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Inclined orbit
Analysis of Perturbations and Station-Keeping Requirements in Highly-Inclined Geosynchronous Orbits
Astrodynamics
Small Satellites in Inclined Orbits to Increase Observation Capability Feasibility Analysis
Open Rosen Thesis.Pdf
Single Axis Tracking with the RC1500B the Apparent Motion Of
Measurement Techniques and New Technologies for Satellite Monitoring
P.Roceedings
Computing GPS Satellite Velocity and Acceleration from the Broadcast
This Article Presents the Rudiments of Constellation Design to Familiarize
University of Cincinnati
For Earth Applications
Tracking Techniques for Inclined Orbit Satellites
Demonstration of the COBRA Teardrop Concept Using Two Smallsats in 8-Hour Elliptic Orbits
The Benefits of Inclined-Orbit Operations for Geostationary Orbit Communication Satellites
5 Orbit and Ground Track of a Satellite
Software Design for a Cubesat's Orbit Simulator
A Satellite Footprint Visualisation Tool
A Non-Hohmann Method for Orbital Element Database Pre-Processing
Top View
Satellite Orbit and Ephemeris Determination Using Inter Satellite Links
From Order to Chaos in Earth Satellite Orbits
Satellite Mod 1
Optimization of Electric Propulsion Orbit Raising
Satellite Orbits Orbit Classification
Towards a Satellite System for Archaeology?
Very Low Earth Orbit (VLEO) Satellite Communication Link
Method and Apparatus for Inclined Orbit Attitude Control for Momentum Bias Spacecraft
Evolution in Binary and Triple Stars, with an Application to SS
Inclined Satellite Orbits and Resulting Ground Station Network Solutions for Near Equatorial Areas
T3icsr?- Ir; <Geor9ia Inst- °F
Satellite Toolkit (Cap-Stk) Aerospace Program
Geosynchronous Inclined Orbits for High-Latitude Communications
Spatial Formation of High Inclined Orbits with Use of Gravity Assists
Determination of Coverage Oscillation for Inclined Communication Satellite
ABSTRACT the TILTS and SPINS of PLANETS and MOONS Zeeve
On Ultimately the Most Highly Inclined, the Most Consice Solar Polar Trajectory with Practically the Shortest Period
Appendix – Ephemeris Tracking Option
Satellite Orbit and Ephemeris Determination Using Inter Satellite Links
On the Dynamics and Collisional Growth of Planetesimals In
L1/L5 SBAS MOPS Ephemeris Message to Support Multiple Orbit Classes
Numerical Model for the Orbit of the Earth
A Systematic Approach to Station-Keeping of Constellations of Satellites by Brian Kantsiper
4.1.5 Maneuvering in Space
THE DRIFT of an INCLINED-ORBIT 24-HOUR SATELLITE in an EARTH GRAVITY FIELD THROUGH FOURTH ORDER TECH LIBRARY KAFB, NM I111111 11111 Lllll Lllll Illlll1llll Ill1 Ill1
Celestial Mechanics and Satellite Orbits Introduction to Space
An Analytical and Numerical Treatment of Inclined Elliptical Orbits About a Kerr Black Hole
ITU/ITSO Workshop
Spacecraft Propulsion, Launch and Orbit Design Rocket Scientists Gift to Exoplanet Scientists
Sun-Synchronous Orbits
Space-Based Observations
Advantages of a Continuous Thrust Strategy from a Geosynchronous Transfer Orbit, Using High Specific Impulse Thrusters
Global Coverage 24Hr Per Day from Inclined Circular Orbits
NIAC 2016 Phase I Janson Brane Craft Final Report
Orbital Mechanics
Appendix A: Useful Data
Orbit Determination Using Vinti's Solution Steven P