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ORESAT0.5, 60525

Orbit data source: Space-Track

ORESAT0.5, 60525 is a payload satellite owned by Portland State (US) 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). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
60525, 2024-149BK
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Portland State
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1.5U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
Icon of a cake. It is the launch day of the satellite!2024-08-16 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Ant, 0.3 m
Radar Cross Section
0.040 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 ORESAT0.5
1 60525U 24149BK  26227.20631002  .00013958  00000-0  27633-3 0  9991
2 60525  97.3705 314.1952 0006253  73.8566 286.3372 15.47172957111593
Epoch: 2026-08-15T04:57Z
TLE epoch observation values (Epoch: 2026-08-15T04:57:05.185Z)
Latitude
-0.00002°
Longitude
-83.69692°
Altitude
426.934 km
Speed
7.656 km/s
True Right ascension
20h 56m 46s
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
20:54:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
426.181 km
Perigee altitude
417.677 km
Semi-major axis
6,800.066 km
Eccentricity
0.00063
Inclination
97.3705°
RAAN
314.1952°
Arg. of periapsis
73.8566°
True anomaly
286.26842°
Mean anomaly
286.3372°
Eccentric anomaly
286.30281°
Mean motion
3.87056 °/min
Orbital period
93.01 mins
BSTAR
0.00027633
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