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 26253.08727071 .00015106 00000-0 28519-3 0 9993
2 46292 97.2325 315.9872 0002587 134.6198 225.5265 15.48542474334159Epoch: 2026-09-10T02:05Z
TLE epoch observation values (Epoch: 2026-09-10T02:05:40.189Z)
Latitude
0.00004°
Longitude
-64.56027°
Altitude
425.356 km
Speed
7.655 km/s
True Right ascension
21h 03m 56s
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
03:03:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
419.668 km
Perigee altitude
416.151 km
Semi-major axis
6,796.047 km
Eccentricity
0.00026
Inclination
97.2325°
RAAN
315.9872°
Arg. of periapsis
134.6198°
True anomaly
225.50535°
Mean anomaly
225.5265°
Eccentric anomaly
225.51593°
Mean motion
3.87399 °/min
Orbital period
92.93 mins
BSTAR
0.00028519
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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 | 2026-09-10 16:36:59.533Z | 38.965° NE | 2026-09-10 16:39:59.533Z | 114.339° SE | 26.196° | 2026-09-10 16:41:59.533Z | 155.026° SSE |
| 4 mins | 2026-09-11 04:35:59.533Z | 190.772° SSW | 2026-09-11 04:37:59.533Z | 278.521° WNW | 51.402° | 2026-09-11 04:39:59.533Z | 333.428° 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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