3CAT-4, 60236
Orbit data source: Space-Track
3CAT-4, 60236 is a payload satellite owned by UPC (ES) 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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60236 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
UPC
Mission
Non-operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Rod, 0.3 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 3CAT-4
1 60236U 24128B 25299.24037676 .00002508 00000-0 20531-3 0 9995
2 60236 61.9928 320.1160 0058919 87.4059 273.3774 15.00900519 70978Epoch: 2025-10-26T05:46Z
TLE epoch observation values (Epoch: 2025-10-26T05:46:08.552Z)
Latitude
0.00001°
Longitude
-161.27904°
Altitude
563.718 km
Speed
7.581 km/s
True Right ascension
21h 20m 27s
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
10:23:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
603.946 km
Perigee altitude
522.152 km
Semi-major axis
6,941.186 km
Eccentricity
0.00589
Inclination
61.9928°
RAAN
320.116°
Arg. of periapsis
87.4059°
True anomaly
272.70313°
Mean anomaly
273.3774°
Eccentric anomaly
273.04029°
Mean motion
3.75312 °/min
Orbital period
95.92 mins
BSTAR
0.00020531
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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.3CAT-4 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-27 02:41:45.707Z | 170.213° S | 2025-10-27 02:44:45.707Z | 107.36° ESE | 24.747° | 2025-10-27 02:46:45.707Z | 68.331° E |
| 4 mins | 2025-10-27 04:21:45.707Z | 277.545° WNW | 2025-10-27 04:23:45.707Z | 327.225° NNW | 24.133° | 2025-10-27 04:25:45.707Z | 5.273° NNE |
| 5 mins | 2025-10-27 11:04:45.707Z | 0.382° NNE | 2025-10-27 11:06:45.707Z | 49.526° ENE | 26.89° | 2025-10-27 11:09:45.707Z | 106.251° ESE |
| 5 mins | 2025-10-27 12:43:45.707Z | 280.501° WNW | 2025-10-27 12:45:45.707Z | 236.644° WSW | 22.577° | 2025-10-27 12:48:45.707Z | 187.882° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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