OBJECT BA, 61783 (Decayed)
Orbit data source: Space-Track
OBJECT BA, 61783 was a satellite in LEO that was launched on Mon, 04 Nov 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.
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61783 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Zimbabwe National Geospatial and Space Agency (ZW)Manufacturer
Yugo-Zapad. GU
Mission
Decayed Civil Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 OBJECT BA
1 61783U 24199BA 26020.03020647 .10538765 26509-5 13731-2 0 9991
2 61783 97.2775 260.7788 0001295 180.7662 179.3634 16.35808916115084Epoch: 2026-01-20T00:43Z
TLE epoch observation values (Epoch: 2026-01-20T00:43:29.839Z)
Latitude
-0.00004°
Longitude
130.48655°
Altitude
181.074 km
Speed
7.797 km/s
True Right ascension
17h 23m 06s
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
09:09:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
174.631 km
Perigee altitude
172.934 km
Semi-major axis
6,551.92 km
Eccentricity
0.00013
Inclination
97.2775°
RAAN
260.7788°
Arg. of periapsis
180.7662°
True anomaly
179.36356°
Mean anomaly
179.3634°
Eccentric anomaly
179.36348°
Mean motion
4.09252 °/min
Orbital period
87.97 mins
BSTAR
0.0013731
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Other satellites on launch #199 in the year 2024 (2024-11-04 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 BA Visibility
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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. |
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| This satellite is decayed. |
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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