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OBJECT T, 61752

Orbit data source: Space-Track

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Recently launched and/or uncataloged RSOs may have evolving metadata. Metadata may include the following, but is not limited to: Owner, Manufacturer, Bus, Motor, and Mission.

OBJECT T, 61752 is a payload satellite in SSO that was launched on Mon, 04 Nov 2024 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
61752, 2024-199T
Orbit
SSO
Country
Flag of TBDTBD
Related business
Manufacturer
Sputniks
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U?, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
2024-11-04 (2 years ago)
Launch vehicle
SOYUZ-2-1B
Launch site
Vostochny Cosmodrome (VOSTO)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 OBJECT T
1 61752U 24199T   26309.93578534  .00001910  00000-0  16530-3 0  9999
2 61752  97.3134 140.5352 0005049 313.5469  46.5334 14.98237414156346
Epoch: 2026-11-05T22:27Z
TLE epoch observation values (Epoch: 2026-11-05T22:27:31.853Z)
Latitude
-0.00009°
Longitude
118.48989°
Altitude
572.992 km
Speed
7.576 km/s
True Right ascension
09h 22m 08s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
09:27:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.841 km
Perigee altitude
565.825 km
Semi-major axis
6,947.47 km
Eccentricity
0.0005
Inclination
97.3134°
RAAN
140.5352°
Arg. of periapsis
313.5469°
True anomaly
46.57541°
Mean anomaly
46.5334°
Eccentric anomaly
46.5544°
Mean motion
3.74803 °/min
Orbital period
96.05 mins
BSTAR
0.0001653
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