OBJECT BE, 67482
Orbit data source: Space-Track
OBJECT BE, 67482 is a satellite in SSO that was launched on Sun, 28 Dec 2025 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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67482 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Manufacturer
OKB5P/QAU
Mission
Operational Amateur Technology
Bus & Motor
TRISAT, Unknown motor
Mass
0.5 kg wet, 0.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.048 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 OBJECT BE
1 67482U 25313BE 26169.46909006 .00131143 00000-0 22331-2 0 9995
2 67482 97.3867 247.0387 0005060 282.7680 77.3006 15.50908576 23479Epoch: 2026-06-18T11:15Z
TLE epoch observation values (Epoch: 2026-06-18T11:15:29.381Z)
Latitude
-0.00003°
Longitude
171.45431°
Altitude
416.451 km
Speed
7.662 km/s
True Right ascension
16h 28m 09s
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
10:18:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
414.431 km
Perigee altitude
407.561 km
Semi-major axis
6,789.133 km
Eccentricity
0.00051
Inclination
97.3867°
RAAN
247.0387°
Arg. of periapsis
282.768°
True anomaly
77.35717°
Mean anomaly
77.3006°
Eccentric anomaly
77.32889°
Mean motion
3.87991 °/min
Orbital period
92.79 mins
BSTAR
0.0022331
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Other satellites on launch #313 in the year 2025 (2025-12-28 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 BE 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. |
|---|---|---|---|---|---|---|---|
| OBJECT BE is likely not visible in the next few days. |
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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