Landing day · 🇺🇸 United States · Voyager Technologies (formerly Astrobotic)
Griffin Mission One
PlannedNobile crater region, near the south pole (target region; landing coordinates not published)
Facts last verified against primary sources on 2026-10-13. Mission page →
Launch
no earlier than Nov 2026Target
85.28°S 53.27°E
Target region (approximate) · 40 km radius
Landing
date not set
Launch no earlier than Nov 2026
Sun · today
+5.58°
NE (az 26°) · whole disk up
Earth · today
−0.42°
NW (az 303°) · Earth below the horizon
Target region (approximate)
2 km reference ring
Drag to turn · scroll to zoom
Site plan
North up, true scale around the target point. Arrows: where the Sun and the Earth sit on the horizon at the current time. The dashed outline is the named target region, not a landing ellipse: no ellipse is published.
The sky from the landing site
The landing date is not set yet, so this shows the next 30 days at the target. Predicted by JPL Horizons for a smooth Moon: hills and crater walls are not included, and near the poles they can hide a Sun that is a degree or two up.
- Sun up
- 63% of the window
- Next sunset
- 2026-10-30 14:00 UTC
- Earth up
- 62% of the window
- Earth elevation
- -3.8° to 9.0°
Source: JPL Horizons observer tables (DE441, Moon mean-Earth frame), Sun and Earth seen from 85.280°S 53.270°E at 0 m on the 1,737.4 km sphere, hourly, 2026-10-19 to 2026-11-18. “Sun up” means any part of the disk is above the smooth horizon. Method: landing-site sky.
Terrain-aware light and Earth view (Atlas)
Our data engine computes sunlight and Earth visibility with the real terrain horizon for 80°S–90°S. It has no value for this point yet, and a region center is not a landing pad anyway.
Engine plume: reference distances
- 155 mApollo 12 → Surveyor 3. Apollo 12 landed about 155 m from Surveyor 3, and its plume sandblasted the older lander. source
- 600 m1 cm gravel, Apollo-sized lander. Gravel 1 cm across leaves a Lunar Module–sized lander's plume at about 30 m/s and lands within 600 m; NASA gives up to about 1.5 km for 1–10 cm rocks. source
- 2 kmNASA heritage-site standoff. NASA recommends targeting touchdown at least 2 km from U.S. lander heritage sites (0.5 km from impact sites). source
No CLPS or Artemis lander has a published plume keep-out distance; these are reference cases, drawn around the target point, not limits for this lander. Fine dust leaves a plume at up to kilometres per second and is not stopped by any ring. No recorded hardware is within 2 km of the target point.
Hardware already nearby
- IM-2 AthenaIntuitive Machines · 2025 · hard landing64 km W
Great-circle distance from the target point on the 1,737.4 km sphere, to landing and impact sites in our curated table. The target is a region, so real distances can differ by tens of kilometres.
Landing-day timeline
- no earlier than Nov 2026Launch (Falcon Heavy), no earlier than November 2026 planned
Official livestream links appear here once the operator announces them. We link to streams; we never re-host them.