OBJECT D, 59509 (Decayed)
Orbit data source: Space-Track
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.
59509 intel report (Beta)
OBJECT D details
Identifier | |
Orbit | Decayed |
Last TLE update | 10 months ago |
Origin | |
Manufacturer | Avant Space |
Mission | Decayed spacecraft |
Bus & Motor | CUBESAT 3U, Unknown motor |
Mass | 4 kg wet, 4 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Unknown |
Shape & HBR | Unknown |
Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
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
Definitive object data (Epoch: 2024-04-18T08:56:53.132Z)
Latitude | 0.03522° |
Longitude | -3.07234° |
Altitude | 375.957 km |
Speed | 7.665 km/s |
True Right ascension | 22h 32m 28s |
True Declination | 0° 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 altitude | 488.307 km |
Perigee altitude | 189.959 km |
Semi-major axis | 6,717.27 km |
Eccentricity | 0.0222076 |
Inclination | 51.4865° |
RAAN | 338.0912° |
Arg. of periapsis | 105.5926° |
True anomaly | 254.5519° |
Mean anomaly | 257.0155° |
Eccentric anomaly | 255.78207° |
Mean motion | 3.94234 °/min |
BSTAR | 0.0051767 |
Orbital period | 91.32 mins |
Other satellites on launch #69 in the year 2024 (2024-04-11 UTC)
DUMMY SAT 3/ORION, 59479 |
OBJECT B, 59480 (Decayed) |
OBJECT C, 59482 (Decayed) |
OBJECT D, 59509 (Decayed) |
OBJECT D Visibility forecast
Observer location: undefined°, undefined
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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