NUSAT-52, 66692
Orbit data source: Space-Track
NUSAT-52, 66692 is a payload satellite owned by URUGUS S.A. (AR) in SSO that was launched on Fri, 28 Nov 2025 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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66692 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ARGNRelated business
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)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m²
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 NUSAT-52
1 66692U 25276AC 26034.48471718 .00007666 00000-0 37894-3 0 9995
2 66692 97.4351 110.3363 0004402 113.2831 246.8867 15.18109068 10120Epoch: 2026-02-03T11:37Z
TLE epoch observation values (Epoch: 2026-02-03T11:37:59.564Z)
Latitude
0.00001°
Longitude
162.17313°
Altitude
515.835 km
Speed
7.605 km/s
True Right ascension
07h 21m 20s
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
07:46:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.557 km
Perigee altitude
505.494 km
Semi-major axis
6,886.662 km
Eccentricity
0.00044
Inclination
97.4351°
RAAN
110.3363°
Arg. of periapsis
113.2831°
True anomaly
246.84032°
Mean anomaly
246.8867°
Eccentric anomaly
246.86351°
Mean motion
3.79778 °/min
Orbital period
94.79 mins
BSTAR
0.00037894
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Other satellites on launch #276 in the year 2025 (2025-11-28 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.NUSAT-52 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 | 2026-02-04 18:16:05.034Z | 340.687° N | 2026-02-04 18:18:05.034Z | 274.814° WNW | 32.355° | 2026-02-04 18:21:05.034Z | 217.83° SW |
| 6 mins | 2026-02-05 04:54:05.034Z | 159.454° S | 2026-02-05 04:56:05.034Z | 127.768° SE | 42.811° | 2026-02-05 05:00:05.034Z | 351.51° N |
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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