AIST 2

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AIST 2 is classified as:

NORAD ID: 39133

Int'l Code: 2013-015D

Perigee: 529.1 km

Apogee: 540.4 km

Inclination: 64.9 °

Period: 95.2 minutes

Semi major axis: 6905 km

RCS: 0.324 m² (medium)

Launch date: April 19, 2013
Source: Commonwealth of Independent States (former USSR) (CIS)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

Uplink (MHz):
Downlink (MHz): 435.215
Beacon (MHz): 435.265
Mode: FM CW
Call sign:
Status: Inactive

Uplink (MHz):
Downlink (MHz): 435.215
Beacon (MHz): 435.215/435.265
Mode: CW
Call sign:
Status: Inactive

AIST is a russian microsatellite developed by designed by a group of students, postgraduates and scientists of Samara Aerospace University in cooperation with TsSKB Progress. The satellite will measure the geomagnetic field, test the new small space vehicle bus, test methods to decrease microaccelerations to a minimum level and measure micrometeoroids of natural and artificial origin.

1 39133U 13015D   24140.55971724  .00009545  00000-0  55036-3 0  9995
2 39133  64.8716 194.3489 0008223 302.9433  57.0899 15.12820850608598

Source of the keplerian elements: Caltech