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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Identifier
Orbit
Country
CL / 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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LEMU-NGE
1 60532U 24149BS 26269.17567273 .00001351 00000-0 12784-3 0 9994
2 60532 97.6762 342.0709 0002354 70.5807 289.5669 14.95281406115047Epoch: 2026-09-26T04:12Z
TLE epoch observation values (Epoch: 2026-09-26T04:12:58.123Z)
Latitude
0.00003°
Longitude
-86.15879°
Altitude
584 km
Speed
7.569 km/s
True Right ascension
22h 48m 17s
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
14:18:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.148 km
Perigee altitude
576.872 km
Semi-major axis
6,956.647 km
Eccentricity
0.00024
Inclination
97.6762°
RAAN
342.0709°
Arg. of periapsis
70.5807°
True anomaly
289.54148°
Mean anomaly
289.5669°
Eccentric anomaly
289.55419°
Mean motion
3.74062 °/min
Orbital period
96.24 mins
BSTAR
0.00012784
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-27 04:26:44.257Z | 131.756° SE | 2026-09-27 04:29:44.257Z | 67.343° ENE | 35.547° | 2026-09-27 04:32:44.257Z | 9.738° NNE |
| 4 mins | 2026-09-27 06:03:44.257Z | 243.729° WSW | 2026-09-27 06:04:44.257Z | 260.871° W | 16.817° | 2026-09-27 06:07:44.257Z | 307.921° NW |
| 7 mins | 2026-09-27 17:43:44.257Z | 18.427° NNE | 2026-09-27 17:46:44.257Z | 99.55° ESE | 72.952° | 2026-09-27 17:50:44.257Z | 186.756° SSW |
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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