Showing default

OPTSAT 3000, 42900

Orbit data source: Public

OPTSAT 3000, 42900 is a payload satellite owned by M.d. Difesa (IT) that was launched on Wed, 02 Aug 2017 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/42900?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/42900?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

Max 10 NORAD IDs; Separated by commas

Initial load time (optional)

ISO8601 Format

TLE date request (optional)

ISO8601 Format

Identifier

42900, 2017-044A

Orbit

Unknown

Last TLE update

Unknown

Origin

Ministry of Defense, Defense Administration (IT)

Manufacturer

IAI

Mission

Operational Defense Imaging

Bus & Motor

'OFEQ, AOCS

Mass

368 kg wet, ~350 kg dry

Launch date (UTC)

2017-08-02 (8 years ago)

Launch vehicle

VEGA

Launch site

French Guiana (FRGUI)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 4.5 m

Radar Cross Section

5.873 m²

Expand to show TLE details & history

Historical TLE search

Format must be ISO8601 or YYYY-MM-DD

Definitive object data

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

True Right ascension

Unknown

True Declination

Unknown

Sunlit

N/A

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.