DELTA 1 DEB, 3812

Orbit data source: Space-Track

DELTA 1 DEB, 3812 is space debris in SSO originally from a launch on Sun, 15 Dec 1968 UTC launched from the Air Force Western Test Range (AFWTR). 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
3812, 1968-114D
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Icon of a cake. It is the launch day of the satellite!1968-12-15 (57 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
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  3812U 68114D   25345.99886632 -.00000006  00000-0  30893-3 0  9997
2  3812 102.4542 359.7954 0070686 153.7008 281.6418 12.37782781574469
Epoch: 2025-12-11T23:58Z
TLE epoch observation values (Epoch: 2025-12-11T23:58:22.050Z)
Latitude
70.32445°
Longitude
-118.66913°
Altitude
1,517.101 km
Speed
7.118 km/s
True Right ascension
21h 27m 28s
True Declination
70° 13' 32"
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
13:22:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,569.405 km
Perigee altitude
1,457.837 km
Semi-major axis
7,891.758 km
Eccentricity
0.00707
Inclination
102.4542°
RAAN
359.7954°
Arg. of periapsis
153.7008°
True anomaly
280.84707°
Mean anomaly
281.6418°
Eccentric anomaly
281.24457°
Mean motion
3.09587 °/min
Orbital period
116.28 mins
BSTAR
0.00030893
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