OBJECT BP, 60529 (Decayed)
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 BP, 60529 was a satellite in LEO that was launched on Fri, 16 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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. This object's orbit decayed before it could be identified.
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60529 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
Senegalese Space Project, Ministry of Higher Education, Research and Innovation (SN)Manufacturer
Montpellier
Mission
Decayed Civil Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 OBJECT BP
1 60529U 24149BP 26021.20605179 .13334605 25086-5 92795-3 0 9999
2 60529 97.3696 117.4933 0010153 281.2791 78.7368 16.40534344 80575Epoch: 2026-01-21T04:56Z
TLE epoch observation values (Epoch: 2026-01-21T04:56:42.874Z)
Latitude
0°
Longitude
-77.26224°
Altitude
166.343 km
Speed
7.807 km/s
True Right ascension
07h 49m 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
12:30:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167.826 km
Perigee altitude
154.548 km
Semi-major axis
6,539.324 km
Eccentricity
0.00102
Inclination
97.3696°
RAAN
117.4933°
Arg. of periapsis
281.2791°
True anomaly
78.85093°
Mean anomaly
78.7368°
Eccentric anomaly
78.79386°
Mean motion
4.10435 °/min
Orbital period
87.71 mins
BSTAR
0.00092795
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Other satellites on launch #149 in the year 2024 (2024-08-16 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 BP 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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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