LEMUR 2 DILIGHTFUL, 58260 (Decayed)
Orbit data source: Space-Track
LEMUR 2 DILIGHTFUL, 58260 was an American payload satellite in LEO that was launched on Sat, 11 Nov 2023 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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58260 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Decayed Commercial Com/MetRO
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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 LEMUR 2 DILIGHTFUL
1 58260U 23174E 25146.12574566 .09616195 25911-5 61089-3 0 9999
2 58260 97.3814 234.6849 0025178 293.5552 66.3102 16.38527941 86632Epoch: 2025-05-26T03:01Z
TLE epoch observation values (Epoch: 2025-05-26T03:01:04.425Z)
Latitude
0°
Longitude
-54.52592°
Altitude
166.381 km
Speed
7.81 km/s
True Right ascension
15h 38m 44s
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
07:41:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
183.008 km
Perigee altitude
150.052 km
Semi-major axis
6,544.667 km
Eccentricity
0.00252
Inclination
97.3814°
RAAN
234.6849°
Arg. of periapsis
293.5552°
True anomaly
66.57474°
Mean anomaly
66.3102°
Eccentric anomaly
66.44244°
Mean motion
4.09932 °/min
Orbital period
87.82 mins
BSTAR
0.00061089
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Other satellites on launch #174 in the year 2023 (2023-11-11 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.LEMUR 2 DILIGHTFUL Visibility
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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. |
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| This satellite is decayed. |
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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