DELTA 1 DEB, 27788

Orbit data source: Space-Track

DELTA 1 DEB, 27788 is space debris in LEO originally from a launch on Sat, 06 Nov 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
27788, 1965-089E
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1965-11-06 (60 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
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: 6 days ago

TLE from 6 days ago
0 DELTA 1 DEB
1 27788U 65089E   25301.49993118  .00000797  00000-0  41512-2 0  9993
2 27788  59.3774 312.4173 0606751  73.3064   7.1816 12.28595548585424
Epoch: 2025-10-28T11:59Z
TLE epoch observation values (Epoch: 2025-10-28T11:59:54.053Z)
Latitude
58.44361°
Longitude
168.85259°
Altitude
1,086.653 km
Speed
7.532 km/s
True Right ascension
01h 43m 39s
True Declination
58° 17' 48"
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
02:46:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,036.034 km
Perigee altitude
1,073.382 km
Semi-major axis
7,932.845 km
Eccentricity
0.06068
Inclination
59.3774°
RAAN
312.4173°
Arg. of periapsis
73.3064°
True anomaly
8.12124°
Mean anomaly
7.1816°
Eccentric anomaly
7.64403°
Mean motion
3.07185 °/min
Orbital period
117.19 mins
BSTAR
0.0041512
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