OBJECT A, 67160
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 A, 67160 is a satellite owned by EU SPA (ESA) that was launched on Wed, 17 Dec 2025 UTC via an ARIANE 62 launch vehicle from the French Guiana (FRGUI). 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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67160 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ESARelated business
Manufacturer
OHB
Mission
Operational spacecraft
Bus & Motor
GALILEO, AOCS
Mass
733 kg wet, 660 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 OBJECT A
1 67160U 25302A 25352.14605887 -.00000007 00000-0 00000-0 0 9996
2 67160 54.2406 107.2544 0008424 237.6458 122.2317 1.72906186 29Epoch: 2025-12-18T03:30Z
TLE epoch observation values (Epoch: 2025-12-18T03:30:19.486Z)
Latitude
0.00002°
Longitude
-32.34501°
Altitude
22,957.421 km
Speed
3.685 km/s
True Right ascension
07h 08m 58s
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
12:18:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
22,968.683 km
Perigee altitude
22,919.282 km
Semi-major axis
29,322.12 km
Eccentricity
0.00084
Inclination
54.2406°
RAAN
107.2544°
Arg. of periapsis
237.6458°
True anomaly
122.31331°
Mean anomaly
122.2317°
Eccentric anomaly
122.27251°
Mean motion
0.43227 °/min
Orbital period
832.82 mins
BSTAR
0
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Other satellites on launch #302 in the year 2025 (2025-12-17 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 A 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. |
|---|---|---|---|---|---|---|---|
| 364 mins | 2025-12-21 16:49:20.406Z | 304.41° NW | 2025-12-21 19:58:20.406Z | 268.117° W | 41.12° | 2025-12-21 22:53:20.406Z | 202.873° SW |
| 265 mins | 2025-12-22 04:17:20.406Z | 123.113° SE | 2025-12-22 06:31:20.406Z | 74.762° E | 30.733° | 2025-12-22 08:42:20.406Z | 40.436° NE |
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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