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 25302.47019605 .00004301 00000-0 39420-3 0 9999
2 60532 97.7073 16.7961 0002240 81.5304 278.6171 14.95429606 65481Epoch: 2025-10-29T11:17Z
TLE epoch observation values (Epoch: 2025-10-29T11:17:04.938Z)
Latitude
-0.00001°
Longitude
169.48265°
Altitude
583.855 km
Speed
7.569 km/s
True Right ascension
01h 07m 11s
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
13:13:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.609 km
Perigee altitude
576.493 km
Semi-major axis
6,956.188 km
Eccentricity
0.00022
Inclination
97.7073°
RAAN
16.7961°
Arg. of periapsis
81.5304°
True anomaly
278.59172°
Mean anomaly
278.6171°
Eccentric anomaly
278.60441°
Mean motion
3.74099 °/min
Orbital period
96.23 mins
BSTAR
0.0003942
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-29 18:16:33.676Z | 358.944° N | 2025-10-29 18:19:33.676Z | 287.892° WNW | 38.93° | 2025-10-29 18:23:33.676Z | 208.943° SW |
| 6 mins | 2025-10-30 05:05:33.676Z | 164.137° S | 2025-10-30 05:07:33.676Z | 141.578° SSE | 44.611° | 2025-10-30 05:11:33.676Z | 348.772° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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