LEMUR 2 SANITA-VETRA, 58267 (Decayed)
Orbit data source: Space-Track
LEMUR 2 SANITA-VETRA, 58267 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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58267 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 SANITA-VETRA
1 58267U 23174M 25154.21356369 .07824277 25184-5 13366-2 0 9990
2 58267 97.3750 242.7761 0023472 286.1126 73.7586 16.32171300 87908Epoch: 2025-06-03T05:07Z
TLE epoch observation values (Epoch: 2025-06-03T05:07:31.902Z)
Latitude
0.00002°
Longitude
-86.02094°
Altitude
185.675 km
Speed
7.797 km/s
True Right ascension
16h 11m 06s
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
21:12:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
198.929 km
Perigee altitude
168.126 km
Semi-major axis
6,561.665 km
Eccentricity
0.00235
Inclination
97.375°
RAAN
242.7761°
Arg. of periapsis
286.1126°
True anomaly
74.01705°
Mean anomaly
73.7586°
Eccentric anomaly
73.8878°
Mean motion
4.0834 °/min
Orbital period
88.16 mins
BSTAR
0.0013366
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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 SANITA-VETRA 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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