DELTA 1 DEB, 27720

Orbit data source: Space-Track

DELTA 1 DEB, 27720 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
27720, 1965-004E
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
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
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 week ago

TLE from 1 week ago
0 DELTA 1 DEB
1 27720U 65004E   26184.92248368  .00000194  00000-0  27058-3 0  9995
2 27720  96.4940  64.2815 1166976 331.5282  22.6516 12.09263013517235
Epoch: 2026-07-03T22:08Z
TLE epoch observation values (Epoch: 2026-07-03T22:08:22.589Z)
Latitude
-0.00008°
Longitude
170.24382°
Altitude
797.993 km
Speed
7.837 km/s
True Right ascension
04h 17m 07s
True Declination
0° 00' 00"
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
11:52:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,572.305 km
Perigee altitude
701.619 km
Semi-major axis
8,015.099 km
Eccentricity
0.1167
Inclination
96.494°
RAAN
64.2815°
Arg. of periapsis
331.5282°
True anomaly
28.58619°
Mean anomaly
22.6516°
Eccentric anomaly
25.53366°
Mean motion
3.02468 °/min
Orbital period
119.02 mins
BSTAR
0.00027058
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)

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