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PD0RDD > NASA 04.11.98 18:50l 99 Lines 3643 Bytes #-9820 (0) @ WW
BID : 36527_PI8WNO
Read: GUEST
Subj: Nasa Information 237
Path: DB0AAB<DB0ZKA<DB0ABH<DB0SRS<DB0SIF<DB0HSK<PI8DRS<PI8DAZ<PI8GCB<PI8WNO
Sent: 981104/1205Z @:PI8WNO.#UTR.NLD.EU #:36527 [DeMeern] FBB5.15c $:36527_PI8W
From: PD0RDD@PI8WNO.#UTR.NLD.EU
To : NASA@WW
Onderwerp: STS-95 TLEs and State Vector <Rev 08, Set 03>
STS-95
1 25519U 98064A 98303.29499903 .00000064 00000-0 45654-5 0 32
2 25519 28.4675 155.0990 0006799 40.2592 172.4387 15.03431416 86
Launch time for STS-95: 29 OCT 98 @ 19:19:34.064 UTC
Earth-Centered Inertial State Vector:
Vector format = 7
Satellite Name: STS-95
Catalog Number: 25519 98064A
Epoch Date/Time: 98303.29499902800
10/30/1998 07:04:47.916 UTC
ECI X: 6683.02239670831 km
Y: 537.383767550473 km
Z: -1788.8189999999 km
Xdot: -1.3579905169924 km/s
Ydot: 6.80856783565273 km/s
Zdot: -3.0406010000000 km/s
ndot/2 (drag): 0.00000063813 rev/day^2
nddt/6: 0.00000E+00 rev/day^3
Bstar: 4.56543E-06 1/Earth Radii
Elset #: 3
Rev @ Epoch: 8.59078494049
Keplerian Elements (Amsat format):
Satellite: STS-95
Catalog number: 25519
Epoch time: 98303.29499903
Element set: 3
Inclination: 28.4675 deg
RA of node: 155.0990 deg
Eccentricity: 0.0006799
Arg of perigee: 40.2592 deg
Mean anomaly: 172.4387 deg
Mean motion: 15.03431416 rev/day
Decay rate: 6.38130e-07 rev/day^2
Epoch rev: 8
Checksum: 321
Drag Factor is 0.1
SPACE SHUTTLE ORBITAL DATA:
These 2-line elements have been generated using Ken Ernandes' program
VEC2TLE using real time state vector data supplied by DOD C-Band
Radar Network courtesy Dave Simonson. Note that the epoch of the
2-line elements is the same as the state vector time.
Occasionally these elements are derived from the Goddard Space Flight
Center (GSFC) NASA Orbital Information Group (OIG), using Curtis
Haases' program VEC2VIF that formats the OIG vectors for use by
VEC2TLE.
The source of the data can be confirmed by the data format of the
vector ;
EFG, ft, ft/s = DOD C-Band Radar Network
ECI, km, km/s = NASA OIG RAID RBBS
ECI M50, ft, ft/s = Rockwell/Boeing Mission Support Room
Drag and B-Star parameters are internally calculated by VEC2TLE
using the drag factor. Rev numbers use NASA orbit numbering
convention.
David Cottle
-----------------------------------------------------
David Cottle
Director Of Engineering
IDB Communications.
Sydney, NSW, Australia.
-----------------------------------------------------
- Email Primary : dcottle@ozemail.com.au
- Email Backup : David_Cottle@compuserve.com
- W.W.W. Page : http://www.ozemail.com.au/~dcottle/
.
.
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