DELTA 1 DEB, 27575

Orbit data source: Space-Track

DELTA 1 DEB, 27575 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
27575, 1977-065GG
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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DELTA 1 DEB
1 27575U 77065GG  26262.10906829  .00004665  00000-0  16623-2 0  9995
2 27575  29.1179 240.4448 0408002 276.6064 149.9880 13.94920072404833
Epoch: 2026-09-19T02:37Z
TLE epoch observation values (Epoch: 2026-09-19T02:37:03.500Z)
Latitude
27.10029°
Longitude
-90.76416°
Altitude
1,170.596 km
Speed
7.142 km/s
True Right ascension
20h 26m 05s
True Declination
26° 58' 07"
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
02:41:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,212.927 km
Perigee altitude
617.775 km
Semi-major axis
7,293.488 km
Eccentricity
0.0408
Inclination
29.1179°
RAAN
240.4448°
Arg. of periapsis
276.6064°
True anomaly
152.2269°
Mean anomaly
149.988°
Eccentric anomaly
151.11715°
Mean motion
3.4845 °/min
Orbital period
103.31 mins
BSTAR
0.0016623
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