DELTA 1 DEB, 10626

Orbit data source: Space-Track

DELTA 1 DEB, 10626 is space debris in LEO originally from a launch on Thu, 14 Jul 1977 UTC launched from the Air Force Eastern Test Range (AFETR). 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
10626, 1977-065EV
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1977-07-14 (49 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 DELTA 1 DEB
1 10626U 77065EV  26082.49508494  .00003856  00000-0  91932-3 0  9990
2 10626  29.1772 213.4684 0655795 241.2286 112.0886 13.67955829370871
Epoch: 2026-03-23T11:52Z
TLE epoch observation values (Epoch: 2026-03-23T11:52:55.338Z)
Latitude
Longitude
-145.74845°
Altitude
1,213.636 km
Speed
7.147 km/s
True Right ascension
14h 13m 52s
True Declination
0° 00' 00"
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
06:28:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,495.349 km
Perigee altitude
526.226 km
Semi-major axis
7,388.924 km
Eccentricity
0.06558
Inclination
29.1772°
RAAN
213.4684°
Arg. of periapsis
241.2286°
True anomaly
118.82792°
Mean anomaly
112.0886°
Eccentric anomaly
115.48055°
Mean motion
3.41721 °/min
Orbital period
105.35 mins
BSTAR
0.00091932
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