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cbassa/artemis_1_tle.txt

Created November 16, 2022 07:15
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Artemis 1 TLE estimates
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artemis_1_tle.txt
These are TLE estimates for the actual launch time of 2022-11-16T06:47:44.
Orbital elements have been estimated from the timeline and parameters by Jonathan
McDowell (https://planet4589.org/space/misc/artemis1.txt).
The TLE describing translunar orbit is only valid for the first 2 days after launch,
as TLEs do not properly model the influence of the Moon at large distances from Earth.
Parking orbit (valid until 2022-11-16T08:32UTC)
1 84001U 22320.31928241 .00000000 00000-0 50000-4 0 04
2 84001 34.0000 15.0000 1103405 21.0000 180.0000 13.71415011 08
Translunar orbit (valid from 2022-11-16T08:32UTC to 2022-11-18)
1 84002U 22320.35606481 .00000000 00000-0 00000-0 0 09
2 84002 34.0000 15.0000 9498617 21.0000 2.2000 0.13938693 02
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