This articlerelies largely or entirely on asingle source. Relevant discussion may be found on thetalk page. Please helpimprove this article byintroducing citations to additional sources. Find sources: "Flock-1" – news ·newspapers ·books ·scholar ·JSTOR(December 2015) |
| Mission type | Earth imaging |
|---|---|
| Operator | Planet Labs |
| Website | www |
| Spacecraft properties | |
| Spacecraft type | CubeSat |
| Bus | Dove |
| Launch mass | 5 kg (11 lb) |
| Dimensions | 10 cm × 10 cm × 30 cm (3.9 in × 3.9 in × 11.8 in) (3U) |
| Power | 20 watts |
| Orbital parameters | |
| Reference system | Geocentric orbit |
| Regime | Low Earth orbit |
| Inclination | 51.66° |
Flock-1 is aCubeSatsatellite constellation launched on 9 January2014. The satellite is built in aCubeSat bus, and each constellation consists of 28 satellites.All instruments are powered bysolar cells mounted on the spacecraft body, along with triple-folded wings, providing approximately 20 watts at maximal power.
Flock-1 constellation was launched fromMid-Atlantic Regional Spaceport Launch Pad 0,Wallops Island, on 9 January 2014 by anAntares 120 rocket. The satellites were deployed from theInternational Space Station (ISS) from 11 February 2014 to 28 February 2014.[1]
Another Flock start in January 2015 on aFalcon 9launch vehicle.
The satellite is intended for commercialEarth observation service. For this purpose, each satellite is equipped with a camera capable of 3 to 5 m (9.8 to 16.4 ft) ground resolution. Details of intended service by individual satellites were never released publicly and are largely unknown.
This article about one or more spacecraft of the United States is astub. You can help Wikipedia byexpanding it. |