[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 3rd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18029 55 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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 1642)
---------------------------------------
Vector Time (GMT): 2015/093/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3587332
78 A = 6779102
72 meter
Y = -4103179
37 meter E =
0007971
Z = -4034630
60 I = 51
99988
XDOT = 2493
845709 Wp = 117
32524
YDOT = 6068
812524 meter/sec RA = 95
82711 deg
ZDOT = -3964
100608 TA = 111
70399
MA = 111
61911
Ha = 220
312 n
mi
Hp = 212
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11769464
50 X = 3652547
73
Y = -13461874
56 feet Y = -4062699
42 meter
Z = -13236977
04 Z = -4017044
93
XDOT = 8181
908493 XDOT = 2445
053691
YDOT = 19910
802245 feet/sec YDOT = 6096
426940 meter/sec
ZDOT = -13005
579424 ZDOT = -3952
105328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1214384
63 X = -370144
43
Y = -17896282
11 feet Y = -5454786
79 meter
Z = -13160861
65 Z = -4011430
63
XDOT = 18651
762104 XDOT = 5685
057089
YDOT = 8238
368924 feet/sec YDOT = 2511
054848 meter/sec
ZDOT = -12955
162628 ZDOT = -3948
733569
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 15093
61921248
00016717 00000-0 10270-3 0 9008
2 25544 51
6415 96
5539 0005806 175
8870 184
2332 15
55296907 16432
Satellite: ISS
Catalog Number: 25544
Epoch time: 15093
61921248 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 96
5539 deg
Eccentricity:
0005806
Arg of perigee: 175
8870 deg
Mean anomaly: 184
2332 deg
Mean motion: 15
55296907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1643
Checksum: 324
Coasting Arc #2 (Orbit 1658)
---------------------------------------
Vector Time (GMT): 2015/094/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3990312
82 A = 6774964
55 meter
Y = 2074719
75 meter E =
0010056
Z = 5065518
47 I = 51
98919
XDOT = -1375
497246 Wp = 153
21990
YDOT = -7304
599973 meter/sec RA = 90
84838 deg
ZDOT = 1898
058171 TA = 278
42127
MA = 278
53524
Ha = 220
114 n
mi
Hp = 212
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13091577
49 X = -4037822
88
Y = 6806823
34 feet Y = 2029832
53 meter
Z = 16619155
07 Z = 5046018
43
XDOT = -4512
786241 XDOT = -1302
933389
YDOT = -23965
223009 feet/sec YDOT = -7319
575688 meter/sec
ZDOT = 6227
224972 ZDOT = 1891
553486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4212861
41 X = -1284080
16
Y = 14239331
59 feet Y = 4340148
27 meter
Z = 16535168
43 Z = 5039919
34
XDOT = -19415
930007 XDOT = -5917
975466
YDOT = -12983
797082 feet/sec YDOT = -3957
461351 meter/sec
ZDOT = 6200
580238 ZDOT = 1889
936856
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 15094
64725618
00016717 00000-0 10270-3 0 9016
2 25544 51
6418 91
4203 0005802 181
4944 178
6193 15
55356365 16592
Satellite: ISS
Catalog Number: 25544
Epoch time: 15094
64725618 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 91
4203 deg
Eccentricity:
0005802
Arg of perigee: 181
4944 deg
Mean anomaly: 178
6193 deg
Mean motion: 15
55356365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1659
Checksum: 322
Coasting Arc #3 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2015/095/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4193315
13 A = 6773844
18 meter
Y = 261061
28 meter E =
0015807
Z = -5326248
21 I = 51
98538
XDOT = 163
278310 Wp = 115
20390
YDOT = 7641
707156 meter/sec RA = 85
85832 deg
ZDOT = 497
705384 TA = 159
55858
MA = 159
49524
Ha = 219
935 n
mi
Hp = 212
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13757595
56 X = 4215957
46
Y = 856500
26 feet Y = 308079
59 meter
Z = -17474567
63 Z = -5305822
69
XDOT = 535
689992 XDOT = 75
397095
YDOT = 25071
217704 feet/sec YDOT = 7643
041732 meter/sec
ZDOT = 1632
891680 ZDOT = 498
284138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10047464
09 X = 3062467
05
Y = -9597176
64 feet Y = -2925219
44 meter
Z = -17387012
63 Z = -5299561
45
XDOT = 18056
968109 XDOT = 5503
763880
YDOT = 15911
587745 feet/sec YDOT = 4849
851945 meter/sec
ZDOT = 1634
046423 ZDOT = 498
057350
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 15095
61102470
00016717 00000-0 10270-3 0 9020
2 25544 51
6422 86
6058 0005756 184
2895 175
8210 15
55364387 16744
Satellite: ISS
Catalog Number: 25544
Epoch time: 15095
61102470 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 86
6058 deg
Eccentricity:
0005756
Arg of perigee: 184
2895 deg
Mean anomaly: 175
8210 deg
Mean motion: 15
55364387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1674
Checksum: 318
Coasting Arc #4 (Orbit 1689)
---------------------------------------
Vector Time (GMT): 2015/096/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4143006
54 A = 6776224
00 meter
Y = -2532735
94 meter E =
0006652
Z = 4719923
45 I = 51
99135
XDOT = 1098
436761 Wp = 108
57636
YDOT = -7053
042171 meter/sec RA = 80
87217 deg
ZDOT = -2819
352312 TA = 9
22015
MA = 9
20794
Ha = 219
876 n
mi
Hp = 212
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13592541
13 X = -4137304
91
Y = -8309501
11 feet Y = -2579033
34 meter
Z = 15485313
16 Z = 4699811
38
XDOT = 3603
795147 XDOT = 1190
919464
YDOT = -23139
902137 feet/sec YDOT = -7040
241946 meter/sec
ZDOT = -9249
843543 ZDOT = -2813
790828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15318661
38 X = -4669127
99
Y = 4668386
80 feet Y = 1422924
30 meter
Z = 15399502
75 Z = 4693768
44
XDOT = -14469
415960 XDOT = -4410
277985
YDOT = -17037
136510 feet/sec YDOT = -5192
919208 meter/sec
ZDOT = -9224
749512 ZDOT = -2811
703651
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 15096
63901819
00016717 00000-0 10270-3 0 9038
2 25544 51
6429 81
4718 0005749 188
1841 171
9220 15
55412112 16909
Satellite: ISS
Catalog Number: 25544
Epoch time: 15096
63901819 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 81
4718 deg
Eccentricity:
0005749
Arg of perigee: 188
1841 deg
Mean anomaly: 171
9220 deg
Mean motion: 15
55412112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1690
Checksum: 311
Coasting Arc #5 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2015/097/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3833186
09 A = 6780793
76 meter
Y = 4476325
88 meter E =
0006347
Z = -3362511
22 I = 52
00112
XDOT = -2382
748040 Wp = 146
37050
YDOT = 5567
352861 meter/sec RA = 75
89757 deg
ZDOT = 4694
318147 TA = 174
66171
MA = 174
65494
Ha = 219
555 n
mi
Hp = 212
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12576069
85 X = 3799179
91
Y = 14686108
54 feet Y = 4519000
62 meter
Z = -11031860
94 Z = -3343973
10
XDOT = -7817
414829 XDOT = -2467
629977
YDOT = 18265
593375 feet/sec YDOT = 5540
233253 meter/sec
ZDOT = 15401
306256 ZDOT = 4682
536359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19379601
36 X = 5906902
49
Y = 27516
36 feet Y = 8386
99 meter
Z = -10953153
29 Z = -3338521
12
XDOT = 8653
795530 XDOT = 2637
676878
YDOT = 16516
536556 feet/sec YDOT = 5034
240342 meter/sec
ZDOT = 15349
782393 ZDOT = 4678
613673
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 15097
60273725
00016717 00000-0 10270-3 0 9045
2 25544 51
6431 76
6579 0005705 192
3564 167
7451 15
55438986 17057
Satellite: ISS
Catalog Number: 25544
Epoch time: 15097
60273725 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 76
6579 deg
Eccentricity:
0005705
Arg of perigee: 192
3564 deg
Mean anomaly: 167
7451 deg
Mean motion: 15
55438986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 336
Coasting Arc #6 (Orbit 1720)
---------------------------------------
Vector Time (GMT): 2015/098/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3185200
38 A = 6784554
01 meter
Y = -5806420
22 meter E =
0016241
Z = 1426507
39 I = 52
00669
XDOT = 3631
443106 Wp = 139
30198
YDOT = -3430
183678 meter/sec RA = 70
93821 deg
ZDOT = -5828
433803 TA = 25
20091
MA = 25
12175
Ha = 219
462 n
mi
Hp = 212
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10450132
49 X = -3126964
41
Y = -19049935
10 feet Y = -5841713
48 meter
Z = 4680142
37 Z = 1411176
01
XDOT = 11914
183420 XDOT = 3697
843063
YDOT = -11253
883459 feet/sec YDOT = -3389
203702 meter/sec
ZDOT = -19122
158147 ZDOT = -5810
631175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21341480
35 X = -6504883
21
Y = -4153068
46 feet Y = -1265855
27 meter
Z = 4615438
00 Z = 1406785
50
XDOT = -1238
259491 XDOT = -377
421493
YDOT = -14895
518786 feet/sec YDOT = -4540
154126 meter/sec
ZDOT = -19045
184484 ZDOT = -5804
972231
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 15098
63067870
00016717 00000-0 10270-3 0 9052
2 25544 51
6443 71
5232 0005753 195
4144 164
6835 15
55484768 17210
Satellite: ISS
Catalog Number: 25544
Epoch time: 15098
63067870 = yrday
fracday
Element set: 905
Inclination: 51
6443 deg
RA of node: 71
5232 deg
Eccentricity:
0005753
Arg of perigee: 195
4144 deg
Mean anomaly: 164
6835 deg
Mean motion: 15
55484768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1721
Checksum: 326
Coasting Arc #7 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2015/099/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2210899
67 A = 6785011
63 meter
Y = 6369938
88 meter E =
0009052
Z = 733012
33 I = 51
99738
XDOT = -4701
574746 Wp = 73
18740
YDOT = 936
509751 meter/sec RA = 65
98622 deg
ZDOT = 5984
137922 TA = 294
69580
MA = 294
79001
Ha = 219
202 n
mi
Hp = 212
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7253607
84 X = 2135944
44
Y = 20898749
60 feet Y = 6394243
55 meter
Z = 2404896
08 Z = 743570
08
XDOT = -15425
113997 XDOT = -4740
766609
YDOT = 3072
538554 feet/sec YDOT = 883
714936 meter/sec
ZDOT = 19632
998431 ZDOT = 5961
203079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20817265
10 X = 6345102
40
Y = 7469933
09 feet Y = 2276835
61 meter
Z = 2449012
07 Z = 746458
88
XDOT = -6813
178305 XDOT = -2076
656747
YDOT = 12521
051345 feet/sec YDOT = 3816
416450 meter/sec
ZDOT = 19534
460767 ZDOT = 5954
103642
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 15099
65859187
00016717 00000-0 10270-3 0 9066
2 25544 51
6441 66
3884 0005748 199
9817 160
1112 15
55533135 17372
Satellite: ISS
Catalog Number: 25544
Epoch time: 15099
65859187 = yrday
fracday
Element set: 906
Inclination: 51
6441 deg
RA of node: 66
3884 deg
Eccentricity:
0005748
Arg of perigee: 199
9817 deg
Mean anomaly: 160
1112 deg
Mean motion: 15
55533135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1737
Checksum: 342
Coasting Arc #8 (Orbit 1751)
---------------------------------------
Vector Time (GMT): 2015/100/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -870518
02 A = 6781740
60 meter
Y = -6106976
20 meter E =
0007771
Z = -2808736
92 I = 51
97425
XDOT = 5469
712890 Wp = 166
15279
YDOT = 1579
877060 meter/sec RA = 61
02872 deg
ZDOT = -5140
603002 TA = 45
58614
MA = 45
52255
Ha = 219
023 n
mi
Hp = 212
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2856030
24 X = -788519
76
Y = -20036011
16 feet Y = -6116252
59 meter
Z = -9215016
14 Z = -2812766
22
XDOT = 17945
252265 XDOT = 5476
611128
YDOT = 5183
323687 feet/sec YDOT = 1641
081220 meter/sec
ZDOT = -16865
495413 ZDOT = -5114
015334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17536745
98 X = -5345200
17
Y = -10087776
48 feet Y = -3074754
27 meter
Z = -9231168
97 Z = -2813660
30
XDOT = 14434
045286 XDOT = 4399
497003
YDOT = -9793
875234 feet/sec YDOT = -2985
173171 meter/sec
ZDOT = -16751
752680 ZDOT = -5105
934217
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 15100
62223536
00016717 00000-0 10270-3 0 9070
2 25544 51
6451 61
5743 0005727 203
4388 156
6505 15
55582023 17528
Satellite: ISS
Catalog Number: 25544
Epoch time: 15100
62223536 = yrday
fracday
Element set: 907
Inclination: 51
6451 deg
RA of node: 61
5743 deg
Eccentricity:
0005727
Arg of perigee: 203
4388 deg
Mean anomaly: 156
6505 deg
Mean motion: 15
55582023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1752
Checksum: 292
Coasting Arc #9 (Orbit 1767)
---------------------------------------
Vector Time (GMT): 2015/101/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -703150
33 A = 6776819
88 meter
Y = 5112775
64 meter E =
0010435
Z = 4391552
17 I = 51
94172
XDOT = -5751
791740 Wp = 142
66324
YDOT = -3743
279497 meter/sec RA = 56
05525 deg
ZDOT = 3424
757656 TA = 272
72830
MA = 272
84774
Ha = 218
859 n
mi
Hp = 213
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2306923
65 X = -781602
96
Y = 16774198
30 feet Y = 5104474
17 meter
Z = 14407979
55 Z = 4387945
51
XDOT = -18870
707807 XDOT = -5726
142282
YDOT = -12281
100712 feet/sec YDOT = -3807
456163 meter/sec
ZDOT = 11236
081550 ZDOT = 3396
878971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11981043
38 X = 3651822
02
Y = 11984288
57 feet Y = 3652811
16 meter
Z = 14391557
48 Z = 4386546
72
XDOT = -20315
389339 XDOT = -6192
130671
YDOT = 6910
927290 feet/sec YDOT = 2106
450638 meter/sec
ZDOT = 11117
206104 ZDOT = 3388
524420
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 15101
65009472
00016717 00000-0 10270-3 0 9086
2 25544 51
6448 56
4392 0005807 207
0382 153
0469 15
55621541 17686
Satellite: ISS
Catalog Number: 25544
Epoch time: 15101
65009472 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 56
4392 deg
Eccentricity:
0005807
Arg of perigee: 207
0382 deg
Mean anomaly: 153
0469 deg
Mean motion: 15
55621541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 306
Coasting Arc #10 (Orbit 1782)
---------------------------------------
Vector Time (GMT): 2015/102/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2425682
98 A = 6773231
13 meter
Y = -3542441
35 meter E =
0011607
Z = -5247913
77 I = 51
91231
XDOT = 5404
893121 Wp = 104
25734
YDOT = 5320
439214 meter/sec RA = 51
06390 deg
ZDOT = -1097
966083 TA = 155
28197
MA = 155
22631
Ha = 218
674 n
mi
Hp = 213
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7958277
51 X = 2490607
59
Y = -11622182
90 feet Y = -3514953
13 meter
Z = -17217564
87 Z = -5235972
30
XDOT = 17732
588979 XDOT = 5350
330523
YDOT = 17455
509232 feet/sec YDOT = 5380
575106 meter/sec
ZDOT = -3602
250929 ZDOT = -1071
842998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4688465
24 X = -1429044
20
Y = -13349587
41 feet Y = -4068954
24 meter
Z = -17165682
80 Z = -5232100
12
XDOT = 23576
051017 XDOT = 7185
980350
YDOT = -3811
226150 feet/sec YDOT = -1161
661731 meter/sec
ZDOT = -3491
205784 ZDOT = -1064
119523
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 15102
61368753
00016717 00000-0 10270-3 0 9094
2 25544 51
6454 51
6244 0005750 210
6946 149
3882 15
55673050 17835
Satellite: ISS
Catalog Number: 25544
Epoch time: 15102
61368753 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 51
6244 deg
Eccentricity:
0005750
Arg of perigee: 210
6946 deg
Mean anomaly: 149
3882 deg
Mean motion: 15
55673050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1783
Checksum: 313
Coasting Arc #11 (Orbit 1798)
---------------------------------------
Vector Time (GMT): 2015/103/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4029335
01 A = 6773370
13 meter
Y = 1673650
51 meter E =
0002117
Z = 5180194
72 I = 51
89238
XDOT = -4372
613313 Wp = 170
94635
YDOT = -6142
094951 meter/sec RA = 46
06573 deg
ZDOT = -1418
702501 TA = 292
63497
MA = 292
65736
Ha = 218
484 n
mi
Hp = 213
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13219603
04 X = -4072914
18
Y = 5490979
37 feet Y = 1628348
62 meter
Z = 16995389
49 Z = 5160514
97
XDOT = -14345
844203 XDOT = -4296
714428
YDOT = -20151
230154 feet/sec YDOT = -6190
568113 meter/sec
ZDOT = -4654
535765 ZDOT = -1439
758981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3120521
97 X = -951135
10
Y = 14072799
18 feet Y = 4289389
19 meter
Z = 16910667
90 Z = 5154371
58
XDOT = -23692
062420 XDOT = -7221
340626
YDOT = 439
007900 feet/sec YDOT = 133
809608 meter/sec
ZDOT = -4743
688628 ZDOT = -1445
876294
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 15103
64149106
00016717 00000-0 10270-3 0 9109
2 25544 51
6452 46
4890 0005829 216
0593 144
0168 15
55732010 17995
Satellite: ISS
Catalog Number: 25544
Epoch time: 15103
64149106 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 46
4890 deg
Eccentricity:
0005829
Arg of perigee: 216
0593 deg
Mean anomaly: 144
0168 deg
Mean motion: 15
55732010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1799
Checksum: 298
Coasting Arc #12 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2015/104/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5312165
53 A = 6777232
28 meter
Y = 249139
95 meter E =
0008027
Z = -4209139
25 I = 51
88351
XDOT = 2649
151743 Wp = 152
35642
YDOT = 6163
636436 meter/sec RA = 41
07250 deg
ZDOT = 3704
099672 TA = 155
56737
MA = 155
52930
Ha = 218
236 n
mi
Hp = 213
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17428364
61 X = 5329431
26
Y = 817388
28 feet Y = 308640
18 meter
Z = -13809511
99 Z = -4183291
80
XDOT = 8691
442726 XDOT = 2562
038426
YDOT = 20221
904317 feet/sec YDOT = 6192
774265 meter/sec
ZDOT = 12152
557978 ZDOT = 3716
756577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10450333
08 X = 3185261
52
Y = -14080294
47 feet Y = -4291673
75 meter
Z = -13698703
73 Z = -4175364
90
XDOT = 20562
009477 XDOT = 6267
300489
YDOT = 3372
944094 feet/sec YDOT = 1028
073360 meter/sec
ZDOT = 12205
674344 ZDOT = 3720
289540
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 15104
60503285
00016717 00000-0 10270-3 0 9119
2 25544 51
6460 41
6735 0005813 219
1064 140
9671 15
55747167 18140
Satellite: ISS
Catalog Number: 25544
Epoch time: 15104
60503285 = yrday
fracday
Element set: 911
Inclination: 51
6460 deg
RA of node: 41
6735 deg
Eccentricity:
0005813
Arg of perigee: 219
1064 deg
Mean anomaly: 140
9671 deg
Mean motion: 15
55747167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 293
Coasting Arc #13 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2015/105/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5992417
49 A = 6782070
01 meter
Y = -1969935
15 meter E =
0012354
Z = 2470093
07 I = 51
87537
XDOT = -404
147095 Wp = 130
47887
YDOT = -5489
544155 meter/sec RA = 36
09516 deg
ZDOT = -5348
756104 TA = 21
90746
MA = 21
85468
Ha = 218
221 n
mi
Hp = 213
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19660162
38 X = -5981942
69
Y = -6463041
83 feet Y = -2036887
44 meter
Z = 8103979
88 Z = 2441008
57
XDOT = -1325
941914 XDOT = -316
749272
YDOT = -18010
315469 feet/sec YDOT = -5493
575508 meter/sec
ZDOT = -17548
412416 ZDOT = -5350
506500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16139157
56 X = -4919215
22
Y = 13031523
49 feet Y = 3972008
36 meter
Z = 7979622
37 Z = 2432188
90
XDOT = -14828
101880 XDOT = -4519
605453
YDOT = -7594
977092 feet/sec YDOT = -2314
949018 meter/sec
ZDOT = -17554
875289 ZDOT = -5350
725988
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 15105
63278338
00016717 00000-0 10270-3 0 9122
2 25544 51
6460 36
5376 0005871 221
9019 138
1685 15
55762685 18303
Satellite: ISS
Catalog Number: 25544
Epoch time: 15105
63278338 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 36
5376 deg
Eccentricity:
0005871
Arg of perigee: 221
9019 deg
Mean anomaly: 138
1685 deg
Mean motion: 15
55762685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 319
Coasting Arc #14 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2015/106/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5913347
65 A = 6784340
40 meter
Y = 3307210
81 meter E =
0005716
Z = -287891
83 I = 51
85844
XDOT = -2093
064989 Wp = 38
97027
YDOT = 4260
660471 meter/sec RA = 31
12951 deg
ZDOT = 6022
358071 TA = 317
93553
MA = 317
97940
Ha = 217
800 n
mi
Hp = 213
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19400746
89 X = 5877324
63
Y = 10850429
16 feet Y = 3373136
28 meter
Z = -944527
00 Z = -259253
54
XDOT = -6867
011119 XDOT = -2169
807790
YDOT = 13978
544854 feet/sec YDOT = 4236
826041 meter/sec
ZDOT = 19758
392622 ZDOT = 6012
003384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19474864
46 X = 5935938
69
Y = -10726897
08 feet Y = -3269558
23 meter
Z = -822348
69 Z = -250651
88
XDOT = 7381
545237 XDOT = 2249
894988
YDOT = 11910
038715 feet/sec YDOT = 3630
179800 meter/sec
ZDOT = 19713
173923 ZDOT = 6008
575412
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 15106
59627178
00016717 00000-0 10270-3 0 9139
2 25544 51
6468 31
7221 0005921 227
3189 132
7466 15
55835534 18458
Satellite: ISS
Catalog Number: 25544
Epoch time: 15106
59627178 = yrday
fracday
Element set: 913
Inclination: 51
6468 deg
RA of node: 31
7221 deg
Eccentricity:
0005921
Arg of perigee: 227
3189 deg
Mean anomaly: 132
7466 deg
Mean motion: 15
55835534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1845
Checksum: 321
Coasting Arc #15 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2015/107/14:17:55
946
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4964791
55 A = 6782656
97 meter
Y = -4168753
83 meter E =
0009008
Z = -1974501
98 I = 51
82570
XDOT = 4492
630616 Wp = 182
27832
YDOT = -2700
550861 meter/sec RA = 26
16467 deg
ZDOT = -5602
752240 TA = 19
47560
MA = 19
44120
Ha = 217
640 n
mi
Hp = 213
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16288686
18 X = -4908215
03
Y = -13677013
87 feet Y = -4223957
25 meter
Z = -6478024
88 Z = -1998482
44
XDOT = 14739
601758 XDOT = 4549
711371
YDOT = -8860
075004 feet/sec YDOT = -2649
992777 meter/sec
ZDOT = -18381
733070 ZDOT = -5580
788670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20086883
71 X = -6122482
15
Y = 6896871
24 feet Y = 2102166
35 meter
Z = -6580051
82 Z = -2005599
80
XDOT = 545
655697 XDOT = 166
315856
YDOT = -15833
434487 feet/sec YDOT = -4826
030832 meter/sec
ZDOT = -18287
033299 ZDOT = -5573
887750
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 15107
62396682
00016717 00000-0 10270-3 0 9148
2 25544 51
6472 26
5861 0006125 231
0538 129
0070 15
55836970 18615
Satellite: ISS
Catalog Number: 25544
Epoch time: 15107
62396682 = yrday
fracday
Element set: 914
Inclination: 51
6472 deg
RA of node: 26
5861 deg
Eccentricity:
0006125
Arg of perigee: 231
0538 deg
Mean anomaly: 129
0070 deg
Mean motion: 15
55836970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 307
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