[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 9th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
105/14:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 218
1
000/00:00:00
000 0
0 0
0 213
5
111/11:13:10
491 0
8 1
0 1
0
N/A 0
4 -0
0 216
9
000/00:02:20
983 0
3 -0
0 214
6
Coasting Arc #1 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2015/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2965320
91 A = 6784871
92 meter
Y = 5991716
81 meter E =
0004830
Z = -1154375
99 I = 52
00679
XDOT = -3841
430963 Wp = 67
05609
YDOT = 3033
553790 meter/sec RA = 71
42036 deg
ZDOT = 5899
130758 TA = 280
47503
MA = 280
52945
Ha = 219
458 n
mi
Hp = 212
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9728743
14 X = 2903707
32
Y = 19657863
56 feet Y = 6024532
37 meter
Z = -3787322
80 Z = -1140120
98
XDOT = -12603
119957 XDOT = -3903
723532
YDOT = 9952
604298 feet/sec YDOT = 2990
248571 meter/sec
ZDOT = 19354
103537 ZDOT = 5880
318036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14677917
12 X = 4473829
14
Y = 16312267
95 feet Y = 4971979
27 meter
Z = -3727267
13 Z = -1136071
02
XDOT = -8391
811102 XDOT = -2557
824024
YDOT = 11938
476427 feet/sec YDOT = 3638
847615 meter/sec
ZDOT = 19272
870210 ZDOT = 5874
370840
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
50220647
00016717 00000-0 10270-3 0 9006
2 25544 51
6424 72
1687 0005658 193
6048 166
4954 15
55472040 17196
Satellite: ISS
Catalog Number: 25544
Epoch time: 15098
50220647 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 72
1687 deg
Eccentricity:
0005658
Arg of perigee: 193
6048 deg
Mean anomaly: 166
4954 deg
Mean motion: 15
55472040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1719
Checksum: 316
Coasting Arc #2 (Orbit 1734)
---------------------------------------
Vector Time (GMT): 2015/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1920520
62 A = 6784911
01 meter
Y = -6417680
78 meter E =
0013446
Z = -1025744
18 I = 51
99722
XDOT = 4838
199242 Wp = 161
68584
YDOT = -504
611417 meter/sec RA = 66
46840 deg
ZDOT = -5934
910329 TA = 29
38852
MA = 29
31297
Ha = 219
245 n
mi
Hp = 212
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6300920
66 X = -1843631
11
Y = -21055383
15 feet Y = -6438727
45 meter
Z = -3365302
42 Z = -1034886
61
XDOT = 15873
357093 XDOT = 4872
312236
YDOT = -1655
549270 feet/sec YDOT = -450
317177 meter/sec
ZDOT = -19471
490580 ZDOT = -5911
324142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12026562
90 X = -3665696
37
Y = -18388449
59 feet Y = -5604799
44 meter
Z = -3403340
63 Z = -1037338
22
XDOT = 13517
700347 XDOT = 4120
195066
YDOT = -5275
967825 feet/sec YDOT = -1608
114993 meter/sec
ZDOT = -19370
238623 ZDOT = -5904
048732
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
53014639
00016717 00000-0 10270-3 0 9013
2 25544 51
6435 67
0335 0005530 199
2600 160
8345 15
55492632 17355
Satellite: ISS
Catalog Number: 25544
Epoch time: 15099
53014639 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 67
0335 deg
Eccentricity:
0005530
Arg of perigee: 199
2600 deg
Mean anomaly: 160
8345 deg
Mean motion: 15
55492632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1735
Checksum: 302
Coasting Arc #3 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2015/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 594740
62 A = 6781318
86 meter
Y = 6041849
59 meter E =
0011425
Z = 3016717
63 I = 51
97259
XDOT = -5493
589286 Wp = 108
98183
YDOT = -1955
746967 meter/sec RA = 61
51034 deg
ZDOT = 4981
024497 TA = 285
41457
MA = 285
54075
Ha = 219
054 n
mi
Hp = 213
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1951248
77 X = 512480
82
Y = 19822341
17 feet Y = 6048040
61 meter
Z = 9897367
54 Z = 3019406
61
XDOT = -18023
586895 XDOT = -5495
507511
YDOT = -6416
492674 feet/sec YDOT = -2017
190292 meter/sec
ZDOT = 16341
943887 ZDOT = 4954
332952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7782847
26 X = 2372211
84
Y = 18329035
84 feet Y = 5586690
12 meter
Z = 9907784
78 Z = 3019892
80
XDOT = -17881
161402 XDOT = -5450
177995
YDOT = -1212
918825 feet/sec YDOT = -369
697658 meter/sec
ZDOT = 16227
824936 ZDOT = 4946
241040
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
55806366
00016717 00000-0 10270-3 0 9025
2 25544 51
6437 61
8993 0005723 203
3672 156
7222 15
55554083 17514
Satellite: ISS
Catalog Number: 25544
Epoch time: 15100
55806366 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 61
8993 deg
Eccentricity:
0005723
Arg of perigee: 203
3672 deg
Mean anomaly: 156
7222 deg
Mean motion: 15
55554083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 303
Coasting Arc #4 (Orbit 1765)
---------------------------------------
Vector Time (GMT): 2015/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 993560
80 A = 6776462
68 meter
Y = -4938899
51 meter E =
0006813
Z = -4537091
97 I = 51
94081
XDOT = 5670
524801 Wp = 102
66559
YDOT = 4059
508945 meter/sec RA = 56
53464 deg
ZDOT = -3182
723490 TA = 135
53828
MA = 135
48357
Ha = 218
918 n
mi
Hp = 213
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3259713
91 X = 1070754
51
Y = -16203738
54 feet Y = -4927357
52 meter
Z = -14885472
36 Z = -4532077
62
XDOT = 18604
083994 XDOT = 5640
169518
YDOT = 13318
598901 feet/sec YDOT = 4122
750536 meter/sec
ZDOT = -10442
006200 ZDOT = -3155
251026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1975754
65 X = -602210
02
Y = -16430168
31 feet Y = -5007915
30 meter
Z = -14863045
70 Z = -4530256
33
XDOT = 20738
771899 XDOT = 6321
177675
YDOT = 6830
003828 feet/sec YDOT = 2081
785167 meter/sec
ZDOT = -10324
931531 ZDOT = -3147
039131
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
52171887
00016717 00000-0 10270-3 0 9037
2 25544 51
6440 57
0847 0005532 207
2180 152
8684 15
55558346 17669
Satellite: ISS
Catalog Number: 25544
Epoch time: 15101
52171887 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 57
0847 deg
Eccentricity:
0005532
Arg of perigee: 207
2180 deg
Mean anomaly: 152
8684 deg
Mean motion: 15
55558346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1766
Checksum: 310
Coasting Arc #5 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2015/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2638476
08 A = 6773271
18 meter
Y = 3328107
51 meter E =
0006364
Z = 5277173
80 I = 51
91271
XDOT = -5247
838647 Wp = 180
92466
YDOT = -5528
444863 meter/sec RA = 51
54431 deg
ZDOT = 856
578056 TA = 260
88259
MA = 260
95460
Ha = 218
714 n
mi
Hp = 213
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8656417
58 X = -2701130
27
Y = 10918987
91 feet Y = 3298252
39 meter
Z = 17313562
34 Z = 5264204
15
XDOT = -17217
318395 XDOT = -5189
789179
YDOT = -18137
942463 feet/sec YDOT = -5586
804991 meter/sec
ZDOT = 2810
295460 ZDOT = 831
226387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4609534
73 X = -1404986
18
Y = 13223264
11 feet Y = 4030450
90 meter
Z = 17257310
88 Z = 5260028
36
XDOT = -21343
694405 XDOT = -6505
558055
YDOT = -10993
920478 feet/sec YDOT = -3350
946962 meter/sec
ZDOT = 2702
597333 ZDOT = 823
751667
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
54959479
00016717 00000-0 10270-3 0 9042
2 25544 51
6444 51
9503 0005607 212
3242 147
7569 15
55607329 17823
Satellite: ISS
Catalog Number: 25544
Epoch time: 15102
54959479 = yrday
fracday
Element set: 904
Inclination: 51
6444 deg
RA of node: 51
9503 deg
Eccentricity:
0005607
Arg of perigee: 212
3242 deg
Mean anomaly: 147
7569 deg
Mean motion: 15
55607329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1782
Checksum: 319
Coasting Arc #6 (Orbit 1796)
---------------------------------------
Vector Time (GMT): 2015/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4191751
99 A = 6773950
57 meter
Y = -1431534
96 meter E =
0012368
Z = -5135407
95 I = 51
89451
XDOT = 4140
178690 Wp = 126
66429
YDOT = 6236
010081 meter/sec RA = 46
54582 deg
ZDOT = 1636
597425 TA = 159
11155
MA = 159
06098
Ha = 218
540 n
mi
Hp = 213
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13752467
15 X = 4232394
14
Y = -4696637
01 feet Y = -1384433
22 meter
Z = -16848451
28 Z = -5114946
37
XDOT = 13583
263417 XDOT = 4062
188445
YDOT = 20459
350658 feet/sec YDOT = 6281
872329 meter/sec
ZDOT = 5369
414125 ZDOT = 1656
519702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11332554
46 X = 3454162
60
Y = -9258538
08 feet Y = -2822002
41 meter
Z = -16760421
96 Z = -5108576
61
XDOT = 19186
493390 XDOT = 5848
043185
YDOT = 13585
188385 feet/sec YDOT = 4140
765420 meter/sec
ZDOT = 5453
685417 ZDOT = 1662
283315
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
51320980
00016717 00000-0 10270-3 0 9050
2 25544 51
6444 47
1351 0005563 215
7731 144
3050 15
55614016 17977
Satellite: ISS
Catalog Number: 25544
Epoch time: 15103
51320980 = yrday
fracday
Element set: 905
Inclination: 51
6444 deg
RA of node: 47
1351 deg
Eccentricity:
0005563
Arg of perigee: 215
7731 deg
Mean anomaly: 144
3050 deg
Mean motion: 15
55614016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1797
Checksum: 281
Coasting Arc #7 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2015/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5372526
46 A = 6777875
83 meter
Y = -465793
53 meter E =
0007153
Z = 4098598
90 I = 51
88613
XDOT = -2409
863411 Wp = 105
85508
YDOT = -6180
408104 meter/sec RA = 41
55596 deg
ZDOT = -3857
613877 TA = 23
87388
MA = 23
84073
Ha = 218
472 n
mi
Hp = 213
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17626399
13 X = -5386828
05
Y = -1528194
01 feet Y = -525952
21 meter
Z = 13446846
77 Z = 4072465
45
XDOT = -7906
376020 XDOT = -2321
834620
YDOT = -20276
929476 feet/sec YDOT = -6206
864946 meter/sec
ZDOT = -12656
213506 ZDOT = -3869
106144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17037947
51 X = -5193166
40
Y = 5072777
01 feet Y = 1546182
43 meter
Z = 13334852
43 Z = 4064463
02
XDOT = -14345
525615 XDOT = -4372
516207
YDOT = -14754
454274 feet/sec YDOT = -4497
157663 meter/sec
ZDOT = -12704
332432 ZDOT = -3872
280525
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
54104421
00016717 00000-0 10270-3 0 9065
2 25544 51
6451 42
0001 0005575 219
5396 140
5351 15
55652416 18130
Satellite: ISS
Catalog Number: 25544
Epoch time: 15104
54104421 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 42
0001 deg
Eccentricity:
0005575
Arg of perigee: 219
5396 deg
Mean anomaly: 140
5351 deg
Mean motion: 15
55652416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1813
Checksum: 269
Coasting Arc #8 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2015/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5988676
19 A = 6782558
87 meter
Y = 2142008
84 meter E =
0000237
Z = -2356009
41 I = 51
87767
XDOT = 187
487966 Wp = 66
94962
YDOT = 5427
014824 meter/sec RA = 36
57999 deg
ZDOT = 5411
162531 TA = 266
84777
MA = 266
85048
Ha = 218
129 n
mi
Hp = 213
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19647887
77 X = 5975723
32
Y = 7027588
06 feet Y = 2208905
45 meter
Z = -7729689
68 Z = -2326949
13
XDOT = 615
118000 XDOT = 100
502323
YDOT = 17805
166747 feet/sec YDOT = 5428
625660 meter/sec
ZDOT = 17753
157910 ZDOT = 5411
861446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20886441
13 X = 6366187
26
Y = -1043084
74 feet Y = -317932
23 meter
Z = -7605467
86 Z = -2318146
60
XDOT = 7200
580193 XDOT = 2194
736843
YDOT = 14736
795023 feet/sec YDOT = 4491
775123 meter/sec
ZDOT = 17755
123758 ZDOT = 5411
761721
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
50461892
00016717 00000-0 10270-3 0 9071
2 25544 51
6451 37
1852 0005581 223
9516 136
1194 15
55672649 18281
Satellite: ISS
Catalog Number: 25544
Epoch time: 15105
50461892 = yrday
fracday
Element set: 907
Inclination: 51
6451 deg
RA of node: 37
1852 deg
Eccentricity:
0005581
Arg of perigee: 223
9516 deg
Mean anomaly: 136
1194 deg
Mean motion: 15
55672649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 316
Coasting Arc #9 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2015/105/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -150868
32 A = 6774937
45 meter
Y = -4779059
18 meter E =
0006995
Z = -4805627
56 I = 51
85204
XDOT = 6792
677463 Wp = 92
83737
YDOT = 2408
318155 meter/sec RA = 36
05995 deg
ZDOT = -2611
864387 TA = 151
50719
MA = 151
46893
Ha = 218
073 n
mi
Hp = 213
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -494974
80 X = -74072
46
Y = -15679328
01 feet Y = -4780317
42 meter
Z = -15766494
61 Z = -4806173
40
XDOT = 22285
687215 XDOT = 6777
929760
YDOT = 7901
306284 feet/sec YDOT = 2484
195570 meter/sec
ZDOT = -8569
108880 ZDOT = -2578
902784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14163197
70 X = -4316942
66
Y = -6741290
38 feet Y = -2054745
31 meter
Z = -15767926
75 Z = -4806064
07
XDOT = 16660
137178 XDOT = 5078
009812
YDOT = -15316
391327 feet/sec YDOT = -4668
436077 meter/sec
ZDOT = -8428
207443 ZDOT = -2568
917629
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
63309327
00016717 00000-0 10270-3 0 9080
2 25544 51
6472 36
5437 0005577 224
6587 135
4118 15
55707249 18303
Satellite: ISS
Catalog Number: 25544
Epoch time: 15105
63309327 = yrday
fracday
Element set: 908
Inclination: 51
6472 deg
RA of node: 36
5437 deg
Eccentricity:
0005577
Arg of perigee: 224
6587 deg
Mean anomaly: 135
4118 deg
Mean motion: 15
55707249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 317
Coasting Arc #10 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2015/106/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2005022
43 A = 6772664
90 meter
Y = 3678805
39 meter E =
0004412
Z = 5322839
99 I = 51
81882
XDOT = -6632
495956 Wp = 203
89352
YDOT = -3849
291767 meter/sec RA = 31
05876 deg
ZDOT = 158
145762 TA = 244
58062
MA = 244
62628
Ha = 217
920 n
mi
Hp = 213
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6578157
59 X = -2071867
31
Y = 12069571
49 feet Y = 3656010
77 meter
Z = 17463385
81 Z = 5312937
11
XDOT = -21760
157337 XDOT = -6589
727538
YDOT = -12628
909997 feet/sec YDOT = -3923
221523 meter/sec
ZDOT = 518
850925 ZDOT = 126
030395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7934957
42 X = 2418575
02
Y = 11291106
48 feet Y = 3441529
25 meter
Z = 17420215
91 Z = 5309681
81
XDOT = -20045
665954 XDOT = -6109
918983
YDOT = 13478
433755 feet/sec YDOT = 4108
226608 meter/sec
ZDOT = 381
865596 ZDOT = 116
392634
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
66088252
00016717 00000-0 10270-3 0 9096
2 25544 51
6476 31
4081 0005671 228
3429 131
7239 15
55739159 18462
Satellite: ISS
Catalog Number: 25544
Epoch time: 15106
66088252 = yrday
fracday
Element set: 909
Inclination: 51
6476 deg
RA of node: 31
4081 deg
Eccentricity:
0005671
Arg of perigee: 228
3429 deg
Mean anomaly: 131
7239 deg
Mean motion: 15
55739159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 322
Coasting Arc #11 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2015/107/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4066309
65 A = 6774468
37 meter
Y = -2312129
58 meter E =
0009786
Z = -4908755
21 I = 51
79736
XDOT = 5534
604804 Wp = 134
94318
YDOT = 4756
257048 meter/sec RA = 26
05415 deg
ZDOT = 2340
557849 TA = 157
94816
MA = 157
90603
Ha = 217
684 n
mi
Hp = 213
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13340910
93 X = 4115707
45
Y = -7585726
96 feet Y = -2266381
78 meter
Z = -16104839
92 Z = -4888881
36
XDOT = 18158
152244 XDOT = 5469
638146
YDOT = 15604
517873 feet/sec YDOT = 4817
785620 meter/sec
ZDOT = 7678
995566 ZDOT = 2367
285948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1215358
42 X = -370441
25
Y = -15388240
27 feet Y = -4690335
64 meter
Z = -16019175
77 Z = -4882644
77
XDOT = 20661
270025 XDOT = 6297
555104
YDOT = -9757
387546 feet/sec YDOT = -2974
051724 meter/sec
ZDOT = 7792
691190 ZDOT = 2375
212275
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
62441623
00016717 00000-0 10270-3 0 9100
2 25544 51
6476 26
5930 0005701 232
9703 127
0930 15
55763083 18616
Satellite: ISS
Catalog Number: 25544
Epoch time: 15107
62441623 = yrday
fracday
Element set: 910
Inclination: 51
6476 deg
RA of node: 26
5930 deg
Eccentricity:
0005701
Arg of perigee: 232
9703 deg
Mean anomaly: 127
0930 deg
Mean motion: 15
55763083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 290
Coasting Arc #12 (Orbit 1876)
---------------------------------------
Vector Time (GMT): 2015/108/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5669929
33 A = 6779020
47 meter
Y = 859489
69 meter E =
0007674
Z = 3606504
31 I = 51
78439
XDOT = -3599
745928 Wp = 107
91452
YDOT = -5125
855845 meter/sec RA = 21
06101 deg
ZDOT = -4432
296389 TA = 29
43077
MA = 29
38759
Ha = 217
523 n
mi
Hp = 213
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18602130
34 X = -5696638
30
Y = 2819848
05 feet Y = 795935
83 meter
Z = 11832363
23 Z = 3578895
46
XDOT = -11810
190052 XDOT = -3520
629030
YDOT = -16817
112351 feet/sec YDOT = -5165
668600 meter/sec
ZDOT = -14541
654820 ZDOT = -4449
590915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5000145
03 X = -1524044
21
Y = 18214846
87 feet Y = 5551885
33 meter
Z = 11713817
43 Z = 3570371
55
XDOT = -18798
014736 XDOT = -5729
634891
YDOT = 4250
012932 feet/sec YDOT = 1295
403942 meter/sec
ZDOT = -14614
815742 ZDOT = -4454
595838
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 15108
65216467
00016717 00000-0 10270-3 0 9111
2 25544 51
6478 21
4578 0005650 237
6902 122
3705 15
55811571 18777
Satellite: ISS
Catalog Number: 25544
Epoch time: 15108
65216467 = yrday
fracday
Element set: 911
Inclination: 51
6478 deg
RA of node: 21
4578 deg
Eccentricity:
0005650
Arg of perigee: 237
6902 deg
Mean anomaly: 122
3705 deg
Mean motion: 15
55811571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1877
Checksum: 312
Coasting Arc #13 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2015/109/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6554027
08 A = 6783332
55 meter
Y = 531145
42 meter E =
0003539
Z = -1656695
56 I = 51
76832
XDOT = 1041
700003 Wp = 356
01192
YDOT = 4994
207849 meter/sec RA = 16
08187 deg
ZDOT = 5724
933466 TA = 345
86711
MA = 345
87701
Ha = 217
227 n
mi
Hp = 213
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21502713
52 X = 6555648
33
Y = 1742603
08 feet Y = 604445
78 meter
Z = -5435352
88 Z = -1624852
86
XDOT = 3417
650927 XDOT = 957
966046
YDOT = 16385
196356 feet/sec YDOT = 5005
389045 meter/sec
ZDOT = 18782
590113 ZDOT = 5729
790197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10003138
08 X = 3048956
49
Y = -19152153
12 feet Y = -5837576
27 meter
Z = -5298931
45 Z = -1615114
30
XDOT = 14979
116609 XDOT = 4565
634743
YDOT = 2623
918260 feet/sec YDOT = 799
770286 meter/sec
ZDOT = 18802
438053 ZDOT = 5730
983119
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 15109
61566019
00016717 00000-0 10270-3 0 9120
2 25544 51
6472 16
6422 0005773 241
6600 118
3972 15
55810443 18926
Satellite: ISS
Catalog Number: 25544
Epoch time: 15109
61566019 = yrday
fracday
Element set: 912
Inclination: 51
6472 deg
RA of node: 16
6422 deg
Eccentricity:
0005773
Arg of perigee: 241
6600 deg
Mean anomaly: 118
3972 deg
Mean motion: 15
55810443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 300
Coasting Arc #14 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2015/110/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6512287
39 A = 6784270
94 meter
Y = -1772820
33 meter E =
0010850
Z = -614339
99 I = 51
74041
XDOT = 1776
662670 Wp = 170
99080
YDOT = -4460
994096 meter/sec RA = 11
11212 deg
ZDOT = -5984
944652 TA = 15
63844
MA = 15
60495
Ha = 217
124 n
mi
Hp = 214
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21365772
27 X = -6488994
99
Y = -5816339
65 feet Y = -1845514
77 meter
Z = -2015551
16 Z = -645919
34
XDOT = 5828
945769 XDOT = 1855
487677
YDOT = -14635
807401 feet/sec YDOT = -4440
685846 meter/sec
ZDOT = -19635
645184 ZDOT = -5976
122134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13381878
53 X = -4078796
58
Y = 17626365
36 feet Y = 5372516
16 meter
Z = -2150592
80 Z = -655500
69
XDOT = -10062
369236 XDOT = -3067
010143
YDOT = -10021
062067 feet/sec YDOT = -3054
419718 meter/sec
ZDOT = -19596
943171 ZDOT = -5973
148279
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 15110
64336924
00016717 00000-0 10270-3 0 9136
2 25544 51
6468 11
5066 0005913 243
8533 116
2013 15
55807807 19085
Satellite: ISS
Catalog Number: 25544
Epoch time: 15110
64336924 = yrday
fracday
Element set: 913
Inclination: 51
6468 deg
RA of node: 11
5066 deg
Eccentricity:
0005913
Arg of perigee: 243
8533 deg
Mean anomaly: 116
2013 deg
Mean motion: 15
55807807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 295
Coasting Arc #15 (Orbit 1920)
---------------------------------------
Vector Time (GMT): 2015/111/11:14:20
983
Vector Time (MET): N/A
Weight (LBS) : 927275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4100163
21 A = 6776473
51 meter
Y = -3053895
86 meter E =
0005688
Z = -4452952
92 I = 51
68645
XDOT = 6064
506367 Wp = 151
90186
YDOT = 3341
459094 meter/sec RA = 6
80851 deg
ZDOT = 3289
228094 TA = 151
26589
MA = 151
23454
Ha = 216
910 n
mi
Hp = 214
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13451979
03 X = 4155639
00
Y = -10019343
39 feet Y = -3007735
12 meter
Z = -14609425
59 Z = -4432899
95
XDOT = 19896
674434 XDOT = 6010
712545
YDOT = 10962
792302 feet/sec YDOT = 3408
975690 meter/sec
ZDOT = 10791
430754 ZDOT = 3318
558007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10031555
28 X = 3057618
05
Y = -13536357
71 feet Y = -4125881
83 meter
Z = -14522851
53 Z = -4426565
15
XDOT = 21176
793326 XDOT = 6454
686606
YDOT = 3970
359738 feet/sec YDOT = 1210
165648 meter/sec
ZDOT = 10916
513242 ZDOT = 3327
353236
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 15111
47836776
00016717 00000-0 10270-3 0 9149
2 25544 51
6470 7
3328 0006221 253
0439 107
0033 15
55690993 19214
Satellite: ISS
Catalog Number: 25544
Epoch time: 15111
47836776 = yrday
fracday
Element set: 914
Inclination: 51
6470 deg
RA of node: 7
3328 deg
Eccentricity:
0006221
Arg of perigee: 253
0439 deg
Mean anomaly: 107
0033 deg
Mean motion: 15
55690993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1921
Checksum: 297
Coasting Arc #16 (Orbit 1936)
---------------------------------------
Vector Time (GMT): 2015/112/11:14:20
983
Vector Time (MET): N/A
Weight (LBS) : 927275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5779529
96 A = 6781373
40 meter
Y = 2080631
87 meter E =
0008075
Z = 2861982
14 I = 51
67094
XDOT = -4004
026331 Wp = 117
08878
YDOT = -4137
478036 meter/sec RA = 1
81475 deg
ZDOT = -5070
482924 TA = 30
33853
MA = 30
29182
Ha = 216
824 n
mi
Hp = 214
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18961712
47 X = -5816269
15
Y = 6826220
06 feet Y = 2015796
03 meter
Z = 9389705
19 Z = 2833816
66
XDOT = -13136
569326 XDOT = -3932
831641
YDOT = -13574
403004 feet/sec YDOT = -4181
855694 meter/sec
ZDOT = -16635
442664 ZDOT = -5089
760965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15991354
88 X = -4874164
97
Y = 12356416
27 feet Y = 3766235
68 meter
Z = 9268545
17 Z = 2825052
57
XDOT = -15679
139078 XDOT = -4779
001591
YDOT = -7733
458639 feet/sec YDOT = -2357
158193 meter/sec
ZDOT = -16717
268387 ZDOT = -5095
423404
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 15112
50615948
00016717 00000-0 10270-3 0 9151
2 25544 51
6466 2
1974 0006217 256
3216 103
7245 15
55700138 19371
Satellite: ISS
Catalog Number: 25544
Epoch time: 15112
50615948 = yrday
fracday
Element set: 915
Inclination: 51
6466 deg
RA of node: 2
1974 deg
Eccentricity:
0006217
Arg of perigee: 256
3216 deg
Mean anomaly: 103
7245 deg
Mean motion: 15
55700138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1937
Checksum: 296
Coasting Arc #17 (Orbit 1951)
---------------------------------------
Vector Time (GMT): 2015/113/11:14:20
983
Vector Time (MET): N/A
Weight (LBS) : 927275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6665632
49 A = 6784383
69 meter
Y = -974393
85 meter E =
0007058
Z = -764301
83 I = 51
65048
XDOT = 1360
013336 Wp = 3
44460
YDOT = 4641
738567 meter/sec RA = 356
83325 deg
ZDOT = 5953
030124 TA = 348
29054
MA = 348
30695
Ha = 216
384 n
mi
Hp = 214
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21868873
01 X = 6679745
72
Y = -3196830
21 feet Y = -899775
49 meter
Z = -2507551
94 Z = -731886
86
XDOT = 4461
986010 XDOT = 1279
089347
YDOT = 15228
801074 feet/sec YDOT = 4656
494740 meter/sec
ZDOT = 19530
938726 ZDOT = 5959
440245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19662809
20 X = 5993224
24
Y = -10125205
14 feet Y = -3086162
53 meter
Z = -2368396
55 Z = -721887
27
XDOT = 8306
951255 XDOT = 2531
958742
YDOT = 11565
021920 feet/sec YDOT = 3525
018681 meter/sec
ZDOT = 19557
496582 ZDOT = 5961
124958
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 15113
46969423
00016717 00000-0 10270-3 0 9168
2 25544 51
6471 357
3820 0006348 261
0247 99
0188 15
55754285 19526
Satellite: ISS
Catalog Number: 25544
Epoch time: 15113
46969423 = yrday
fracday
Element set: 916
Inclination: 51
6471 deg
RA of node: 357
3820 deg
Eccentricity:
0006348
Arg of perigee: 261
0247 deg
Mean anomaly: 99
0188 deg
Mean motion: 15
55754285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1952
Checksum: 328
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