https://drive.google.com/file/d/1FOHCMS2ZaWeyLnv-y8o-3kAjpwJb_3jX/view?usp=sharing

https://docs.google.com/spreadsheets/d/1pyNE1mC56mU7OjntcM2SEyebWIaT6-NqtrAuEM1JbRo/edit?usp=sharing

Generally, "Active" is used to mean performing some task and drawing power, and "Inactive" means not drawing power

EPS isn't really split into active or inactive, it is assumed that the battery heater/management systems are always active in every mode

Assuming no antenna deployment is necessary, if we do decide to go with that a bunch of things might change

From https://www.issfd.org/ISSFD_2014/ISSFD24_Paper_S1-4_carrara.pdf,

https://phxcubesat.asu.edu/ConOps

Active Secondary Payload Mode (attitude is acceptable, comms/CDH active, both payloads are active, so we are in eclipse):

• Secondary Payload laser is switched on
• Primary payload camera is active (can both the payloads be active at the same time?)
• Solar panels are not receiving solar energy
• ADCS is not actively changing attitude (magnetorquers are inactive or minimally active, determination stuff is still active. Do we have reaction wheels?)
• Comms/CDH equipment might be communicating with the mission control/payload ground station
• Any moving mech parts will not be active (are there any moving mech parts?)

Active Primary Payload Mode (attitude is acceptable, comms/CDH active, primary payload is active, assumed in sunlight):