Completed · Success
NASA's Apollo 10 was a crewed mission to the Moon: the dress rehearsal for the first landing, taking the Lunar Module to within 15 km of the surface without landing.
- Destinations
- Launch vehicle
- Saturn 5
- Launch site
- Cape Canaveral, United States
- Countries
- United States
- Mission types
- Crewed, Orbiter
Chronology
Mission timeline
Launch
Apollo 10 launched
Mission report Table 3-I / Table 6-II, GET 00:00:00.6 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
EarthOrbit insertion
Parking orbit insertion
Mission report Table 3-I / Table 6-II, GET 00:11:53.8 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
EarthMilestone
Translunar injection completed
Mission report Table 3-I / Table 6-II, GET 02:39:20.5 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
EarthMilestone
Charlie Brown separated from the S-IVB
Mission report Table 3-I / Table 6-II, GET 03:02:42 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
EarthMilestone
Apollo 10 S-IVB separated from Charlie Brown
Adamo Table 12 gives CSM/S-IVB separation at 19:51:42 GMT; Table 13 defines the nominal S-IVB initial state at 19:51:42.4 GMT. The event timestamp retains only whole-second catalog precision; historical GMT-to-UTC realization is unresolved.
EarthMilestone
Charlie Brown docked with Snoopy
Mission report Table 3-I / Table 6-II, GET 03:17:37 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
EarthDeployment
Docked spacecraft extracted from the launch stage
Mission report Table 3-I / Table 6-II, GET 03:56:26 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
EarthMilestone
Mated CSM/LM ejected from the S-IVB
Adamo Table 12 reports GET 003:56:26 and GMT 20:45:26. The event falls within the reconstructed coast; the nominal source solution supplies no separately validated impulse state for the ejection.
EarthMilestone
Spacecraft separation maneuver
Mission report Table 3-I / Table 6-II, GET 04:39:10 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
EarthMilestone
Spacecraft separation maneuver cutoff
Mission report Table 6-II, GET 04:39:12.7 from range zero 1969-05-18 16:49:00 GMT.
EarthMilestone
Finite post-TLI S-IVB propulsive accelerations began
Adamo Table 12 gives the finite acceleration start. The nominal model replaces these finite accelerations with an impulse at 21:46 GMT; no states are published through the finite-burn interval.
EarthMilestone
Finite post-TLI S-IVB propulsive accelerations ended
Adamo Table 12 gives the finite acceleration end. The supported reconstructed coasts stop at 21:34:35 and resume at 22:18:06 GMT, leaving the documented event interval unsupported.
EarthMilestone
First midcourse correction
Mission report Table 6-II, GET 26:32:56.8 from range zero 1969-05-18 16:49:00 GMT.
EarthOrbit insertion
Lunar orbit insertion began
Mission report Table 3-I / Table 6-II, GET 75:55:54 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonFlyby
Apollo 10 S-IVB lunar pericynthion
Adamo Table 12 reports lunar pericynthion at 23:40:04 GMT on May 21 at 3,112 km altitude. This event is a reconstruction constraint, not an independently published state vector.
MoonMilestone
Lunar orbit circularization
Mission report Table 3-I / Table 6-II, GET 80:25:08 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Snoopy undocked for the lunar landing rehearsal
Mission report Table 3-I / Table 6-II, GET 98:11:57 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Snoopy entered the descent rehearsal orbit
Mission report Table 3-I / Table 6-II, GET 99:46:02 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Snoopy phasing maneuver
Mission report Table 3-I / Table 6-II, GET 100:58:26 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Snoopy jettisoned its descent stage
Mission report Table 3-I / Table 6-II, GET 102:45:17 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Snoopy ascent-stage insertion maneuver
Mission report Table 3-I / Table 6-II, GET 102:55:02 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Coelliptic sequence initiation
Mission report Table 3-I / Table 6-II, GET 103:45:55 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Constant differential height maneuver
Mission report Table 3-I / Table 6-II, GET 104:43:53 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Terminal rendezvous phase initiation
Mission report Table 3-I / Table 6-II, GET 105:22:56 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Snoopy ascent stage redocked with Charlie Brown
Mission report Table 3-I / Table 6-II, GET 106:22:02 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Snoopy ascent stage jettisoned after crew transfer
Mission report Table 3-I / Table 6-II, GET 108:24:36 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Snoopy final separation burn
Mission report Table 6-II, GET 108:43:23.3 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Snoopy ascent-engine depletion burn began
Mission report Table 6-II, GET 108:52:05.5 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Snoopy ascent-engine depletion burn ended
Mission report Table 6-II, GET 108:56:14.5 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonDeparture
Charlie Brown departed lunar orbit
Mission report Table 3-I / Table 6-II, GET 137:36:29 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
MoonMilestone
Earth-return midcourse correction
Mission report Table 3-I / Table 6-II, GET 188:49:58 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
EarthMilestone
Command module separated from service module
Mission report Table 3-I / Table 6-II, GET 191:33:26 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
EarthMilestone
Command module crossed entry interface
Mission report Table 3-I / Table 6-II, GET 191:48:55 from 1969-05-18 16:49:00 UTC. Fractional source seconds are retained in the lifecycle provenance.
EarthLanding
Apollo 10 splashed down in the Pacific Ocean
The 1969 mission report gives GET 192:03:23 (1652 GMT). It records the recovery-forces estimate as 15°02′ S, 164°39′ W; the onboard estimate at drogue deployment is 15°04.2′ S, 164°39′ W, and its best-estimated trajectory gives 15°03.6′ S, 164°39′ W. NASA's later mission-details page instead states 5°08′ S, 165° W, a discrepancy unresolved here. The descent stage was left in lunar orbit and was not tracked to impact.
Earth
Mission architecture
Vehicles
Trajectory record
Time-dependent navigation trajectory
Source states place the model at the selected time. Reconstructed flight, estimates, predictions and historical mission plans are identified by interval; gaps remain visible.
Source records and sampling assumptions are retained with the repository data. Model attitude and surface appearance are illustrative.
- Snoopy ascent stage (Apollo 10): Reconstructed · May 23, 1969 to May 28, 1969
- Apollo 10 S-IVB-505: Reconstructed · May 18, 1969 to May 29, 1969
- Charlie Brown (Apollo 10 CSM): Physically reconstructed based on publicly available data · May 18, 1969 to May 19, 1969
Provenance
Sources
Each source is listed once and labeled with the mission, event, trajectory, or destination/body context it supports.
Data verified through October 7, 2026
- Apollo 10 Command and Service Module - NASA NSSDCA Spacecraft Details — NSSDCAArchive · Supports: mission claims · event claims
- Apollo 10 Mission Report, MSC-00126, August 1969 — NASATechnical document · Supports: mission claims · event claims
- Apollo 10: Mission Details — NASAMission page · Supports: mission claims · event claims
- Earth Departure Trajectory Reconstruction of Apollo Program Components Undergoing Disposal in Interplanetary Space — OTHERPaper · Supports: mission claims · event claims
- JPL Horizons Apollo 10 S-IVB-505 reconstructed trajectory vectors — JPLEphemeris · Supports: mission claims
- DE421 lunar mean-Earth and principal-axes frame specification — NAIFTechnical document · Supports: destination/body context
- DE440 lunar mean-Earth and principal-axes frame specification — NAIFSpice · Supports: destination/body context
- IAU rotational elements and body radii (PCK 00011) — NAIFSpice · Supports: destination/body context
- LOLA global lunar height maps, LDEM_4 V3 original PDS source label — NASATechnical document · Supports: destination/body context
- LOLA 2023 south-polar elevation, uncertainty and effective-resolution maps — NASATechnical document · Supports: destination/body context
- Blue Ghost Lunar Lander Seen From Above: LROC site and terrain context — NASATechnical document · Supports: destination/body context
- Moon Facts — NASAOther · Supports: destination/body context
- SLDEM2015 Blue Ghost region: original PDS elevation-grid label — NASATechnical document · Supports: destination/body context
- JPL Solar System Dynamics Astrodynamic Parameters — JPLOther · Supports: destination/body context
- Planet Sizes and Locations in Our Solar System — NASAOther · Supports: destination/body context