Enhanced-color view of Phobos obtained by Mars Reconnaissance Orbiter on March 23 2008.
|Discovered by||Asaph Hall|
|Discovery date||August 18, 1877|
|Reference date J2000|
|Shortest distance from what it orbits||9235.6 km|
|Longest distance from what it orbits||9518.8 km|
|Longest distance from the center of its orbital path|
|How long it takes to complete an orbit||0.31891023 d|
(7 h 39.2 min)
|Average speed||2.138 km/s|
|Angle above the reference plane|
|1.093° (to Mars's equator)|
0.046° (to local Laplace plane)
26.04° (to the ecliptic)
|What it orbits||Mars|
|Size and other qualities|
|Measurements||26.8 × 22.4 × 18.4 km|
|Average radius||11.1 km|
|Surface area||~6100 km²|
|Average density||1.887 g/cm³|
|Surface gravity||0.0084–0.0019 m/s²|
|Escape velocity||11.3 m/s (40 km/h)|
|Turning speed||11.0 km/h (at longest axis' tips)|
|Angle at which it turns|
(in relation to its orbit)
|How much light it reflects||0.071|
|Avg. surface temp.||~233 K|
Phobos is trapped in tidal drag, with its orbit lowering roughly 1.8 meters per century. In about 50 million years, Phobos will reach the Roche limit, where it is likely to be torn apart. Some fragments will fall on Mars and some will form a planetary ring or rings around Mars.
The other moon, Deimos, is the smaller of the two.
Spacecraft[change | change source]
The Russians have sent at least two space craft to this moon, Phobos 1 and Phobos 2. Both failed or lost contact with Earth, but Phobos 2 managed to take some pictures of the moon before dying.
Features[change | change source]
There is one large crater on Phobos called Stickney. It is the size of the moon itself.
References[change | change source]
- NASA Celestia
- "Mars: Moons: Phobos". NASA Solar System Exploration. 2003-09-30. Retrieved 2008-08-18.
- "Planetary Satellite Physical Parameters". JPL (Solar System Dynamics). 2006-07-13. Retrieved 2008-01-29.
- "Mars Express closes in on the origin of Mars' larger moon". DLR. 2008-10-16. Retrieved 2008-10-16.
- use a spherical radius of 11.1 km; volume of a sphere * density of 1.877 g/cm³ yields a mass (m=d*v) of 1.07×1016 kg and an escape velocity (sqrt((2*g*m)/r)) of 11.3 m/s (40 km/h)
- "Classic Satellites of the Solar System". Observatorio ARVAL. Retrieved 2007-09-28.
- Gater, Will (2009). Space 3D. Bristol Magazines. p. 67.