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.
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60243 intel report (Beta)
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ROBUSTA-3A radio frequencies
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
Montpellier
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 0.3 m
Radar Cross Section
0.072 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 ROBUSTA-3A
1 60243U 24128J 25256.16855789 .00005411 00000-0 37114-3 0 9991
2 60243 61.9868 104.0057 0055996 72.4497 288.2703 15.05993828 64616Epoch: 2025-09-13T04:02Z
TLE epoch observation values (Epoch: 2025-09-13T04:02:43.401Z)
Latitude
-0.00001°
Longitude
50.91907°
Altitude
538.266 km
Speed
7.601 km/s
True Right ascension
06h 56m 01s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
15:40:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.166 km
Perigee altitude
508.606 km
Semi-major axis
6,925.523 km
Eccentricity
0.0056
Inclination
61.9868°
RAAN
104.0057°
Arg. of periapsis
72.4497°
True anomaly
287.65965°
Mean anomaly
288.2703°
Eccentric anomaly
287.96511°
Mean motion
3.76586 °/min
Orbital period
95.6 mins
BSTAR
0.00037114
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Other satellites on launch #128 in the year 2024 (2024-07-09 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ROBUSTA-3A Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-13 23:40:23.993Z | 342.85° N | 2025-09-13 23:43:23.993Z | 34.694° NE | 28.173° | 2025-09-13 23:46:23.993Z | 105.17° ESE |
| 4 mins | 2025-09-14 01:20:23.993Z | 280.206° WNW | 2025-09-14 01:22:23.993Z | 239.695° WSW | 20.645° | 2025-09-14 01:24:23.993Z | 202.267° SSW |
| 5 mins | 2025-09-14 15:15:23.993Z | 182.56° SSW | 2025-09-14 15:17:23.993Z | 132.107° SE | 33.948° | 2025-09-14 15:20:23.993Z | 54.397° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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