DECAYED

OBJECT K, 59060 (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 K, 59060 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
59060, 2024-039K
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: 10 months ago

TLE from 10 months ago
0 OBJECT K
1 59060U 24039K   25133.32764041  .15065791  26402-5  17718-3 0  9999
2 59060  97.3885 110.3756 0012027 230.2391 129.7854 16.49499424 67738
Epoch: 2025-05-13T07:51Z
TLE epoch observation values (Epoch: 2025-05-13T07:51:48.131Z)
Latitude
-0.0001°
Longitude
121.09711°
Altitude
148.942 km
Speed
7.814 km/s
True Right ascension
07h 21m 30s
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
04:24:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
145.285 km
Perigee altitude
129.613 km
Semi-major axis
6,515.586 km
Eccentricity
0.0012
Inclination
97.3885°
RAAN
110.3756°
Arg. of periapsis
230.2391°
True anomaly
129.8912°
Mean anomaly
129.7854°
Eccentric anomaly
129.83831°
Mean motion
4.1268 °/min
Orbital period
87.23 mins
BSTAR
0.00017718
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