DECAYED

OBJECT D, 59509 (Decayed)

Orbit data source: Space-Track

You're viewing an Uncataloged Satellite

Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

OBJECT D, 59509 was a satellite owned by Avant Space (CIS) in LEO that was launched on Thu, 11 Apr 2024 UTC via an ANGARA A5/ORION launch vehicle from the Vostochny Cosmodrome (VOSTO). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.

Not visible in the next 10 days
OBJECT D details
Identifier
59509, 2024-069D
Orbit
Decayed
Last TLE update10 months ago
Origin
Flag of CISAvant Space (CIS)
ManufacturerAvant Space
MissionDecayed spacecraft
Bus & MotorCUBESAT 3U, Unknown motor
Mass4 kg wet, 4 kg dry
Launch date (UTC)
2024-04-11 (10 months ago)
Launch vehicle
ANGARA A5/ORION
Launch site
Vostochny Cosmodrome (VOSTO)
Object typeUnknown
Shape & HBRUnknown
Radar Cross SectionSmall (<0.1 m²)

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TLE from 10 months ago
0 OBJECT D
1 59509U 24069D   24109.37283718  .05373416  10814-4  51767-2 0  9999
2 59509  51.4865 338.0912 0222076 105.5926 257.0155 15.77124220   907
Epoch: 2024-04-18T08:56Z
Definitive object data (Epoch: 2024-04-18T08:56:53.132Z)
Latitude0.03522°
Longitude-3.07234°
Altitude375.957 km
Speed7.665 km/s
True Right ascension22h 32m 28s
True Declination0° 02' 06"
Sunlit
Object was in daylight at TLE 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.
Orbital elements
Apogee altitude488.307 km
Perigee altitude189.959 km
Semi-major axis6,717.27 km
Eccentricity0.0222076
Inclination51.4865°
RAAN338.0912°
Arg. of periapsis105.5926°
True anomaly254.5519°
Mean anomaly257.0155°
Eccentric anomaly255.78207°
Mean motion3.94234 °/min
BSTAR0.0051767
Orbital period91.32 mins
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OBJECT D Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
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