OBJECT T, 61752
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 T, 61752 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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61752 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
Manufacturer
Sputniks
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U?, Unknown motor
Mass
3 kg wet, 3 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: 7 hours ago
TLE from 7 hours ago
0 OBJECT T
1 61752U 24199T 25344.50542431 .00005137 00000-0 45794-3 0 9996
2 61752 97.3336 190.6237 0006403 356.7532 3.3648 14.96382631106897Epoch: 2025-12-10T12:07Z
TLE epoch observation values (Epoch: 2025-12-10T12:07:48.660Z)
Latitude
-0°
Longitude
-70.80384°
Altitude
576.697 km
Speed
7.575 km/s
True Right ascension
12h 42m 29s
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
17:13:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.531 km
Perigee altitude
570.627 km
Semi-major axis
6,953.216 km
Eccentricity
0.00064
Inclination
97.3336°
RAAN
190.6237°
Arg. of periapsis
356.7532°
True anomaly
3.36911°
Mean anomaly
3.3648°
Eccentric anomaly
3.36695°
Mean motion
3.74339 °/min
Orbital period
96.17 mins
BSTAR
0.00045794
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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 T 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-11 03:08:40.650Z | 354.523° N | 2025-12-11 03:11:40.650Z | 276.003° WNW | 36.632° | 2025-12-11 03:14:40.650Z | 214.986° SW |
| 6 mins | 2025-12-11 13:56:40.650Z | 165.951° S | 2025-12-11 13:59:40.650Z | 353.648° N | 43.264° | 2025-12-11 14:02:40.650Z | 348.793° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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