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 (61 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
DISK + CABLE, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 DELTA 1 DEB
1 02224U 66016D   26308.20643878 -.00000029  00000-0  82378-4 0  9990
2 02224 101.1490 219.0238 0137821 308.2790 211.0751 12.52182744763429
Epoch: 2026-11-04T04:57Z
TLE epoch observation values (Epoch: 2026-11-04T04:57:16.310Z)
Latitude
21.03415°
Longitude
-74.42692°
Altitude
1,550.557 km
Speed
7.051 km/s
True Right ascension
02h 53m 23s
True Declination
20° 55' 51"
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
18:47:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,560.815 km
Perigee altitude
1,344.959 km
Semi-major axis
7,831.024 km
Eccentricity
0.01378
Inclination
101.149°
RAAN
219.0238°
Arg. of periapsis
308.279°
True anomaly
210.27181°
Mean anomaly
211.0751°
Eccentric anomaly
210.67228°
Mean motion
3.13195 °/min
Orbital period
114.94 mins
BSTAR
0.000082378
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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

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