DECAYED
Showing default

REVELA, 56224 (Decayed)

Orbit data source: Space-Track

REVELA, 56224 was a payload satellite owned by Arca Dynamics (IT) in LEO that was launched on Sat, 15 Apr 2023 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.

Not visible in the next 10 days
Identifier
56224, 2023-054AY
Orbit
Decayed
Country
Flag of ITIT
Related business
Manufacturer
NPC SpaceMind
Mission
Decayed Commercial Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2023-04-15 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

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

TLE from 1 year ago
0 REVELA
1 56224U 23054AY  24365.97606137  .10194361  26446-5  70266-3 0  9998
2 56224  97.3161 271.3897 0006149 194.0579 166.0551 16.41152549 96872
Epoch: 2024-12-30T23:25Z
TLE epoch observation values (Epoch: 2024-12-30T23:25:31.702Z)
Latitude
-0.00003°
Longitude
-179.88271°
Altitude
169.898 km
Speed
7.802 km/s
True Right ascension
18h 05m 33s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
00:16:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
163.561 km
Perigee altitude
155.521 km
Semi-major axis
6,537.678 km
Eccentricity
0.00061
Inclination
97.3161°
RAAN
271.3897°
Arg. of periapsis
194.0579°
True anomaly
166.07207°
Mean anomaly
166.0551°
Eccentric anomaly
166.06359°
Mean motion
4.1059 °/min
Orbital period
87.68 mins
BSTAR
0.00070266
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|