DELTA 1 DEB, 2223

Orbit data source: Space-Track

DELTA 1 DEB, 2223 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
2223, 1966-016C
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: 2 days ago

TLE from 2 days ago
0 DELTA 1 DEB
1 02223U 66016C   25241.03827429 -.00000025  00000-0  68783-4 0  9991
2 02223 100.7688 274.6666 0094211 118.0135 315.8058 12.87757410789358
Epoch: 2025-08-29T00:55Z
TLE epoch observation values (Epoch: 2025-08-29T00:55:06.898Z)
Latitude
70.08767°
Longitude
-108.09932°
Altitude
1,270.825 km
Speed
7.251 km/s
True Right ascension
16h 12m 41s
True Declination
69° 59' 05"
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
05:41:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,380.289 km
Perigee altitude
1,235.467 km
Semi-major axis
7,686.015 km
Eccentricity
0.00942
Inclination
100.7688°
RAAN
274.6666°
Arg. of periapsis
118.0135°
True anomaly
315.04685°
Mean anomaly
315.8058°
Eccentric anomaly
315.42697°
Mean motion
3.221 °/min
Orbital period
111.77 mins
BSTAR
0.000068783
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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

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