Showing default

LEMUR 2 JK0903EM1407, 58336

Orbit data source: Space-Track

LEMUR 2 JK0903EM1407, 58336 is an American payload satellite in SSO 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.

Loading next visibility...
Identifier
58336, 2023-174CJ
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Earth Obs Sci
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 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, 0.2 m
Radar Cross Section
0.240 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 LEMUR 2 JK0903EM1407
1 58336U 23174CJ  25334.96930045  .00022938  00000-0  54855-3 0  9999
2 58336  97.4049  56.3496 0007014 110.0505 250.1498 15.41461792115092
Epoch: 2025-11-30T23:15Z
TLE epoch observation values (Epoch: 2025-11-30T23:15:47.558Z)
Latitude
0.00002°
Longitude
-2.67409°
Altitude
446.541 km
Speed
7.643 km/s
True Right ascension
03h 45m 23s
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
07:37:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.513 km
Perigee altitude
433.95 km
Semi-major axis
6,816.869 km
Eccentricity
0.0007
Inclination
97.4049°
RAAN
56.3496°
Arg. of periapsis
110.0505°
True anomaly
250.07422°
Mean anomaly
250.1498°
Eccentric anomaly
250.11201°
Mean motion
3.85626 °/min
Orbital period
93.35 mins
BSTAR
0.00054855
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
|