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The Optical Inter-orbit Communications Engineering Test Satellite (OICETS), also called Kirari, was an experimental satellite launched by JAXA to demonstrate interorbital communication between satellites through optical (laser) means. OICETS was originally slated for a launch on the second J-I launcher. Due to problems with that launcher, the launch had…
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satellite jaxa launch communications optical mission launched launcher dnepr links inter-orbit engineering test kirari 570 260 lb low earth rocket
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| OICETS | Apogee altitude | 612 km (380 mi) | 1.00 | infobox |
| OICETS | Contractor | ISC Kosmotras | 1.00 | infobox |
| OICETS | COSPAR ID | 2005-031A | 1.00 | infobox |
| OICETS | Deactivated | 24 September 2009, 05:48 (2009-09-24UTC05:49) UTC | 1.00 | infobox |
| OICETS | Dimensions | 0.78 × 1.1 × 1.5 m (2.6 × 3.6 × 4.9 ft) | 1.00 | infobox |
| OICETS | Disposal | Decommissioned | 1.00 | infobox |
| OICETS | Eccentricity | 0.00107 | 1.00 | infobox |
| OICETS | Epoch | 23 August 2005, 17:10:00 UTC | 1.00 | infobox |
| OICETS | Inclination | 97.8° | 1.00 | infobox |
| OICETS | Instruments | InstrumentsLUCELaser-Utilizing Communications EquipmentMVEMicro Vibration Equipment | 1.00 | infobox |
| OICETS | Launch date | 23 August 2005, 21:10 (2005-08-23UTC21:10) UTC | 1.00 | infobox |
| OICETS | Launch mass | 570 kg (1,260 lb) | 1.00 | infobox |
| OICETS | Launch site | Baikonur Pad 109/95 | 1.00 | infobox |
| OICETS | LUCE | Laser-Utilizing Communications Equipment | 1.00 | infobox |
| OICETS | Manufacturer | Toshiba | 1.00 | infobox |
| OICETS | Mission duration | Planned: 1 year Final: 4 years, 1 month | 1.00 | infobox |
| OICETS | Mission type | Technology demonstration | 1.00 | infobox |
| OICETS | MVE | Micro Vibration Equipment | 1.00 | infobox |
| OICETS | Names | OICETS, Kirari | 1.00 | infobox |
| OICETS | Operator | JAXA | 1.00 | infobox |
| OICETS | Perigee altitude | 597 km (371 mi) | 1.00 | infobox |
| OICETS | Period | 96.8 minutes | 1.00 | infobox |
| OICETS | Reference system | Geocentric | 1.00 | infobox |
| OICETS | Regime | Low Earth | 1.00 | infobox |
| OICETS | Rocket | Dnepr | 1.00 | infobox |
| OICETS | SATCAT no. | 28809 | 1.00 | infobox |
| OICETS | Website | global.jaxa.jp/projects/sat/oicets/index.html | 1.00 | infobox |
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