molniya orbit calculator:Orbital Period
Orbital Period
Examplesofellipticorbitsinclude:Hohmanntransferorbit,Molniyaorbitandtundraorbit.Relatedformulas.Variables.T,orbitalperiodofabodytraveling ...。其他文章還包含有:「Molniyaorbit」、「Molniya-2(11F628)」、「OntheuseofsatellitesinMolniyaorbitsformeteorological...」、「Orbitwizard」、「OrbitalMechanicsCalculator」、「OrbitalparametersforMolniyaorbit」、「ResonantOrbitCalculator(KerbalSpaceProgram)...
查看更多 離開網站Molniya orbit
https://en.wikipedia.org
A Molniya orbit is a type of satellite orbit designed to provide communications and remote sensing coverage over high latitudes. It is a highly elliptical ...
Molniya-2 (11F628)
https://space.skyrocket.de
The Molniya were Soviet communication satellites operating from an inclined highly elliptical earth orbit of 500 km × 40000 km with 12 hour ...
On the use of satellites in Molniya orbits for meteorological ...
https://cat.cira.colostate.edu
Orbit Calculations. Escobal (1965) gives the following formulae for the time rate of change of orbital elements in an orbit per- turbed by a quadrupole ...
Orbit wizard
https://www.mathworks.com
This application is a program for the calculation of Initial Conditions of Orbit (SSO, GSO, Molniya) through 6 Orbital Elements. There are ...
Orbital Mechanics Calculator
https://elainecoe.github.io
The average time between the Sun's successive passages over a given longitude. Molniya Orbit. A semi-synchronous, eccentric orbit used for specific ...
Orbital parameters for Molniya orbit
https://www.reddit.com
Orbital parameters for Molniya orbit ; Orbital period: 10800 seconds ; Semi-major axis: 2184.94km (from surface) ; Incclination: 63.4°.
Resonant Orbit Calculator (Kerbal Space Program)
https://meyerweb.com
Calculate the resonant orbit needed for a carrier craft to inject craft it carries, like satellites, into equidistant positions of a shared circular orbit. This ...
smallsats.org
https://smallsats.org
Solved For Molniya orbit (highly elliptical orbit with
https://www.chegg.com
For Molniya orbit (highly elliptical orbit with e (eccentricity)= 0.74 and a (semi-major axis length) = 26600 km, Calculate the orbital velocity ...