DECAYED
Showing default

ELO-4, 56990 (Decayed)

Orbit data source: Space-Track

ELO-4, 56990 was a UK payload satellite in LEO that was launched on Mon, 12 Jun 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
56990, 2023-084BS
Orbit
Decayed
Country
Flag of UKUK
Related business
Manufacturer
AAC ClydeSpace
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
2023-06-12 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.067 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 months ago

TLE from 11 months ago
0 ELO-4
1 56990U 23084BS  25021.26101222  .12988763  25949-5  80082-3 0  9991
2 56990  97.5138 157.8621 0011086 289.3580  70.6521 16.40898474 90040
Epoch: 2025-01-21T06:15Z
TLE epoch observation values (Epoch: 2025-01-21T06:15:51.455Z)
Latitude
-0.00001°
Longitude
-56.97208°
Altitude
164.267 km
Speed
7.809 km/s
True Right ascension
10h 31m 26s
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
06:44:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167.474 km
Perigee altitude
152.977 km
Semi-major axis
6,538.362 km
Eccentricity
0.00111
Inclination
97.5138°
RAAN
157.8621°
Arg. of periapsis
289.358°
True anomaly
70.77202°
Mean anomaly
70.6521°
Eccentric anomaly
70.71205°
Mean motion
4.10525 °/min
Orbital period
87.69 mins
BSTAR
0.00080082
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|