
YDOT = -7024
892160 feet/sec YDOT = -2202
137560 meter/sec
ZDOT = -16150
616878 ZDOT = -4949
184941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7196346
81 X = -2193446
51
Y = 18602484
56 feet Y = 5670037
29 meter
Z = 9868586
69 Z = 3007945
22
XDOT = -17793
510638 XDOT = -5423
462042
YDOT = 1765
118598 feet/sec YDOT = 538
008149 meter/sec
ZDOT = -16264
322729 ZDOT = -4957
365568
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 15261
11984287
00016717 00000-0 10270-3 0 9046
2 25544 51
6458 340
0489 0005689 292
4349 67
6201 15
54095962 2505
Satellite: ISS
Catalog Number: 25544
Epoch time: 15261
11984287 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 340
0489 deg
Eccentricity:
0005689
Arg of perigee: 292
4349 deg
Mean anomaly: 67
6201 deg
Mean motion: 15
54095962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 250
Checksum: 325
Coasting Arc #6 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2015/262/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5364319
26 A = 6788475
26 meter
Y = -3866744
26 meter E =
0009186
Z = -1508011
82 I = 51
50940
XDOT = 3926
212429 Wp = 358
72649
YDOT = 3205
200828 meter/sec RA = 334
66256 deg
ZDOT = 5756
126398 TA = 344
77059
MA = 344
79823
Ha = 219
857 n
mi
Hp = 216
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17599472
63 X = 5414484
86
Y = -12686168
83 feet Y = -3806476
57 meter
Z = -4947545
34 Z = -1481830
52
XDOT = 12881
274372 XDOT = 3862
117934
YDOT = 10515
750749 feet/sec YDOT = 3248
748541 meter/sec
ZDOT = 18884
929127 ZDOT = 5775
043331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10228299
67 X = 3117585
74
Y = -19161766
97 feet Y = -5840506
57 meter
Z = -4833952
18 Z = -1473388
63
XDOT = 14693
605708 XDOT = 4478
611020
YDOT = 3065
773582 feet/sec YDOT = 934
447788 meter/sec
ZDOT = 18965
839284 ZDOT = 5780
787814
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 15262
08439552
00016717 00000-0 10270-3 0 9054
2 25544 51
6451 335
2399 0005834 296
0343 64
0209 15
54105142 2657
Satellite: ISS
Catalog Number: 25544
Epoch time: 15262
08439552 = yrday
fracday
Element set: 905
Inclination: 51
6451 deg
RA of node: 335
2399 deg
Eccentricity:
0005834
Arg of perigee: 296
0343 deg
Mean anomaly: 64
0209 deg
Mean motion: 15
54105142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 295
Coasting Arc #7 (Orbit 280)
---------------------------------------
Vector Time (GMT): 2015/263/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5933239
57 A = 6789373
81 meter
Y = 3286596
62 meter E =
0006417
Z = -198452
38 I = 51
48382
XDOT = -2163
084209 Wp = 152
01811
YDOT = -4261
840266 meter/sec RA = 329
68228 deg
ZDOT = -5994
371421 TA = 30
12401
MA = 30
08712
Ha = 219
928 n
mi
Hp = 216
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19466009
10 X = -5968586
11
Y = 10782797
30 feet Y = 3220049
57 meter
Z = -651090
49 Z = -227361
27
XDOT = -7096
732969 XDOT = -2086
147878
YDOT = -13982
415571 feet/sec YDOT = -4285
599666 meter/sec
ZDOT = -19666
572903 ZDOT = -6004
692083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12395066
88 X = -3778016
38
Y = 18476411
71 feet Y = 5631610
29 meter
Z = -776320
89 Z = -236622
61
XDOT = -11237
708602 XDOT = -3425
253582
YDOT = -8357
324980 feet/sec YDOT = -2547
312654 meter/sec
ZDOT = -19710
227898 ZDOT = -6007
677463
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 15263
11323441
00016717 00000-0 10270-3 0 9069
2 25544 51
6448 330
1114 0005735 298
6515 61
4061 15
54104186 2813
Satellite: ISS
Catalog Number: 25544
Epoch time: 15263
11323441 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 330
1114 deg
Eccentricity:
0005735
Arg of perigee: 298
6515 deg
Mean anomaly: 61
4061 deg
Mean motion: 15
54104186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 281
Checksum: 276
Coasting Arc #8 (Orbit 296)
---------------------------------------
Vector Time (GMT): 2015/264/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6039547
18 A = 6787608
39 meter
Y = -2443054
64 meter E =
0011693
Z = 1877969
23 I = 51
45102
XDOT = 363
485674 Wp = 42
23204
YDOT = 5220
052666 meter/sec RA = 324
69731 deg
ZDOT = 5609
957920 TA = 338
50975
MA = 338
55879
Ha = 219
907 n
mi
Hp = 216
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19814787
32 X = 6057294
61
Y = -8015271
12 feet Y = -2375417
06 meter
Z = 6161316
36 Z = 1907351
63
XDOT = 1192
538301 XDOT = 277
835545
YDOT = 17126
157041 feet/sec YDOT = 5223
638968 meter/sec
ZDOT = 18405
373752 ZDOT = 5611
515203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13657439
32 X = 4162787
50
Y = -16393972
19 feet Y = -4996882
72 meter
Z = 6288419
05 Z = 1916710
13
XDOT = 7830
588301 XDOT = 2386
763314
YDOT = 13600
238114 feet/sec YDOT = 4145
352577 meter/sec
ZDOT = 18411
077766 ZDOT = 5611
696503
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 15264
14205154
00016717 00000-0 10270-3 0 9074
2 25544 51
6441 324
9810 0005885 303
1077 56
9511 15
54185500 2976
Satellite: ISS
Catalog Number: 25544
Epoch time: 15264
14205154 = yrday
fracday
Element set: 907
Inclination: 51
6441 deg
RA of node: 324
9810 deg
Eccentricity:
0005885
Arg of perigee: 303
1077 deg
Mean anomaly: 56
9511 deg
Mean motion: 15
54185500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 297
Checksum: 294
Coasting Arc #9 (Orbit 311)
---------------------------------------
Vector Time (GMT): 2015/265/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5734007
95 A = 6784218
75 meter
Y = 1328571
80 meter E =
0003589
Z = -3377599
35 I = 51
41340
XDOT = 1339
571850 Wp = 2
88991
YDOT = -5966
701340 meter/sec RA = 319
70470 deg
ZDOT = -4617
824146 TA = 216
65922
MA = 216
68378
Ha = 220
188 n
mi
Hp = 216
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18812362
05 X = -5732031
05
Y = 4358831
37 feet Y = 1264461
13 meter
Z = -11081362
69 Z = -3405449
42
XDOT = 4394
920768 XDOT = 1428
625108
YDOT = -19575
791797 feet/sec YDOT = -5951
223813 meter/sec
ZDOT = -15150
341687 ZDOT = -4611
099966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14250263
87 X = -4343480
43
Y = 12928811
04 feet Y = 3940701
60 meter
Z = -11201642
77 Z = -3414260
72
XDOT = -4662
523363 XDOT = -1421
137121
YDOT = -18248
657775 feet/sec YDOT = -5562
190890 meter/sec
ZDOT = -15120
217494 ZDOT = -4608
642292
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 15265
10655294
00016717 00000-0 10270-3 0 9086
2 25544 51
6431 320
1725 0005881 307
5602 52
5016 15
54187414 3122
Satellite: ISS
Catalog Number: 25544
Epoch time: 15265
10655294 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 320
1725 deg
Eccentricity:
0005881
Arg of perigee: 307
5602 deg
Mean anomaly: 52
5016 deg
Mean motion: 15
54187414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 312
Checksum: 282
Coasting Arc #10 (Orbit 327)
---------------------------------------
Vector Time (GMT): 2015/266/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5058070
96 A = 6780386
52 meter
Y = 13465
16 meter E =
0003730
Z = 4511954
35 I = 51
37683
XDOT = -2816
020538 Wp = 81
09886
YDOT = 6408
024978 meter/sec RA = 314
69857 deg
ZDOT = 3136
085944 TA = 337
33532
MA = 337
35179
Ha = 220
239 n
mi
Hp = 216
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16594721
00 X = 5035627
08
Y = 44177
02 feet Y = 69902
74 meter
Z = 14802999
85 Z = 4536470
96
XDOT = -9238
912527 XDOT = -2902
701264
YDOT = 21023
703996 feet/sec YDOT = 6376
049995 meter/sec
ZDOT = 10288
995879 ZDOT = 3122
195167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14295992
16 X = 4357418
41
Y = -8238454
96 feet Y = -2511081
07 meter
Z = 14908654
84 Z = 4544158
00
XDOT = 1898
331595 XDOT = 578
611470
YDOT = 21812
747902 feet/sec YDOT = 6648
525561 meter/sec
ZDOT = 10227
911400 ZDOT = 3117
467395
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15266
13533623
00016717 00000-0 10270-3 0 9092
2 25544 51
6430 315
0421 0005893 312
5679 47
4976 15
54189360 3287
Satellite: ISS
Catalog Number: 25544
Epoch time: 15266
13533623 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 315
0421 deg
Eccentricity:
0005893
Arg of perigee: 312
5679 deg
Mean anomaly: 47
4976 deg
Mean motion: 15
54189360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 328
Checksum: 313
Coasting Arc #11 (Orbit 342)
---------------------------------------
Vector Time (GMT): 2015/267/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4129742
45 A = 6777550
37 meter
Y = -1499325
78 meter E =
0011743
Z = -5170391
73 I = 51
34488
XDOT = 3970
190206 Wp = 56
02246
YDOT = -6420
107291 meter/sec RA = 309
68157 deg
ZDOT = -1305
081828 TA = 201
35208
MA = 201
40111
Ha = 220
353 n
mi
Hp = 215
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13549023
77 X = -4087553
91
Y = -4919047
83 feet Y = -1545271
92 meter
Z = -16963227
47 Z = -5190350
55
XDOT = 13025
558420 XDOT = 4048
025918
YDOT = -21063
344131 feet/sec YDOT = -6375
274937 meter/sec
ZDOT = -4281
764529 ZDOT = -1285
605746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14050354
88 X = -4282548
17
Y = 2728497
88 feet Y = 831646
15 meter
Z = -17048958
62 Z = -5196522
59
XDOT = 496
465238 XDOT = 151
322605
YDOT = -23753
709131 feet/sec YDOT = -7240
130543 meter/sec
ZDOT = -4196
619946 ZDOT = -1279
129760
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15267
09980106
00016717 00000-0 10270-3 0 9102
2 25544 51
6417 310
2328 0005780 315
6094 44
4595 15
54248255 3435
Satellite: ISS
Catalog Number: 25544
Epoch time: 15267
09980106 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 310
2328 deg
Eccentricity:
0005780
Arg of perigee: 315
6094 deg
Mean anomaly: 44
4595 deg
Mean motion: 15
54248255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 343
Checksum: 301
Coasting Arc #12 (Orbit 358)
---------------------------------------
Vector Time (GMT): 2015/268/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3020870
76 A = 6777170
19 meter
Y = 3030296
78 meter E =
0005840
Z = 5257106
94 I = 51
32404
XDOT = -4780
536111 Wp = 349
74133
YDOT = 5956
368674 meter/sec RA = 304
65850 deg
ZDOT = -680
816471 TA = 106
82113
MA = 106
75707
Ha = 220
455 n
mi
Hp = 215
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9910993
30 X = 2961223
73
Y = 9941918
56 feet Y = 3063745
28 meter
Z = 17247726
19 Z = 5271636
46
XDOT = -15684
173594 XDOT = -4843
479228
YDOT = 19541
891975 feet/sec YDOT = 5902
557550 meter/sec
ZDOT = -2233
649838 ZDOT = -704
192938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13585343
25 X = 4140812
62
Y = 3219271
95 feet Y = 981234
09 meter
Z = 17309775
51 Z = 5276019
58
XDOT = -2662
202251 XDOT = -811
439246
YDOT = 23889
476108 feet/sec YDOT = 7281
512318 meter/sec
ZDOT = -2335
501741 ZDOT = -711
860931
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15268
12854663
00016717 00000-0 10270-3 0 9116
2 25544 51
6418 305
1031 0005743 319
3680 40
7044 15
54247866 3593
Satellite: ISS
Catalog Number: 25544
Epoch time: 15268
12854663 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 305
1031 deg
Eccentricity:
0005743
Arg of perigee: 319
3680 deg
Mean anomaly: 40
7044 deg
Mean motion: 15
54247866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 359
Checksum: 303
Coasting Arc #13 (Orbit 373)
---------------------------------------
Vector Time (GMT): 2015/269/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1871785
82 A = 6779104
41 meter
Y = -4440782
34 meter E =
0007429
Z = -4773816
74 I = 51
31271
XDOT = 5218
316576 Wp = 82
52527
YDOT = -4978
724713 meter/sec RA = 299
63538 deg
ZDOT = 2589
744898 TA = 213
10608
MA = 213
15260
Ha = 220
500 n
mi
Hp = 215
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6141029
60 X = -1798799
40
Y = -14569495
88 feet Y = -4461306
47 meter
Z = -15662128
40 Z = -4782731
59
XDOT = 17120
461207 XDOT = 5261
022044
YDOT = -16334
398666 feet/sec YDOT = -4920
130909 meter/sec
ZDOT = 8496
538379 ZDOT = 2615
198880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13012899
41 X = -3966331
74
Y = -8914469
09 feet Y = -2717130
18 meter
Z = -15699726
45 Z = -4785276
62
XDOT = 4739
051722 XDOT = 1444
462965
YDOT = -22050
834354 feet/sec YDOT = -6721
094311 meter/sec
ZDOT = 8607
147281 ZDOT = 2623
458491
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15269
09297683
00016717 00000-0 10270-3 0 9127
2 25544 51
6408 300
2928 0005629 323
3833 36
6934 15
54307457 3743
Satellite: ISS
Catalog Number: 25544
Epoch time: 15269
09297683 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 300
2928 deg
Eccentricity:
0005629
Arg of perigee: 323
3833 deg
Mean anomaly: 36
6934 deg
Mean motion: 15
54307457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 324
Coasting Arc #14 (Orbit 389)
---------------------------------------
Vector Time (GMT): 2015/270/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 719725
11 A = 6782809
80 meter
Y = 5613213
13 meter E =
0010311
Z = 3736972
54 I = 51
31012
XDOT = -5340
044540 Wp = 54
36349
YDOT = 3513
028836 meter/sec RA = 294
62055 deg
ZDOT = -4234
206285 TA = 80
72841
MA = 80
61182
Ha = 220
634 n
mi
Hp = 215
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2361302
86 X = 638750
44
Y = 18416053
58 feet Y = 5620809
40 meter
Z = 12260408
58 Z = 3740271
28
XDOT = -17519
831167 XDOT = -5358
362944
YDOT = 11525
685159 feet/sec YDOT = 3453
209854 meter/sec
ZDOT = -13891
752903 ZDOT = -4260
192298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12204667
32 X = 3719982
60
Y = 13980317
04 feet Y = 4261200
63 meter
Z = 12273598
92 Z = 3740992
95
XDOT = -6968
597692 XDOT = -2124
028577
YDOT = 18418
961298 feet/sec YDOT = 5614
099404 meter/sec
ZDOT = -14004
373262 ZDOT = -4268
532970
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15270
12168314
00016717 00000-0 10270-3 0 9132
2 25544 51
6405 295
1627 0005719 326
4238 33
6552 15
54330426 3904
Satellite: ISS
Catalog Number: 25544
Epoch time: 15270
12168314 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 295
1627 deg
Eccentricity:
0005719
Arg of perigee: 326
4238 deg
Mean anomaly: 33
6552 deg
Mean motion: 15
54330426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 390
Checksum: 290
Coasting Arc #15 (Orbit 404)
---------------------------------------
Vector Time (GMT): 2015/271/01:57:23
393
Vector Time (MET): N/A
Weight (LBS) : 926984
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 321622
39 A = 6786425
98 meter
Y = -6373656
75 meter E =
0009160
Z = -2293305
00 I = 51
30991
XDOT = 5185
569222 Wp = 8
99746
YDOT = -1675
883644 meter/sec RA = 289
61468 deg
ZDOT = 5396
745704 TA = 325
32759
MA = 325
38727
Ha = 220
688 n
mi
Hp = 215
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1055191
58 X = 404010
37
Y = -20910947
35 feet Y = -6369599
86 meter
Z = -7523966
54 Z = -2291541
49
XDOT = 17013
022381 XDOT = 5177
708374
YDOT = -5498
305918 feet/sec YDOT = -1617
938292 meter/sec
ZDOT = 17705
858610 ZDOT = 5421
917559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11103096
44 X = -3384223
80
Y = -17754830
87 feet Y = -5411672
45 meter
Z = -7515214
62 Z = -2290637
42
XDOT = 9385
951375 XDOT = 2860
837979
YDOT = -13393
671730 feet/sec YDOT = -4082
391143 meter/sec
ZDOT = 17814
628577 ZDOT = 5429
898790
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15271
08607841
00016717 00000-0 10270-3 0 9142
2 25544 51
6403 290
3522 0005519 331
3359 28
7490 15
54360451 4054
Satellite: ISS
Catalog Number: 25544
Epoch time: 15271
08607841 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 290
3522 deg
Eccentricity:
0005519
Arg of perigee: 331
3359 deg
Mean anomaly: 28
7490 deg
Mean motion: 15
54360451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 405
Checksum: 290
Coasting Arc #16 (Orbit 413)
---------------------------------------
Vector Time (GMT): 2015/271/15:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 892142
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3957785
80 A = 6784526
91 meter
Y = 4582082
45 meter E =
0004511
Z = -3067765
75 I = 51
29875
XDOT = -2449
368089 Wp = 25
58012
YDOT = -5379
826199 meter/sec RA = 286
86881 deg
ZDOT = -4874
144748 TA = 189
80990
MA = 189
81871
Ha = 220
886 n
mi
Hp = 214
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12984861
53 X = -3993827
38
Y = 15033078
89 feet Y = 4537621
89 meter
Z = -10064848
27 Z = -3087080
35
XDOT = -8035
984545 XDOT = -2365
350497
YDOT = -17650
348422 feet/sec YDOT = -5406
747624 meter/sec
ZDOT = -15991
288542 ZDOT = -4885
838530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5317932
68 X = -1620905
88
Y = -19095043
45 feet Y = -5820169
24 meter
Z = -10148899
87 Z = -3093384
68
XDOT = 17691
755308 XDOT = 5392
447018
YDOT = 3600
673402 feet/sec YDOT = 1097
485253 meter/sec
ZDOT = -16040
707860 ZDOT = -4889
207756
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15271
66470699
00016717 00000-0 10270-3 0 9156
2 25544 51
6410 287
4694 0005808 335
8712 24
2168 15
54385443 4143
Satellite: ISS
Catalog Number: 25544
Epoch time: 15271
66470699 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 287
4694 deg
Eccentricity:
0005808
Arg of perigee: 335
8712 deg
Mean anomaly: 24
2168 deg
Mean motion: 15
54385443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 414
Checksum: 323
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