Mission record
Mars Pathfinder
Also known as MESUR Pathfinder, Carl Sagan Memorial Station, Pathfinder, MarsPathfinder
NASA-Office of Space Science · Launched
Explore trajectoryCompleted · Success
The Mars Pathfinder was the second of NASA's low-cost planetary Discovery missions to be launched. The mission consists of a stationary lander and a surface rover, and had the primary objective of demonstrating the feasibility of low-cost landings on and exploration of the Martian surface. The spacecraft entered the Martian atmosphere on 4 July 1997 directly from its approach hyperbola at about 7300 m/s according to NSSDCA; NASA PDS describes the entry-capsule speed as 7.6 km/s. These source values are kept attributed because their exact state epochs are not reconciled. It did not go into orbit around Mars, and the airbag-encased lander bounced about 12 meters into the air, bouncing at least another 15 times and rolling before coming to rest. Images were taken and experiments performed by the lander and rover until 27 September 1997 when communications were lost for unknown reasons. The lander has been named the Sagan Memorial Station.
- Destinations
- Launch vehicle
- Delta II 7925
- Launch site
- Cape Canaveral, United States
- Countries
- United States
- Mission types
- Lander, Rover
Chronology
Mission timeline
Launch
Launched on a Delta II 7925
Mars Pathfinder was launched on a Delta 7925 (a Delta II Lite launch vehicle with nine strap-on solid-rocket boosters and a Star 48 (PAM-D) third stage) at 6:58:00 UT (1:58 a.m. EST) on 4 December 1996, and the launch/orbital information page gives the same instant as 1996-12-04T06:58:00Z. That page also prints Decay Date: 1996-07-04, five months before the launch it prints at the head of the same page and one year before the 4 July 1997 landing; the wrong value is recorded rather than repaired, and this record takes the landing date from the master catalog page. NASA PDS independently gives 6:58 am UTC and launch complex 17B, agreeing at minute precision.
EarthLanding
Bounced to a stop in Ares Vallis
The lander dropped to the ground in 3.8 seconds and impacted at 16:56:55 UT (12:56:55 p.m. EDT) on 4 July 1997 at a velocity of 18 m/s and bounced about 12 meters (40 feet) into the air, bouncing at least another 15 times and rolling before coming to rest approximately 2.5 minutes after impact and about 1 km from the initial impact site. The launch/orbital information page places the lander at Latitude: 19.330 degrees, Longitude: 33.550 degrees with an epoch beginning 1997-07-04 16:56:00, one round minute before the second-precision time the master catalog page prints. The PDS IMP dataset identifies 19.17° N, 33.21° W as the USGS cartographic solution and 19.30° N, 33.52° W as the two-way-ranging/Doppler inertial solution. The PDS mission description uses the cartographic coordinate and says the lander came to rest about 12 miles southwest of the target. NSSDCA reports 19.330° N, 33.550° W and about 1 km from initial impact; its coordinate relation to the PDS solutions is not established, so the values and reference points remain separate.
MarsDeployment
Sojourner rolled onto the surface
After some maneuvers to clear an airbag out of the way, ramps were deployed and the rover, stowed against one of the petals, rolled onto the surface on 6 July at about 05:40 UT (1:40 a.m. EDT). NSSDCA gives the rover its own page under the name Sojourner Rover, which this record models as a vehicle of the lander rather than as a mission of its own. GCAT deepcat gives the rover as D00734, Name Sojourner, PLName MFEX Rover, parent D00727, and the cruise stage as D00729, which is where this record's third vehicle comes from. NASA PDS separately dates rover deployment at 05:37 UTC; NSSDCA describes rolling onto the surface at about 05:40 UT. The three-minute source time difference is retained unresolved.
MarsLoss of contact
Communications lost for unknown reasons
Images were taken and experiments performed by the lander and rover until 27 September 1997 when communications were lost for unknown reasons. The landing site in the Ares Vallis region of Mars is at 19.33 N, 33.55 W. The lander has been named the Sagan Memorial Station. NASA PDS says the final science data arrived on 27 September and suggests a dead battery combined with increasing winter cold; NSSDCA describes the communications loss as for unknown reasons. The cause remains an attributed hypothesis.
Mars
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.
- Mars Pathfinder cruise navigation states: Reconstructed to 23 Jun; predicted afterward · February 4, 1997 to July 4, 1997
Provenance
Sources
Each source is listed once and labeled with the mission, event, trajectory, or destination/body context it supports.
Data verified through October 6, 2026
- Mars Pathfinder - NSSDCA Master Catalog (spacecraft 1996-068A), archived snapshot — NSSDCAArchive · Supports: mission claims · event claims
- Mars Pathfinder - NSSDCA launch/orbital information (1996-068A), archived snapshot — NSSDCAArchive · Supports: mission claims · event claims
- Chronology of Mars Exploration - NASA NSSDCA, archived snapshot — NSSDCAArchive · Supports: mission claims · event claims
- GCAT: General Catalog of Artificial Space Objects (deep-space catalog), J. McDowell — OTHEROther · Supports: mission claims · event claims
- Mars Pathfinder ASI/MET Derived EDL Profiles (PDS MPFL-M-ASIMET-4-DDR-EDL-V1.0) — NASAArchive · Supports: mission claims
- Mars Pathfinder Project: Planetary Constants and Models (JPL D-12947) — NASATechnical document · Supports: mission claims
- Mars Pathfinder EDL Trajectory and Atmosphere Reconstruction Using NewSTEP (NASA/TM-20260002020) — NASAMission page · Supports: mission claims
- Mars Pathfinder spacecraft-clock and leap-second SPICE kernels — NAIFSpice · Supports: mission claims
- Navigation Flight Operations for Mars Pathfinder (AAS 98-145) — JPLTechnical document · Supports: mission claims
- JPL Horizons planetary mass parameters, DE440-compatible GM kernel — JPLSpice · Supports: mission claims
- Mars Pathfinder Mission Description (NASA PDS) — NASAMission page · Supports: mission claims · event claims
- Mars Pathfinder IMP EDR Data Set Description: Landing Site Coordinate Solutions — JPLArchive · Supports: mission claims · event claims
- Mars Pathfinder Cruise Trajectory Tracking Data SPK (mpf_crus.bsp) — NAIFSpice · Supports: mission claims
- Mars Pathfinder Radio Tracking Data Set (PDS) — NASAArchive · Supports: mission claims
- Planet Sizes and Locations in Our Solar System — NASAOther · Supports: destination/body context