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@Einstein100, actually, the apogee should be from 20,000km to 24,000km ASL. The perigee should be what it was.
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@Einstein100, if you can, apogee: 100,000km ASL, perigee: 1,000km ASL. Inclination so that it doesn't collide with the other payload. If it's too difficult, then any orbit will do.
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This is perfect! Will launch as secondary payload on Aurora Mission-1 NET February 4.
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@VectronTechnologies, other payload is going to a heliocentric orbit. Should be well clear of yours. I think that’ll work.