DECAYED

OBJECT M, 59062 (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 M, 59062 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.

Loading next visibility...
Identifier
59062, 2024-039M
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 M
1 59062U 24039M   25123.79643292  .17653738  27301-5  24352-3 0  9992
2 59062  97.3990 100.4955 0009406 213.6684 146.4024 16.48757372 66254
Epoch: 2025-05-03T19:06Z
TLE epoch observation values (Epoch: 2025-05-03T19:06:51.804Z)
Latitude
0.00003°
Longitude
-48.1539°
Altitude
150.985 km
Speed
7.812 km/s
True Right ascension
06h 41m 58s
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
02:36:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
145.536 km
Perigee altitude
133.276 km
Semi-major axis
6,517.543 km
Eccentricity
0.00094
Inclination
97.399°
RAAN
100.4955°
Arg. of periapsis
213.6684°
True anomaly
146.46199°
Mean anomaly
146.4024°
Eccentric anomaly
146.4322°
Mean motion
4.12494 °/min
Orbital period
87.27 mins
BSTAR
0.00024352
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|