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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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Iframe URL

https://www.satcat.com/sats-embedded/46292?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

46292, 2020-061W

Orbit

SSO

Country

ES / SPN

Related business

Polytechnic University of Catalonia (ES)

Manufacturer

UPC

Mission

Non-operational Amateur Technology

Bus & Motor

CUBESAT 6U, Unknown motor

Mass

~10 kg wet, ~10 kg dry

Launch date (UTC)

2020-09-03 (6 years ago)

Launch vehicle

VEGA

Launch site

French Guiana (FRGUI)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box, 0.2 m

Radar Cross Section

0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago

0 3CAT-5/A (TYVAK-0161)
1 46292U 20061W   26307.92020579  .00014234  00000-0  25343-3 0  9998
2 46292  97.2242  10.9090 0001221  41.0712 319.0631 15.50234994342645

Epoch: 2026-11-03T22:05Z

TLE epoch observation values (Epoch: 2026-11-03T22:05:05.780Z)

Latitude

-0.00008°

Longitude

-3.54103°

Altitude

418.549 km

Speed

7.66 km/s

True Right ascension

00h 43m 38s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

00:28:22

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

413.786 km

Perigee altitude

412.128 km

Semi-major axis

6,791.094 km

Eccentricity

0.00012

Inclination

97.2242°

RAAN

10.909°

Arg. of periapsis

41.0712°

True anomaly

319.05393°

Mean anomaly

319.0631°

Eccentric anomaly

319.05852°

Mean motion

3.87823 °/min

Orbital period

92.83 mins

BSTAR

0.00025343

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Other satellites on launch #61 in the year 2020 (2020-09-03 UTC)

3CAT-5/B (TYVAK-0162), 46293

FLOCK 4V 24, 46738 (Decayed)

FLOCK 4V 19, 46609 (Decayed)

FLOCK 4V 21, 46596 (Decayed)

LEMUR 2 DJUPROERA, 46316 (Decayed)

SPACEBEE-13, 46310 (Decayed)

SPACEBEE-20, 46301 (Decayed)

FLOCK 4V 5, 46290 (Decayed)

LEMUR 2 OSCARLATOR, 46299 (Decayed)

DIDO 3, 46284 (Decayed)

FLOCK 4V 12, 46283 (Decayed)

FLOCK 4V 9, 46282 (Decayed)

NUSAT-6 HYPATIA, 46272 (Decayed)

SPACEBEE-19, 46303 (Decayed)

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

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	2026-11-04 17:14:04.679Z	10.944° NNE	2026-11-04 17:16:04.679Z	7.05° NNE	62.903°	2026-11-04 17:19:04.679Z	193.65° SSW

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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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Check out 3CAT-5/A (TYVAK-0161), 46292 on other resources

View 3CAT-5/A (TYVAK-0161), 46292 on NASA - NSSDCA Website

View 3CAT-5/A (TYVAK-0161), 46292 on Heavens-Above

View 3CAT-5/A (TYVAK-0161), 46292 on Keep Track

View 3CAT-5/A (TYVAK-0161), 46292 on Celestrak

View 3CAT-5/A (TYVAK-0161), 46292 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

Go to standalone docs website

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