OBJECT BP, 60529

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 is a satellite in SSO 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.

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Identifier
60529, 2024-149BP
Orbit
SSO
Country
Flag of TBDTBD
Related business
Flag of SNSenegalese Space Project, Ministry of Higher Education, Research and Innovation (SN)
Manufacturer
Montpellier
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2024-08-16 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 OBJECT BP
1 60529U 24149BP  25339.19480192  .00247324  00000-0  18393-2 0  9996
2 60529  97.3924  66.5411 0004260 249.8289 110.2516 15.72075915 73115
Epoch: 2025-12-05T04:40Z
TLE epoch observation values (Epoch: 2025-12-05T04:40:30.885Z)
Latitude
-0.00007°
Longitude
-77.82796°
Altitude
357.12 km
Speed
7.694 km/s
True Right ascension
04h 26m 09s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
14:32:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
352.727 km
Perigee altitude
346.995 km
Semi-major axis
6,727.998 km
Eccentricity
0.00043
Inclination
97.3924°
RAAN
66.5411°
Arg. of periapsis
249.8289°
True anomaly
110.29739°
Mean anomaly
110.2516°
Eccentric anomaly
110.2745°
Mean motion
3.93291 °/min
Orbital period
91.54 mins
BSTAR
0.0018393
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