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ARTHUR-1, 48953

Orbit data source: Space-Track

ARTHUR-1, 48953 is a payload satellite owned by Aerospacelab (BE) in SSO 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
SSO
Country
Flag of BEBE / BEL
Related business
Manufacturer
Aerospacelab
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
2021-06-30 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 4 hours ago

TLE from 4 hours ago
0 ARTHUR-1
1 48953U 21059CC  25309.50078088  .00128618  00000-0  67145-3 0  9993
2 48953  97.6617 137.2352 0003317  24.9706 335.1721 15.80509647243705
Epoch: 2025-11-05T12:01Z
TLE epoch observation values (Epoch: 2025-11-05T12:01:07.468Z)
Latitude
0.00002°
Longitude
-88.01847°
Altitude
330.143 km
Speed
7.712 km/s
True Right ascension
09h 08m 56s
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
11:33:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
328.119 km
Perigee altitude
323.672 km
Semi-major axis
6,704.032 km
Eccentricity
0.00033
Inclination
97.6617°
RAAN
137.2352°
Arg. of periapsis
24.9706°
True anomaly
335.15613°
Mean anomaly
335.1721°
Eccentric anomaly
335.16412°
Mean motion
3.95402 °/min
Orbital period
91.05 mins
BSTAR
0.00067145
Loading maneuver chart data...
Computing Atmospheric mass density...

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