LEMUR 2 GOOD-VIBES, 58263 (Decayed)
Orbit data source: Space-Track
LEMUR 2 GOOD-VIBES, 58263 was a payload satellite owned by Spire (US) 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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58263 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Decayed Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4.6 kg wet, 4.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.054 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 LEMUR 2 GOOD-VIBES
1 58263U 23174H 25146.37121936 .14329262 25741-5 30732-3 0 9992
2 58263 97.3572 234.3138 0019003 284.4741 75.4452 16.45008202 86678Epoch: 2025-05-26T08:54Z
TLE epoch observation values (Epoch: 2025-05-26T08:54:33.352Z)
Latitude
-0.0001°
Longitude
-143.50948°
Altitude
152.676 km
Speed
7.816 km/s
True Right ascension
15h 37m 15s
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
08:29:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
161.717 km
Perigee altitude
136.909 km
Semi-major axis
6,527.45 km
Eccentricity
0.0019
Inclination
97.3572°
RAAN
234.3138°
Arg. of periapsis
284.4741°
True anomaly
75.6561°
Mean anomaly
75.4452°
Eccentric anomaly
75.55064°
Mean motion
4.11555 °/min
Orbital period
87.47 mins
BSTAR
0.00030732
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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 GOOD-VIBES 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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