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UPMSAT-2, 46276

Orbit data source: Space-Track

UPMSAT-2, 46276 is a payload satellite owned by IDR/UPM (ES) in LEO 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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/46276?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/46276?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

46276, 2020-061E

Orbit

LEO

Country

ES / SPN

Related business

Polytechnic University of Madrid (ES)

Manufacturer

IDR/UPM

Mission

Decayed Amateur Technology

Bus & Motor

UPMSAT-2, Unknown motor

Mass

45 kg wet, 45 kg dry

Launch date (UTC)

2020-09-03 (5 years ago)

Launch vehicle

VEGA

Launch site

French Guiana (FRGUI)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box, Unknown HBR

Radar Cross Section

0.425 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 5 days ago

TLE from 5 days ago

0 UPMSAT-2
1 46276U 20061E   25284.11510829  .12115553  24945-5  13983-3 0  9991
2 46276  97.2106   5.1352 0012001 257.8540 102.1421 16.49625583285008

Epoch: 2025-10-11T02:45Z

TLE epoch observation values (Epoch: 2025-10-11T02:45:45.356Z)

Latitude

0.00001°

Longitude

-56.25501°

Altitude

145.246 km

Speed

7.818 km/s

True Right ascension

00h 20m 32s

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

10:39:15

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

144.927 km

Perigee altitude

129.289 km

Semi-major axis

6,515.245 km

Eccentricity

0.0012

Inclination

97.2106°

RAAN

5.1352°

Arg. of periapsis

257.854°

True anomaly

102.2765°

Mean anomaly

102.1421°

Eccentric anomaly

102.20931°

Mean motion

4.12712 °/min

Orbital period

87.23 mins

BSTAR

0.00013983

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

FLOCK 4V 20, 46612 (Decayed)

LEMUR 2 SCHMIDTFALL, 46315 (Decayed)

FLOCK 4V 14, 46286 (Decayed)

SPACEBEE-14, 46311 (Decayed)

SPACEBEE-13, 46310 (Decayed)

OSM-1 CICERO, 46294 (Decayed)

FLOCK 4V 22, 46735 (Decayed)

GHGSAT-C1, 46278

ION-MK01, 46274

FLOCK 4V 15, 46528 (Decayed)

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

SPACEBEE-21, 46300 (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

UPMSAT-2 Visibility

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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.
UPMSAT-2 is likely not visible in the next few days.

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

Please sign-in to view Co-orbital & Co-planar RSOs.

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out UPMSAT-2, 46276 on other resources

View UPMSAT-2, 46276 on NASA - NSSDCA Website

View UPMSAT-2, 46276 on Heavens-Above

View UPMSAT-2, 46276 on Keep Track

View UPMSAT-2, 46276 on Celestrak

View UPMSAT-2, 46276 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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