DELTA 1 DEB, 21327

Orbit data source: Space-Track

DELTA 1 DEB, 21327 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
21327, 1975-052AV
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, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 DELTA 1 DEB
1 21327U 75052AV  25348.75246322 -.00000117  00000-0 -25043-3 0  9995
2 21327  99.7504 268.5522 0281584 303.0652 110.6247 12.89987605627380
Epoch: 2025-12-14T18:03Z
TLE epoch observation values (Epoch: 2025-12-14T18:03:32.822Z)
Latitude
55.52616°
Longitude
-100.41586°
Altitude
1,392.116 km
Speed
7.131 km/s
True Right ascension
16h 56m 31s
True Declination
55° 22' 43"
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
13:36:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,515.129 km
Perigee altitude
1,082.78 km
Semi-major axis
7,677.092 km
Eccentricity
0.02816
Inclination
99.7504°
RAAN
268.5522°
Arg. of periapsis
303.0652°
True anomaly
113.60626°
Mean anomaly
110.6247°
Eccentric anomaly
112.11932°
Mean motion
3.22662 °/min
Orbital period
111.57 mins
BSTAR
-0.00025043
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