[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 3rd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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 471)
---------------------------------------
Vector Time (GMT): 2015/275/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2984511
97 A = 6782923
10 meter
Y = -4678392
59 meter E =
0010870
Z = 3888295
16 I = 51
27488
XDOT = 3412
181257 Wp = 66
34351
YDOT = 5550
294819 meter/sec RA = 268
35091 deg
ZDOT = 4054
319103 TA = 341
00952
MA = 341
05002
Ha = 221
782 n
mi
Hp = 214
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9791705
92 X = 3017716
93
Y = -15349057
04 feet Y = -4644831
81 meter
Z = 12756873
88 Z = 3902874
59
XDOT = 11194
820397 XDOT = 3330
168271
YDOT = 18209
628670 feet/sec YDOT = 5587
993866 meter/sec
ZDOT = 13301
571859 ZDOT = 4070
695362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17897902
65 X = -5455280
73
Y = 3083528
17 feet Y = 939859
39 meter
Z = 12820523
50 Z = 3907695
56
XDOT = 6290
368136 XDOT = 1917
304208
YDOT = -19146
464939 feet/sec YDOT = -5835
842513 meter/sec
ZDOT = 13371
161874 ZDOT = 4075
530139
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 15275
39532257
00016717 00000-0 10270-3 0 9003
2 25544 51
6425 268
8936 0006260 350
5313 9
5721 15
54101048 4727
Satellite: ISS
Catalog Number: 25544
Epoch time: 15275
39532257 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 268
8936 deg
Eccentricity:
0006260
Arg of perigee: 350
5313 deg
Mean anomaly: 9
5721 deg
Mean motion: 15
54101048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 472
Checksum: 294
Coasting Arc #2 (Orbit 486)
---------------------------------------
Vector Time (GMT): 2015/276/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3528057
52 A = 6779438
37 meter
Y = 3206952
09 meter E =
0014417
Z = -4832666
50 I = 51
26545
XDOT = -2755
158448 Wp = 47
19728
YDOT = -6715
051350 meter/sec RA = 263
33383 deg
ZDOT = -2439
744014 TA = 198
66862
MA = 198
72155
Ha = 222
003 n
mi
Hp = 214
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11574991
86 X = -3540180
68
Y = 10521496
36 feet Y = 3167430
86 meter
Z = -15855205
06 Z = -4849835
01
XDOT = -9039
233752 XDOT = -2668
012845
YDOT = -22031
008365 feet/sec YDOT = -6745
374281 meter/sec
ZDOT = -8004
409494 ZDOT = -2452
915985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15520493
22 X = 4730646
33
Y = 1194630
06 feet Y = 364123
24 meter
Z = -15929752
01 Z = -4855388
41
XDOT = -9865
656151 XDOT = -3007
051995
YDOT = 20481
243341 feet/sec YDOT = 6242
682970 meter/sec
ZDOT = -8059
998492 ZDOT = -2456
687540
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 15276
35986911
00016717 00000-0 10270-3 0 9011
2 25544 51
6429 264
0851 0006285 354
4981 5
6102 15
54102244 4871
Satellite: ISS
Catalog Number: 25544
Epoch time: 15276
35986911 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 264
0851 deg
Eccentricity:
0006285
Arg of perigee: 354
4981 deg
Mean anomaly: 5
6102 deg
Mean motion: 15
54102244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 487
Checksum: 306
Coasting Arc #3 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2015/277/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4003406
48 A = 6777396
54 meter
Y = -1482136
09 meter E =
0005770
Z = 5261338
11 I = 51
26318
XDOT = 1993
853101 Wp = 25
72538
YDOT = 7385
792220 meter/sec RA = 258
30931 deg
ZDOT = 568
335028 TA = 58
85280
MA = 58
79623
Ha = 221
942 n
mi
Hp = 214
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13134535
68 X = 3994124
72
Y = -4862651
22 feet Y = -1437418
84 meter
Z = 17261607
96 Z = 5280763
61
XDOT = 6541
512798 XDOT = 1908
354407
YDOT = 24231
601771 feet/sec YDOT = 7407
610793 meter/sec
ZDOT = 1864
616232 ZDOT = 577
812595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12550957
10 X = -3825531
72
Y = -5977353
44 feet Y = -1821897
33 meter
Z = 17345582
60 Z = 5286933
58
XDOT = 12434
290592 XDOT = 3789
971773
YDOT = -20629
412367 feet/sec YDOT = -6287
844889 meter/sec
ZDOT = 1904
181564 ZDOT = 580
394541
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 15277
38870248
00016717 00000-0 10270-3 0 9021
2 25544 51
6423 258
9562 0006351 359
0462 1
0677 15
54148257 5035
Satellite: ISS
Catalog Number: 25544
Epoch time: 15277
38870248 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 258
9562 deg
Eccentricity:
0006351
Arg of perigee: 359
0462 deg
Mean anomaly: 1
0677 deg
Mean motion: 15
54148257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 310
Coasting Arc #4 (Orbit 517)
---------------------------------------
Vector Time (GMT): 2015/278/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4403266
14 A = 6777918
18 meter
Y = -285985
04 meter E =
0014500
Z = -5156216
12 I = 51
27296
XDOT = -1100
441375 Wp = 74
45935
YDOT = -7456
396522 meter/sec RA = 253
28282 deg
ZDOT = 1360
328395 TA = 208
66068
MA = 208
74044
Ha = 222
144 n
mi
Hp = 214
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14446411
21 X = -4374693
81
Y = -938271
14 feet Y = -335065
96 meter
Z = -16916719
54 Z = -5177537
02
XDOT = -3610
371964 XDOT = -1023
588353
YDOT = -24463
243182 feet/sec YDOT = -7468
272553 meter/sec
ZDOT = 4463
019669 ZDOT = 1355
169957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9483808
87 X = 2890664
94
Y = 10794475
54 feet Y = 3290156
14 meter
Z = -17008563
04 Z = -5184210
01
XDOT = -13919
627417 XDOT = -4242
702437
YDOT = 19192
656581 feet/sec YDOT = 5849
921726 meter/sec
ZDOT = 4442
065728 ZDOT = 1353
941634
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 15278
35322107
00016717 00000-0 10270-3 0 9036
2 25544 51
6430 254
1476 0006414 2
3280 357
7901 15
54142015 5184
Satellite: ISS
Catalog Number: 25544
Epoch time: 15278
35322107 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 254
1476 deg
Eccentricity:
0006414
Arg of perigee: 2
3280 deg
Mean anomaly: 357
7901 deg
Mean motion: 15
54142015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 518
Checksum: 274
Coasting Arc #5 (Orbit 533)
---------------------------------------
Vector Time (GMT): 2015/279/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4669928
97 A = 6780462
73 meter
Y = 2017668
35 meter E =
0013291
Z = 4480249
29 I = 51
29096
XDOT = 44
327279 Wp = 42
80378
YDOT = 6980
960706 meter/sec RA = 248
26120 deg
ZDOT = -3174
910131 TA = 79
31189
MA = 79
16226
Ha = 222
132 n
mi
Hp = 213
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15321289
28 X = 4625256
37
Y = 6619646
83 feet Y = 2069641
24 meter
Z = 14698980
60 Z = 4502826
28
XDOT = 145
430705 XDOT = -18
316226
YDOT = 22903
414390 feet/sec YDOT = 6981
105829 meter/sec
ZDOT = -10416
371820 ZDOT = -3174
847640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6364207
80 X = -1939810
54
Y = -15336177
76 feet Y = -4674466
98 meter
Z = 14795951
16 Z = 4509805
91
XDOT = 14627
674164 XDOT = 4458
515085
YDOT = -16168
166092 feet/sec YDOT = -4928
057025 meter/sec
ZDOT = -10417
286227 ZDOT = -3175
188842
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 15279
38202420
00016717 00000-0 10270-3 0 9046
2 25544 51
6418 249
0182 0006462 6
9082 353
2159 15
54210576 5342
Satellite: ISS
Catalog Number: 25544
Epoch time: 15279
38202420 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 249
0182 deg
Eccentricity:
0006462
Arg of perigee: 6
9082 deg
Mean anomaly: 353
2159 deg
Mean motion: 15
54210576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 534
Checksum: 292
Coasting Arc #6 (Orbit 548)
---------------------------------------
Vector Time (GMT): 2015/280/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4760282
50 A = 6784194
90 meter
Y = -3480854
22 meter E =
0008867
Z = -3352380
99 I = 51
31725
XDOT = 1132
218292 Wp = 43
58838
YDOT = -5999
729188 meter/sec RA = 243
25002 deg
ZDOT = 4635
586859 TA = 277
13328
MA = 277
23410
Ha = 222
222 n
mi
Hp = 213
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15617724
73 X = -4704720
27
Y = -11420125
40 feet Y = -3533776
54 meter
Z = -10998625
29 Z = -3375370
26
XDOT = 3714
626942 XDOT = 1176
706540
YDOT = -19684
150879 feet/sec YDOT = -5986
818713 meter/sec
ZDOT = 15208
618304 ZDOT = 4641
195701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3588969
88 X = 1093918
02
Y = 18954555
53 feet Y = 5777348
52 meter
Z = -11097137
84 Z = -3382407
61
XDOT = -14682
200290 XDOT = -4475
134648
YDOT = 11672
820279 feet/sec YDOT = 3557
875621 meter/sec
ZDOT = 15233
800968 ZDOT = 4643
262535
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 15280
34651426
00016717 00000-0 10270-3 0 9059
2 25544 51
6428 244
2095 0006462 11
4358 348
6941 15
54224264 5492
Satellite: ISS
Catalog Number: 25544
Epoch time: 15280
34651426 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 244
2095 deg
Eccentricity:
0006462
Arg of perigee: 11
4358 deg
Mean anomaly: 348
6941 deg
Mean motion: 15
54224264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 549
Checksum: 305
Coasting Arc #7 (Orbit 564)
---------------------------------------
Vector Time (GMT): 2015/281/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4590127
58 A = 6787557
16 meter
Y = 4653509
11 meter E =
0014485
Z = 1818183
85 I = 51
34241
XDOT = -2433
386363 Wp = 87
61891
YDOT = 4611
616690 meter/sec RA = 238
24953 deg
ZDOT = -5620
388015 TA = 72
31022
MA = 72
15214
Ha = 222
365 n
mi
Hp = 213
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15059473
69 X = 4528917
66
Y = 15267418
34 feet Y = 4704496
92 meter
Z = 5965170
10 Z = 1840332
65
XDOT = -7983
551060 XDOT = -2457
471851
YDOT = 15129
976018 feet/sec YDOT = 4584
269597 meter/sec
ZDOT = -18439
593226 ZDOT = -5632
268060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -949871
24 X = -289520
75
Y = -21397212
23 feet Y = -6521870
29 meter
Z = 6059877
73 Z = 1847050
73
XDOT = 14406
867591 XDOT = 4391
213242
YDOT = -5912
621020 feet/sec YDOT = -1802
166887 meter/sec
ZDOT = -18491
569749 ZDOT = -5636
230459
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 15281
37528719
00016717 00000-0 10270-3 0 9062
2 25544 51
6414 239
0793 0006509 15
2335 344
9013 15
54241210 5650
Satellite: ISS
Catalog Number: 25544
Epoch time: 15281
37528719 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 239
0793 deg
Eccentricity:
0006509
Arg of perigee: 15
2335 deg
Mean anomaly: 344
9013 deg
Mean motion: 15
54241210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 565
Checksum: 296
Coasting Arc #8 (Orbit 579)
---------------------------------------
Vector Time (GMT): 2015/282/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4131993
62 A = 6788864
25 meter
Y = -5373023
95 meter E =
0017786
Z = -121232
43 I = 51
36531
XDOT = 3738
023163 Wp = 35
52569
YDOT = -2999
538928 meter/sec RA = 233
25791 deg
ZDOT = 5992
609409 TA = 323
16250
MA = 323
28456
Ha = 222
292 n
mi
Hp = 213
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13556409
53 X = -4071015
16
Y = -17628031
35 feet Y = -5418889
70 meter
Z = -397744
19 Z = -141156
17
XDOT = 12263
855522 XDOT = 3742
176855
YDOT = -9841
006983 feet/sec YDOT = -2957
713867 meter/sec
ZDOT = 19660
792025 ZDOT = 6010
778614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1338175
04 X = -407875
75
Y = 22195904
22 feet Y = 6765311
61 meter
Z = -482754
89 Z = -147143
69
XDOT = -13997
195121 XDOT = -4266
345073
YDOT = -441
411936 feet/sec YDOT = -134
542358 meter/sec
ZDOT = 19739
611863 ZDOT = 6016
633696
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 15282
33974700
00016717 00000-0 10270-3 0 9075
2 25544 51
6420 234
2708 0006388 18
3596 341
7786 15
54286438 5808
Satellite: ISS
Catalog Number: 25544
Epoch time: 15282
33974700 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 234
2708 deg
Eccentricity:
0006388
Arg of perigee: 18
3596 deg
Mean anomaly: 341
7786 deg
Mean motion: 15
54286438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 580
Checksum: 327
Coasting Arc #9 (Orbit 595)
---------------------------------------
Vector Time (GMT): 2015/283/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3319705
44 A = 6787797
49 meter
Y = 5690397
91 meter E =
0007299
Z = -1640524
88 I = 51
38046
XDOT = -4968
272925 Wp = 92
27660
YDOT = 1263
322416 meter/sec RA = 228
26696 deg
ZDOT = -5693
874812 TA = 105
73900
MA = 105
65849
Ha = 222
475 n
mi
Hp = 213
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10891422
04 X = 3263796
43
Y = 18669284
49 feet Y = 5727208
22 meter
Z = -5382299
48 Z = -1624534
82
XDOT = -16300
108022 XDOT = -4954
371453
YDOT = 4144
758583 feet/sec YDOT = 1207
840849 meter/sec
ZDOT = -18680
691639 ZDOT = -5717
976368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3638011
77 X = 1108865
99
Y = -21322702
26 feet Y = -6499159
65 meter
Z = -5314286
76 Z = -1619794
61
XDOT = 13500
669054 XDOT = 4115
003928
YDOT = 6966
754702 feet/sec YDOT = 2123
466833 meter/sec
ZDOT = -18784
805208 ZDOT = -5725
608627
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 15283
36848850
00016717 00000-0 10270-3 0 9086
2 25544 51
6411 229
1400 0006482 22
1950 337
9483 15
54270543 5960
Satellite: ISS
Catalog Number: 25544
Epoch time: 15283
36848850 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 229
1400 deg
Eccentricity:
0006482
Arg of perigee: 22
1950 deg
Mean anomaly: 337
9483 deg
Mean motion: 15
54270543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 596
Checksum: 310
Coasting Arc #10 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2015/284/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2191562
70 A = 6784504
93 meter
Y = -5560678
11 meter E =
0016936
Z = 3189044
36 I = 51
39158
XDOT = 5989
739688 Wp = 66
72878
YDOT = 391
275045 meter/sec RA = 223
27191 deg
ZDOT = 4784
847415 TA = 330
31397
MA = 330
40998
Ha = 222
450 n
mi
Hp = 213
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7190166
33 X = -2144710
36
Y = -18243694
59 feet Y = -5584923
20 meter
Z = 10462743
98 Z = 3178512
62
XDOT = 19651
376928 XDOT = 5961
675865
YDOT = 1283
710777 feet/sec YDOT = 458
100021 meter/sec
ZDOT = 15698
318290 ZDOT = 4813
876580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5852129
39 X = -1783729
04
Y = 18740674
87 feet Y = 5712157
70 meter
Z = 10418233
20 Z = 3175477
48
XDOT = -13010
428131 XDOT = -3965
578494
YDOT = -12884
250322 feet/sec YDOT = -3927
119498 meter/sec
ZDOT = 15823
414910 ZDOT = 4822
976864
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 15284
39721247
00016717 00000-0 10270-3 0 9091
2 25544 51
6410 224
0104 0006473 24
7607 335
3855 15
54315503 6121
Satellite: ISS
Catalog Number: 25544
Epoch time: 15284
39721247 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 224
0104 deg
Eccentricity:
0006473
Arg of perigee: 24
7607 deg
Mean anomaly: 335
3855 deg
Mean motion: 15
54315503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 286
Coasting Arc #11 (Orbit 626)
---------------------------------------
Vector Time (GMT): 2015/285/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 764178
29 A = 6780534
58 meter
Y = 5097337
98 meter E =
0014656
Z = -4420794
81 I = 51
40195
XDOT = -6643
846452 Wp = 52
86499
YDOT = -1875
553197 meter/sec RA = 218
26678 deg
ZDOT = -3309
969277 TA = 183
54405
MA = 183
55444
Ha = 222
542 n
mi
Hp = 212
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2507146
61 X = 728596
75
Y = 16723549
79 feet Y = 5105683
97 meter
Z = -14503919
98 Z = -4417169
64
XDOT = -21797
396495 XDOT = -6606
300901
YDOT = -6153
389755 feet/sec YDOT = -1949
639593 meter/sec
ZDOT = -10859
479254 ZDOT = -3342
152890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8259175
16 X = 2517396
59
Y = -14770863
37 feet Y = -4502159
15 meter
Z = -14489106
85 Z = -4416279
77
XDOT = 12239
952381 XDOT = 3730
737486
YDOT = 17635
605167 feet/sec YDOT = 5375
332455 meter/sec
ZDOT = -10997
947264 ZDOT = -3352
174326
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 15285
36162743
00016717 00000-0 10270-3 0 9101
2 25544 51
6408 219
2005 0006540 28
7753 331
3759 15
54317382 6277
Satellite: ISS
Catalog Number: 25544
Epoch time: 15285
36162743 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 219
2005 deg
Eccentricity:
0006540
Arg of perigee: 28
7753 deg
Mean anomaly: 331
3759 deg
Mean motion: 15
54317382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 627
Checksum: 302
Coasting Arc #12 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2015/286/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 854482
55 A = 6777472
65 meter
Y = -4335532
03 meter E =
0007820
Z = 5131849
85 I = 51
41741
XDOT = 6866
190996 Wp = 68
73879
YDOT = 3096
407329 meter/sec RA = 213
25353 deg
ZDOT = 1473
643311 TA = 7
04786
MA = 7
03687
Ha = 222
499 n
mi
Hp = 212
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2803420
44 X = 877970
91
Y = -14224186
45 feet Y = -4325844
66 meter
Z = 16836777
72 Z = 5136058
45
XDOT = 22526
873346 XDOT = 6823
897348
YDOT = 10158
816695 feet/sec YDOT = 3172
953316 meter/sec
ZDOT = 4834
787765 ZDOT = 1506
895479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10723101
75 X = -3268401
41
Y = 9724553
18 feet Y = 2964043
81 meter
Z = 16855618
78 Z = 5137592
60
XDOT = -11118
759284 XDOT = -3388
997830
YDOT = -20882
790787 feet/sec YDOT = -6365
074632 meter/sec
ZDOT = 4977
679246 ZDOT = 1517
196634
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 15286
39031992
00016717 00000-0 10270-3 0 9117
2 25544 51
6405 214
0705 0006560 31
3847 328
7696 15
54344639 6433
Satellite: ISS
Catalog Number: 25544
Epoch time: 15286
39031992 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 214
0705 deg
Eccentricity:
0006560
Arg of perigee: 31
3847 deg
Mean anomaly: 328
7696 deg
Mean motion: 15
54344639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 314
Coasting Arc #13 (Orbit 657)
---------------------------------------
Vector Time (GMT): 2015/287/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2530429
77 A = 6776774
07 meter
Y = 3424922
49 meter E =
0019008
Z = -5287494
20 I = 51
44244
XDOT = -6513
132476 Wp = 77
07470
YDOT = -3986
663637 meter/sec RA = 208
23668 deg
ZDOT = 540
466106 TA = 198
07125
MA = 198
13891
Ha = 222
589 n
mi
Hp = 212
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8301934
93 X = -2542854
77
Y = 11236622
33 feet Y = 3396555
47 meter
Z = -17347421
90 Z = -5299817
38
XDOT = -21368
544870 XDOT = -6470
694000
YDOT = -13079
605109 feet/sec YDOT = -4059
260431 meter/sec
ZDOT = 1773
182762 ZDOT = 508
929407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13236186
09 X = 4034389
52
Y = -4256940
67 feet Y = -1297515
51 meter
Z = -17401111
62 Z = -5303858
82
XDOT = 9266
685718 XDOT = 2824
485807
YDOT = 22195
793712 feet/sec YDOT = 6765
277923 meter/sec
ZDOT = 1637
818526 ZDOT = 499
207087
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 15287
35470375
00016717 00000-0 10270-3 0 9127
2 25544 51
6406 209
2612 0006571 35
1732 324
9853 15
54357618 6584
Satellite: ISS
Catalog Number: 25544
Epoch time: 15287
35470375 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 209
2612 deg
Eccentricity:
0006571
Arg of perigee: 35
1732 deg
Mean anomaly: 324
9853 deg
Mean motion: 15
54357618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 658
Checksum: 315
Coasting Arc #14 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2015/288/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4128496
45 A = 6778596
50 meter
Y = -2394020
63 meter E =
0013417
Z = 4808497
49 I = 51
47728
XDOT = 5609
708870 Wp = 49
71072
YDOT = 4588
799718 meter/sec RA = 203
22308 deg
ZDOT = -2518
609000 TA = 65
16672
MA = 65
02725
Ha = 222
454 n
mi
Hp = 212
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13544935
86 X = 4131601
70
Y = -7854398
39 feet Y = -2347835
22 meter
Z = 15775910
40 Z = 4828561
18
XDOT = 18404
556661 XDOT = 5570
213614
YDOT = 15055
117186 feet/sec YDOT = 4651
310101 meter/sec
ZDOT = -8263
152887 ZDOT = -2491
453874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15514790
02 X = -4728908
00
Y = -1303192
55 feet Y = -397213
09 meter
Z = 15862824
16 Z = 4834988
80
XDOT = -6542
501897 XDOT = -1994
154578
YDOT = -21797
320600 feet/sec YDOT = -6643
823319 meter/sec
ZDOT = -8146
768576 ZDOT = -2483
135062
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 15288
38336328
00016717 00000-0 10270-3 0 9131
2 25544 51
6403 204
1309 0006556 37
6962 322
4649 15
54403851 6748
Satellite: ISS
Catalog Number: 25544
Epoch time: 15288
38336328 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 204
1309 deg
Eccentricity:
0006556
Arg of perigee: 37
6962 deg
Mean anomaly: 322
4649 deg
Mean motion: 15
54403851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 313
Coasting Arc #15 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2015/289/08:08:49
441
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5443048
15 A = 6782279
21 meter
Y = 1392700
93 meter E =
0010957
Z = -3805289
50 I = 51
51922
XDOT = -4167
569765 Wp = 72
28213
YDOT = -4877
679068 meter/sec RA = 198
22056 deg
ZDOT = 4189
285558 TA = 241
96347
MA = 242
07433
Ha = 222
587 n
mi
Hp = 212
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17857769
52 X = -5439732
02
Y = 4569228
78 feet Y = 1331851
40 meter
Z = -12484545
60 Z = -3831723
45
XDOT = -13673
129150 XDOT = -4133
067084
YDOT = -16002
884080 feet/sec YDOT = -4924
090316 meter/sec
ZDOT = 13744
375189 ZDOT = 4169
124052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17281341
38 X = 5267352
85
Y = 6186072
34 feet Y = 1885514
85 meter
Z = -12598786
12 Z = -3840110
01
XDOT = 2872
312775 XDOT = 875
480934
YDOT = 19705
180689 feet/sec YDOT = 6006
139074 meter/sec
ZDOT = 13658
190353 ZDOT = 4163
016420
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 15289
34771681
00016717 00000-0 10270-3 0 9144
2 25544 51
6402 199
3215 0006634 41
4053 318
7602 15
54402868 6899
Satellite: ISS
Catalog Number: 25544
Epoch time: 15289
34771681 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 199
3215 deg
Eccentricity:
0006634
Arg of perigee: 41
4053 deg
Mean anomaly: 318
7602 deg
Mean motion: 15
54402868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 317
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