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: 4 days ago

TLE from 4 days ago
0 DELTA 1 DEB
1 01312U 65004C   25255.31116310  .00000050  00000-0  64602-4 0  9994
2 01312  96.3539  19.2692 1116868  15.2939 347.9191 12.28155794692479
Epoch: 2025-09-12T07:28Z
TLE epoch observation values (Epoch: 2025-09-12T07:28:04.491Z)
Latitude
0.00001°
Longitude
-84.31021°
Altitude
698.311 km
Speed
7.904 km/s
True Right ascension
01h 17m 04s
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
00:01:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,440.467 km
Perigee altitude
668.526 km
Semi-major axis
7,932.634 km
Eccentricity
0.11169
Inclination
96.3539°
RAAN
19.2692°
Arg. of periapsis
15.2939°
True anomaly
344.82173°
Mean anomaly
347.9191°
Eccentric anomaly
346.41613°
Mean motion
3.07197 °/min
Orbital period
117.19 mins
BSTAR
0.000064602
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)

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