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: 18 hours ago

TLE from 18 hours ago
0 OBJECT BP
1 60529U 24149BP  25286.91006521  .00096424  00000-0  13264-2 0  9992
2 60529  97.3989  11.7961 0003183  82.5063 277.6553 15.56942192 64945
Epoch: 2025-10-13T21:50Z
TLE epoch observation values (Epoch: 2025-10-13T21:50:29.634Z)
Latitude
-0.00006°
Longitude
21.46656°
Altitude
399.367 km
Speed
7.671 km/s
True Right ascension
00h 47m 11s
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
10:30:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
395.585 km
Perigee altitude
391.274 km
Semi-major axis
6,771.566 km
Eccentricity
0.00032
Inclination
97.3989°
RAAN
11.7961°
Arg. of periapsis
82.5063°
True anomaly
277.61915°
Mean anomaly
277.6553°
Eccentric anomaly
277.63722°
Mean motion
3.89502 °/min
Orbital period
92.43 mins
BSTAR
0.0013264
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