Showing default

ROBUSTA-3A, 60243

Orbit data source: Space-Track

ROBUSTA-3A, 60243 is a payload satellite owned by Montpellier (FR) in LEO that was launched on Tue, 09 Jul 2024 UTC via an ARIANE 62 launch vehicle from the French Guiana (FRGUI). 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
60243, 2024-128J
Orbit
LEO
Country
Flag of FRFR
Related business
Manufacturer
Montpellier
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
2024-07-09 (2 years ago)
Launch vehicle
ARIANE 62
Launch site
French Guiana (FRGUI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 4 Pan, 1.0 m
Radar Cross Section
0.072 m², Small (<0.1 m²)

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

TLE from 11 hours ago
0 ROBUSTA-3A
1 60243U 24128J   26134.12903920  .00005248  00000-0  31713-3 0  9991
2 60243  61.9867 328.6362 0045854 121.4904 239.0684 15.11118441101271
Epoch: 2026-05-14T03:05Z
TLE epoch observation values (Epoch: 2026-05-14T03:05:48.986Z)
Latitude
-0.00005°
Longitude
50.30292°
Altitude
550.962 km
Speed
7.578 km/s
True Right ascension
21h 54m 32s
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
22:42:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.399 km
Perigee altitude
500.03 km
Semi-major axis
6,909.852 km
Eccentricity
0.00459
Inclination
61.9867°
RAAN
328.6362°
Arg. of periapsis
121.4904°
True anomaly
238.61901°
Mean anomaly
239.0684°
Eccentric anomaly
238.84357°
Mean motion
3.77868 °/min
Orbital period
95.27 mins
BSTAR
0.00031713
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|