DELTA 1 DEB, 21566

Orbit data source: Space-Track

DELTA 1 DEB, 21566 is space debris in SSO originally from a launch on Thu, 12 Jun 1975 UTC launched from the Air Force Western Test Range (AFWTR). 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
21566, 1975-052HL
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1975-06-12 (51 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

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

TLE from 2 weeks ago
0 DELTA 1 DEB
1 21566U 75052HL  26151.96457519  .00000149  00000-0  61044-3 0  9992
2 21566  99.5726 161.7005 0324693 176.3098 214.6753 12.83920388641587
Epoch: 2026-05-31T23:08Z
TLE epoch observation values (Epoch: 2026-05-31T23:08:59.296Z)
Latitude
28.53789°
Longitude
-80.2418°
Altitude
1,537.372 km
Speed
7.003 km/s
True Right ascension
10h 25m 51s
True Declination
28° 24' 29"
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
20:16:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,573.182 km
Perigee altitude
1,073.073 km
Semi-major axis
7,701.265 km
Eccentricity
0.03247
Inclination
99.5726°
RAAN
161.7005°
Arg. of periapsis
176.3098°
True anomaly
212.62739°
Mean anomaly
214.6753°
Eccentric anomaly
213.64459°
Mean motion
3.21144 °/min
Orbital period
112.1 mins
BSTAR
0.00061044
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