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  • IAC-25
  • A6
  • 9
  • session 9

    Title

    Orbit Determination and Propagation - SST

    type

    oral

    Description

    This session will address every aspect of orbit determination coming from the SST (Space Surveillance and Tracking), related to assessment of raw and derived data accuracy, optical measurements processing and modelling and risk analysis of space debris.

    Date

    2025-10-01

    Time

    10:15

    Room

    Room C4.10

    IPC members
    • Co-Chair: Dr. Darren McKnight, LeoLabs, United States;

    • Co-Chair: Dr. Paolo Marzioli, Sapienza University of Rome, Italy;

    • Rapporteur: Mr. Juan Carlos Dolado Perez, Centre National d'Etudes Spatiales (CNES), France;

    • Rapporteur: Dr. Jan Siminski, ESA - European Space Agency, Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    An Analysis of Bounds and Stability in Lunar Debris Destinations

    15

    Mr. Patrick Miga

    Advanced Space

    United States

    2

    10:30

    Maintaining the resonance mode to ensure orbit degradation for an object belonging to the Global Positioning System

    15

    Dr. Dmitriy Grishko

    Bauman Moscow State Technical University

    Russian Federation

    3

    10:45

    High-Fidelity Simulation of Orbital Forces and Torques

    15

    Mr. Valerio Levi

    GMV GmbH

    Germany

    4

    11:00

    Interpolation of the gravitational field and atmosphere of the Earth in the problem of orbit refinement

    15

    Mr. Ivan Khripunov

    Moscow Institute of Physics and Technology (MIPT)

    Russian Federation

    5

    11:15

    Probabilistic Tracklet Clustering and Initial Orbit Determination

    15

    Mr. Yihang Jiang

    Beijing Institude of technology

    China

    6

    11:30

    Constrained Admissible Region Multi Hypothesis Filter for Initial Orbit Determination using Optical Observations

    15

    Dr. Simone Varanese

    Sapienza University of Rome

    Italy

    7

    11:45

    Deep Extended Kalman Filter for State Estimation for Satellite Constellations

    15

    Mr. Francisco Caldas

    Faculdade de Ciências e Tecnologia - UNL

    Portugal

    8

    12:00

    data-driven orbit determination for low-earth orbit space debris using ground-based measurements

    15

    confirmed

    Mr. Hanyu Liu

    Beihang University

    China

    9

    12:15

    Data fusion for a space catalog with heterogeneous sensor data rate

    15

    Dr. Emmanuel Delande

    Centre National d'Etudes Spatiales (CNES)

    France

    10

    12:30

    Characterising Satellite conjunction "Walk-Ins" for enhanced collision prediction and spaceflight safety

    15

    Dr. Anne Bettens

    Deneb Space

    Australia

    1*

    10:15

    Predictive Framework for Space Debris Trajectory Forecasting and Collision Avoidance

    15

    Mr. Aidan Correa

    Australia

    2*

    10:30

    orbital decay prediction for low earth orbit satellites using a single two line element

    15

    Mr. MINSUP JEON

    UZURO Tech Inc.

    Korea, Republic of

    3*

    10:45

    Novel Approaches to Computation of State Error Covariance Matrix for Near-Earth Objects

    15

    Mr. Ilya Fukin

    Moscow Institute of Physics and Technology (MIPT)

    Russian Federation