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LDPE-3A, 55264

Orbit data source: Space-Track

LDPE-3A, 55264 is a payload satellite owned by AFRL/RV (US) in GEO that was launched on Sun, 15 Jan 2023 UTC via an FALCON HEAVY launch vehicle from the Air Force Eastern Test Range (AFETR). 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
55264, 2023-008B
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
NGIS
Mission
Operational Defense Technology
Bus & Motor
LDPE, Unknown motor
Mass
~500 kg wet, 500 kg dry
Launch date (UTC)
2023-01-15 (3 years ago)
Launch vehicle
FALCON HEAVY
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Pan, 1.8 m
Radar Cross Section
3.054 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 LDPE-3A
1 55264U 23008B   26171.36780369  .00000074  00000-0  00000+0 0  9994
2 55264   2.3572  81.6285 0001203  57.3943 140.0346  0.99145584 11847
Epoch: 2026-06-20T08:49Z
TLE epoch observation values (Epoch: 2026-06-20T08:49:38.238Z)
Latitude
-0.72713°
Longitude
-121.92506°
Altitude
36,108.82 km
Speed
3.063 km/s
True Right ascension
18h 36m 16s
True Declination
0° 43' 35"
Sunlit
Object was in daylight 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
21:38:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,111.466 km
Perigee altitude
36,101.244 km
Semi-major axis
42,484.492 km
Eccentricity
0.00012
Inclination
2.3572°
RAAN
81.6285°
Arg. of periapsis
57.3943°
True anomaly
140.04345°
Mean anomaly
140.0346°
Eccentric anomaly
140.03903°
Mean motion
0.24785 °/min
Orbital period
1,452.46 mins
BSTAR
0
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Other satellites on launch #8 in the year 2023 (2023-01-15 UTC)

Documentation

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