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BRIO, 43813

Orbit data source: Space-Track

BRIO, 43813 is an American payload satellite in LEO that was launched on Mon, 03 Dec 2018 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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/43813?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/43813?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

43813, 2018-099BH

Orbit

LEO

Last TLE update

3 days ago

Origin

Myriota (US)

Manufacturer

SpaceQuest

Mission

Decayed Commercial Technology

Bus & Motor

CUBESAT 3U, Unknown motor

Mass

5 kg wet, 5 kg dry

Launch date (UTC)

2018-12-03 (7 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box, 0.3 m

Radar Cross Section

0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 3 days ago

0 BRIO
1 43813U 18099BH  25191.37859399  .13516868  26109-5  79058-3 0  9990
2 43813  97.4926 278.1281 0016455 271.5932  88.3482 16.40313559362468

Epoch: 2025-07-10T09:05Z

TLE epoch observation values (Epoch: 2025-07-10T09:05:10.52Z)

Latitude

-0.00008°

Longitude

-146.71145°

Altitude

167.925 km

Speed

7.806 km/s

True Right ascension

18h 32m 30s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

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.