DELTA 1 DEB, 1313

Orbit data source: Space-Track

DELTA 1 DEB, 1313 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
1313, 1965-004D
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 01313U 65004D   25257.72948571 -.00000050  00000-0 -55456-4 0  9993
2 01313  96.4332 331.8087 1172580 190.1043 167.4427 12.00813994653382
Epoch: 2025-09-14T17:30Z
TLE epoch observation values (Epoch: 2025-09-14T17:30:27.565Z)
Latitude
-0.00005°
Longitude
75.24954°
Altitude
2,606.482 km
Speed
6.267 km/s
True Right ascension
22h 07m 14s
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
00:00:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,618.778 km
Perigee altitude
730.297 km
Semi-major axis
8,052.675 km
Eccentricity
0.11726
Inclination
96.4332°
RAAN
331.8087°
Arg. of periapsis
190.1043°
True anomaly
169.99614°
Mean anomaly
167.4427°
Eccentric anomaly
168.75304°
Mean motion
3.00354 °/min
Orbital period
119.86 mins
BSTAR
-0.000055456
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)

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