DELTA 1 DEB, 1312

Orbit data source: Space-Track

DELTA 1 DEB, 1312 is space debris in SSO originally from a launch on Fri, 22 Jan 1965 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
1312, 1965-004C
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~1 kg wet, ~1 kg dry
Launch date (UTC)
1965-01-22 (61 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Cable, 1.8 m
Radar Cross Section
6.125 m², Small (<0.1 m²)

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

TLE from 2 days ago
0 DELTA 1 DEB
1 01312U 65004C   25260.27995520  .00000083  00000-0  98874-4 0  9997
2 01312  96.3554  21.8820 1116617   4.2066 356.7508 12.28156877693080
Epoch: 2025-09-17T06:43Z
TLE epoch observation values (Epoch: 2025-09-17T06:43:08.129Z)
Latitude
-0.00004°
Longitude
-75.36004°
Altitude
675.529 km
Speed
7.927 km/s
True Right ascension
01h 27m 31s
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
12:35:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,440.263 km
Perigee altitude
668.721 km
Semi-major axis
7,932.629 km
Eccentricity
0.11166
Inclination
96.3554°
RAAN
21.882°
Arg. of periapsis
4.2066°
True anomaly
355.90908°
Mean anomaly
356.7508°
Eccentric anomaly
356.3427°
Mean motion
3.07197 °/min
Orbital period
117.19 mins
BSTAR
0.000098874
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)

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