DECAYED
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ARTHUR-1, 48953 (Decayed)

Orbit data source: Space-Track

ARTHUR-1, 48953 was a payload satellite owned by Aerospacelab (BE) in LEO that was launched on Wed, 30 Jun 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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
48953, 2021-059CC
Orbit
Decayed
Country
Flag of BEBE / BEL
Related business
Manufacturer
Aerospacelab
Mission
Decayed Commercial Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
2021-06-30 (5 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 months ago

TLE from 8 months ago
0 ARTHUR-1
1 48953U 21059CC  25365.60281262  .11494332  27284-5  45979-3 0  9996
2 48953  97.6253 200.8647 0007407 260.6373  99.4091 16.43316269252647
Epoch: 2025-12-31T14:28Z
TLE epoch observation values (Epoch: 2025-12-31T14:28:03.010Z)
Latitude
0.00007°
Longitude
-116.41722°
Altitude
161.039 km
Speed
7.809 km/s
True Right ascension
13h 23m 27s
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
06:40:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
158.647 km
Perigee altitude
148.971 km
Semi-major axis
6,531.946 km
Eccentricity
0.00074
Inclination
97.6253°
RAAN
200.8647°
Arg. of periapsis
260.6373°
True anomaly
99.49282°
Mean anomaly
99.4091°
Eccentric anomaly
99.45096°
Mean motion
4.1113 °/min
Orbital period
87.56 mins
BSTAR
0.00045979
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