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 (1 year ago)
Launch vehicle
ARIANE 62
Launch site
French Guiana (FRGUI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 4 Pan, 0.3 m
Radar Cross Section
0.072 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 ROBUSTA-3A
1 60243U 24128J   25258.09404787  .00006334  00000-0  43149-3 0  9993
2 60243  61.9871  97.2561 0056032  72.8696 287.8521 15.06018216 64905
Epoch: 2025-09-15T02:15Z
TLE epoch observation values (Epoch: 2025-09-15T02:15:25.735Z)
Latitude
-0.00013°
Longitude
69.09516°
Altitude
538.454 km
Speed
7.6 km/s
True Right ascension
06h 29m 01s
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
12:38:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.116 km
Perigee altitude
508.506 km
Semi-major axis
6,925.448 km
Eccentricity
0.0056
Inclination
61.9871°
RAAN
97.2561°
Arg. of periapsis
72.8696°
True anomaly
287.23963°
Mean anomaly
287.8521°
Eccentric anomaly
287.546°
Mean motion
3.76592 °/min
Orbital period
95.59 mins
BSTAR
0.00043149
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
|