DECAYED
Showing default

LEMUR 2 DILIGHTFUL, 58260 (Decayed)

Orbit data source: Space-Track

LEMUR 2 DILIGHTFUL, 58260 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.

Not visible in the next 10 days
Identifier
58260, 2023-174E
Orbit
Decayed
Country
Flag of USUS
Related 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)
2023-11-11 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 5 months ago

TLE from 5 months 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 86632
Epoch: 2025-05-26T03:01Z
TLE epoch observation values (Epoch: 2025-05-26T03:01:04.425Z)
Latitude
Longitude
-54.52592°
Altitude
166.381 km
Speed
7.81 km/s
True Right ascension
15h 38m 44s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:58:59
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
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|