OBJECT E, 67252
Orbit data source: Space-Track
OBJECT E, 67252 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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67252 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Manufacturer
Sputniks
Mission
Operational Amateur Imaging
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
20 kg wet, 20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.240 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 OBJECT E
1 67252U 25313E 26171.46503546 .00005705 00000-0 23613-3 0 9991
2 67252 97.3938 246.4155 0009126 341.0557 19.0340 15.24298547 26476Epoch: 2026-06-20T11:09Z
TLE epoch observation values (Epoch: 2026-06-20T11:09:39.063Z)
Latitude
-0.00001°
Longitude
170.32347°
Altitude
490.061 km
Speed
7.623 km/s
True Right ascension
16h 25m 39s
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
07:13:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.12 km
Perigee altitude
483.584 km
Semi-major axis
6,867.989 km
Eccentricity
0.00091
Inclination
97.3938°
RAAN
246.4155°
Arg. of periapsis
341.0557°
True anomaly
19.06814°
Mean anomaly
19.034°
Eccentric anomaly
19.05107°
Mean motion
3.81328 °/min
Orbital period
94.41 mins
BSTAR
0.00023613
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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 E 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 | 2026-06-21 04:37:36.923Z | 138.22° SSE | 2026-06-21 04:40:36.923Z | 61.695° ENE | 31.437° | 2026-06-21 04:43:36.923Z | 4.903° NNE |
| 5 mins | 2026-06-21 17:40:36.923Z | 29.782° NE | 2026-06-21 17:42:36.923Z | 109.694° ESE | 40.024° | 2026-06-21 17:45:36.923Z | 178.554° S |
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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