[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 10th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17276 08 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
077/23:46:39
058 -2
3 2
3 2
3
N/A 0
0 0
0 222
1
000/00:05:14
116 0
3 -0
0 211
1
Coasting Arc #1 (Orbit 1252)
---------------------------------------
Vector Time (GMT): 2015/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3103422
99 A = 6784032
79 meter
Y = -5433658
81 meter E =
0022186
Z = 2595828
02 I = 51
41109
XDOT = 5582
896258 Wp = 80
28404
YDOT = -676
335623 meter/sec RA = 220
93603 deg
ZDOT = 5224
408849 TA = 309
07089
MA = 309
26806
Ha = 222
819 n
mi
Hp = 210
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10181833
96 X = -3055041
41
Y = -17826964
59 feet Y = -5468092
42 meter
Z = 8516496
14 Z = 2580870
53
XDOT = 18316
588772 XDOT = 5564
666106
YDOT = -2218
948894 feet/sec YDOT = -614
005217 meter/sec
ZDOT = 17140
448981 ZDOT = 5251
485223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5627883
20 X = -1715378
80
Y = -19770410
35 feet Y = -6026021
07 meter
Z = 8453337
87 Z = 2576577
38
XDOT = 16762
482526 XDOT = 5109
204674
YDOT = 2655
476680 feet/sec YDOT = 809
389292 meter/sec
ZDOT = 17256
424032 ZDOT = 5259
758045
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 15068
55909434
00016717 00000-0 10270-3 0 9006
2 25544 51
6429 221
6695 0008603 85
5616 274
6520 15
54983109 12530
Satellite: ISS
Catalog Number: 25544
Epoch time: 15068
55909434 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 221
6695 deg
Eccentricity:
0008603
Arg of perigee: 85
5616 deg
Mean anomaly: 274
6520 deg
Mean motion: 15
54983109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1253
Checksum: 320
Coasting Arc #2 (Orbit 1267)
---------------------------------------
Vector Time (GMT): 2015/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1493981
49 A = 6779525
63 meter
Y = 5165548
51 meter E =
0016051
Z = -4144426
40 I = 51
42151
XDOT = -6590
481398 Wp = 80
26626
YDOT = -1089
084297 meter/sec RA = 215
93209 deg
ZDOT = -3742
903386 TA = 151
07511
MA = 150
98605
Ha = 222
784 n
mi
Hp = 210
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4901514
09 X = 1456240
13
Y = 16947337
62 feet Y = 5182043
62 meter
Z = -13597199
47 Z = -4137261
28
XDOT = -21622
314298 XDOT = -6559
631572
YDOT = -3573
111211 feet/sec YDOT = -1162
611358 meter/sec
ZDOT = -12279
866751 ZDOT = -3774
843559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1051205
80 X = 320407
53
Y = 17633581
15 feet Y = 5374715
54 meter
Z = -13567339
76 Z = -4135325
16
XDOT = -18903
610755 XDOT = -5761
820558
YDOT = -8401
629217 feet/sec YDOT = -2560
816585 meter/sec
ZDOT = -12416
390856 ZDOT = -3784
515933
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 15069
52309193
00016717 00000-0 10270-3 0 9011
2 25544 51
6436 216
8580 0008661 87
9742 272
2403 15
55010648 12687
Satellite: ISS
Catalog Number: 25544
Epoch time: 15069
52309193 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 216
8580 deg
Eccentricity:
0008661
Arg of perigee: 87
9742 deg
Mean anomaly: 272
2403 deg
Mean motion: 15
55010648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1268
Checksum: 312
Coasting Arc #3 (Orbit 1283)
---------------------------------------
Vector Time (GMT): 2015/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 374445
59 A = 6775674
89 meter
Y = -4478480
20 meter E =
0013353
Z = 5060471
62 I = 51
43548
XDOT = 7018
708956 Wp = 104
60290
YDOT = 2574
832938 meter/sec RA = 210
91523 deg
ZDOT = 1752
184803 TA = 328
38916
MA = 328
46929
Ha = 222
618 n
mi
Hp = 210
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1228496
03 X = 399915
32
Y = -14693176
49 feet Y = -4474149
90 meter
Z = 16602597
19 Z = 5062353
00
XDOT = 23027
260355 XDOT = 6980
883467
YDOT = 8447
614626 feet/sec YDOT = 2653
109433 meter/sec
ZDOT = 5748
637805 ZDOT = 1786
188122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4154011
20 X = 1266142
61
Y = -14136911
91 feet Y = -4308930
75 meter
Z = 16611345
05 Z = 5063137
97
XDOT = 19699
901892 XDOT = 6004
530097
YDOT = 12741
694850 feet/sec YDOT = 3883
668590 meter/sec
ZDOT = 5893
774852 ZDOT = 1796
422575
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 15070
55132978
00016717 00000-0 10270-3 0 9022
2 25544 51
6436 211
7248 0008503 91
5571 268
6556 15
55068664 12845
Satellite: ISS
Catalog Number: 25544
Epoch time: 15070
55132978 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 211
7248 deg
Eccentricity:
0008503
Arg of perigee: 91
5571 deg
Mean anomaly: 268
6556 deg
Mean motion: 15
55068664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1284
Checksum: 321
Coasting Arc #4 (Orbit 1298)
---------------------------------------
Vector Time (GMT): 2015/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2375039
23 A = 6774613
62 meter
Y = 3532034
24 meter E =
0023431
Z = -5290994
61 I = 51
46039
XDOT = -6675
676871 Wp = 94
42460
YDOT = -3704
486224 meter/sec RA = 205
89354 deg
ZDOT = 523
888259 TA = 180
59514
MA = 180
59794
Ha = 222
641 n
mi
Hp = 209
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7792123
46 X = -2388657
14
Y = 11588038
83 feet Y = 3505398
30 meter
Z = -17358906
20 Z = -5302565
51
XDOT = -21901
827005 XDOT = -6636
301127
YDOT = -12153
826194 feet/sec YDOT = -3778
917782 meter/sec
ZDOT = 1718
793502 ZDOT = 491
555218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9754602
27 X = -2973202
77
Y = 9904872
95 feet Y = 3019005
27 meter
Z = -17408982
83 Z = -5306257
97
XDOT = -18463
464627 XDOT = -5627
664018
YDOT = -15405
994521 feet/sec YDOT = -4695
747130 meter/sec
ZDOT = 1580
964313 ZDOT = 481
877922
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 15071
51528049
00016717 00000-0 10270-3 0 9038
2 25544 51
6441 206
9140 0008668 94
5283 265
6861 15
55099672 12998
Satellite: ISS
Catalog Number: 25544
Epoch time: 15071
51528049 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 206
9140 deg
Eccentricity:
0008668
Arg of perigee: 94
5283 deg
Mean anomaly: 265
6861 deg
Mean motion: 15
55099672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1299
Checksum: 330
Coasting Arc #5 (Orbit 1314)
---------------------------------------
Vector Time (GMT): 2015/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4227453
39 A = 6776974
48 meter
Y = -2398297
38 meter E =
0015610
Z = 4710369
52 I = 51
49723
XDOT = 5605
975749 Wp = 81
63033
YDOT = 4473
559996 meter/sec RA = 200
87364 deg
ZDOT = -2743
504936 TA = 35
58548
MA = 35
48148
Ha = 222
552 n
mi
Hp = 209
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13869597
75 X = 4231076
42
Y = -7868429
73 feet Y = -2351002
53 meter
Z = 15453968
23 Z = 4730914
60
XDOT = 18392
308889 XDOT = 5568
861555
YDOT = 14677
034109 feet/sec YDOT = 4536
041893 meter/sec
ZDOT = -9001
000445 ZDOT = -2716
362899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14931192
92 X = 4551027
60
Y = -5347865
55 feet Y = -1630029
42 meter
Z = 15542293
08 Z = 4737290
93
XDOT = 15220
423035 XDOT = 4639
184941
YDOT = 16576
813742 feet/sec YDOT = 5052
612829 meter/sec
ZDOT = -8885
494651 ZDOT = -2708
298770
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 15072
54346903
00016717 00000-0 10270-3 0 9040
2 25544 51
6441 201
7800 0008703 98
0207 262
1934 15
55090469 13156
Satellite: ISS
Catalog Number: 25544
Epoch time: 15072
54346903 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 201
7800 deg
Eccentricity:
0008703
Arg of perigee: 98
0207 deg
Mean anomaly: 262
1934 deg
Mean motion: 15
55090469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1315
Checksum: 290
Coasting Arc #6 (Orbit 1329)
---------------------------------------
Vector Time (GMT): 2015/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5699957
55 A = 6781168
35 meter
Y = 1244724
66 meter E =
0013558
Z = -3469815
60 I = 51
54217
XDOT = -3816
601244 Wp = 98
35335
YDOT = -4839
341441 meter/sec RA = 195
86868 deg
ZDOT = 4546
931468 TA = 220
89602
MA = 220
99781
Ha = 222
472 n
mi
Hp = 209
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18700648
13 X = -5696597
78
Y = 4083742
32 feet Y = 1181002
48 meter
Z = -11383909
45 Z = -3497496
63
XDOT = -12521
657624 XDOT = -3784
290051
YDOT = -15877
104464 feet/sec YDOT = -4881
840080 meter/sec
ZDOT = 14917
754160 ZDOT = 4528
470232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19038321
41 X = -5802880
37
Y = 1103011
93 feet Y = 336198
04 meter
Z = -11502620
08 Z = -3505998
60
XDOT = -9882
458146 XDOT = -3012
173243
YDOT = -16273
671942 feet/sec YDOT = -4960
215208 meter/sec
ZDOT = 14839
454981 ZDOT = 4523
065878
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 15073
50736883
00016717 00000-0 10270-3 0 9058
2 25544 51
6446 196
9681 0008491 100
3024 259
9087 15
55143281 13302
Satellite: ISS
Catalog Number: 25544
Epoch time: 15073
50736883 = yrday
fracday
Element set: 905
Inclination: 51
6446 deg
RA of node: 196
9681 deg
Eccentricity:
0008491
Arg of perigee: 100
3024 deg
Mean anomaly: 259
9087 deg
Mean motion: 15
55143281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1330
Checksum: 314
Coasting Arc #7 (Orbit 1345)
---------------------------------------
Vector Time (GMT): 2015/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6571967
40 A = 6785044
11 meter
Y = -65964
81 meter E =
0022409
Z = 1645919
88 I = 51
58627
XDOT = 1493
993698 Wp = 111
88967
YDOT = 4901
719302 meter/sec RA = 190
87935 deg
ZDOT = -5714
694886 TA = 50
04863
MA = 49
85200
Ha = 222
398 n
mi
Hp = 209
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21561572
85 X = 6564221
42
Y = -216419
97 feet Y = 7484
07 meter
Z = 5399999
61 Z = 1677826
08
XDOT = 4901
554127 XDOT = 1466
830037
YDOT = 16081
756241 feet/sec YDOT = 4918
273679 meter/sec
ZDOT = -18748
998970 ZDOT = -5707
503884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21344492
68 X = 6505801
37
Y = 2804734
81 feet Y = 854883
17 meter
Z = 5536637
23 Z = 1687567
03
XDOT = 2920
495043 XDOT = 890
166889
YDOT = 15068
734122 feet/sec YDOT = 4592
950160 meter/sec
ZDOT = -18718
956640 ZDOT = -5705
537984
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 15074
53550430
00016717 00000-0 10270-3 0 9065
2 25544 51
6447 191
8342 0008565 104
4343 255
7761 15
55189594 13469
Satellite: ISS
Catalog Number: 25544
Epoch time: 15074
53550430 = yrday
fracday
Element set: 906
Inclination: 51
6447 deg
RA of node: 191
8342 deg
Eccentricity:
0008565
Arg of perigee: 104
4343 deg
Mean anomaly: 255
7761 deg
Mean motion: 15
55189594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1346
Checksum: 318
Coasting Arc #8 (Orbit 1361)
---------------------------------------
Vector Time (GMT): 2015/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6697393
78 A = 6786068
32 meter
Y = -993439
83 meter E =
0018738
Z = 378302
90 I = 51
62219
XDOT = 1044
326882 Wp = 71
83006
YDOT = -4666
281264 meter/sec RA = 185
90114 deg
ZDOT = 5996
419848 TA = 292
25070
MA = 292
44933
Ha = 222
336 n
mi
Hp = 209
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21973076
70 X = -6687624
77
Y = -3259317
02 feet Y = -1068279
79 meter
Z = 1241151
23 Z = 345792
51
XDOT = 3426
269297 XDOT = 1067
300728
YDOT = -15309
321733 feet/sec YDOT = -4654
473811 meter/sec
ZDOT = 19673
293464 ZDOT = 6001
549230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21411702
64 X = -6526286
96
Y = -5941728
27 feet Y = -1811038
78 meter
Z = 1102070
21 Z = 335911
00
XDOT = 4728
451955 XDOT = 1441
232156
YDOT = -13223
029893 feet/sec YDOT = -4030
379511 meter/sec
ZDOT = 19695
972025 ZDOT = 6003
332273
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 15075
56361247
00016717 00000-0 10270-3 0 9076
2 25544 51
6456 186
7009 0008540 106
5561 253
6531 15
55234956 13623
Satellite: ISS
Catalog Number: 25544
Epoch time: 15075
56361247 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 186
7009 deg
Eccentricity:
0008540
Arg of perigee: 106
5561 deg
Mean anomaly: 253
6531 deg
Mean motion: 15
55234956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1362
Checksum: 313
Coasting Arc #9 (Orbit 1376)
---------------------------------------
Vector Time (GMT): 2015/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6006098
10 A = 6783558
55 meter
Y = 2015166
50 meter E =
0013835
Z = -2424072
83 I = 51
64595
XDOT = -3551
936860 Wp = 119
92545
YDOT = 4180
551760 meter/sec RA = 180
92320 deg
ZDOT = -5354
881278 TA = 87
18570
MA = 87
02737
Ha = 222
281 n
mi
Hp = 209
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19705046
26 X = 5994892
73
Y = 6611438
64 feet Y = 2082267
65 meter
Z = -7952994
86 Z = -2394924
24
XDOT = -11653
336156 XDOT = -3572
409127
YDOT = 13715
720999 feet/sec YDOT = 4140
716534 meter/sec
ZDOT = -17568
508131 ZDOT = -5372
185924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18942344
26 X = 5773626
53
Y = 8669085
58 feet Y = 2642337
28 meter
Z = -7828451
05 Z = -2386111
88
XDOT = -12299
213763 XDOT = -3748
800355
YDOT = 11031
141678 feet/sec YDOT = 3362
291983 meter/sec
ZDOT = -17643
260941 ZDOT = -5377
665935
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 15076
52743929
00016717 00000-0 10270-3 0 9085
2 25544 51
6458 181
8881 0008502 110
2804 249
9264 15
55280786 13778
Satellite: ISS
Catalog Number: 25544
Epoch time: 15076
52743929 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 181
8881 deg
Eccentricity:
0008502
Arg of perigee: 110
2804 deg
Mean anomaly: 249
9264 deg
Mean motion: 15
55280786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1377
Checksum: 337
Coasting Arc #10 (Orbit 1392)
---------------------------------------
Vector Time (GMT): 2015/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4607403
30 A = 6778941
46 meter
Y = -2878010
95 meter E =
0019200
Z = 4043284
20 I = 51
66331
XDOT = 5617
776340 Wp = 107
15396
YDOT = -3488
985731 meter/sec RA = 175
93475 deg
ZDOT = 3897
290749 TA = 302
41549
MA = 302
60109
Ha = 222
193 n
mi
Hp = 209
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15116152
56 X = -4594518
80
Y = -9442293
16 feet Y = -2929461
31 meter
Z = 13265368
11 Z = 4020934
32
XDOT = 18431
024737 XDOT = 5637
442123
YDOT = -11446
803578 feet/sec YDOT = -3426
053553 meter/sec
ZDOT = 12786
386971 ZDOT = 3924
628769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14299818
17 X = -4358584
58
Y = -10755908
98 feet Y = -3278401
06 meter
Z = 13170063
85 Z = 4014235
46
XDOT = 18510
694137 XDOT = 5642
059573
YDOT = -8725
141142 feet/sec YDOT = -2659
423020 meter/sec
ZDOT = 12904
019413 ZDOT = 3933
145117
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 15077
55549458
00016717 00000-0 10270-3 0 9091
2 25544 51
6464 176
7544 0008478 113
5170 246
6875 15
55345914 13933
Satellite: ISS
Catalog Number: 25544
Epoch time: 15077
55549458 = yrday
fracday
Element set: 909
Inclination: 51
6464 deg
RA of node: 176
7544 deg
Eccentricity:
0008478
Arg of perigee: 113
5170 deg
Mean anomaly: 246
6875 deg
Mean motion: 15
55345914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1393
Checksum: 348
Coasting Arc #11 (Orbit 1399)
---------------------------------------
Vector Time (GMT): 2015/077/23:49:16
116
Vector Time (MET): N/A
Weight (LBS) : 890095
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1786780
93 A = 6776356
13 meter
Y = 4203775
18 meter E =
0019388
Z = -5023234
47 I = 51
66547
XDOT = -7352
855516 Wp = 108
24819
YDOT = -741
973117 meter/sec RA = 173
43759 deg
ZDOT = 1994
907479 TA = 181
15448
MA = 181
15897
Ha = 222
085 n
mi
Hp = 211
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5862142
17 X = -1809255
00
Y = 13791913
31 feet Y = 4183667
78 meter
Z = -16480428
06 Z = -5031969
46
XDOT = -24123
541720 XDOT = -7353
702533
YDOT = -2434
295003 feet/sec YDOT = -824
201974 meter/sec
ZDOT = 6544
972044 ZDOT = 1959
187168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7463394
47 X = 2274842
64
Y = -12946954
43 feet Y = -3946231
71 meter
Z = -16518480
75 Z = -5034832
93
XDOT = 22715
231977 XDOT = 6923
602707
YDOT = 4940
732367 feet/sec YDOT = 1505
935225 meter/sec
ZDOT = 6392
064564 ZDOT = 1948
301279
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 15078
00526310
00016717 00000-0 10270-3 0 9106
2 25544 51
6457 174
5111 0006545 114
3135 245
8702 15
54905410 14005
Satellite: ISS
Catalog Number: 25544
Epoch time: 15078
00526310 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 174
5111 deg
Eccentricity:
0006545
Arg of perigee: 114
3135 deg
Mean anomaly: 245
8702 deg
Mean motion: 15
54905410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1400
Checksum: 265
Coasting Arc #12 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2015/078/23:49:16
116
Vector Time (MET): N/A
Weight (LBS) : 890095
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3713910
86 A = 6780040
94 meter
Y = -3993672
97 meter E =
0016362
Z = 4013399
37 I = 51
70934
XDOT = 6309
213508 Wp = 93
25335
YDOT = 1889
144421 meter/sec RA = 168
44146 deg
ZDOT = -3945
601909 TA = 37
70695
MA = 37
59239
Ha = 221
953 n
mi
Hp = 211
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12184746
92 X = 3738797
55
Y = -13102601
62 feet Y = -3952001
77 meter
Z = 13167320
75 Z = 4031501
83
XDOT = 20699
519382 XDOT = 6306
785879
YDOT = 6197
980385 feet/sec YDOT = 1959
683933 meter/sec
ZDOT = -12944
888154 ZDOT = -3914
959375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13468779
56 X = -4105284
01
Y = 11690761
24 feet Y = 3563344
03 meter
Z = 13245476
26 Z = 4037221
17
XDOT = -19120
888787 XDOT = -5828
046902
YDOT = -7463
128086 feet/sec YDOT = -2274
761441 meter/sec
ZDOT = -12813
895194 ZDOT = -3905
675255
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 15079
03356702
00016717 00000-0 10270-3 0 9117
2 25544 51
6455 169
3794 0006574 117
6002 242
5819 15
54938876 14165
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
03356702 = yrday
fracday
Element set: 911
Inclination: 51
6455 deg
RA of node: 169
3794 deg
Eccentricity:
0006574
Arg of perigee: 117
6002 deg
Mean anomaly: 242
5819 deg
Mean motion: 15
54938876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1416
Checksum: 326
Coasting Arc #13 (Orbit 1430)
---------------------------------------
Vector Time (GMT): 2015/079/23:49:16
116
Vector Time (MET): N/A
Weight (LBS) : 890095
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5206995
97 A = 6784135
64 meter
Y = 3581406
89 meter E =
0009624
Z = -2475079
15 I = 51
75487
XDOT = -4601
206594 Wp = 89
79941
YDOT = -3017
395425 meter/sec RA = 163
45994 deg
ZDOT = 5331
696196 TA = 242
53363
MA = 242
63151
Ha = 221
861 n
mi
Hp = 211
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17083320
11 X = -5234634
12
Y = 11750022
62 feet Y = 3523023
92 meter
Z = -8120338
43 Z = -2500441
43
XDOT = -15095
822158 XDOT = -4593
022754
YDOT = -9899
591290 feet/sec YDOT = -3068
802474 meter/sec
ZDOT = 17492
441589 ZDOT = 5309
364836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18049251
22 X = 5501411
77
Y = -10116417
00 feet Y = -3083483
90 meter
Z = -8229543
81 Z = -2508364
95
XDOT = 13483
554559 XDOT = 4109
787430
YDOT = 9951
654912 feet/sec YDOT = 3033
264417 meter/sec
ZDOT = 17397
219213 ZDOT = 5302
672416
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 15079
99757753
00016717 00000-0 10270-3 0 9124
2 25544 51
6460 164
5676 0006506 120
8209 239
3585 15
54995367 14316
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
99757753 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 164
5676 deg
Eccentricity:
0006506
Arg of perigee: 120
8209 deg
Mean anomaly: 239
3585 deg
Mean motion: 15
54995367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1431
Checksum: 344
Coasting Arc #14 (Orbit 1446)
---------------------------------------
Vector Time (GMT): 2015/080/23:49:16
116
Vector Time (MET): N/A
Weight (LBS) : 890095
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6122549
42 A = 6786680
92 meter
Y = -2858546
02 meter E =
0019570
Z = 526959
80 I = 51
79311
XDOT = 2447
922053 Wp = 127
93550
YDOT = 4111
290227 meter/sec RA = 158
49201 deg
ZDOT = -5999
731057 TA = 46
38593
MA = 46
22373
Ha = 221
856 n
mi
Hp = 211
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20087104
40 X = 6151499
54
Y = -9378431
84 feet Y = -2789917
73 meter
Z = 1728870
75 Z = 556772
80
XDOT = 8031
240331 XDOT = 2430
911233
YDOT = 13488
484996 feet/sec YDOT = 4138
568446 meter/sec
ZDOT = -19684
157012 ZDOT = -5987
881450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20728467
65 X = -6318036
94
Y = 7830564
47 feet Y = 2386756
05 meter
Z = 1857048
73 Z = 566028
45
XDOT = -6539
829927 XDOT = -1993
340162
YDOT = -12554
290287 feet/sec YDOT = -3826
547680 meter/sec
ZDOT = -19634
008792 ZDOT = -5984
445880
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 15081
02583152
00016717 00000-0 10270-3 0 9132
2 25544 51
6458 159
4348 0006524 124
7864 235
3904 15
54995010 14475
Satellite: ISS
Catalog Number: 25544
Epoch time: 15081
02583152 = yrday
fracday
Element set: 913
Inclination: 51
6458 deg
RA of node: 159
4348 deg
Eccentricity:
0006524
Arg of perigee: 124
7864 deg
Mean anomaly: 235
3904 deg
Mean motion: 15
54995010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1447
Checksum: 311
Coasting Arc #15 (Orbit 1462)
---------------------------------------
Vector Time (GMT): 2015/081/23:49:16
116
Vector Time (MET): N/A
Weight (LBS) : 890095
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6349299
21 A = 6785808
41 meter
Y = 1883476
57 meter E =
0017456
Z = 1455058
09 I = 51
81946
XDOT = -147
486157 Wp = 80
53809
YDOT = -5019
520112 meter/sec RA = 153
52844 deg
ZDOT = 5797
500435 TA = 295
30409
MA = 295
48483
Ha = 221
701 n
mi
Hp = 211
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20831034
16 X = -6376956
96
Y = 6179385
08 feet Y = 1812320
12 meter
Z = 4773812
62 Z = 1424146
84
XDOT = -483
878469 XDOT = -119
507961
YDOT = -16468
241836 feet/sec YDOT = -5021
012175 meter/sec
ZDOT = 19020
670719 ZDOT = 5796
852612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21187118
63 X = 6457833
76
Y = -4946979
91 feet Y = -1507839
48 meter
Z = 4641062
97 Z = 1414595
99
XDOT = -722
022231 XDOT = -220
072376
YDOT = 14928
714509 feet/sec YDOT = 4550
272182 meter/sec
ZDOT = 19018
664694 ZDOT = 5796
888999
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 15082
05405894
00016717 00000-0 10270-3 0 9143
2 25544 51
6456 154
3019 0006351 126
7062 233
4676 15
55049363 14637
Satellite: ISS
Catalog Number: 25544
Epoch time: 15082
05405894 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 154
3019 deg
Eccentricity:
0006351
Arg of perigee: 126
7062 deg
Mean anomaly: 233
4676 deg
Mean motion: 15
55049363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1463
Checksum: 304
Coasting Arc #16 (Orbit 1477)
---------------------------------------
Vector Time (GMT): 2015/082/23:49:16
116
Vector Time (MET): N/A
Weight (LBS) : 890095
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5902448
54 A = 6782062
08 meter
Y = -575139
95 meter E =
0010398
Z = -3293065
18 I = 51
83523
XDOT = -2087
665575 Wp = 117
47147
YDOT = 5646
610363 meter/sec RA = 148
55933 deg
ZDOT = -4744
232827 TA = 100
65871
MA = 100
54160
Ha = 221
599 n
mi
Hp = 211
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19364988
65 X = 5924437
76
Y = -1886942
08 feet Y = -509012
34 meter
Z = -10804019
60 Z = -3264338
61
XDOT = -6849
296507 XDOT = -2127
606329
YDOT = 18525
624552 feet/sec YDOT = 5623
040854 meter/sec
ZDOT = -15565
068330 ZDOT = -4754
472014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19494626
10 X = -5941962
03
Y = 1081585
19 feet Y = 329667
16 meter
Z = -10680819
37 Z = -3255513
74
XDOT = 7590
565818 XDOT = 2313
604461
YDOT = -16807
274499 feet/sec YDOT = -5122
857267 meter/sec
ZDOT = -15609
824448 ZDOT = -4757
874492
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 15083
01799851
00016717 00000-0 10270-3 0 9150
2 25544 51
6457 149
4895 0006243 131
5692 228
5997 15
55080501 14784
Satellite: ISS
Catalog Number: 25544
Epoch time: 15083
01799851 = yrday
fracday
Element set: 915
Inclination: 51
6457 deg
RA of node: 149
4895 deg
Eccentricity:
0006243
Arg of perigee: 131
5692 deg
Mean anomaly: 228
5997 deg
Mean motion: 15
55080501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1478
Checksum: 338
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