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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)
2024-08-16 (1 year 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, Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 ORESAT0.5
1 60525U 24149BK  25340.47511373  .00029029  00000-0  80415-3 0  9996
2 60525  97.3905  59.5370 0005218 249.7583 110.3100 15.36914121 72790
Epoch: 2025-12-06T11:24Z
TLE epoch observation values (Epoch: 2025-12-06T11:24:09.826Z)
Latitude
-0.00007°
Longitude
172.99375°
Altitude
459.594 km
Speed
7.636 km/s
True Right ascension
03h 58m 08s
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
04:04:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.748 km
Perigee altitude
448.62 km
Semi-major axis
6,830.321 km
Eccentricity
0.00052
Inclination
97.3905°
RAAN
59.537°
Arg. of periapsis
249.7583°
True anomaly
110.36606°
Mean anomaly
110.31°
Eccentric anomaly
110.33803°
Mean motion
3.84487 °/min
Orbital period
93.63 mins
BSTAR
0.00080415
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