SDS-4

SDS-4
Mission typeTechnology
OperatorJAXA
COSPAR ID2012-025C Edit this at Wikidata
SATCAT no.38339
Spacecraft properties
Spacecraft typeSDS
Launch mass50 kilograms (110 lb)
Start of mission
Launch date17 May 2012, 16:39 (2012-05-17UTC16:39Z) UTC
RocketH-IIA 202
Launch siteTanegashima Yoshinobu 1
ContractorMitsubishi
End of mission
Deactivated1 July 2021 (2021-08)
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude666 kilometres (414 mi)
Apogee altitude678 kilometres (421 mi)
Inclination98.23 degrees
Period98.05 minutes
Epoch30 October 2013, 08:31:20 UTC

SDS-4 (Small Demonstration Satellite 4) is a small satellite (50 cm cube with mass of 50 kg) developed by JAXA. It was launched as a secondary payload on the Shizuku mission on 17 May 2012 UTC.

In 2019, its ownership was transferred to the SKY Perfect JSAT Corporation (JSAT). Operation was terminated by the end of June 2021.

There are four rather specialised systems on the satellite:

References

  1. ↑ Krebs, Gunter. "SDS 4". Gunter's Space Page. Retrieved 31 October 2013.
  2. ↑ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 31 October 2013.
  3. ↑ "SDS-4 Satellite details 2012-025C NORAD 38339". N2YO. 30 October 2013. Retrieved 31 October 2013.
  4. ↑ "Small Demonstration Satellite-4 (SDS-4)". JAXA. Retrieved 3 December 2019.
  5. ↑ "JAXA and SKY Perfect JSAT Conclude an Agreement on the Transfer of the Small Demonstration Satellite-4". JAXA. 24 April 2019. Retrieved 3 December 2019.
  6. ↑ 2022年3月期 第1四半期 決算説明会 (PDF) (in Japanese). SKY Perfect JSAT Holdings Inc. 4 August 2021. Retrieved 7 August 2021.
  7. ↑ "In-flight thermal coatings ageing on the THERME experiment" (PDF).