LEMU-NGE, 60532
Orbit data source: Space-Track
LEMU-NGE, 60532 is a Chilean payload satellite in SSO that was launched on Fri, 16 Aug 2024 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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60532 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / CHLERelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 LEMU-NGE
1 60532U 24149BS 25364.15479262 .00005666 00000-0 51508-3 0 9997
2 60532 97.7023 77.4531 0001525 139.0532 221.0804 14.95617216 74706Epoch: 2025-12-30T03:42Z
TLE epoch observation values (Epoch: 2025-12-30T03:42:54.082Z)
Latitude
0.00001°
Longitude
-77.11438°
Altitude
584.306 km
Speed
7.568 km/s
True Right ascension
05h 09m 48s
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
09:20:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.53 km
Perigee altitude
576.408 km
Semi-major axis
6,955.606 km
Eccentricity
0.00015
Inclination
97.7023°
RAAN
77.4531°
Arg. of periapsis
139.0532°
True anomaly
221.06892°
Mean anomaly
221.0804°
Eccentric anomaly
221.07466°
Mean motion
3.74146 °/min
Orbital period
96.22 mins
BSTAR
0.00051508
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Other satellites on launch #149 in the year 2024 (2024-08-16 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.LEMU-NGE 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 | 2025-12-30 17:08:44.600Z | 48.137° ENE | 2025-12-30 17:11:44.600Z | 103.802° ESE | 21.152° | 2025-12-30 17:13:44.600Z | 139.275° SSE |
| 5 mins | 2025-12-30 18:44:44.600Z | 330.371° NNW | 2025-12-30 18:46:44.600Z | 287.546° WNW | 23.638° | 2025-12-30 18:49:44.600Z | 236.181° WSW |
| 6 mins | 2025-12-31 05:32:44.600Z | 202.235° SSW | 2025-12-31 05:34:44.600Z | 255.631° W | 34.198° | 2025-12-31 05:38:44.600Z | 333.554° NNW |
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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