[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 3rd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
186/07:13:02
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 211
5
191/02:58:39
135 3
2 3
9 3
9
N/A -2
1 -0
4 219
4
000/00:11:54
271 0
5 -0
0 214
0
Coasting Arc #1 (Orbit 3029)
---------------------------------------
Vector Time (GMT): 2015/182/16:01:04
389
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3937404
35 A = 6778865
76 meter
Y = 3906509
90 meter E =
0013981
Z = 3888095
72 I = 51
71681
XDOT = -6139
348189 Wp = 103
09233
YDOT = 2088
055933 meter/sec RA = 11
18203 deg
ZDOT = 4103
760262 TA = 303
89993
MA = 304
03282
Ha = 219
797 n
mi
Hp = 211
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12917993
26 X = 3874541
39
Y = 12816633
52 feet Y = 3950188
47 meter
Z = 12756219
55 Z = 3907070
64
XDOT = -20142
218468 XDOT = -6182
175444
YDOT = 6850
577207 feet/sec YDOT = 2019
161656 meter/sec
ZDOT = 13463
780388 ZDOT = 4073
832967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7337975
24 X = -2236614
85
Y = -16589981
59 feet Y = -5056626
39 meter
Z = 12836993
89 Z = 3912715
74
XDOT = 20126
938889 XDOT = 6134
690973
YDOT = 1454
751188 feet/sec YDOT = 443
408162 meter/sec
ZDOT = 13334
625670 ZDOT = 4064
393904
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 15182
72319628
00016717 00000-0 10270-3 0 9002
2 25544 51
6434 11
4347 0002972 119
2870 240
8581 15
55490380 30307
Satellite: ISS
Catalog Number: 25544
Epoch time: 15182
72319628 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 11
4347 deg
Eccentricity:
0002972
Arg of perigee: 119
2870 deg
Mean anomaly: 240
8581 deg
Mean motion: 15
55490380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3030
Checksum: 293
Coasting Arc #2 (Orbit 3044)
---------------------------------------
Vector Time (GMT): 2015/183/16:01:04
389
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1817689
99 A = 6774699
86 meter
Y = -4187867
13 meter E =
0015092
Z = -5018948
50 I = 51
67148
XDOT = 7350
134485 Wp = 82
72833
YDOT = -795
468742 meter/sec RA = 6
18170 deg
ZDOT = -2001
515671 TA = 167
83168
MA = 167
79518
Ha = 219
843 n
mi
Hp = 211
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5963549
83 X = -1746345
25
Y = -13739721
55 feet Y = -4207794
12 meter
Z = -16466366
47 Z = -5027605
69
XDOT = 24114
614451 XDOT = 7368
205840
YDOT = -2609
805585 feet/sec YDOT = -713
173405 meter/sec
ZDOT = -6566
652465 ZDOT = -1965
766732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 754542
74 X = 229984
63
Y = 14918995
51 feet Y = 4547309
83 meter
Z = -16502706
99 Z = -5030025
09
XDOT = -22484
085245 XDOT = -6853
149183
YDOT = -5944
374943 feet/sec YDOT = -1811
845483 meter/sec
ZDOT = -6412
736377 ZDOT = -1954
602048
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 15183
68689498
00016717 00000-0 10270-3 0 9014
2 25544 51
6436 6
6211 0002886 120
2333 239
9106 15
55475606 30457
Satellite: ISS
Catalog Number: 25544
Epoch time: 15183
68689498 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 6
6211 deg
Eccentricity:
0002886
Arg of perigee: 120
2333 deg
Mean anomaly: 239
9106 deg
Mean motion: 15
55475606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3045
Checksum: 315
Coasting Arc #3 (Orbit 3060)
---------------------------------------
Vector Time (GMT): 2015/184/16:01:04
389
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -554856
11 A = 6773379
28 meter
Y = 4181255
94 meter E =
0004977
Z = 5295496
22 I = 51
63630
XDOT = -7648
252048 Wp = 96
18651
YDOT = -486
473742 meter/sec RA = 1
16825 deg
ZDOT = -417
449984 TA = 357
79007
MA = 357
79227
Ha = 219
773 n
mi
Hp = 211
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1820394
06 X = -627293
86
Y = 13718031
31 feet Y = 4174645
49 meter
Z = 17373675
26 Z = 5292625
45
XDOT = -25092
690447 XDOT = -7640
215962
YDOT = -1596
042462 feet/sec YDOT = -571
956520 meter/sec
ZDOT = -1369
586562 ZDOT = -454
583742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6337669
26 X = 1931721
59
Y = -12320383
80 feet Y = -3755252
98 meter
Z = 17360440
69 Z = 5291462
32
XDOT = 22263
172078 XDOT = 6785
814849
YDOT = 9298
415486 feet/sec YDOT = 2834
157040 meter/sec
ZDOT = -1529
183634 ZDOT = -466
095172
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 15184
71482728
00016717 00000-0 10270-3 0 9027
2 25544 51
6442 1
4856 0002834 122
2815 237
8613 15
55514997 30617
Satellite: ISS
Catalog Number: 25544
Epoch time: 15184
71482728 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 1
4856 deg
Eccentricity:
0002834
Arg of perigee: 122
2815 deg
Mean anomaly: 237
8613 deg
Mean motion: 15
55514997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3061
Checksum: 308
Coasting Arc #4 (Orbit 3075)
---------------------------------------
Vector Time (GMT): 2015/185/16:01:04
389
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2874488
76 A = 6775904
01 meter
Y = -3939079
50 meter E =
0013537
Z = -4717808
70 I = 51
61323
XDOT = 6926
081217 Wp = 112
32215
YDOT = 1735
690030 meter/sec RA = 356
15607 deg
ZDOT = 2772
106614 TA = 185
16940
MA = 185
18339
Ha = 219
718 n
mi
Hp = 211
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9430737
42 X = 2941239
85
Y = -12923489
18 feet Y = -3906561
36 meter
Z = -15478374
99 Z = -4703683
49
XDOT = 22723
363572 XDOT = 6892
691909
YDOT = 5694
521095 feet/sec YDOT = 1812
955022 meter/sec
ZDOT = 9094
837972 ZDOT = 2805
670743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13093257
74 X = -3990824
96
Y = 9296478
56 feet Y = 2833566
67 meter
Z = -15416794
78 Z = -4699039
05
XDOT = -19069
005031 XDOT = -5812
232734
YDOT = -11543
165937 feet/sec YDOT = -3518
356978 meter/sec
ZDOT = 9238
815491 ZDOT = 2815
990962
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 15185
67850351
00016717 00000-0 10270-3 0 9035
2 25544 51
6445 356
6724 0002860 125
9246 234
2174 15
55529936 30764
Satellite: ISS
Catalog Number: 25544
Epoch time: 15185
67850351 = yrday
fracday
Element set: 903
Inclination: 51
6445 deg
RA of node: 356
6724 deg
Eccentricity:
0002860
Arg of perigee: 125
9246 deg
Mean anomaly: 234
2174 deg
Mean motion: 15
55529936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3076
Checksum: 323
Coasting Arc #5 (Orbit 3085)
---------------------------------------
Vector Time (GMT): 2015/186/07:13:02
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3167792
99 A = 6775092
96 meter
Y = -3502987
91 meter E =
0013839
Z = -4870304
68 I = 51
59156
XDOT = 6733
275820 Wp = 79
45165
YDOT = -2745
917423 meter/sec RA = 353
03392 deg
ZDOT = -2407
859683 TA = 166
91607
MA = 166
88013
Ha = 219
594 n
mi
Hp = 211
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10393021
61 X = -3104728
55
Y = -11492742
49 feet Y = -3538059
18 meter
Z = -15978689
89 Z = -4885540
12
XDOT = 22090
799934 XDOT = 6775
177197
YDOT = -9008
915429 feet/sec YDOT = -2670
387014 meter/sec
ZDOT = -7899
802110 ZDOT = -2375
049718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14691821
22 X = -4478067
11
Y = -4708929
38 feet Y = -1435281
67 meter
Z = -16043470
08 Z = -4890049
68
XDOT = 14197
423119 XDOT = 4327
374567
YDOT = -17900
935520 feet/sec YDOT = -5456
205146 meter/sec
ZDOT = -7758
124192 ZDOT = -2364
676254
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 15186
32094749
00016717 00000-0 10270-3 0 9040
2 25544 51
6452 353
4661 0002431 116
9398 243
2004 15
55541613 30868
Satellite: ISS
Catalog Number: 25544
Epoch time: 15186
32094749 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 353
4661 deg
Eccentricity:
0002431
Arg of perigee: 116
9398 deg
Mean anomaly: 243
2004 deg
Mean motion: 15
55541613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3086
Checksum: 302
Coasting Arc #6 (Orbit 3101)
---------------------------------------
Vector Time (GMT): 2015/187/07:13:02
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 879523
88 A = 6773184
22 meter
Y = 4116604
58 meter E =
0004635
Z = 5302340
24 I = 51
55407
XDOT = -7506
834754 Wp = 104
17993
YDOT = 1596
915081 meter/sec RA = 348
01592 deg
ZDOT = 4
272816 TA = 345
77282
MA = 345
78587
Ha = 219
526 n
mi
Hp = 211
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2885577
03 X = 807669
22
Y = 13505920
55 feet Y = 4126037
84 meter
Z = 17396129
39 Z = 5306438
52
XDOT = -24628
722945 XDOT = -7524
154674
YDOT = 5239
222708 feet/sec YDOT = 1512
871895 meter/sec
ZDOT = 14
018424 ZDOT = -32
235384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9401620
36 X = 2865613
89
Y = 10087746
28 feet Y = 3074745
07 meter
Z = 17412888
10 Z = 5307448
29
XDOT = -17563
642059 XDOT = -5353
398100
YDOT = 16610
101034 feet/sec YDOT = 5062
758795 meter/sec
ZDOT = -143
311977 ZDOT = -43
681491
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 15187
34884922
00016717 00000-0 10270-3 0 9054
2 25544 51
6455 348
3312 0002434 121
3005 238
8387 15
55557572 31029
Satellite: ISS
Catalog Number: 25544
Epoch time: 15187
34884922 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 348
3312 deg
Eccentricity:
0002434
Arg of perigee: 121
3005 deg
Mean anomaly: 238
8387 deg
Mean motion: 15
55557572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3102
Checksum: 307
Coasting Arc #7 (Orbit 3116)
---------------------------------------
Vector Time (GMT): 2015/188/07:13:02
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1472719
80 A = 6775144
13 meter
Y = -4493267
27 meter E =
0013970
Z = -4865416
44 I = 51
52904
XDOT = 7268
176655 Wp = 109
81137
YDOT = -222
883878 meter/sec RA = 342
99476 deg
ZDOT = 2406
852734 TA = 183
84600
MA = 183
85675
Ha = 219
467 n
mi
Hp = 211
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4831757
86 X = 1546489
25
Y = -14741690
50 feet Y = -4476385
57 meter
Z = -15962652
35 Z = -4858083
43
XDOT = 23845
723935 XDOT = 7258
437345
YDOT = -731
246320 feet/sec YDOT = -141
660971 meter/sec
ZDOT = 7896
498472 ZDOT = 2442
136088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3724196
28 X = -1135135
03
Y = -15094016
03 feet Y = -4600656
09 meter
Z = -15930180
01 Z = -4855518
87
XDOT = 18607
733017 XDOT = 5671
637024
YDOT = -13081
784007 feet/sec YDOT = -3987
327765 meter/sec
ZDOT = 8048
264133 ZDOT = 2453
110908
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 15188
31249631
00016717 00000-0 10270-3 0 9065
2 25544 51
6448 343
5163 0002289 124
1651 235
9719 15
55573532 31175
Satellite: ISS
Catalog Number: 25544
Epoch time: 15188
31249631 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 343
5163 deg
Eccentricity:
0002289
Arg of perigee: 124
1651 deg
Mean anomaly: 235
9719 deg
Mean motion: 15
55573532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3117
Checksum: 314
Coasting Arc #8 (Orbit 3132)
---------------------------------------
Vector Time (GMT): 2015/189/07:13:02
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3567583
75 A = 6779625
29 meter
Y = 4510615
15 meter E =
0013866
Z = 3577737
28 I = 51
51445
XDOT = -6127
100426 Wp = 92
32795
YDOT = -1321
252070 meter/sec RA = 337
98462 deg
ZDOT = -4429
660182 TA = 45
23090
MA = 45
11818
Ha = 219
395 n
mi
Hp = 211
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11704671
08 X = -3635136
56
Y = 14798606
13 feet Y = 4470342
16 meter
Z = 11737983
22 Z = 3560242
97
XDOT = -20102
035519 XDOT = -6090
353008
YDOT = -4334
816503 feet/sec YDOT = -1389
563583 meter/sec
ZDOT = -14533
005848 ZDOT = -4459
335072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1704416
98 X = -519506
30
Y = 18838131
96 feet Y = 5741862
62 meter
Z = 11661820
85 Z = 3554523
00
XDOT = -17724
697103 XDOT = -5402
487677
YDOT = 7501
067849 feet/sec YDOT = 2286
325480 meter/sec
ZDOT = -14660
325334 ZDOT = -4468
467162
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 15189
34037417
00016717 00000-0 10270-3 0 9077
2 25544 51
6450 338
3814 0002147 125
0223 235
1133 15
55619948 31333
Satellite: ISS
Catalog Number: 25544
Epoch time: 15189
34037417 = yrday
fracday
Element set: 907
Inclination: 51
6450 deg
RA of node: 338
3814 deg
Eccentricity:
0002147
Arg of perigee: 125
0223 deg
Mean anomaly: 235
1133 deg
Mean motion: 15
55619948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3133
Checksum: 294
Coasting Arc #9 (Orbit 3147)
---------------------------------------
Vector Time (GMT): 2015/190/07:13:02
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5103364
76 A = 6783893
54 meter
Y = -4127288
96 meter E =
0007946
Z = -1708605
44 I = 51
49803
XDOT = 4247
060230 Wp = 52
90655
YDOT = 2908
608172 meter/sec RA = 332
98768 deg
ZDOT = 5682
324235 TA = 288
31478
MA = 288
40121
Ha = 219
367 n
mi
Hp = 211
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16743322
70 X = 5157437
53
Y = -13540974
26 feet Y = -4069917
33 meter
Z = -5605660
88 Z = -1683683
33
XDOT = 13933
924640 XDOT = 4186
617328
YDOT = 9542
677730 feet/sec YDOT = 2955
763226 meter/sec
ZDOT = 18642
796045 ZDOT = 5702
808949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6218230
06 X = 1895316
52
Y = -20645332
44 feet Y = -6292697
33 meter
Z = -5497648
26 Z = -1675683
19
XDOT = 15285
582330 XDOT = 4659
045494
YDOT = -363
326489 feet/sec YDOT = -110
741914 meter/sec
ZDOT = 18730
265784 ZDOT = 5708
985011
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 15190
30400019
00016717 00000-0 10270-3 0 9088
2 25544 51
6437 333
5662 0002107 130
3782 229
7555 15
55587411 31483
Satellite: ISS
Catalog Number: 25544
Epoch time: 15190
30400019 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 333
5662 deg
Eccentricity:
0002107
Arg of perigee: 130
3782 deg
Mean anomaly: 229
7555 deg
Mean motion: 15
55587411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3148
Checksum: 295
Coasting Arc #10 (Orbit 3160)
---------------------------------------
Vector Time (GMT): 2015/191/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 837473
52 A = 6777986
90 meter
Y = -4852743
06 meter E =
0009773
Z = -4666955
13 I = 51
44874
XDOT = 6941
627969 Wp = 118
36489
YDOT = -1543
356059 meter/sec RA = 328
83650 deg
ZDOT = 2850
462139 TA = 180
04378
MA = 180
04387
Ha = 219
407 n
mi
Hp = 214
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2747616
55 X = 914346
08
Y = -15921073
04 feet Y = -4842947
68 meter
Z = -15311532
59 Z = -4662700
55
XDOT = 22774
369978 XDOT = 6944
523787
YDOT = -5063
504132 feet/sec YDOT = -1465
714273 meter/sec
ZDOT = 9351
909905 ZDOT = 2884
190048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9754497
01 X = 2973170
69
Y = -12902341
18 feet Y = -3932633
59 meter
Z = -15292232
46 Z = -4661072
45
XDOT = 21600
267389 XDOT = 6583
761500
YDOT = 5073
974624 feet/sec YDOT = 1546
547465 meter/sec
ZDOT = 9497
240552 ZDOT = 2894
758920
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 15191
13913636
00016717 00000-0 10270-3 0 9095
2 25544 51
6444 329
3927 0001787 229
4285 130
6713 15
54864409 31614
Satellite: ISS
Catalog Number: 25544
Epoch time: 15191
13913636 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 329
3927 deg
Eccentricity:
0001787
Arg of perigee: 229
4285 deg
Mean anomaly: 130
6713 deg
Mean motion: 15
54864409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3161
Checksum: 323
Coasting Arc #11 (Orbit 3176)
---------------------------------------
Vector Time (GMT): 2015/192/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2566173
48 A = 6782258
76 meter
Y = 5256243
11 meter E =
0011089
Z = 3422422
22 I = 51
43600
XDOT = -6157
534159 Wp = 95
21657
YDOT = -18
379190 meter/sec RA = 323
82859 deg
ZDOT = -4576
956942 TA = 44
55253
MA = 44
46344
Ha = 219
407 n
mi
Hp = 214
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8419204
34 X = -2641384
13
Y = 17244892
10 feet Y = 5227125
61 meter
Z = 11228419
35 Z = 3409774
12
XDOT = -20201
883724 XDOT = -6134
637915
YDOT = -60
299181 feet/sec YDOT = -87
108293 meter/sec
ZDOT = -15016
262933 ZDOT = -4606
813363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15185976
51 X = -4628685
64
Y = 11785498
06 feet Y = 3592219
81 meter
Z = 11172952
13 Z = 3405515
81
XDOT = -17188
599093 XDOT = -5239
085004
YDOT = -7753
639164 feet/sec YDOT = -2363
309217 meter/sec
ZDOT = -15144
621019 ZDOT = -4616
080487
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 15192
16747783
00016717 00000-0 10270-3 0 9109
2 25544 51
6441 324
2607 0001757 232
6570 127
4423 15
54867037 31779
Satellite: ISS
Catalog Number: 25544
Epoch time: 15192
16747783 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 324
2607 deg
Eccentricity:
0001757
Arg of perigee: 232
6570 deg
Mean anomaly: 127
4423 deg
Mean motion: 15
54867037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3177
Checksum: 312
Coasting Arc #12 (Orbit 3191)
---------------------------------------
Vector Time (GMT): 2015/193/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3919603
08 A = 6785834
38 meter
Y = -5259287
90 meter E =
0006040
Z = -1728750
64 I = 51
42402
XDOT = 4854
702008 Wp = 31
23463
YDOT = 1759
730404 meter/sec RA = 318
83120 deg
ZDOT = 5667
515146 TA = 309
73949
MA = 309
79269
Ha = 219
256 n
mi
Hp = 214
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12859590
16 X = 3986519
97
Y = -17254881
57 feet Y = -5215081
98 meter
Z = -5671754
06 Z = -1709548
12
XDOT = 15927
500027 XDOT = 4807
132935
YDOT = 5773
393714 feet/sec YDOT = 1813
752245 meter/sec
ZDOT = 18594
209798 ZDOT = 5690
982899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18977589
31 X = 5784369
22
Y = -10192787
29 feet Y = -3106761
57 meter
Z = -5588110
78 Z = -1703256
17
XDOT = 11146
101806 XDOT = 3397
331830
YDOT = 10528
793021 feet/sec YDOT = 3209
176113 meter/sec
ZDOT = 18694
740668 ZDOT = 5698
156956
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 15193
13153640
00016717 00000-0 10270-3 0 9111
2 25544 51
6448 319
4486 0001796 240
3857 119
7117 15
54906097 31925
Satellite: ISS
Catalog Number: 25544
Epoch time: 15193
13153640 = yrday
fracday
Element set: 911
Inclination: 51
6448 deg
RA of node: 319
4486 deg
Eccentricity:
0001796
Arg of perigee: 240
3857 deg
Mean anomaly: 119
7117 deg
Mean motion: 15
54906097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3192
Checksum: 320
Coasting Arc #13 (Orbit 3207)
---------------------------------------
Vector Time (GMT): 2015/194/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4826600
33 A = 6787108
91 meter
Y = 4757313
91 meter E =
0011202
Z = -233100
15 I = 51
40511
XDOT = -3217
795796 Wp = 145
50025
YDOT = -3550
759935 meter/sec RA = 313
84109 deg
ZDOT = -5989
338221 TA = 37
02055
MA = 36
94331
Ha = 219
215 n
mi
Hp = 214
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15835302
91 X = -4878306
73
Y = 15607985
28 feet Y = 4703050
63 meter
Z = -764764
27 Z = -256671
67
XDOT = -10557
072822 XDOT = -3148
757468
YDOT = -11649
474854 feet/sec YDOT = -3586
356697 meter/sec
ZDOT = -19650
059779 ZDOT = -6004
802268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20810174
66 X = -6342941
23
Y = 7818931
13 feet Y = 2383210
21 meter
Z = -867083
58 Z = -264287
08
XDOT = -4219
983154 XDOT = -1286
250865
YDOT = -13369
674993 feet/sec YDOT = -4075
076938 meter/sec
ZDOT = -19715
814483 ZDOT = -6009
380254
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 15194
15985599
00016717 00000-0 10270-3 0 9121
2 25544 51
6451 314
3162 0001851 242
9082 117
1882 15
54882514 32080
Satellite: ISS
Catalog Number: 25544
Epoch time: 15194
15985599 = yrday
fracday
Element set: 912
Inclination: 51
6451 deg
RA of node: 314
3162 deg
Eccentricity:
0001851
Arg of perigee: 242
9082 deg
Mean anomaly: 117
1882 deg
Mean motion: 15
54882514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3208
Checksum: 315
Coasting Arc #14 (Orbit 3223)
---------------------------------------
Vector Time (GMT): 2015/195/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5221092
93 A = 6785038
12 meter
Y = -3758075
43 meter E =
0012169
Z = 2139111
60 I = 51
37738
XDOT = 1462
995036 Wp = 69
72475
YDOT = 5164
213355 meter/sec RA = 308
84766 deg
ZDOT = 5480
621350 TA = 314
09584
MA = 314
19592
Ha = 219
113 n
mi
Hp = 214
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17129569
97 X = 5252337
71
Y = -12329643
81 feet Y = -3699515
31 meter
Z = 7018082
68 Z = 2164549
80
XDOT = 4799
852479 XDOT = 1378
516338
YDOT = 16942
957200 feet/sec YDOT = 5180
100511 meter/sec
ZDOT = 17981
041173 ZDOT = 5487
523651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20545070
68 X = 6262137
54
Y = -4667369
06 feet Y = -1422614
09 meter
Z = 7128218
93 Z = 2172681
13
XDOT = -2653
533735 XDOT = -808
797083
YDOT = 15929
436678 feet/sec YDOT = 4855
292300 meter/sec
ZDOT = 18009
661933 ZDOT = 5489
344957
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 15195
18816365
00016717 00000-0 10270-3 0 9130
2 25544 51
6452 309
1835 0001737 255
5286 104
5674 15
54916864 32242
Satellite: ISS
Catalog Number: 25544
Epoch time: 15195
18816365 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 309
1835 deg
Eccentricity:
0001737
Arg of perigee: 255
5286 deg
Mean anomaly: 104
5674 deg
Mean motion: 15
54916864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3224
Checksum: 326
Coasting Arc #15 (Orbit 3238)
---------------------------------------
Vector Time (GMT): 2015/196/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5158037
43 A = 6780823
83 meter
Y = 2268492
93 meter E =
0004165
Z = -3776478
60 I = 51
34454
XDOT = 253
558967 Wp = 74
07900
YDOT = -6407
337728 meter/sec RA = 303
84318 deg
ZDOT = -4197
889098 TA = 151
39407
MA = 151
37121
Ha = 219
000 n
mi
Hp = 213
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16922694
99 X = -5164676
47
Y = 7442562
12 feet Y = 2210775
69 meter
Z = -12390021
66 Z = -3801550
84
XDOT = 831
886375 XDOT = 345
579973
YDOT = -21021
449240 feet/sec YDOT = -6403
987261 meter/sec
ZDOT = -13772
602029 ZDOT = -4196
434610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18404858
00 X = -5609800
72
Y = 579830
36 feet Y = 176732
29 meter
Z = -12498278
77 Z = -3809475
37
XDOT = 8780
642860 XDOT = 2676
339944
YDOT = -17800
580853 feet/sec YDOT = -5425
617044 meter/sec
ZDOT = -13765
050510 ZDOT = -4195
587395
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 15196
15219128
00016717 00000-0 10270-3 0 9143
2 25544 51
6455 304
3721 0001949 260
0555 100
0378 15
54937188 32391
Satellite: ISS
Catalog Number: 25544
Epoch time: 15196
15219128 = yrday
fracday
Element set: 914
Inclination: 51
6455 deg
RA of node: 304
3721 deg
Eccentricity:
0001949
Arg of perigee: 260
0555 deg
Mean anomaly: 100
0378 deg
Mean motion: 15
54937188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3239
Checksum: 308
Coasting Arc #16 (Orbit 3254)
---------------------------------------
Vector Time (GMT): 2015/197/03:04:36
271
Vector Time (MET): N/A
Weight (LBS) : 891730
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4692335
68 A = 6776744
73 meter
Y = -443177
96 meter E =
0005392
Z = 4867141
84 I = 51
31412
XDOT = -1762
793167 Wp = 132
18787
YDOT = 7089
667669 meter/sec RA = 298
82325 deg
ZDOT = 2339
805523 TA = 294
78268
MA = 294
83877
Ha = 218
916 n
mi
Hp = 214
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15394802
12 X = 4673300
34
Y = -1453995
92 feet Y = -390812
12 meter
Z = 15968313
12 Z = 4889889
61
XDOT = -5783
442149 XDOT = -1853
306215
YDOT = 23260
064531 feet/sec YDOT = 7069
448629 meter/sec
ZDOT = 7676
527306 ZDOT = 2331
023261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14794248
51 X = 4509286
95
Y = 4136210
78 feet Y = 1260717
05 meter
Z = 16066207
75 Z = 4896980
12
XDOT = -13494
800673 XDOT = -4113
215245
YDOT = 18535
917678 feet/sec YDOT = 5649
747708 meter/sec
ZDOT = 7637
345378 ZDOT = 2327
862871
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 15197
18047852
00016717 00000-0 10270-3 0 9151
2 25544 51
6455 299
2397 0001767 265
7883 94
3068 15
54952632 32556
Satellite: ISS
Catalog Number: 25544
Epoch time: 15197
18047852 = yrday
fracday
Element set: 915
Inclination: 51
6455 deg
RA of node: 299
2397 deg
Eccentricity:
0001767
Arg of perigee: 265
7883 deg
Mean anomaly: 94
3068 deg
Mean motion: 15
54952632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3255
Checksum: 351
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