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
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 9 months ago

TLE from 9 months ago
0 DELTA 1 DEB
1 27788U 65089E   24355.68815587  .00000327  00000-0  19033-2 0  9997
2 27788  59.3860 334.6826 0615575 217.0709 321.5455 12.28013798547116
Epoch: 2024-12-20T16:30Z
TLE epoch observation values (Epoch: 2024-12-20T16:30:56.667Z)
Latitude
5.14849°
Longitude
174.15588°
Altitude
1,188.603 km
Speed
7.428 km/s
True Right ascension
10h 06m 34s
True Declination
5° 07' 11"
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
10:22:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,045.692 km
Perigee altitude
1,068.732 km
Semi-major axis
7,935.349 km
Eccentricity
0.06156
Inclination
59.386°
RAAN
334.6826°
Arg. of periapsis
217.0709°
True anomaly
316.88337°
Mean anomaly
321.5455°
Eccentric anomaly
319.24289°
Mean motion
3.07039 °/min
Orbital period
117.25 mins
BSTAR
0.0019033
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