DELTA 1 DEB, 42082

Orbit data source: Space-Track

DELTA 1 DEB, 42082 is space debris in SSO originally from a launch on Sun, 15 Dec 1968 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
42082, 1968-114J
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Aerojet
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1968-12-15 (58 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: 22 hours ago

TLE from 22 hours ago
0 DELTA 1 DEB
1 42082U 68114J   26266.32626843  .00000076  00000-0  85493-3 0  9997
2 42082 101.9803 213.8869 0086717 125.1250  29.0802 12.42854626582604
Epoch: 2026-09-23T07:49Z
TLE epoch observation values (Epoch: 2026-09-23T07:49:49.592Z)
Latitude
24.7465°
Longitude
-80.16352°
Altitude
1,437.671 km
Speed
7.172 km/s
True Right ascension
02h 37m 53s
True Declination
24° 37' 39"
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
22:33:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,560.343 km
Perigee altitude
1,423.847 km
Semi-major axis
7,870.232 km
Eccentricity
0.00867
Inclination
101.9803°
RAAN
213.8869°
Arg. of periapsis
125.125°
True anomaly
29.56778°
Mean anomaly
29.0802°
Eccentric anomaly
29.32353°
Mean motion
3.10858 °/min
Orbital period
115.81 mins
BSTAR
0.00085493
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