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
Unknown
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  1312U 65004C   26192.93516816  .00000096  00000-0  10459-3 0  9998
2  1312  96.3319 178.2446 1117445  59.7345 310.9582 12.28266371729620
Epoch: 2026-07-11T22:26Z
TLE epoch observation values (Epoch: 2026-07-11T22:26:38.529Z)
Latitude
0.00007°
Longitude
-88.2572°
Altitude
1,041.158 km
Speed
7.567 km/s
True Right ascension
11h 52m 58s
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
11:49:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,440.394 km
Perigee altitude
667.645 km
Semi-major axis
7,932.157 km
Eccentricity
0.11174
Inclination
96.3319°
RAAN
178.2446°
Arg. of periapsis
59.7345°
True anomaly
300.37886°
Mean anomaly
310.9582°
Eccentric anomaly
305.76295°
Mean motion
3.07225 °/min
Orbital period
117.18 mins
BSTAR
0.00010459
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)

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