Showing default

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.

Loading next visibility...
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 (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  26174.20564288  .00016269  00000-0  34339-3 0  9992
2 60525  97.3720 260.2984 0004401 244.4348 115.6446 15.45274453103402
Epoch: 2026-06-23T04:56Z
TLE epoch observation values (Epoch: 2026-06-23T04:56:07.544Z)
Latitude
-0.00007°
Longitude
-85.11357°
Altitude
434.995 km
Speed
7.65 km/s
True Right ascension
17h 21m 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
16:56:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
430.498 km
Perigee altitude
424.507 km
Semi-major axis
6,805.64 km
Eccentricity
0.00044
Inclination
97.372°
RAAN
260.2984°
Arg. of periapsis
244.4348°
True anomaly
115.69005°
Mean anomaly
115.6446°
Eccentric anomaly
115.66733°
Mean motion
3.8658 °/min
Orbital period
93.12 mins
BSTAR
0.00034339
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|