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NUSAT-43 (R DIENG-KUNTZ), 56968

Orbit data source: Space-Track

NUSAT-43 (R DIENG-KUNTZ), 56968 is a payload satellite owned by URUGUS S.A. (AR) in SSO that was launched on Mon, 12 Jun 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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https://www.satcat.com/sats-embedded/56968?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

56968, 2023-084AN

Orbit

SSO

Country

Unknown / ARGN

Related business

Satellogic Inc (US)

Manufacturer

URUGUS S.A.

Mission

Operational Commercial Imaging

Bus & Motor

NEWSAT V, Unknown motor

Mass

41.5 kg wet, 38.5 kg dry

Launch date (UTC)

2023-06-12 (3 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

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: 6 hours ago

TLE from 6 hours ago

0 NUSAT-43 (R DIENG-KUNTZ)
1 56968U 23084AN  25354.91334187  .00047480  00000-0  59008-3 0  9994
2 56968  97.4345 127.6198 0005440 160.5524 199.5941 15.59834819141230

Epoch: 2025-12-20T21:55Z

TLE epoch observation values (Epoch: 2025-12-20T21:55:12.737Z)

Latitude

-0.00004°

Longitude

69.08341°

Altitude

394.747 km

Speed

7.671 km/s

True Right ascension

08h 30m 28s

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

03:12:18

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

388.728 km

Perigee altitude

381.37 km

Semi-major axis

6,763.186 km

Eccentricity

0.00054

Inclination

97.4345°

RAAN

127.6198°

Arg. of periapsis

160.5524°

True anomaly

199.57321°

Mean anomaly

199.5941°

Eccentric anomaly

199.58365°

Mean motion

3.90226 °/min

Orbital period

92.25 mins

BSTAR

0.00059008

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Other satellites on launch #84 in the year 2023 (2023-06-12 UTC)

MUSAT1, 56967 (Decayed)

AYRIS-2, 56986 (Decayed)

ICEYE-X26, 56961

ELO-4, 56990 (Decayed)

ORBITER SN3, 56960

SPACEBEE-177, 56972 (Decayed)

OTTER PUP, 56933

SPACEBEE-169, 56982 (Decayed)

BLACKJACK ACES-1, 56956

GEISAT PRECURSOR, 56934

SPACEBEE-178, 56973 (Decayed)

TOMORROW-R2, 56962

DROID-001, 56965

SPEI SATELLES, 56991 (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-43 (R DIENG-KUNTZ) 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	2025-12-21 08:49:49.204Z	149.333° SSE	2025-12-21 08:52:49.204Z	41.494° NE	34.694°	2025-12-21 08:54:49.204Z	1.409° NNE

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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 NUSAT-43 (R DIENG-KUNTZ), 56968 on other resources

View NUSAT-43 (R DIENG-KUNTZ), 56968 on NASA - NSSDCA Website

View NUSAT-43 (R DIENG-KUNTZ), 56968 on Heavens-Above

View NUSAT-43 (R DIENG-KUNTZ), 56968 on Keep Track

View NUSAT-43 (R DIENG-KUNTZ), 56968 on Celestrak

View NUSAT-43 (R DIENG-KUNTZ), 56968 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

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