DECAYED

OBJECT E, 59055 (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 E, 59055 was a satellite in LEO that was launched on Thu, 29 Feb 2024 UTC via a SOYUZ-2-1B 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
Identifier
59055, 2024-039E
Orbit
Decayed
Country
Flag of TBDTBD
Related business
Manufacturer
Sputniks
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 3U?, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
2024-02-29 (2 years ago)
Launch vehicle
SOYUZ-2-1B
Launch site
Vostochny Cosmodrome (VOSTO)
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 11 months ago

TLE from 11 months ago
0 OBJECT E
1 59055U 24039E   25128.42299177  .11506220  26303-5  44338-3 0  9992
2 59055  97.3945 105.1751 0009726 224.1785 135.8740 16.43188711 66961
Epoch: 2025-05-08T10:09Z
TLE epoch observation values (Epoch: 2025-05-08T10:09:06.488Z)
Latitude
-0.00008°
Longitude
86.40437°
Altitude
165.156 km
Speed
7.804 km/s
True Right ascension
07h 00m 42s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
22:04:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
160.49 km
Perigee altitude
147.784 km
Semi-major axis
6,532.274 km
Eccentricity
0.00097
Inclination
97.3945°
RAAN
105.1751°
Arg. of periapsis
224.1785°
True anomaly
135.95153°
Mean anomaly
135.874°
Eccentric anomaly
135.91277°
Mean motion
4.11099 °/min
Orbital period
87.57 mins
BSTAR
0.00044338
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