[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 7th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21226 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 219 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): 2015/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1284043
38 A = 6776608
82 meter
Y = -4002690
76 meter E =
0013406
Z = -5325761
98 I = 51
72819
XDOT = 7333
704559 Wp = 66
02845
YDOT = 2209
374902 meter/sec RA = 16
09754 deg
ZDOT = 113
195339 TA = 205
01754
MA = 205
08257
Ha = 220
971 n
mi
Hp = 214
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4212740
75 X = 1354577
00
Y = -13132187
55 feet Y = -3987937
78 meter
Z = -17472972
37 Z = -5319352
86
XDOT = 24060
710495 XDOT = 7307
903906
YDOT = 7248
605320 feet/sec YDOT = 2291
240911 meter/sec
ZDOT = 371
375785 ZDOT = 148
757476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12292320
77 X = 3746699
37
Y = -6331310
83 feet Y = -1929783
54 meter
Z = -17444759
99 Z = -5317162
85
XDOT = 11606
065476 XDOT = 3537
528757
YDOT = 21142
089055 feet/sec YDOT = 6444
108744 meter/sec
ZDOT = 523
130732 ZDOT = 159
450247
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 15037
51581041
00016717 00000-0 10270-3 0 9008
2 25544 51
6434 16
5794 0006225 335
6336 24
4522 15
54387313 7704
Satellite: ISS
Catalog Number: 25544
Epoch time: 15037
51581041 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 16
5794 deg
Eccentricity:
0006225
Arg of perigee: 335
6336 deg
Mean anomaly: 24
4522 deg
Mean motion: 15
54387313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 770
Checksum: 286
Coasting Arc #2 (Orbit 785)
---------------------------------------
Vector Time (GMT): 2015/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3121625
52 A = 6778020
57 meter
Y = 3388524
70 meter E =
0009774
Z = 4971880
29 I = 51
70292
XDOT = -6710
772270 Wp = 17
79342
YDOT = -3034
710244 meter/sec RA = 11
10065 deg
ZDOT = -2134
925705 TA = 93
04070
MA = 92
92886
Ha = 221
079 n
mi
Hp = 214
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10241553
53 X = -3183435
90
Y = 11117207
02 feet Y = 3353271
46 meter
Z = 16311943
20 Z = 4956565
90
XDOT = -22016
969390 XDOT = -6665
968183
YDOT = -9956
398439 feet/sec YDOT = -3109
504132 meter/sec
ZDOT = -7004
349427 ZDOT = -2167
415679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15158043
83 X = -4620171
76
Y = 933087
60 feet Y = 284405
10 meter
Z = 16245745
80 Z = 4951703
32
XDOT = -8999
367195 XDOT = -2743
007121
YDOT = -21248
638073 feet/sec YDOT = -6476
584885 meter/sec
ZDOT = -7142
785874 ZDOT = -2177
121134
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 15038
54444863
00016717 00000-0 10270-3 0 9013
2 25544 51
6436 11
4493 0006304 338
7723 21
3167 15
54439601 7864
Satellite: ISS
Catalog Number: 25544
Epoch time: 15038
54444863 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 11
4493 deg
Eccentricity:
0006304
Arg of perigee: 338
7723 deg
Mean anomaly: 21
3167 deg
Mean motion: 15
54439601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 786
Checksum: 301
Coasting Arc #3 (Orbit 800)
---------------------------------------
Vector Time (GMT): 2015/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4712951
71 A = 6781512
16 meter
Y = -2715323
68 meter E =
0006192
Z = -4051446
75 I = 51
68391
XDOT = 5472
037139 Wp = 50
77815
YDOT = 3686
933048 meter/sec RA = 6
10940 deg
ZDOT = 3902
285560 TA = 259
63826
MA = 259
70807
Ha = 221
188 n
mi
Hp = 214
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15462440
01 X = 4762644
95
Y = -8908542
25 feet Y = -2662342
87 meter
Z = -13292148
13 Z = -4028431
56
XDOT = 17952
877752 XDOT = 5411
446728
YDOT = 12096
237033 feet/sec YDOT = 3747
786479 meter/sec
ZDOT = 12802
774146 ZDOT = 3928
719785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17477349
02 X = 5327095
98
Y = 3951430
61 feet Y = 1204396
05 meter
Z = -13193136
30 Z = -4021267
95
XDOT = 5270
532904 XDOT = 1606
458429
YDOT = 19723
393496 feet/sec YDOT = 6011
690338 meter/sec
ZDOT = 12915
160877 ZDOT = 3936
541035
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 15039
50877290
00016717 00000-0 10270-3 0 9025
2 25544 51
6440 6
6399 0006323 342
8569 17
2370 15
54457362 8017
Satellite: ISS
Catalog Number: 25544
Epoch time: 15039
50877290 = yrday
fracday
Element set: 902
Inclination: 51
6440 deg
RA of node: 6
6399 deg
Eccentricity:
0006323
Arg of perigee: 342
8569 deg
Mean anomaly: 17
2370 deg
Mean motion: 15
54457362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 801
Checksum: 306
Coasting Arc #4 (Orbit 816)
---------------------------------------
Vector Time (GMT): 2015/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5945672
89 A = 6785364
06 meter
Y = 1952688
44 meter E =
0012129
Z = 2616974
93 I = 51
66633
XDOT = -3696
514247 Wp = 75
30531
YDOT = -4211
163957 meter/sec RA = 1
12707 deg
ZDOT = -5232
834197 TA = 75
23360
MA = 75
09923
Ha = 221
151 n
mi
Hp = 214
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19506800
82 X = -5979778
55
Y = 6406458
13 feet Y = 1886009
57 meter
Z = 8585875
76 Z = 2588009
36
XDOT = -12127
671414 XDOT = -3623
730440
YDOT = -13816
154713 feet/sec YDOT = -4252
094253 meter/sec
ZDOT = -17168
091197 ZDOT = -5250
613806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18885522
36 X = -5756307
22
Y = -8186225
10 feet Y = -2495161
41 meter
Z = 8461560
75 Z = 2579083
72
XDOT = -419
674165 XDOT = -127
916686
YDOT = -16935
295005 feet/sec YDOT = -5161
877917 meter/sec
ZDOT = -17243
337382 ZDOT = -5255
769234
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 15040
53735935
00016717 00000-0 10270-3 0 9030
2 25544 51
6444 1
5095 0006342 346
3763 13
7218 15
54523056 8177
Satellite: ISS
Catalog Number: 25544
Epoch time: 15040
53735935 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 1
5095 deg
Eccentricity:
0006342
Arg of perigee: 346
3763 deg
Mean anomaly: 13
7218 deg
Mean motion: 15
54523056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 817
Checksum: 291
Coasting Arc #5 (Orbit 831)
---------------------------------------
Vector Time (GMT): 2015/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6621757
16 A = 6787771
78 meter
Y = -1148797
01 meter E =
0015017
Z = -886951
34 I = 51
64319
XDOT = 1586
772822 Wp = 20
44181
YDOT = 4599
329729 meter/sec RA = 356
15267 deg
ZDOT = 5933
346312 TA = 329
95333
MA = 330
03941
Ha = 221
194 n
mi
Hp = 214
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21724925
06 X = 6638419
57
Y = -3769019
05 feet Y = -1074655
10 meter
Z = -2909945
33 Z = -854743
89
XDOT = 5205
947580 XDOT = 1506
402412
YDOT = 15089
664464 feet/sec YDOT = 4616
625117 meter/sec
ZDOT = 19466
359290 ZDOT = 5940
858919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18964502
80 X = 5780380
45
Y = 11283160
74 feet Y = 3439107
39 meter
Z = -2771925
83 Z = -844882
99
XDOT = -5135
659269 XDOT = -1565
348945
YDOT = 13384
606677 feet/sec YDOT = 4079
628115 meter/sec
ZDOT = 19497
598516 ZDOT = 5942
868028
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 15041
50163430
00016717 00000-0 10270-3 0 9044
2 25544 51
6443 356
6999 0006265 349
9733 10
1294 15
54560610 8322
Satellite: ISS
Catalog Number: 25544
Epoch time: 15041
50163430 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 356
6999 deg
Eccentricity:
0006265
Arg of perigee: 349
9733 deg
Mean anomaly: 10
1294 deg
Mean motion: 15
54560610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 832
Checksum: 300
Coasting Arc #6 (Orbit 847)
---------------------------------------
Vector Time (GMT): 2015/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6709694
22 A = 6787489
52 meter
Y = 244136
49 meter E =
0005401
Z = -994137
96 I = 51
61223
XDOT = 694
148808 Wp = 103
16261
YDOT = -4839
175650 meter/sec RA = 351
17961 deg
ZDOT = -5901
610176 TA = 87
60727
MA = 87
54543
Ha = 221
195 n
mi
Hp = 213
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22013432
50 X = -6707096
43
Y = 800972
74 feet Y = 169118
78 meter
Z = -3261607
48 Z = -1026725
75
XDOT = 2277
391101 XDOT = 776
877568
YDOT = -15876
560533 feet/sec YDOT = -4830
951036 meter/sec
ZDOT = -19362
238110 ZDOT = -5898
036923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17455685
51 X = -5320492
94
Y = -13401590
24 feet Y = -4084804
71 meter
Z = -3401069
42 Z = -1036645
96
XDOT = 10993
228552 XDOT = 3350
736063
YDOT = -9431
670116 feet/sec YDOT = -2874
773051 meter/sec
ZDOT = -19346
001872 ZDOT = -5896
661370
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 15042
53016792
00016717 00000-0 10270-3 0 9057
2 25544 51
6452 351
5690 0006323 353
2735 6
8332 15
54602567 8489
Satellite: ISS
Catalog Number: 25544
Epoch time: 15042
53016792 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 351
5690 deg
Eccentricity:
0006323
Arg of perigee: 353
2735 deg
Mean anomaly: 6
8332 deg
Mean motion: 15
54602567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 848
Checksum: 300
Coasting Arc #7 (Orbit 863)
---------------------------------------
Vector Time (GMT): 2015/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6156678
58 A = 6784565
16 meter
Y = 721437
36 meter E =
0015515
Z = 2734091
98 I = 51
57181
XDOT = -2869
074933 Wp = 55
52080
YDOT = 4913
659109 meter/sec RA = 346
19981 deg
ZDOT = 5151
855280 TA = 335
48623
MA = 335
55992
Ha = 221
115 n
mi
Hp = 213
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20199076
72 X = 6134872
66
Y = 2366920
49 feet Y = 790163
57 meter
Z = 8970118
03 Z = 2763946
63
XDOT = -9412
975503 XDOT = -2948
832927
YDOT = 16120
928835 feet/sec YDOT = 4881
129555 meter/sec
ZDOT = 16902
412337 ZDOT = 5137
724037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14260396
08 X = 4346568
73
Y = 14420163
70 feet Y = 4395265
90 meter
Z = 9097692
72 Z = 2772976
74
XDOT = -16448
597853 XDOT = -5013
532626
YDOT = 5616
405625 feet/sec YDOT = 1711
880435 meter/sec
ZDOT = 16840
996141 ZDOT = 5133
135624
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 15043
55867390
00016717 00000-0 10270-3 0 9069
2 25544 51
6452 346
4383 0006249 356
9373 3
1741 15
54644959 8649
Satellite: ISS
Catalog Number: 25544
Epoch time: 15043
55867390 = yrday
fracday
Element set: 906
Inclination: 51
6452 deg
RA of node: 346
4383 deg
Eccentricity:
0006249
Arg of perigee: 356
9373 deg
Mean anomaly: 3
1741 deg
Mean motion: 15
54644959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 864
Checksum: 332
Coasting Arc #8 (Orbit 878)
---------------------------------------
Vector Time (GMT): 2015/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5060433
50 A = 6780239
82 meter
Y = -1772081
55 meter E =
0011681
Z = -4162739
86 I = 51
52780
XDOT = 4726
313411 Wp = 39
31603
YDOT = -4736
204432 meter/sec RA = 341
20608 deg
ZDOT = -3726
237454 TA = 192
24748
MA = 192
27590
Ha = 221
254 n
mi
Hp = 213
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16602472
10 X = -5020020
77
Y = -5813915
84 feet Y = -1828444
82 meter
Z = -13657283
02 Z = -4187223
94
XDOT = 15506
277596 XDOT = 4797
023945
YDOT = -15538
728452 feet/sec YDOT = -4682
956501 meter/sec
ZDOT = -12225
188498 ZDOT = -3703
106282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9529621
98 X = -2904628
78
Y = -14689033
33 feet Y = -4477217
36 meter
Z = -13761674
37 Z = -4194558
35
XDOT = 20758
401645 XDOT = 6327
160821
YDOT = -2097
913905 feet/sec YDOT = -639
444158 meter/sec
ZDOT = -12125
310211 ZDOT = -3695
794552
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 15044
52287343
00016717 00000-0 10270-3 0 9072
2 25544 51
6456 341
6276 0006318
6262 359
4898 15
54693745 8791
Satellite: ISS
Catalog Number: 25544
Epoch time: 15044
52287343 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 341
6276 deg
Eccentricity:
0006318
Arg of perigee:
6262 deg
Mean anomaly: 359
4898 deg
Mean motion: 15
54693745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 879
Checksum: 337
Coasting Arc #9 (Orbit 894)
---------------------------------------
Vector Time (GMT): 2015/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3509252
58 A = 6776577
30 meter
Y = 2842440
12 meter E =
0005651
Z = 5047553
42 I = 51
48667
XDOT = -6098
921143 Wp = 56
27039
YDOT = 4282
200047 meter/sec RA = 336
19828 deg
ZDOT = 1830
360838 TA = 15
98994
MA = 15
97211
Ha = 221
087 n
mi
Hp = 213
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11513295
86 X = 3452688
18
Y = 9325590
93 feet Y = 2881366
76 meter
Z = 16560214
63 Z = 5064462
95
XDOT = -20009
583802 XDOT = -6155
243502
YDOT = 14049
212754 feet/sec YDOT = 4213
683083 meter/sec
ZDOT = 6005
120858 ZDOT = 1800
596973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3586787
03 X = 1093252
69
Y = 14292482
39 feet Y = 4356348
63 meter
Z = 16631994
54 Z = 5069431
94
XDOT = -23428
329145 XDOT = -7140
954724
YDOT = -953
378366 feet/sec YDOT = -290
589726 meter/sec
ZDOT = 5876
962821 ZDOT = 1791
298268
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 15045
55132500
00016717 00000-0 10270-3 0 9081
2 25544 51
6458 336
4967 0006178 2
9498 357
1691 15
54755231 8955
Satellite: ISS
Catalog Number: 25544
Epoch time: 15045
55132500 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 336
4967 deg
Eccentricity:
0006178
Arg of perigee: 2
9498 deg
Mean anomaly: 357
1691 deg
Mean motion: 15
54755231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 895
Checksum: 330
Coasting Arc #10 (Orbit 909)
---------------------------------------
Vector Time (GMT): 2015/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1728570
11 A = 6775551
92 meter
Y = -3868740
77 meter E =
0016537
Z = -5300284
29 I = 51
45508
XDOT = 6820
884064 Wp = 70
13570
YDOT = -3468
092228 meter/sec RA = 331
17996 deg
ZDOT = 313
221535 TA = 202
82502
MA = 202
89862
Ha = 221
280 n
mi
Hp = 212
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5671161
78 X = -1659434
16
Y = -12692719
08 feet Y = -3887684
39 meter
Z = -17389384
14 Z = -5308513
13
XDOT = 22378
228555 XDOT = 6857
636664
YDOT = -11378
255341 feet/sec YDOT = -3391
611153 meter/sec
ZDOT = 1027
629709 ZDOT = 346
444819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2881767
05 X = 878362
60
Y = -13555932
64 feet Y = -4131848
27 meter
Z = -17423833
77 Z = -5310784
53
XDOT = 23821
246072 XDOT = 7260
715803
YDOT = 3586
137490 feet/sec YDOT = 1093
054707 meter/sec
ZDOT = 1170
422513 ZDOT = 356
744782
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 15046
51547595
00016717 00000-0 10270-3 0 9093
2 25544 51
6462 331
6856 0006269 7
2883 352
8360 15
54762308 9107
Satellite: ISS
Catalog Number: 25544
Epoch time: 15046
51547595 = yrday
fracday
Element set: 909
Inclination: 51
6462 deg
RA of node: 331
6856 deg
Eccentricity:
0006269
Arg of perigee: 7
2883 deg
Mean anomaly: 352
8360 deg
Mean motion: 15
54762308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 910
Checksum: 324
Coasting Arc #11 (Orbit 925)
---------------------------------------
Vector Time (GMT): 2015/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -152136
90 A = 6777423
37 meter
Y = 4743700
65 meter E =
0012181
Z = 4835603
65 I = 51
43447
XDOT = -6903
778240 Wp = 36
72517
YDOT = 2282
666835 meter/sec RA = 326
16152 deg
ZDOT = -2443
715888 TA = 77
38618
MA = 77
24999
Ha = 221
320 n
mi
Hp = 212
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -499136
82 X = -228659
79
Y = 15563322
34 feet Y = 4741571
71 meter
Z = 15864841
39 Z = 4834678
54
XDOT = -22650
191076 XDOT = -6916
920072
YDOT = 7489
064420 feet/sec YDOT = 2205
390698 meter/sec
ZDOT = -8017
440577 ZDOT = -2477
284360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9347646
27 X = -2849162
58
Y = 12459622
09 feet Y = 3797692
81 meter
Z = 15859970
32 Z = 4834118
95
XDOT = -21937
216636 XDOT = -6686
463631
YDOT = -6015
891790 feet/sec YDOT = -1833
643818 meter/sec
ZDOT = -8161
475436 ZDOT = -2487
617713
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 15047
54387565
00016717 00000-0 10270-3 0 9108
2 25544 51
6462 326
5544 0006265 10
8500 349
2787 15
54809613 9267
Satellite: ISS
Catalog Number: 25544
Epoch time: 15047
54387565 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 326
5544 deg
Eccentricity:
0006265
Arg of perigee: 10
8500 deg
Mean anomaly: 349
2787 deg
Mean motion: 15
54809613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 926
Checksum: 319
Coasting Arc #12 (Orbit 940)
---------------------------------------
Vector Time (GMT): 2015/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1856619
09 A = 6781297
06 meter
Y = -5337120
29 meter E =
0008712
Z = -3750920
71 I = 51
42270
XDOT = 6340
613785 Wp = 56
03351
YDOT = -765
270832 meter/sec RA = 321
15017 deg
ZDOT = 4239
201678 TA = 258
94139
MA = 259
03939
Ha = 221
324 n
mi
Hp = 212
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6091269
97 X = 1934382
14
Y = -17510237
18 feet Y = -5315923
82 meter
Z = -12306170
31 Z = -3741712
62
XDOT = 20802
538666 XDOT = 6328
108046
YDOT = -2510
731076 feet/sec YDOT = -694
435599 meter/sec
ZDOT = 13908
141989 ZDOT = 4269
972043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14845887
89 X = 4525026
63
Y = -11149191
09 feet Y = -3398273
44 meter
Z = -12265763
50 Z = -3738604
72
XDOT = 17814
646782 XDOT = 5429
904339
YDOT = 8318
325206 feet/sec YDOT = 2535
425523 meter/sec
ZDOT = 14039
911984 ZDOT = 4279
365173
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 15048
50797571
00016717 00000-0 10270-3 0 9118
2 25544 51
6468 321
7432 0006233 14
3991 345
7338 15
54850665 9417
Satellite: ISS
Catalog Number: 25544
Epoch time: 15048
50797571 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 321
7432 deg
Eccentricity:
0006233
Arg of perigee: 14
3991 deg
Mean anomaly: 345
7338 deg
Mean motion: 15
54850665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 941
Checksum: 319
Coasting Arc #13 (Orbit 956)
---------------------------------------
Vector Time (GMT): 2015/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3315941
44 A = 6785323
29 meter
Y = 5525164
48 meter E =
0014997
Z = 2114656
89 I = 51
41210
XDOT = -5249
649650 Wp = 85
83931
YDOT = -1034
923133 meter/sec RA = 316
15061 deg
ZDOT = -5493
021891 TA = 70
65077
MA = 70
48868
Ha = 221
360 n
mi
Hp = 212
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10879072
96 X = -3387750
63
Y = 18127180
07 feet Y = 5487682
15 meter
Z = 6937850
68 Z = 2098374
18
XDOT = -17223
260005 XDOT = -5211
004369
YDOT = -3395
417102 feet/sec YDOT = -1093
412563 meter/sec
ZDOT = -18021
725363 ZDOT = -5518
429057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18985193
33 X = -5786686
93
Y = 9353460
50 feet Y = 2850934
76 meter
Z = 6867158
71 Z = 2093109
98
XDOT = -11879
679850 XDOT = -3620
926418
YDOT = -10717
238366 feet/sec YDOT = -3266
614254 meter/sec
ZDOT = -18130
209697 ZDOT = -5526
087916
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 15049
53632322
00016717 00000-0 10270-3 0 9125
2 25544 51
6466 316
6115 0006165 18
2101 341
9271 15
54868326 9570
Satellite: ISS
Catalog Number: 25544
Epoch time: 15049
53632322 = yrday
fracday
Element set: 912
Inclination: 51
6466 deg
RA of node: 316
6115 deg
Eccentricity:
0006165
Arg of perigee: 18
2101 deg
Mean anomaly: 341
9271 deg
Mean motion: 15
54868326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 957
Checksum: 299
Coasting Arc #14 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2015/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4324213
85 A = 6787026
98 meter
Y = -5214215
43 meter E =
0017634
Z = -220517
34 I = 51
39632
XDOT = 3806
829611 Wp = 35
49923
YDOT = 2914
413800 meter/sec RA = 311
15866 deg
ZDOT = 5992
317532 TA = 322
11461
MA = 322
23857
Ha = 221
335 n
mi
Hp = 212
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14187053
31 X = 4383270
22
Y = -17107006
01 feet Y = -5165529
08 meter
Z = -723482
08 Z = -199367
60
XDOT = 12489
598462 XDOT = 3744
849256
YDOT = 9561
725067 feet/sec YDOT = 2956
638385 meter/sec
ZDOT = 19659
834423 ZDOT = 6010
659066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21065339
08 X = 6420715
35
Y = -7092078
13 feet Y = -2161665
41 meter
Z = -632044
15 Z = -192647
06
XDOT = 4973
652533 XDOT = 1515
969292
YDOT = 13099
401422 feet/sec YDOT = 3992
697554 meter/sec
ZDOT = 19737
743965 ZDOT = 6016
064361
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 15050
50037336
00016717 00000-0 10270-3 0 9139
2 25544 51
6467 311
8003 0006244 20
4741 339
6661 15
54916421 9721
Satellite: ISS
Catalog Number: 25544
Epoch time: 15050
50037336 = yrday
fracday
Element set: 913
Inclination: 51
6467 deg
RA of node: 311
8003 deg
Eccentricity:
0006244
Arg of perigee: 20
4741 deg
Mean anomaly: 339
6661 deg
Mean motion: 15
54916421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 972
Checksum: 284
Coasting Arc #15 (Orbit 987)
---------------------------------------
Vector Time (GMT): 2015/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4913061
80 A = 6785614
93 meter
Y = 4339707
63 meter E =
0007038
Z = -1758683
08 I = 51
37181
XDOT = -2146
973916 Wp = 91
70051
YDOT = -4711
722942 meter/sec RA = 306
16631 deg
ZDOT = -5648
640160 TA = 107
67104
MA = 107
59419
Ha = 221
308 n
mi
Hp = 212
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16118969
16 X = -4952681
42
Y = 14237885
93 feet Y = 4284544
82 meter
Z = -5769957
60 Z = -1782646
11
XDOT = -7043
877678 XDOT = -2066
688290
YDOT = -15458
408604 feet/sec YDOT = -4735
283625 meter/sec
ZDOT = -18532
283991 ZDOT = -5658
873938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21099088
90 X = -6431002
30
Y = 4020487
34 feet Y = 1225444
54 meter
Z = -5873253
10 Z = -1790167
55
XDOT = 2239
349531 XDOT = 682
553737
YDOT = -15289
949575 feet/sec YDOT = -4660
376630 meter/sec
ZDOT = -18575
185370 ZDOT = -5661
716501
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 15051
52866814
00016717 00000-0 10270-3 0 9144
2 25544 51
6467 306
6679 0006057 23
7963 336
3469 15
54936758 9888
Satellite: ISS
Catalog Number: 25544
Epoch time: 15051
52866814 = yrday
fracday
Element set: 914
Inclination: 51
6467 deg
RA of node: 306
6679 deg
Eccentricity:
0006057
Arg of perigee: 23
7963 deg
Mean anomaly: 336
3469 deg
Mean motion: 15
54936758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 988
Checksum: 356
Coasting Arc #16 (Orbit 1003)
---------------------------------------
Vector Time (GMT): 2015/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5019031
02 A = 6781641
03 meter
Y = -2947057
14 meter E =
0015998
Z = 3462245
19 I = 51
34072
XDOT = 496
500514 Wp = 70
67371
YDOT = 6179
579369 meter/sec RA = 301
16308 deg
ZDOT = 4528
382781 TA = 330
22356
MA = 330
31451
Ha = 221
258 n
mi
Hp = 211
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16466637
22 X = 5034794
64
Y = -9668822
65 feet Y = -2890842
48 meter
Z = 11359072
15 Z = 3486664
98
XDOT = 1628
938695 XDOT = 405
365226
YDOT = 20274
210529 feet/sec YDOT = 6184
622581 meter/sec
ZDOT = 14856
898889 ZDOT = 4530
572494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19030828
41 X = 5800596
50
Y = -260398
05 feet Y = -79369
33 meter
Z = 11464054
95 Z = 3494243
95
XDOT = -8745
688899 XDOT = -2665
685977
YDOT = 16977
898047 feet/sec YDOT = 5174
863325 meter/sec
ZDOT = 14865
132820 ZDOT = 4530
892484
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 15052
55693608
00016717 00000-0 10270-3 0 9158
2 25544 51
6463 301
5350 0006270 27
6520 332
4965 15
54988113 10043
Satellite: ISS
Catalog Number: 25544
Epoch time: 15052
55693608 = yrday
fracday
Element set: 915
Inclination: 51
6463 deg
RA of node: 301
5350 deg
Eccentricity:
0006270
Arg of perigee: 27
6520 deg
Mean anomaly: 332
4965 deg
Mean motion: 15
54988113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1004
Checksum: 295
Coasting Arc #17 (Orbit 1018)
---------------------------------------
Vector Time (GMT): 2015/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4755151
96 A = 6777127
23 meter
Y = 1123216
06 meter E =
0016168
Z = -4712108
94 I = 51
31047
XDOT = 1037
138519 Wp = 56
02952
YDOT = -7077
431584 meter/sec RA = 296
14457 deg
ZDOT = -2731
542198 TA = 186
76281
MA = 186
78466
Ha = 221
276 n
mi
Hp = 211
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15600892
25 X = -4744469
20
Y = 3685092
07 feet Y = 1070100
02 meter
Z = -15459674
99 Z = -4735182
47
XDOT = 3402
685431 XDOT = 1129
471612
YDOT = -23219
919896 feet/sec YDOT = -7065
317689 meter/sec
ZDOT = -8961
752618 ZDOT = -2726
278919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15362744
31 X = -4682564
47
Y = -4229249
38 feet Y = -1289075
21 meter
Z = -15558561
32 Z = -4742249
49
XDOT = 13896
238661 XDOT = 4235
573544
YDOT = -17571
897609 feet/sec YDOT = -5355
914391 meter/sec
ZDOT = -8937
955954 ZDOT = -2724
288975
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 15053
52091141
00016717 00000-0 10270-3 0 9161
2 25544 51
6461 296
7229 0006189 29
2511 330
8987 15
55053619 10195
Satellite: ISS
Catalog Number: 25544
Epoch time: 15053
52091141 = yrday
fracday
Element set: 916
Inclination: 51
6461 deg
RA of node: 296
7229 deg
Eccentricity:
0006189
Arg of perigee: 29
2511 deg
Mean anomaly: 330
8987 deg
Mean motion: 15
55053619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1019
Checksum: 310
Coasting Arc #18 (Orbit 1034)
---------------------------------------
Vector Time (GMT): 2015/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4154202
98 A = 6774636
23 meter
Y = 947851
08 meter E =
0007222
Z = 5261386
83 I = 51
28940
XDOT = -2346
855252 Wp = 55
29115
YDOT = 7287
519515 meter/sec RA = 291
11295 deg
ZDOT = 543
642070 TA = 29
52129
MA = 29
48053
Ha = 221
142 n
mi
Hp = 211
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13629274
86 X = 4117737
52
Y = 3109747
64 feet Y = 994102
75 meter
Z = 17261767
80 Z = 5281478
28
XDOT = -7699
656339 XDOT = -2430
812378
YDOT = 23909
184762 feet/sec YDOT = 7260
806075 meter/sec
ZDOT = 1783
602593 ZDOT = 532
036917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10512403
62 X = 3204180
62
Y = 9052573
39 feet Y = 2759224
37 meter
Z = 17347523
63 Z = 5287525
20
XDOT = -17303
402014 XDOT = -5274
076934
YDOT = 16795
447880 feet/sec YDOT = 5119
252514 meter/sec
ZDOT = 1732
653843 ZDOT = 528
112891
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 15054
54912740
00016717 00000-0 10270-3 0 9172
2 25544 51
6461 291
5896 0006148 33
4060 326
7480 15
55088930 10353
Satellite: ISS
Catalog Number: 25544
Epoch time: 15054
54912740 = yrday
fracday
Element set: 917
Inclination: 51
6461 deg
RA of node: 291
5896 deg
Eccentricity:
0006148
Arg of perigee: 33
4060 deg
Mean anomaly: 326
7480 deg
Mean motion: 15
55088930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1035
Checksum: 309
Coasting Arc #19 (Orbit 1049)
---------------------------------------
Vector Time (GMT): 2015/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3361577
36 A = 6775446
11 meter
Y = -3009180
67 meter E =
0016613
Z = -5068626
52 I = 51
28136
XDOT = 3362
862811 Wp = 83
04604
YDOT = -6659
504350 meter/sec RA = 286
07719 deg
ZDOT = 1730
241451 TA = 203
74748
MA = 203
82423
Ha = 221
208 n
mi
Hp = 211
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11028797
12 X = -3303056
88
Y = -9872639
98 feet Y = -3046445
27 meter
Z = -16629352
11 Z = -5084813
85
XDOT = 11033
014471 XDOT = 3428
676235
YDOT = -21848
767551 feet/sec YDOT = -6621
530484 meter/sec
ZDOT = 5676
645182 ZDOT = 1746
737893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5300904
03 X = -1615715
55
Y = -13737340
80 feet Y = -4187141
48 meter
Z = -16698042
46 Z = -5089563
34
XDOT = 18661
522753 XDOT = 5688
032135
YDOT = -14161
040564 feet/sec YDOT = -4316
285164 meter/sec
ZDOT = 5748
391944 ZDOT = 1752
109864
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 15055
51305540
00016717 00000-0 10270-3 0 9185
2 25544 51
6455 286
7766 0006130 35
4093 324
7466 15
55132317 10505
Satellite: ISS
Catalog Number: 25544
Epoch time: 15055
51305540 = yrday
fracday
Element set: 918
Inclination: 51
6455 deg
RA of node: 286
7766 deg
Eccentricity:
0006130
Arg of perigee: 35
4093 deg
Mean anomaly: 324
7466 deg
Mean motion: 15
55132317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1050
Checksum: 294
Coasting Arc #20 (Orbit 1065)
---------------------------------------
Vector Time (GMT): 2015/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2396854
64 A = 6779041
78 meter
Y = 4838483
32 meter E =
0015788
Z = 4091787
18 I = 51
28648
XDOT = -4116
251595 Wp = 62
27296
YDOT = 5254
592526 meter/sec RA = 281
04916 deg
ZDOT = -3783
847736 TA = 67
00927
MA = 66
84280
Ha = 221
127 n
mi
Hp = 211
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7863696
33 X = 2322695
27
Y = 15874289
12 feet Y = 4864872
19 meter
Z = 13424498
63 Z = 4103250
01
XDOT = -13504
762451 XDOT = -4156
323434
YDOT = 17239
476791 feet/sec YDOT = 5208
337563 meter/sec
ZDOT = -12414
198609 ZDOT = -3803
941224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 93062
83 X = 28365
55
Y = 17678423
12 feet Y = 5388383
37 meter
Z = 13472662
46 Z = 4106467
52
XDOT = -18301
335284 XDOT = -5578
246994
YDOT = 9669
335012 feet/sec YDOT = 2947
213312 meter/sec
ZDOT = -12501
072166 ZDOT = -3810
326796
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 15056
54121875
00016717 00000-0 10270-3 0 9197
2 25544 51
6458 281
6432 0006164 37
6689 322
4895 15
55203537 10665
Satellite: ISS
Catalog Number: 25544
Epoch time: 15056
54121875 = yrday
fracday
Element set: 919
Inclination: 51
6458 deg
RA of node: 281
6432 deg
Eccentricity:
0006164
Arg of perigee: 37
6689 deg
Mean anomaly: 322
4895 deg
Mean motion: 15
55203537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1066
Checksum: 326
Coasting Arc #21 (Orbit 1080)
---------------------------------------
Vector Time (GMT): 2015/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1393202
66 A = 6783496
25 meter
Y = -6133994
56 meter E =
0011258
Z = -2533795
92 I = 51
29503
XDOT = 4573
839267 Wp = 45
31493
YDOT = -3201
002903 meter/sec RA = 276
03432 deg
ZDOT = 5256
492953 TA = 286
07832
MA = 286
20224
Ha = 221
179 n
mi
Hp = 211
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4570874
86 X = -1312199
26
Y = -20124654
06 feet Y = -6149121
53 meter
Z = -8312978
76 Z = -2540366
55
XDOT = 15006
034342 XDOT = 4583
759951
YDOT = -10501
978028 feet/sec YDOT = -3149
799394 meter/sec
ZDOT = 17245
711789 ZDOT = 5278
735823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4345872
38 X = 1324621
90
Y = -20163284
12 feet Y = -6145769
00 meter
Z = -8339998
83 Z = -2542031
64
XDOT = 16457
659123 XDOT = 5016
294501
YDOT = -3595
604438 feet/sec YDOT = -1095
940233 meter/sec
ZDOT = 17341
410863 ZDOT = 5285
662031
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 15057
50509959
00016717 00000-0 10270-3 0 9209
2 25544 51
6447 276
8301 0006079 40
8895 319
2713 15
55189953 10819
Satellite: ISS
Catalog Number: 25544
Epoch time: 15057
50509959 = yrday
fracday
Element set: 920
Inclination: 51
6447 deg
RA of node: 276
8301 deg
Eccentricity:
0006079
Arg of perigee: 40
8895 deg
Mean anomaly: 319
2713 deg
Mean motion: 15
55189953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1081
Checksum: 332
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