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 shape, 0.1 m
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 02700U 65089C   25279.91557789 -.00000214  00000-0 -71263-3 0  9994
2 02700  59.5980 154.4599 0712745 277.8860  88.9100 12.08974717680835
Epoch: 2025-10-06T21:58Z
TLE epoch observation values (Epoch: 2025-10-06T21:58:25.929Z)
Latitude
12.84383°
Longitude
176.69076°
Altitude
1,671.326 km
Speed
7.027 km/s
True Right ascension
10h 48m 26s
True Declination
12° 46' 41"
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
02:45:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,211.801 km
Perigee altitude
1,068.782 km
Semi-major axis
8,018.428 km
Eccentricity
0.07127
Inclination
59.598°
RAAN
154.4599°
Arg. of periapsis
277.886°
True anomaly
97.06224°
Mean anomaly
88.91°
Eccentric anomaly
92.98818°
Mean motion
3.0228 °/min
Orbital period
119.09 mins
BSTAR
-0.00071263
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