Was sind Perihel und Aphel der zweiten Stufe der Falcon Heavy, die den Tesla enthält, nach der gestrigen Mission?
Es scheint, dass Musks Tweet fehlerhaft war und das Aphel der Umlaufbahn näher bei 1,71 AE statt bei 2,61 AE liegt. Siehe Jonathan McDowells Tweet .
Dies stimmt mit der Umlaufbahnprojektion überein, die jetzt in JPLs Horizonten gezeigt wird :QR= 9.86...E-01 & AD= 1.711...
2458158.500000000 = A.D. 2018-Feb-09 00:00:00.0000 TDB
EC= 2.688810432654559E-01 QR= 9.860573082453878E-01 IN= 1.101912591245855E+00
OM= 3.175070416981074E+02 W = 1.772620363138233E+02 Tp= 2458153.729308890179
N = 6.292640287243981E-01 MA= 3.002024307551933E+00 TA= 5.405918374698258E+00
A = 1.348696130995557E+00 AD= 1.711334953745726E+00 PR= 5.720968998176613E+02
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
JDTDB Julian Day Number, Barycentric Dynamical Time
EC Eccentricity, e
QR Periapsis distance, q (au)
IN Inclination w.r.t XY-plane, i (degrees)
OM Longitude of Ascending Node, OMEGA, (degrees)
W Argument of Perifocus, w (degrees)
Tp Time of periapsis (Julian Day Number)
N Mean motion, n (degrees/day)
MA Mean anomaly, M (degrees)
TA True anomaly, nu (degrees)
A Semi-major axis, a (au)
AD Apoapsis distance (au)
PR Sidereal orbit period (day)
Die Überschrift erklärt, dass die Datenquelle die Telemetrie der 3. Stufe selbst ist, die von ihrem GPS und anderen internen Daten abgeleitet wird:
Revised: Feb 07, 2018 Tesla Roadster (spacecraft) -143205
Tesla Roadster (Starman, 2018-017A)
Dummy payload from first launch of SpaceX Falcon Heavy launch vehicle
consisting of a standard Tesla Roadster automobile and a spacesuit-wearing
mannequin nicknamed Starman.
Also includes a Hot Wheels toy model Roadster on the car's dash with a
mini-Starman inside. A data storage device placed inside the car contains
a copy of Isaac Asimov's "Foundation" novels. A plaque on the attachment
fitting between the Falcon Heavy upper stage and the Tesla is etched with
the names of more than 6,000 SpaceX employees.
After orbiting the Earth for 6 hours, a third-stage burn-to-depletion
was completed at approximately 02:30 UTC Feb 7, placing the dummy payload
in a heliocentric orbit having a perihelion of 0.99 au and aphelion
~1.7 au.
Payload mass: ~1250 Kg
This trajectory is a ballistic propagation derived from a post-injection
state provided by SpaceX on 2018-Feb-7, and is based on internal GPS data.
Prediction errors could increase significantly over time due to unmodeled
solar presure, thermal radiation, or outgassing accelerations that are not
characterized.
Launched: 2018-Feb-06 20:45 UTC by Falcon Heavy (FH) from Kennedy Space
Center, USA (launchpad 39A)
0,98 AU und 2,61 AU. Siehe diesen Tweet .
Peterh
Benutzer20636
äh