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
Cyl + 1 Cable, 1.8 m
Radar Cross Section
3.500 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 DELTA 1 DEB
1 02224U 66016D   25260.30130605 -.00000012  00000-0  17860-3 0  9991
2 02224 101.1339 191.7566 0138320  43.0754 108.0751 12.52163254711748
Epoch: 2025-09-17T07:13Z
TLE epoch observation values (Epoch: 2025-09-17T07:13:52.842Z)
Latitude
26.83035°
Longitude
-87.50784°
Altitude
1,493.432 km
Speed
7.104 km/s
True Right ascension
01h 09m 45s
True Declination
26° 42' 18"
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
13:55:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,561.288 km
Perigee altitude
1,344.648 km
Semi-major axis
7,831.105 km
Eccentricity
0.01383
Inclination
101.1339°
RAAN
191.7566°
Arg. of periapsis
43.0754°
True anomaly
109.5737°
Mean anomaly
108.0751°
Eccentric anomaly
108.82522°
Mean motion
3.13191 °/min
Orbital period
114.95 mins
BSTAR
0.0001786
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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

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