3CAT-5/A (TYVAK-0161), 46292
Orbit data source: Space-Track
3CAT-5/A (TYVAK-0161), 46292 is a payload satellite owned by UPC (ES) in SSO that was launched on Thu, 03 Sep 2020 UTC via a VEGA 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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46292 intel report (Beta)
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Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
UPC
Mission
Non-operational Amateur Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 3CAT-5/A (TYVAK-0161)
1 46292U 20061W 26237.89960040 .00015672 00000-0 30038-3 0 9996
2 46292 97.2343 300.7851 0001564 152.9540 207.1792 15.48099793331807Epoch: 2026-08-25T21:35Z
TLE epoch observation values (Epoch: 2026-08-25T21:35:25.474Z)
Latitude
-0.00008°
Longitude
2.76864°
Altitude
426.365 km
Speed
7.655 km/s
True Right ascension
20h 03m 08s
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
21:32:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
420.269 km
Perigee altitude
418.143 km
Semi-major axis
6,797.343 km
Eccentricity
0.00016
Inclination
97.2343°
RAAN
300.7851°
Arg. of periapsis
152.954°
True anomaly
207.17102°
Mean anomaly
207.1792°
Eccentric anomaly
207.17511°
Mean motion
3.87288 °/min
Orbital period
92.95 mins
BSTAR
0.00030038
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Other satellites on launch #61 in the year 2020 (2020-09-03 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-5/A (TYVAK-0161) 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 | 2026-08-26 16:45:44.111Z | 28.738° NE | 2026-08-26 16:48:44.111Z | 103.229° ESE | 31.678° | 2026-08-26 16:50:44.111Z | 161.174° S |
| 4 mins | 2026-08-27 04:45:44.111Z | 211.621° SW | 2026-08-27 04:46:44.111Z | 242.739° WSW | 29.474° | 2026-08-27 04:49:44.111Z | 327.588° NNW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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