DELTA 1 DEB, 2700

Orbit data source: Space-Track

DELTA 1 DEB, 2700 is space debris in LEO originally from a launch on Sat, 06 Nov 1965 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
2700, 1965-089C
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1965-11-06 (60 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)

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

TLE from 1 month ago
0 DELTA 1 DEB
1  2700U 65089C   25228.84649148 -.00000137  00000-0 -31724-3 0  9993
2  2700  59.5993 271.1758 0714135 245.4209 300.2397 12.08972330675130
Epoch: 2025-08-16T20:18Z
TLE epoch observation values (Epoch: 2025-08-16T20:18:56.863Z)
Latitude
1.41103°
Longitude
-179.86093°
Altitude
1,385.872 km
Speed
7.281 km/s
True Right ascension
06h 01m 24s
True Declination
1° 24' 12"
Sunlit
Object was in daylight 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
10:17:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,212.926 km
Perigee altitude
1,067.677 km
Semi-major axis
8,018.438 km
Eccentricity
0.07141
Inclination
59.5993°
RAAN
271.1758°
Arg. of periapsis
245.4209°
True anomaly
292.85831°
Mean anomaly
300.2397°
Eccentric anomaly
296.58047°
Mean motion
3.02279 °/min
Orbital period
119.1 mins
BSTAR
-0.00031724
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