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: 8 hours ago
TLE from 8 hours ago
0 OBJECT G
1 59779U 24092G 25259.56092551 .00000181 00000-0 84708-4 0 9991
2 59779 98.6454 14.3505 0010872 295.1427 64.8628 14.31659839 69740Epoch: 2025-09-16T13:27Z
TLE epoch observation values (Epoch: 2025-09-16T13:27:43.964Z)
Latitude
0.00001°
Longitude
176.66785°
Altitude
785.818 km
Speed
7.463 km/s
True Right ascension
00h 57m 24s
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
14:01:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.114 km
Perigee altitude
775.542 km
Semi-major axis
7,161.465 km
Eccentricity
0.00109
Inclination
98.6454°
RAAN
14.3505°
Arg. of periapsis
295.1427°
True anomaly
64.97565°
Mean anomaly
64.8628°
Eccentric anomaly
64.91922°
Mean motion
3.5813 °/min
Orbital period
100.52 mins
BSTAR
0.000084708
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-17 06:25:34.598Z | 81.373° E | 2025-09-17 06:26:34.598Z | 67.476° ENE | 16.757° | 2025-09-17 06:29:34.598Z | 28.393° NE |
| 8 mins | 2025-09-17 08:02:34.598Z | 186.171° SSW | 2025-09-17 08:05:34.598Z | 246.151° WSW | 40.235° | 2025-09-17 08:10:34.598Z | 337.617° N |
| 9 mins | 2025-09-17 20:14:34.598Z | 27.818° NE | 2025-09-17 20:18:34.598Z | 100.709° ESE | 38.159° | 2025-09-17 20:23:34.598Z | 176.459° S |
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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