THORAD DELTA 1 DEB, 8406

Orbit data source: Space-Track

THORAD DELTA 1 DEB, 8406 is space debris in SSO originally from a launch on Fri, 15 Nov 1974 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
8406, 1974-089CJ
Orbit
SSO
Last TLE update
4 hours ago
Origin
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1974-11-15 (51 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history

TLE from 4 hours ago
0 THORAD DELTA 1 DEB
1  8406U 74089CJ  25216.12531167  .00000360  00000-0  23908-2 0  9991
2  8406 101.3382  81.8800 0018944  75.6409  50.0274 12.57738871322363
Epoch: 2025-08-04T03:00Z
TLE epoch observation values (Epoch: 2025-08-04T03:00:26.928Z)
Latitude
52.73918°
Longitude
-80.96377°
Altitude
1,431.193 km
Speed
7.155 km/s
True Right ascension
18h 28m 20s
True Declination
52° 35' 16"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-58.96393°
Longitude
-115.35775°
Altitude
1,469.224 km
Speed
7.121 km/s
Apparent Right ascension
12h 17m 18s
Apparent Declination
-62° 31' 12"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
21:18:07
Azimuth
214.655° SW
Elevation
-55.126°
Doppler factor
1
Orbital elements
Apogee altitude
1,444.596 km
Perigee altitude
1,415.013 km
Semi-major axis
7,807.941 km
Eccentricity
0.00189
Inclination
101.3382°
RAAN
81.88°
Arg. of periapsis
75.6409°
True anomaly
50.19401°
Mean anomaly
50.0274°
Eccentric anomaly
50.11068°
Mean motion
3.14585 °/min
Orbital period
114.44 mins
BSTAR
0.0023908
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