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 (48 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
Small (<0.1 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  25302.85807282  .00000080  00000-0  69652-4 0  9997
2 14528  28.0755   5.7312 0313834 143.3326 218.9097 12.46527546547331
Epoch: 2025-10-29T20:35Z
TLE epoch observation values (Epoch: 2025-10-29T20:35:37.491Z)
Latitude
-0.00002°
Longitude
18.39977°
Altitude
1,672.271 km
Speed
6.952 km/s
True Right ascension
00h 22m 55s
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
00:20:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,729.511 km
Perigee altitude
1,236.104 km
Semi-major axis
7,860.945 km
Eccentricity
0.03138
Inclination
28.0755°
RAAN
5.7312°
Arg. of periapsis
143.3326°
True anomaly
216.71842°
Mean anomaly
218.9097°
Eccentric anomaly
217.80743°
Mean motion
3.11409 °/min
Orbital period
115.6 mins
BSTAR
0.000069652
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