DELTA 1 DEB, 21325

Orbit data source: Space-Track

DELTA 1 DEB, 21325 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
21325, 1975-052AT
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: 10 hours ago

TLE from 10 hours ago
0 DELTA 1 DEB
1 21325U 75052AT  26168.98318329  .00002883  00000-0  16369-2 0  9996
2 21325  99.7446 175.2981 0098465 125.2041 265.3834 14.08404071763639
Epoch: 2026-06-17T23:35Z
TLE epoch observation values (Epoch: 2026-06-17T23:35:47.036Z)
Latitude
29.04615°
Longitude
-90.32494°
Altitude
874.828 km
Speed
7.414 km/s
True Right ascension
11h 19m 24s
True Declination
28° 54' 10"
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
20:15:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
933.355 km
Perigee altitude
790.773 km
Semi-major axis
7,240.201 km
Eccentricity
0.00985
Inclination
99.7446°
RAAN
175.2981°
Arg. of periapsis
125.2041°
True anomaly
264.25992°
Mean anomaly
265.3834°
Eccentric anomaly
264.82154°
Mean motion
3.52304 °/min
Orbital period
102.18 mins
BSTAR
0.0016369
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