DELTA 1 DEB, 39102

Orbit data source: Space-Track

DELTA 1 DEB, 39102 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
39102, 1977-065GP
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: 4 days ago

TLE from 4 days ago
0 DELTA 1 DEB
1 39102U 77065GP  25347.01502440  .00000354  00000-0  90805-4 0  9995
2 39102  28.9910 243.6544 0926850 297.2949  53.6203 13.03293665531507
Epoch: 2025-12-13T00:21Z
TLE epoch observation values (Epoch: 2025-12-13T00:21:38.108Z)
Latitude
-0.00001°
Longitude
156.29723°
Altitude
874.519 km
Speed
7.596 km/s
True Right ascension
16h 14m 37s
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
19:05:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,960.3 km
Perigee altitude
545.714 km
Semi-major axis
7,631.144 km
Eccentricity
0.09269
Inclination
28.991°
RAAN
243.6544°
Arg. of periapsis
297.2949°
True anomaly
62.76093°
Mean anomaly
53.6203°
Eccentric anomaly
58.13021°
Mean motion
3.25581 °/min
Orbital period
110.57 mins
BSTAR
0.000090805
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