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  26276.20224555  .00014174  00000-0  26396-3 0  9992
2 60525  97.3660   4.1300 0003993 232.6547 127.4341 15.48950126119174
Epoch: 2026-10-03T04:51Z
TLE epoch observation values (Epoch: 2026-10-03T04:51:14.015Z)
Latitude
0.00002°
Longitude
-80.59163°
Altitude
424.578 km
Speed
7.656 km/s
True Right ascension
00h 16m 31s
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
05:28:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
419.435 km
Perigee altitude
414.009 km
Semi-major axis
6,794.859 km
Eccentricity
0.0004
Inclination
97.366°
RAAN
4.13°
Arg. of periapsis
232.6547°
True anomaly
127.47042°
Mean anomaly
127.4341°
Eccentric anomaly
127.45226°
Mean motion
3.87501 °/min
Orbital period
92.9 mins
BSTAR
0.00026396
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|