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
Last TLE update
10 hours ago
Origin
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
1966-02-28 (59 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

TLE from 10 hours ago
0 DELTA 1 DEB
1  2223U 66016C   25199.08231606 -.00000038  00000-0  22166-4 0  9993
2  2223 100.7708 234.0729 0093329 207.4804 211.4550 12.87755504784395
Epoch: 2025-07-18T01:58Z
TLE epoch observation values (Epoch: 2025-07-18T01:58:32.107Z)
Latitude
56.87319°
Longitude
-108.56217°
Altitude
1,381.221 km
Speed
7.145 km/s
True Right ascension
14h 28m 50s
True Declination
56° 43' 42"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
62.74097°
Longitude
110.24157°
Altitude
1,322.085 km
Speed
7.201 km/s
Apparent Right ascension
09h 34m 09s
Apparent Declination
28° 48' 39"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
00:21:24
Azimuth
36.529° NE
Elevation
-11.049°
Doppler factor
1
Orbital elements
Apogee altitude
1,379.619 km
Perigee altitude
1,236.153 km
Semi-major axis
7,686.023 km
Eccentricity
0.00933
Inclination
100.7708°
RAAN
234.0729°
Arg. of periapsis
207.4804°
True anomaly
210.90243°
Mean anomaly
211.455°
Eccentric anomaly
211.17817°
Mean motion
3.221 °/min
Orbital period
111.77 mins
BSTAR
0.000022166
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