DELTA 1 DEB, 2224

Orbit data source: Space-Track

DELTA 1 DEB, 2224 is space debris in SSO originally from a launch on Mon, 28 Feb 1966 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
2224, 1966-016D
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)
1966-02-28 (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: 4 days ago

TLE from 4 days ago
0 DELTA 1 DEB
1 02224U 66016D   25310.63002611 -.00000021  00000-0  12954-3 0  9997
2 02224 101.1417 238.9165 0137564 303.8608 179.4419 12.52166722718044
Epoch: 2025-11-06T15:07Z
TLE epoch observation values (Epoch: 2025-11-06T15:07:14.255Z)
Latitude
55.1659°
Longitude
162.37979°
Altitude
1,572.178 km
Speed
7.038 km/s
True Right ascension
05h 01m 05s
True Declination
55° 01' 16"
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
15:39:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,560.681 km
Perigee altitude
1,345.226 km
Semi-major axis
7,831.091 km
Eccentricity
0.01376
Inclination
101.1417°
RAAN
238.9165°
Arg. of periapsis
303.8608°
True anomaly
179.45699°
Mean anomaly
179.4419°
Eccentric anomaly
179.44947°
Mean motion
3.13191 °/min
Orbital period
114.95 mins
BSTAR
0.00012954
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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

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