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IGS R-8, 61439

Orbit data source: Public

IGS R-8, 61439 is a payload satellite owned by CSICE (JP) that was launched on Thu, 26 Sep 2024 UTC via an H-IIA 202 launch vehicle from the Tanegashima Space Center (TNSTA). 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/61439?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/61439?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

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ISO8601 Format

Identifier

61439, 2024-176A

Orbit

Unknown

Last TLE update

Unknown

Origin

Cabinet Intelligence and Research Office (JP / JPN)

Manufacturer

MELCO

Mission

Operational spacecraft

Bus & Motor

IGS-R, Unknown motor

Mass

~1,500 kg wet, ~1,000 kg dry

Launch date (UTC)

2024-09-26 (7 months ago)

Launch vehicle

H-IIA 202

Launch site

Tanegashima Space Center (TNSTA)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

RCS unknown

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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.