OBJECT J, 59781

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 J, 59781 is a satellite owned by Byuro 1440 (CIS) in SSO that was launched on Thu, 16 May 2024 UTC via a SOYUZ-2-1B launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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.

Loading next visibility...
Identifier
59781, 2024-092J
Orbit
SSO
Country
Flag of CISCIS
Related business
Manufacturer
Byuro 1440
Mission
Operational Commercial Communications
Bus & Motor
RASSVET-2, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
2024-05-16 (2 years ago)
Launch vehicle
SOYUZ-2-1B
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Unknown
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
1.622 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 3 hours ago

TLE from 3 hours ago
0 OBJECT J
1 59781U 24092J   26128.88087554  .00000146  00000-0  71109-4 0  9994
2 59781  98.6644 247.9715 0011416 330.3100  29.7433 14.31832104103275
Epoch: 2026-05-08T21:08Z
TLE epoch observation values (Epoch: 2026-05-08T21:08:27.646Z)
Latitude
-0.00014°
Longitude
64.15002°
Altitude
781.446 km
Speed
7.467 km/s
True Right ascension
16h 31m 53s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
08:20:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
790.929 km
Perigee altitude
774.579 km
Semi-major axis
7,160.891 km
Eccentricity
0.00114
Inclination
98.6644°
RAAN
247.9715°
Arg. of periapsis
330.31°
True anomaly
29.80828°
Mean anomaly
29.7433°
Eccentric anomaly
29.77578°
Mean motion
3.58173 °/min
Orbital period
100.51 mins
BSTAR
0.000071109
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
|