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
Unknown
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 DELTA 1 DEB
1  2223U 66016C   25293.01236294  .00000004  00000-0  18282-3 0  9994
2  2223 100.7620 324.9218 0093627   7.2566  63.7705 12.87760829796043
Epoch: 2025-10-20T00:17Z
TLE epoch observation values (Epoch: 2025-10-20T00:17:48.158Z)
Latitude
69.19232°
Longitude
-98.09498°
Altitude
1,290.996 km
Speed
7.232 km/s
True Right ascension
19h 40m 18s
True Declination
69° 05' 09"
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
05:33:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,379.826 km
Perigee altitude
1,235.902 km
Semi-major axis
7,686.001 km
Eccentricity
0.00936
Inclination
100.762°
RAAN
324.9218°
Arg. of periapsis
7.2566°
True anomaly
64.73787°
Mean anomaly
63.7705°
Eccentric anomaly
64.25369°
Mean motion
3.22101 °/min
Orbital period
111.77 mins
BSTAR
0.00018282
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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

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