Foresail-2 Orbital Lifetime Analysis

The dataset has been created with the following inputs for DRAMAs CROC. Inputs for DRAMA Outputs for DRAMA Orbital elements CROC Inclination 15 ° F3. Randomly tumbling satellite RAAN 0 ° Average cross section for 6U 0.170 m^2 Argument of perigee 0 ° Minimum Cross Section 0.028 m^2 Drag coefficient 2.2 N/A Maximum Cross Section 0.268 m^2 SRP coefficient 1.3 N/A Orbit Predigtion Update 08.02.2023 6U CubeSat with 2 folding panel + boom Dry mass 14 kg Main body dimensions 0.11x0.34x0.25 m^3 Solar Panel X+ 0.007x0.34x0.25 m^3 Solar Panel X- 0.007x0.34x0.25 m^3 Extended boom dimensions 0.07x0.68x0.01 m^3 Magnetometer dimensions 0.05x0.05x0.05 m^3 OSCAR simulations have been conducted with orbits with apogee varying from 15000 km to 65000 km in 5000 km steps.<br> The perigee has been varied for every apogee height from 250 km to 400 km in 50 km steps.<br> Every simulation has been done for 4 different launch dates: 21.03.2025 12:00:00 Spring 21.06.2025 12:00:00 Summer 21.09.2025 12:00:00 Autumn 21.12.2025 12:00:00 Winter If not specified otherwise all settings in DRAMA have been kept to the default values.