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Pointing Analysis and Design Drivers for Low Earth Orbit Satellite Quantum Key Distribution Jeremiah A
SATELLITES ORBIT ELEMENTS : EPHEMERIS, Keplerian ELEMENTS, STATE VECTORS
Orbital Mechanics
TLE-Tools's Documentation!
Orbital Mechanics Joe Spier, K6WAO – AMSAT Director for Education ARRL 100Th Centennial Educational Forum 1 History
Artifical Earth-Orbiting Satellites
Two-Line Element Estimation Using Machine Learning 3
Debris Assessment Software User’S Guide
Artificial Intelligence for All Vs. All Conjunction Screening
Mission Planning for Close-Proximity Satellites
AERO2705 – Week 3
A Satellite Footprint Visualisation Tool
Revisiting Spacetrack Report #3
Study of the Interlink Between Small Satellites in a Constellation
Hybrid SGP4 Propagator Based on Machine-Learning Techniques Applied to GALILEO-Type Orbits Juan F. San-Juana∗, Iván Pérezb
Appendix B Orbits
Black Box” RF Sat-Link for Space Debris, Mission Success and Risk Mitigation
Instanttrack 1.50 User Manual
Top View
Improved Ssa Through Orbit Determination of Two- Line Element Sets
Debris Assessment Software User’S Guide Version 2.1
Orbital Mechanics and Space Geometry
Debris Assessment Software User's Guide
Appendix – Ephemeris Tracking Option
Modeling, Simulation, and Characterization of Space Debris in Low-Earth Orbit Paul D
Technical and Economic Feasibility of Telerobotic On-Orbit Satellite Servicing
HISTORY of ON-ORBIT SATELLITE FRAGMENTATIONS 13Th Edition
Arxiv:1103.1690V3 [Physics.Space-Ph] 19 Jul 2011
Asterisk: Computation of Satellite Position
Odm-Spaceops-Presentation-2010
Refinded Study of Space Debris Collision Warning Techniques
AU-18 Space Primer
Software and Hardware Implements for Tracking Low Earth Orbit (LEO) Satellites Wassila Leila Rahal, Noureddine Banabadji, Ahmed Hafid Belbachir
Orbit Data Messages
Evolution of the Debris Cloud Generated by the Fengyun-1C Fragmentation Event
SGP4 Orbit Determination
Covariance Estimation and Autocorrelation of NORAD Two-Line Element Sets
Orbit Determinator Documentation Release 1.0.0
Predicting Simultaneous Nadir Overpasses Among Polar-Orbiting Meteorological Satellites for the Intersatellite Calibration of Radiometers
Masters Thesis: Maintenance of a Long Baseline Along-Track Formation for the Delffi Mission
An Investigation Into Satellite Drag Modeling Performance
Orbit Determination Using Vinti's Solution Steven P