DECAYED

OBJECT N, 59063 (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 N, 59063 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
59063, 2024-039N
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: 5 months ago

TLE from 5 months ago
0 OBJECT N
1 59063U 24039N   25123.19697148  .15262011  26408-5  23866-3 0  9990
2 59063  97.3867  99.9366 0010702 236.9191 123.1086 16.47867169 66163
Epoch: 2025-05-03T04:43Z
TLE epoch observation values (Epoch: 2025-05-03T04:43:38.335Z)
Latitude
-0.00002°
Longitude
167.68418°
Altitude
152.04 km
Speed
7.813 km/s
True Right ascension
06h 39m 44s
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
14:01:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
148.732 km
Perigee altitude
134.777 km
Semi-major axis
6,519.892 km
Eccentricity
0.00107
Inclination
97.3867°
RAAN
99.9366°
Arg. of periapsis
236.9191°
True anomaly
123.21125°
Mean anomaly
123.1086°
Eccentric anomaly
123.15993°
Mean motion
4.12271 °/min
Orbital period
87.32 mins
BSTAR
0.00023866
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