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.

Loading next visibility...
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 (50 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: 6 hours ago

TLE from 6 hours ago
0 DELTA 1 DEB
1 21327U 75052AV  25292.31132630 -.00000082  00000-0 -14798-3 0  9997
2 21327  99.7431 218.8178 0281991  68.5568  80.3597 12.89991996620107
Epoch: 2025-10-19T07:28Z
TLE epoch observation values (Epoch: 2025-10-19T07:28:18.592Z)
Latitude
27.48328°
Longitude
-96.1907°
Altitude
1,274.449 km
Speed
7.235 km/s
True Right ascension
02h 55m 39s
True Declination
27° 21' 08"
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
08:37:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,515.423 km
Perigee altitude
1,082.45 km
Semi-major axis
7,677.074 km
Eccentricity
0.0282
Inclination
99.7431°
RAAN
218.8178°
Arg. of periapsis
68.5568°
True anomaly
83.56269°
Mean anomaly
80.3597°
Eccentric anomaly
81.95951°
Mean motion
3.22663 °/min
Orbital period
111.57 mins
BSTAR
-0.00014798
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|