OBJECT R, 61750
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 R, 61750 is a satellite in SSO 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.
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61750 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.045 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 OBJECT R
1 61750U 24199R 25344.53114729 .00037125 00000-0 86241-3 0 9996
2 61750 97.3222 212.9464 0007375 250.2270 109.8183 15.42235603108352Epoch: 2025-12-10T12:44Z
TLE epoch observation values (Epoch: 2025-12-10T12:44:51.125Z)
Latitude
0.00001°
Longitude
-57.76676°
Altitude
444.344 km
Speed
7.645 km/s
True Right ascension
14h 11m 47s
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
16:05:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.471 km
Perigee altitude
431.42 km
Semi-major axis
6,814.582 km
Eccentricity
0.00074
Inclination
97.3222°
RAAN
212.9464°
Arg. of periapsis
250.227°
True anomaly
109.89778°
Mean anomaly
109.8183°
Eccentric anomaly
109.85804°
Mean motion
3.8582 °/min
Orbital period
93.31 mins
BSTAR
0.00086241
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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 R 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-11 15:21:53.447Z | 157.018° SSE | 2025-12-11 15:23:53.447Z | 38.611° NE | 42.963° | 2025-12-11 15:26:53.447Z | 352.374° N |
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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