STARS-2

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

STARS-2

Microsatellite from Kagawa University. Composed of two sections and a tether, deployed length 300 metres. Believed to have succeeded based on later orbital decay rate.

Status: Operational 2014. First Launch: 2014-02-27. Last Launch: 2014-02-27. Number: 1 . Gross mass: 22 kg (48 lb). Apogee: 178 km (110 mi).

Family: Technology. Country: Japan. Launch Vehicles: H-IIA 202. Launch Sites: Tanegashima Y.

2014 February 27 - . 18:37 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.

STARS-2 - . Mass: 22 kg (48 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft: STARS-2. Decay Date: 2014-05-18 . USAF Sat Cat: 39578 . COSPAR: 2014-009G. Apogee: 178 km (110 mi). Perigee: 164 km (101 mi). Inclination: 64.97 deg. Period: 87.91 min. Microsatellite from Kagawa University. Composed of two sections and a tether, deployed length 300 metres. Believed to have succeeded based on later orbital decay rate..

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z