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NUSAT-25 (MARIA TELKES), 52171

Orbit data source: Space-Track

NUSAT-25 (MARIA TELKES), 52171 is a payload satellite owned by URUGUS S.A. (AR) in SSO that was launched on Fri, 01 Apr 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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

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Iframe URL

https://www.satcat.com/sats-embedded/52171?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

52171, 2022-033Q

Orbit

SSO

Country

Unknown / ARGN

Related business

Satellogic Inc (US)

Manufacturer

URUGUS S.A.

Mission

Operational Commercial Imaging

Bus & Motor

NEWSAT IV, Unknown motor

Mass

41.5 kg wet, 38.5 kg dry

Launch date (UTC)

2022-04-01 (4 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box, 1.0 m

Radar Cross Section

0.542 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago

0 NUSAT-25 (MARIA TELKES)
1 52171U 22033Q   25340.92710502  .00616654  16387-3  14619-2 0  9995
2 52171  97.2346  68.9535 0004459 287.6993  72.3796 15.96731673206562

Epoch: 2025-12-06T22:15Z

TLE epoch observation values (Epoch: 2025-12-06T22:15:01.873Z)

Latitude

-0.00013°

Longitude

19.24789°

Altitude

285.794 km

Speed

7.737 km/s

True Right ascension

04h 35m 48s

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

04:23:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

283.319 km

Perigee altitude

277.381 km

Semi-major axis

6,658.487 km

Eccentricity

0.00045

Inclination

97.2346°

RAAN

68.9535°

Arg. of periapsis

287.6993°

True anomaly

72.42831°

Mean anomaly

72.3796°

Eccentric anomaly

72.40395°

Mean motion

3.99466 °/min

Orbital period

90.12 mins

BSTAR

0.0014619

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Other satellites on launch #33 in the year 2022 (2022-04-01 UTC)

SPACEBEE-130, 52176 (Decayed)

SPACEBEE-137, 52186 (Decayed)

KSF2-D, 52190 (Decayed)

ION SCV-005, 52163 (Decayed)

SPACEBEE-128, 52182 (Decayed)

NUSAT-26 (M SOMERVILLE), 52184

KSF2-A, 52194 (Decayed)

KSF2-B, 52193 (Decayed)

HAWK-4B, 52165 (Decayed)

HAWK-4C, 52170 (Decayed)

ALFACRUX, 52160 (Decayed)

SPACEBEE-132, 52185 (Decayed)

SUCHAI-2, 52192 (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

NUSAT-25 (MARIA TELKES) 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.
NUSAT-25 (MARIA TELKES) 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

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

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Check out NUSAT-25 (MARIA TELKES), 52171 on other resources

View NUSAT-25 (MARIA TELKES), 52171 on NASA - NSSDCA Website

View NUSAT-25 (MARIA TELKES), 52171 on Heavens-Above

View NUSAT-25 (MARIA TELKES), 52171 on Keep Track

View NUSAT-25 (MARIA TELKES), 52171 on Celestrak

View NUSAT-25 (MARIA TELKES), 52171 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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