OBJECT G, 59779
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 G, 59779 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.
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59779 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Bureau 1440 (RU)Manufacturer
Byuro 1440
Mission
Operational spacecraft
Bus & Motor
RASSVET-2, Unknown motor
Mass
~200 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 OBJECT G
1 59779U 24092G 25261.30814613 .00000192 00000-0 88841-4 0 9991
2 59779 98.6456 16.0903 0010847 289.5129 70.4883 14.31660726 69991Epoch: 2025-09-18T07:23Z
TLE epoch observation values (Epoch: 2025-09-18T07:23:43.825Z)
Latitude
0.00004°
Longitude
-92.31392°
Altitude
786.529 km
Speed
7.462 km/s
True Right ascension
01h 04m 21s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
20:52:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.093 km
Perigee altitude
775.557 km
Semi-major axis
7,161.462 km
Eccentricity
0.00108
Inclination
98.6456°
RAAN
16.0903°
Arg. of periapsis
289.5129°
True anomaly
70.60551°
Mean anomaly
70.4883°
Eccentric anomaly
70.5469°
Mean motion
3.5813 °/min
Orbital period
100.52 mins
BSTAR
0.000088841
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Other satellites on launch #92 in the year 2024 (2024-05-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT G Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-19 07:00:08.326Z | 134.01° SE | 2025-09-19 07:05:08.326Z | 55.695° ENE | 30.701° | 2025-09-19 07:09:08.326Z | 4.25° NNE |
| 7 mins | 2025-09-19 08:41:08.326Z | 220.334° SW | 2025-09-19 08:44:08.326Z | 265.967° W | 23.227° | 2025-09-19 08:48:08.326Z | 318.963° NNW |
| 8 mins | 2025-09-19 20:53:08.326Z | 5.401° NNE | 2025-09-19 20:57:08.326Z | 249.697° W | 42.193° | 2025-09-19 21:01:08.326Z | 204.905° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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