[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 6th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 34444 51 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
072/04:01:16
229 -1
6 2
9 2
9
N/A -2
2 0
0 224
2
000/00:06:32
458 1
0 0
1 221
5
Coasting Arc #1 (Orbit 3523)
---------------------------------------
Vector Time (GMT): 2014/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4462627
81 A = 6787112
77 meter
Y = -605653
25 meter E =
0012416
Z = -5088760
25 I = 51
28530
XDOT = -908
110393 Wp = 117
07321
YDOT = -7412
920835 meter/sec RA = 252
65114 deg
ZDOT = 1676
272179 TA = 169
24055
MA = 169
21397
Ha = 225
371 n
mi
Hp = 219
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14641167
35 X = -4430804
14
Y = -1987051
36 feet Y = -655379
89 meter
Z = -16695407
65 Z = -5110361
59
XDOT = -2979
364807 XDOT = -833
292707
YDOT = -24320
606415 feet/sec YDOT = -7422
657377 meter/sec
ZDOT = 5499
580639 ZDOT = 1672
043341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13247630
22 X = -4037877
69
Y = -6305828
41 feet Y = -1922016
50 meter
Z = -16786471
13 Z = -5116516
40
XDOT = 4048
673691 XDOT = 1234
035741
YDOT = -23121
848885 feet/sec YDOT = -7047
539540 meter/sec
ZDOT = 5482
816900 ZDOT = 1671
162591
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 14064
51322984
00016717 00000-0 10270-3 0 9006
2 25544 51
6457 253
5027 0003366 216
6556 143
4365 15
51100479 35246
Satellite: ISS
Catalog Number: 25544
Epoch time: 14064
51322984 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 253
5027 deg
Eccentricity:
0003366
Arg of perigee: 216
6556 deg
Mean anomaly: 143
4365 deg
Mean motion: 15
51100479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3524
Checksum: 296
Coasting Arc #2 (Orbit 3539)
---------------------------------------
Vector Time (GMT): 2014/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4635327
65 A = 6788071
24 meter
Y = 1087824
08 meter E =
0003882
Z = 4835340
00 I = 51
29912
XDOT = 853
149063 Wp = 75
00544
YDOT = 7216
688274 meter/sec RA = 247
66048 deg
ZDOT = -2438
792580 TA = 39
06775
MA = 39
03972
Ha = 225
066 n
mi
Hp = 220
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15207767
87 X = 4599330
44
Y = 3568976
63 feet Y = 1139458
51 meter
Z = 15863976
39 Z = 4857770
11
XDOT = 2799
045483 XDOT = 784
233837
YDOT = 23676
798800 feet/sec YDOT = 7225
843155 meter/sec
ZDOT = -8001
287993 ZDOT = -2434
816258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13447839
88 X = 4098901
60
Y = 7756435
27 feet Y = 2364161
47 meter
Z = 15958472
95 Z = 4864142
56
XDOT = -3500
781084 XDOT = -1067
038074
YDOT = 22517
059061 feet/sec YDOT = 6863
199602 meter/sec
ZDOT = -7985
553276 ZDOT = -2433
996639
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 14065
54406001
00016717 00000-0 10270-3 0 9014
2 25544 51
6459 248
3876 0003395 222
3119 137
7771 15
51123534 35405
Satellite: ISS
Catalog Number: 25544
Epoch time: 14065
54406001 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 248
3876 deg
Eccentricity:
0003395
Arg of perigee: 222
3119 deg
Mean anomaly: 137
7771 deg
Mean motion: 15
51123534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3540
Checksum: 293
Coasting Arc #3 (Orbit 3554)
---------------------------------------
Vector Time (GMT): 2014/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4852719
10 A = 6789236
37 meter
Y = -1542941
87 meter E =
0008886
Z = -4499469
54 I = 51
31618
XDOT = -730
960994 Wp = 130
50937
YDOT = -6932
640192 meter/sec RA = 242
67020 deg
ZDOT = 3164
138541 TA = 171
46824
MA = 171
45313
Ha = 225
073 n
mi
Hp = 219
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15920994
43 X = -4813248
08
Y = -5062145
25 feet Y = -1596987
80 meter
Z = -14762039
18 Z = -4522947
19
XDOT = -2398
165990 XDOT = -668
754594
YDOT = -22744
882521 feet/sec YDOT = -6940
466162 meter/sec
ZDOT = 10381
031958 ZDOT = 3160
739385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13868646
56 X = -4227163
47
Y = -9156172
92 feet Y = -2790801
51 meter
Z = -14860899
00 Z = -4529602
02
XDOT = 3113
379561 XDOT = 948
958090
YDOT = -21551
072316 feet/sec YDOT = -6568
766842 meter/sec
ZDOT = 10367
683541 ZDOT = 3160
069943
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 14066
51043509
00016717 00000-0 10270-3 0 9023
2 25544 51
6458 243
5908 0003313 224
1436 135
9451 15
51188590 35553
Satellite: ISS
Catalog Number: 25544
Epoch time: 14066
51043509 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 243
5908 deg
Eccentricity:
0003313
Arg of perigee: 224
1436 deg
Mean anomaly: 135
9451 deg
Mean motion: 15
51188590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3555
Checksum: 300
Coasting Arc #4 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2014/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5078001
78 A = 6790753
28 meter
Y = 1961479
82 meter E =
0007788
Z = 4053004
84 I = 51
33623
XDOT = 529
757709 Wp = 88
81521
YDOT = 6605
522437 meter/sec RA = 237
68353 deg
ZDOT = -3853
927166 TA = 41
29378
MA = 41
23492
Ha = 224
767 n
mi
Hp = 220
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16660110
83 X = 5036002
64
Y = 6435301
24 feet Y = 2018030
81 meter
Z = 13297259
98 Z = 4077570
66
XDOT = 1738
050227 XDOT = 474
574874
YDOT = 21671
661540 feet/sec YDOT = 6611
137651 meter/sec
ZDOT = -12644
117999 ZDOT = -3851
488303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14399216
34 X = 4388881
14
Y = 10434286
06 feet Y = 3180370
39 meter
Z = 13400662
72 Z = 4084522
00
XDOT = -2983
757352 XDOT = -909
449241
YDOT = 20371
846178 feet/sec YDOT = 6209
338715 meter/sec
ZDOT = -12634
766724 ZDOT = -3851
076897
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 14067
54120445
00016717 00000-0 10270-3 0 9033
2 25544 51
6454 238
4752 0003332 230
0404 130
0455 15
51216186 35712
Satellite: ISS
Catalog Number: 25544
Epoch time: 14067
54120445 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 238
4752 deg
Eccentricity:
0003332
Arg of perigee: 230
0404 deg
Mean anomaly: 130
0455 deg
Mean motion: 15
51216186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 269
Coasting Arc #5 (Orbit 3585)
---------------------------------------
Vector Time (GMT): 2014/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5319529
82 A = 6792255
36 meter
Y = -2325049
85 meter E =
0003665
Z = -3530609
35 I = 51
35988
XDOT = -247
047551 Wp = 133
96704
YDOT = -6215
769641 meter/sec RA = 232
69894 deg
ZDOT = 4465
969019 TA = 184
33208
MA = 184
33526
Ha = 224
759 n
mi
Hp = 219
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17452525
65 X = -5275984
86
Y = -7628116
30 feet Y = -2384293
08 meter
Z = -11583364
02 Z = -3556344
61
XDOT = -810
523460 XDOT = -199
217054
YDOT = -20392
945018 feet/sec YDOT = -6218
264457 meter/sec
ZDOT = 14652
129327 ZDOT = 4464
885632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15073825
96 X = -4594502
15
Y = -11534206
05 feet Y = -3515626
00 meter
Z = -11691663
43 Z = -3563619
01
XDOT = 3119
958571 XDOT = 950
963372
YDOT = -18924
473181 feet/sec YDOT = -5768
179426 meter/sec
ZDOT = 14648
434879 ZDOT = 4464
842951
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 14068
50752175
00016717 00000-0 10270-3 0 9042
2 25544 51
6460 233
6786 0003231 232
2170 127
8689 15
51281719 35868
Satellite: ISS
Catalog Number: 25544
Epoch time: 14068
50752175 = yrday
fracday
Element set: 904
Inclination: 51
6460 deg
RA of node: 233
6786 deg
Eccentricity:
0003231
Arg of perigee: 232
2170 deg
Mean anomaly: 127
8689 deg
Mean motion: 15
51281719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3586
Checksum: 314
Coasting Arc #6 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2014/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5537536
24 A = 6793872
72 meter
Y = 2642210
31 meter E =
0010910
Z = 2903662
54 I = 51
38435
XDOT = -134
301447 Wp = 109
26840
YDOT = 5800
813391 meter/sec RA = 227
71784 deg
ZDOT = -5010
467796 TA = 37
53808
MA = 37
46196
Ha = 224
489 n
mi
Hp = 220
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18167769
81 X = 5493474
01
Y = 8668669
00 feet Y = 2703888
50 meter
Z = 9526451
90 Z = 2930455
47
XDOT = -440
621546 XDOT = -174
818545
YDOT = 19031
539998 feet/sec YDOT = 5799
084525 meter/sec
ZDOT = -16438
542637 ZDOT = -5011
219169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15750789
89 X = 4800840
76
Y = 12448521
78 feet Y = 3794309
44 meter
Z = 9639185
20 Z = 2938023
65
XDOT = -3617
502425 XDOT = -1102
614739
YDOT = 17338
853738 feet/sec YDOT = 5284
882619 meter/sec
ZDOT = -16442
526034 ZDOT = -5011
681935
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 14069
53822825
00016717 00000-0 10270-3 0 9057
2 25544 51
6452 228
5622 0003257 238
3473 121
7361 15
51314910 36021
Satellite: ISS
Catalog Number: 25544
Epoch time: 14069
53822825 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 228
5622 deg
Eccentricity:
0003257
Arg of perigee: 238
3473 deg
Mean anomaly: 121
7361 deg
Mean motion: 15
51314910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 292
Coasting Arc #7 (Orbit 3616)
---------------------------------------
Vector Time (GMT): 2014/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5734865
11 A = 6795188
29 meter
Y = -2888502
20 meter E =
0003144
Z = -2219021
87 I = 51
41219
XDOT = 596
589653 Wp = 25
97474
YDOT = -5359
710490 meter/sec RA = 222
73989 deg
ZDOT = 5440
608307 TA = 309
32560
MA = 309
35347
Ha = 224
432 n
mi
Hp = 219
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18815174
25 X = -5691359
86
Y = -9476713
27 feet Y = -2952390
13 meter
Z = -7280255
49 Z = -2246774
65
XDOT = 1957
315136 XDOT = 630
050457
YDOT = -17584
352001 feet/sec YDOT = -5352
851375 meter/sec
ZDOT = 17849
764788 ZDOT = 5443
588255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16445628
72 X = -5012627
63
Y = -13101387
99 feet Y = -3993303
06 meter
Z = -7397021
39 Z = -2254612
12
XDOT = 4432
675403 XDOT = 1351
079463
YDOT = -15639
225437 feet/sec YDOT = -4766
835913 meter/sec
ZDOT = 17863
087178 ZDOT = 5444
668972
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 14070
50448584
00016717 00000-0 10270-3 0 9063
2 25544 51
6465 223
7656 0003146 241
7209 118
3625 15
51376985 36172
Satellite: ISS
Catalog Number: 25544
Epoch time: 14070
50448584 = yrday
fracday
Element set: 906
Inclination: 51
6465 deg
RA of node: 223
7656 deg
Eccentricity:
0003146
Arg of perigee: 241
7209 deg
Mean anomaly: 118
3625 deg
Mean motion: 15
51376985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3617
Checksum: 319
Coasting Arc #8 (Orbit 3632)
---------------------------------------
Vector Time (GMT): 2014/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5870535
87 A = 6796268
53 meter
Y = 3088549
49 meter E =
0012061
Z = 1447176
39 I = 51
43890
XDOT = -1159
296832 Wp = 130
41127
YDOT = 4916
673109 meter/sec RA = 217
76489 deg
ZDOT = -5766
286621 TA = 33
77024
MA = 33
69347
Ha = 224
216 n
mi
Hp = 219
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19260288
27 X = 5828532
89
Y = 10133036
40 feet Y = 3153962
91 meter
Z = 4747954
03 Z = 1475591
81
XDOT = -3803
467296 XDOT = -1186
179662
YDOT = 16130
817288 feet/sec YDOT = 4903
558111 meter/sec
ZDOT = -18918
263193 ZDOT = -5771
984119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16998824
63 X = 5181241
75
Y = 13547234
16 feet Y = 4129196
97 meter
Z = 4867505
14 Z = 1483615
57
XDOT = -5645
241637 XDOT = -1720
669651
YDOT = 13917
440145 feet/sec YDOT = 4242
035756 meter/sec
ZDOT = -18942
991761 ZDOT = -5773
823889
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 14071
53512764
00016717 00000-0 10270-3 0 9070
2 25544 51
6457 218
6486 0003177 248
4814 111
5999 15
51426001 36339
Satellite: ISS
Catalog Number: 25544
Epoch time: 14071
53512764 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 218
6486 deg
Eccentricity:
0003177
Arg of perigee: 248
4814 deg
Mean anomaly: 111
5999 deg
Mean motion: 15
51426001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3633
Checksum: 313
Coasting Arc #9 (Orbit 3642)
---------------------------------------
Vector Time (GMT): 2014/072/04:04:32
458
Vector Time (MET): N/A
Weight (LBS) : 901433
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5318974
84 A = 6791094
90 meter
Y = 418950
92 meter E =
0003323
Z = -4205060
81 I = 51
43682
XDOT = -3352
292015 Wp = 131
60176
YDOT = -5833
596823 meter/sec RA = 214
42355 deg
ZDOT = 3658
824081 TA = 176
05958
MA = 176
05696
Ha = 224
188 n
mi
Hp = 221
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17450704
85 X = -5302837
78
Y = 1374510
90 feet Y = 359560
42 meter
Z = -13796131
28 Z = -4230860
12
XDOT = -10998
333381 XDOT = -3304
583409
YDOT = -19139
097187 feet/sec YDOT = -5870
817076 meter/sec
ZDOT = 12004
016014 ZDOT = 3642
655988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9852866
03 X = 3003153
57
Y = -14363781
24 feet Y = -4378080
52 meter
Z = -13905122
71 Z = -4238281
40
XDOT = 20796
051339 XDOT = 6338
636448
YDOT = 2708
816726 feet/sec YDOT = 825
647338 meter/sec
ZDOT = 11936
540884 ZDOT = 3638
257662
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 14072
17926175
00016717 00000-0 10270-3 0 9087
2 25544 51
6492 215
4558 0005122 276
4299 83
6269 15
50918462 36439
Satellite: ISS
Catalog Number: 25544
Epoch time: 14072
17926175 = yrday
fracday
Element set: 908
Inclination: 51
6492 deg
RA of node: 215
4558 deg
Eccentricity:
0005122
Arg of perigee: 276
4299 deg
Mean anomaly: 83
6269 deg
Mean motion: 15
50918462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3643
Checksum: 330
Coasting Arc #10 (Orbit 3658)
---------------------------------------
Vector Time (GMT): 2014/073/04:04:32
458
Vector Time (MET): N/A
Weight (LBS) : 901433
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5643361
55 A = 6792434
39 meter
Y = -259451
48 meter E =
0006818
Z = 3767752
19 I = 51
46780
XDOT = 3082
520689 Wp = 69
56592
YDOT = 5602
090893 meter/sec RA = 209
44881 deg
ZDOT = -4222
703183 TA = 65
25597
MA = 65
18503
Ha = 224
197 n
mi
Hp = 221
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18514965
72 X = 5627541
08
Y = -851218
77 feet Y = -196431
71 meter
Z = 12361391
71 Z = 3795128
10
XDOT = 10113
256854 XDOT = 3040
160020
YDOT = 18379
563296 feet/sec YDOT = 5636
324160 meter/sec
ZDOT = -13854
013066 ZDOT = -4207
832620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10677197
44 X = -3254409
78
Y = 15055025
02 feet Y = 4588771
63 meter
Z = 12477027
31 Z = 3802997
92
XDOT = -19665
015450 XDOT = -5993
896709
YDOT = -2493
369686 feet/sec YDOT = -759
979080 meter/sec
ZDOT = -13791
972472 ZDOT = -4203
793210
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 14073
21021268
00016717 00000-0 10270-3 0 9093
2 25544 51
6491 210
3416 0005103 281
4957 78
5621 15
50964446 36596
Satellite: ISS
Catalog Number: 25544
Epoch time: 14073
21021268 = yrday
fracday
Element set: 909
Inclination: 51
6491 deg
RA of node: 210
3416 deg
Eccentricity:
0005103
Arg of perigee: 281
4957 deg
Mean anomaly: 78
5621 deg
Mean motion: 15
50964446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3659
Checksum: 303
Coasting Arc #11 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2014/074/04:04:32
458
Vector Time (MET): N/A
Weight (LBS) : 901433
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5950607
67 A = 6793766
61 meter
Y = 150799
15 meter E =
0001912
Z = -3272157
47 I = 51
50107
XDOT = -2733
998375 Wp = 348
64968
YDOT = -5374
518453 meter/sec RA = 204
47639 deg
ZDOT = 4725
610048 TA = 333
36010
MA = 333
36993
Ha = 224
218 n
mi
Hp = 221
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19522991
03 X = -5935956
75
Y = 494747
87 feet Y = 84337
05 meter
Z = -10735424
77 Z = -3301028
81
XDOT = -8969
810942 XDOT = -2696
651364
YDOT = -17632
934557 feet/sec YDOT = -5404
882223 meter/sec
ZDOT = 15503
969975 ZDOT = 4712
420357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11313982
09 X = 3448501
74
Y = -15835170
91 feet Y = -4826560
09 meter
Z = -10857369
42 Z = -3309326
20
XDOT = 18383
033760 XDOT = 5603
148690
YDOT = 2544
840534 feet/sec YDOT = 775
667395 meter/sec
ZDOT = 15448
986295 ZDOT = 4708
851023
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 14074
17669807
00016717 00000-0 10270-3 0 9108
2 25544 51
6500 205
5462 0005263 286
1907 73
8665 15
51015480 36747
Satellite: ISS
Catalog Number: 25544
Epoch time: 14074
17669807 = yrday
fracday
Element set: 910
Inclination: 51
6500 deg
RA of node: 205
5462 deg
Eccentricity:
0005263
Arg of perigee: 286
1907 deg
Mean anomaly: 73
8665 deg
Mean motion: 15
51015480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 309
Coasting Arc #12 (Orbit 3689)
---------------------------------------
Vector Time (GMT): 2014/075/04:04:32
458
Vector Time (MET): N/A
Weight (LBS) : 901433
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6233346
16 A = 6795130
62 meter
Y = -64070
29 meter E =
0008394
Z = 2696169
95 I = 51
53466
XDOT = 2294
788671 Wp = 95
68488
YDOT = 5169
977610 meter/sec RA = 199
50822 deg
ZDOT = -5169
448538 TA = 53
85064
MA = 53
77299
Ha = 224
397 n
mi
Hp = 221
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20450610
77 X = 6220502
30
Y = -210204
36 feet Y = 5563
61 meter
Z = 8845701
95 Z = 2726419
27
XDOT = 7528
834223 XDOT = 2261
917616
YDOT = 16961
868798 feet/sec YDOT = 5195
454776 meter/sec
ZDOT = -16960
132998 ZDOT = -5158
381537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11822319
09 X = -3603442
86
Y = 16620103
51 feet Y = 5065807
55 meter
Z = 8973463
12 Z = 2735111
56
XDOT = -16996
075211 XDOT = -5180
403724
YDOT = -2934
737817 feet/sec YDOT = -894
508086 meter/sec
ZDOT = -16914
078560 ZDOT = -5155
411145
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 14075
20758511
00016717 00000-0 10270-3 0 9115
2 25544 51
6501 200
4317 0005184 290
8569 69
2027 15
51051308 36907
Satellite: ISS
Catalog Number: 25544
Epoch time: 14075
20758511 = yrday
fracday
Element set: 911
Inclination: 51
6501 deg
RA of node: 200
4317 deg
Eccentricity:
0005184
Arg of perigee: 290
8569 deg
Mean anomaly: 69
2027 deg
Mean motion: 15
51051308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3690
Checksum: 286
Coasting Arc #13 (Orbit 3704)
---------------------------------------
Vector Time (GMT): 2014/076/04:04:32
458
Vector Time (MET): N/A
Weight (LBS) : 901433
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6466937
28 A = 6796220
49 meter
Y = 23066
60 meter E =
0007163
Z = -2074591
80 I = 51
56874
XDOT = -1789
597423 Wp = 355
15738
YDOT = -4996
238310 meter/sec RA = 194
54233 deg
ZDOT = 5528
580274 TA = 341
89158
MA = 341
91708
Ha = 224
412 n
mi
Hp = 221
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21216985
84 X = -6456636
91
Y = 75677
83 feet Y = -49193
58 meter
Z = -6806403
54 Z = -2105982
16
XDOT = -5871
382623 XDOT = -1760
451348
YDOT = -16391
857974 feet/sec YDOT = -5016
086872 meter/sec
ZDOT = 18138
386726 ZDOT = 5519
958295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12091902
81 X = 3685611
98
Y = -17381878
06 feet Y = -5297996
43 meter
Z = -6938987
40 Z = -2115003
36
XDOT = 15589
206333 XDOT = 4751
590090
YDOT = 3625
263115 feet/sec YDOT = 1104
980197 meter/sec
ZDOT = 18102
630432 ZDOT = 5517
681756
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 14076
17400954
00016717 00000-0 10270-3 0 9128
2 25544 51
6504 195
6360 0005428 295
6446 64
4144 15
51111817 37057
Satellite: ISS
Catalog Number: 25544
Epoch time: 14076
17400954 = yrday
fracday
Element set: 912
Inclination: 51
6504 deg
RA of node: 195
6360 deg
Eccentricity:
0005428
Arg of perigee: 295
6446 deg
Mean anomaly: 64
4144 deg
Mean motion: 15
51111817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3705
Checksum: 299
Coasting Arc #14 (Orbit 3720)
---------------------------------------
Vector Time (GMT): 2014/077/04:04:32
458
Vector Time (MET): N/A
Weight (LBS) : 901433
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6650608
00 A = 6797186
28 meter
Y = 10072
28 meter E =
0008511
Z = 1384166
99 I = 51
60233
XDOT = 1204
035724 Wp = 119
42674
YDOT = 4863
037552 meter/sec RA = 189
58081 deg
ZDOT = -5797
690330 TA = 45
50373
MA = 45
43419
Ha = 224
611 n
mi
Hp = 221
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21819580
04 X = 6643277
23
Y = 33045
55 feet Y = 84402
88 meter
Z = 4541230
28 Z = 1416456
92
XDOT = 3950
248439 XDOT = 1177
730002
YDOT = 15954
847612 feet/sec YDOT = 4876
353867 meter/sec
ZDOT = -19021
293733 ZDOT = -5791
905941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12226323
80 X = -3726583
50
Y = 18037594
74 feet Y = 5497858
88 meter
Z = 4677619
07 Z = 1425738
29
XDOT = -14181
892840 XDOT = -4322
640938
YDOT = -4667
441066 feet/sec YDOT = -1422
636037 meter/sec
ZDOT = -18997
502487 ZDOT = -5790
438758
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 14077
20483213
00016717 00000-0 10270-3 0 9133
2 25544 51
6503 190
5214 0005313 299
4805 60
5816 15
51134995 37215
Satellite: ISS
Catalog Number: 25544
Epoch time: 14077
20483213 = yrday
fracday
Element set: 913
Inclination: 51
6503 deg
RA of node: 190
5214 deg
Eccentricity:
0005313
Arg of perigee: 299
4805 deg
Mean anomaly: 60
5816 deg
Mean motion: 15
51134995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3721
Checksum: 292
Coasting Arc #15 (Orbit 3735)
---------------------------------------
Vector Time (GMT): 2014/078/04:04:32
458
Vector Time (MET): N/A
Weight (LBS) : 901433
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6757250
22 A = 6797602
85 meter
Y = -14968
84 meter E =
0011367
Z = -668812
37 I = 51
63463
XDOT = -576
814053 Wp = 11
52477
YDOT = -4782
513671 meter/sec RA = 184
62069 deg
ZDOT = 5963
191851 TA = 341
25862
MA = 341
30044
Ha = 224
651 n
mi
Hp = 220
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22169456
09 X = -6753331
73
Y = -49110
36 feet Y = -90510
93 meter
Z = -2194266
30 Z = -701628
74
XDOT = -1892
434558 XDOT = -552
259425
YDOT = -15690
661649 feet/sec YDOT = -4788
825833 meter/sec
ZDOT = 19564
277725 ZDOT = 5960
450082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12126401
24 X = 3696127
10
Y = -18542114
79 feet Y = -5651636
59 meter
Z = -2332889
19 Z = -711064
62
XDOT = 12896
366487 XDOT = 3930
812505
YDOT = 5985
033791 feet/sec YDOT = 1824
238300 meter/sec
ZDOT = 19553
327970 ZDOT = 5959
854365
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 14078
17119561
00016717 00000-0 10270-3 0 9143
2 25544 51
6498 185
7250 0005561 304
3696 55
6929 15
51213391 37367
Satellite: ISS
Catalog Number: 25544
Epoch time: 14078
17119561 = yrday
fracday
Element set: 914
Inclination: 51
6498 deg
RA of node: 185
7250 deg
Eccentricity:
0005561
Arg of perigee: 304
3696 deg
Mean anomaly: 55
6929 deg
Mean motion: 15
51213391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3736
Checksum: 324
Coasting Arc #16 (Orbit 3751)
---------------------------------------
Vector Time (GMT): 2014/079/04:04:32
458
Vector Time (MET): N/A
Weight (LBS) : 901433
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6793600
93 A = 6797775
68 meter
Y = 34283
80 meter E =
0006570
Z = -93683
41 I = 51
66578
XDOT = -103
633308 Wp = 141
40617
YDOT = 4751
924973 meter/sec RA = 179
66438 deg
ZDOT = -6008
727604 TA = 39
60104
MA = 39
55307
Ha = 224
800 n
mi
Hp = 220
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22288716
98 X = 6793167
73
Y = 112479
67 feet Y = 110251
77 meter
Z = -307360
26 Z = -60681
93
XDOT = -340
004290 XDOT = -127
574064
YDOT = 15590
305028 feet/sec YDOT = 4750
631463 meter/sec
ZDOT = -19713
673242 ZDOT = -6009
289791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11930816
54 X = -3636512
88
Y = 18828739
67 feet Y = 5738999
85 meter
Z = -167945
22 Z = -51189
70
XDOT = -11721
617357 XDOT = -3572
748971
YDOT = -7590
803109 feet/sec YDOT = -2313
676788 meter/sec
ZDOT = -19716
679053 ZDOT = -6009
643775
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 14079
20195324
00016717 00000-0 10270-3 0 9150
2 25544 51
6493 180
6099 0005498 307
6635 52
4017 15
51225965 37526
Satellite: ISS
Catalog Number: 25544
Epoch time: 14079
20195324 = yrday
fracday
Element set: 915
Inclination: 51
6493 deg
RA of node: 180
6099 deg
Eccentricity:
0005498
Arg of perigee: 307
6635 deg
Mean anomaly: 52
4017 deg
Mean motion: 15
51225965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3752
Checksum: 320
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