A crescent Earth as seen from the Artemis II Orion Integrity spacecraft, now over 46,000 km away. The spacecraft is located above the north-east coast of Brazil, where it is night-time

22/n

The serene view of the Pale Blue Crescent from the Artemis II Orion Integrity spacecraft this morning, now located 70,920 km away in its elliptical orbit, high above the Pacific Ocean, west of Peru, as the astronauts grab some sleep after a hectic day yesterday.

https://www.youtube.com/watch?v=m3kR2KK8TEs
23/n

Integrity, the Artemis II Orion Integrity spacecraft, is located 71,245 km away, almost 2x the alt. of GSO, in a highly elliptical orbit, above the Pacific Ocean, west of Peru.

After reaching Apogee, it will turn around and execute a Perigee Raising Burn at around 8:15 a.m. EDT (12:15 UTC) and head back towards Earth.

12 hours later, at Perigee, it will execute the Translunar Injection Burn and shoot for the Moon.

https://www.n2yo.com/?s=99999&live=1
https://eyes.nasa.gov/apps/solar-system/#/sc_artemis_2
https://www.nasa.gov/artemis-ii-press-kit/
24/n

@AkaSci This means they’re out of the elliptical earth orbit and into lunar trajectory?
@photovince
No, not yet; take a look at new toot #24.
@AkaSci Thanks - just noticed. They are taking the scenic route for sure!

RE: https://f.cz/@xChaos/116333479114503737

@photovince
There is some energy optimization related reason for this orbit and trajectory. Also, unlike uncrewed missions, this spacecraft needs to head for the moon within a day or two after launch.

See post by @xChaos for some more info -

@AkaSci @xChaos Thanks! I remember reading about (reasons behind) complex trajectories a while ago, but that included the lunar gateway so n/a for now
@AkaSci Saw that this morning and it was a very serene view. 
@AkaSci For those not familiar with this, the next burn will be when Orion's elliptical orbit takes it close to the earth. The reason is that firing the engines for a fixed time will change its velocity by an amount Δv. For an initial velocity v, its kinetic energy will change to (1/2)m(v + Δv)² = (1/2)mv² + mvΔv + (1/2)m(Δv)². To reach the moon, you have to increase Orion's kinetic + potential energy, and the most efficient way to do that is when Orion's velocity is highest.