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, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LEMU-NGE
1 60532U 24149BS 26192.74885853 .00001456 00000-0 13816-3 0 9992
2 60532 97.6835 267.2124 0000636 71.0274 289.1016 14.95050620103627Epoch: 2026-07-11T17:58Z
TLE epoch observation values (Epoch: 2026-07-11T17:58:21.376Z)
Latitude
-0.00002°
Longitude
67.96572°
Altitude
585.119 km
Speed
7.568 km/s
True Right ascension
17h 48m 50s
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
09:24:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.669 km
Perigee altitude
578.784 km
Semi-major axis
6,957.364 km
Eccentricity
0.00006
Inclination
97.6835°
RAAN
267.2124°
Arg. of periapsis
71.0274°
True anomaly
289.09471°
Mean anomaly
289.1016°
Eccentric anomaly
289.09816°
Mean motion
3.74004 °/min
Orbital period
96.26 mins
BSTAR
0.00013816
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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 | 2026-07-13 05:26:39.985Z | 196.352° SSW | 2026-07-13 05:29:39.985Z | 282.153° WNW | 34.15° | 2026-07-13 05:32:39.985Z | 332.34° NNW |
| 5 mins | 2026-07-13 17:08:39.985Z | 49.378° ENE | 2026-07-13 17:10:39.985Z | 86.675° E | 23.119° | 2026-07-13 17:13:39.985Z | 145.285° SSE |
| 4 mins | 2026-07-13 18:44:39.985Z | 324.533° NNW | 2026-07-13 18:46:39.985Z | 282.125° WNW | 21.644° | 2026-07-13 18:48:39.985Z | 246.682° WSW |
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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