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: 22 hours ago
TLE from 22 hours ago
0 LEMU-NGE
1 60532U 24149BS 26259.47237838 .00001707 00000-0 16022-3 0 9991
2 60532 97.6768 332.5703 0002497 86.5208 273.6298 14.95253358113596Epoch: 2026-09-16T11:20Z
TLE epoch observation values (Epoch: 2026-09-16T11:20:13.492Z)
Latitude
-0.00004°
Longitude
167.09061°
Altitude
584.526 km
Speed
7.568 km/s
True Right ascension
22h 10m 16s
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
02:02:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.334 km
Perigee altitude
576.86 km
Semi-major axis
6,956.734 km
Eccentricity
0.00025
Inclination
97.6768°
RAAN
332.5703°
Arg. of periapsis
86.5208°
True anomaly
273.60124°
Mean anomaly
273.6298°
Eccentric anomaly
273.61552°
Mean motion
3.74055 °/min
Orbital period
96.24 mins
BSTAR
0.00016022
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-17 16:50:32.643Z | 59.659° ENE | 2026-09-17 16:52:32.643Z | 92.254° ESE | 16.919° | 2026-09-17 16:54:32.643Z | 125.322° SE |
| 6 mins | 2026-09-17 18:25:32.643Z | 344.818° N | 2026-09-17 18:28:32.643Z | 271.524° WNW | 34.437° | 2026-09-17 18:31:32.643Z | 223.525° SW |
| 6 mins | 2026-09-18 05:13:32.643Z | 182.019° SSW | 2026-09-18 05:16:32.643Z | 279.367° WNW | 61.013° | 2026-09-18 05:19:32.643Z | 338.441° N |
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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