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 (62 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CABLE + BOX, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 DELTA 1 DEB
1 01312U 65004C   26275.28221366 -.00000007  00000-0  12678-4 0  9990
2 01312  96.3467 221.4735 1115004 235.8046 113.2429 12.28283064739735
Epoch: 2026-10-02T06:46Z
TLE epoch observation values (Epoch: 2026-10-02T06:46:23.260Z)
Latitude
-0.00008°
Longitude
108.87019°
Altitude
1,986.201 km
Speed
6.716 km/s
True Right ascension
14h 45m 53s
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
15:04:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,438.379 km
Perigee altitude
669.518 km
Semi-major axis
7,932.085 km
Eccentricity
0.1115
Inclination
96.3467°
RAAN
221.4735°
Arg. of periapsis
235.8046°
True anomaly
124.30118°
Mean anomaly
113.2429°
Eccentric anomaly
118.83909°
Mean motion
3.07229 °/min
Orbital period
117.18 mins
BSTAR
0.000012678
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)

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