DELTA 1 DEB, 14565

Orbit data source: Space-Track

DELTA 1 DEB, 14565 is space debris in LEO originally from a launch on Thu, 14 Jul 1977 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
14565, 1977-065FT
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1977-07-14 (49 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 DELTA 1 DEB
1 14565U 77065FT  26263.19356014  .00002293  00000-0  38955-2 0  9992
2 14565  29.2124 290.2275 0842762 254.2639  96.3450 12.50123618 53790
Epoch: 2026-09-20T04:38Z
TLE epoch observation values (Epoch: 2026-09-20T04:38:43.596Z)
Latitude
-0.00001°
Longitude
-138.54542°
Altitude
1,589.509 km
Speed
7.019 km/s
True Right ascension
19h 20m 54s
True Declination
0° 00' 00"
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
02:37:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,128.844 km
Perigee altitude
806.421 km
Semi-major axis
7,845.769 km
Eccentricity
0.08428
Inclination
29.2124°
RAAN
290.2275°
Arg. of periapsis
254.2639°
True anomaly
105.78979°
Mean anomaly
96.345°
Eccentric anomaly
101.0836°
Mean motion
3.12313 °/min
Orbital period
115.27 mins
BSTAR
0.0038955
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