An article in apogee at an distance of beneath than almost 200 km is advised ambiguous due to atmospheric drag. For a accessory to be in a abiding apogee (i.e. acceptable for added than a few months), 350 km is a added accepted distance for low Earth orbit. For example, on 1958-02-01 the Explorer 1 accessory was launched into an apogee with a apogee of 358 kilometers (222 mi).[1] It remained in apogee for added than 12 years afore its atmospheric reentry over the Pacific Ocean on 1970-03-31.
However, the exact behaviour of altar in apogee depends on altitude, their ballistic coefficient, and capacity of amplitude acclimate which can affect the acme of the high atmosphere.
However, the exact behaviour of altar in apogee depends on altitude, their ballistic coefficient, and capacity of amplitude acclimate which can affect the acme of the high atmosphere.
No comments:
Post a Comment