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LEMUR 2 HUBBLE-4, 64565

Orbit data source: Space-Track

LEMUR 2 HUBBLE-4, 64565 is an American payload satellite in SSO that was launched on Mon, 23 Jun 2025 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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Identifier
64565, 2025-135AP
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
2025-06-23 (10 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 4 Pan, 1.4 m
Radar Cross Section
0.326 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 LEMUR 2 HUBBLE-4
1 64565U 25135AP  26119.89094226  .00001596  00000-0  15873-3 0  9999
2 64565  97.7639 234.3929 0003982  93.7123 266.4552 14.93061452 46665
Epoch: 2026-04-29T21:22Z
TLE epoch observation values (Epoch: 2026-04-29T21:22:57.411Z)
Latitude
Longitude
55.80828°
Altitude
591.612 km
Speed
7.564 km/s
True Right ascension
15h 37m 34s
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
16:38:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.187 km
Perigee altitude
582.641 km
Semi-major axis
6,963.551 km
Eccentricity
0.0004
Inclination
97.7639°
RAAN
234.3929°
Arg. of periapsis
93.7123°
True anomaly
266.40966°
Mean anomaly
266.4552°
Eccentric anomaly
266.43243°
Mean motion
3.73506 °/min
Orbital period
96.38 mins
BSTAR
0.00015873
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