DELTA 1 DEB, 14528

Orbit data source: Space-Track

DELTA 1 DEB, 14528 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
14528, 1977-065FP
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, 0.086 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DELTA 1 DEB
1 14528U 77065FP  26312.05633002  .00000264  00000-0  10934-2 0  9999
2 14528  28.0736 213.6433 0316429 232.5705 124.5613 12.46648665594052
Epoch: 2026-11-08T01:21Z
TLE epoch observation values (Epoch: 2026-11-08T01:21:06.913Z)
Latitude
-0.00005°
Longitude
146.11168°
Altitude
1,623.173 km
Speed
6.995 km/s
True Right ascension
14h 14m 34s
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
01:30:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,731.026 km
Perigee altitude
1,233.572 km
Semi-major axis
7,860.436 km
Eccentricity
0.03164
Inclination
28.0736°
RAAN
213.6433°
Arg. of periapsis
232.5705°
True anomaly
127.48054°
Mean anomaly
124.5613°
Eccentric anomaly
126.02754°
Mean motion
3.11439 °/min
Orbital period
115.59 mins
BSTAR
0.0010934
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