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: 3 days ago

TLE from 3 days ago
0 DELTA 1 DEB
1 02700U 65089C   26097.03223992  .00000076  00000-0  77563-3 0  9995
2 02700  59.5923  98.1833 0721823  33.2677   1.9370 12.08984649702850
Epoch: 2026-04-07T00:46Z
TLE epoch observation values (Epoch: 2026-04-07T00:46:25.529Z)
Latitude
30.14305°
Longitude
-88.92123°
Altitude
1,064.673 km
Speed
7.582 km/s
True Right ascension
07h 51m 59s
True Declination
30° 00' 00"
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
19:52:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,219.033 km
Perigee altitude
1,061.462 km
Semi-major axis
8,018.385 km
Eccentricity
0.07218
Inclination
59.5923°
RAAN
98.1833°
Arg. of periapsis
33.2677°
True anomaly
2.24417°
Mean anomaly
1.937°
Eccentric anomaly
2.08766°
Mean motion
3.02282 °/min
Orbital period
119.09 mins
BSTAR
0.00077563
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