Showing default

ARCADE, 57485

Orbit data source: Public

ARCADE, 57485 is a payload satellite owned by NTU (SG) that was launched on Sun, 30 Jul 2023 UTC via a PSLV launch vehicle from the Sirharikota (SRI). 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/57485?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/57485?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

57485, 2023-109E

Orbit

Unknown

Last TLE update

Unknown

Origin

Nanyang Technological University (SG / SING)

Manufacturer

NTU

Mission

Operational Amateur Technology

Bus & Motor

CUBESAT 27U, Unknown motor

Mass

24 kg wet, 24 kg dry

Launch date (UTC)

2023-07-30 (2 years ago)

Launch vehicle

PSLV

Launch site

Sirharikota (SRI)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 0.9 m

Radar Cross Section

0.187 m², Medium (>0.1 m² and < 1m²)

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.