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: 19 hours ago

TLE from 19 hours ago
0 DELTA 1 DEB
1 02700U 65089C   26047.49306052  .00000153  00000-0  11611-2 0  9996
2 02700  59.5935 211.4364 0719260   1.9993  29.7666 12.08986711696868
Epoch: 2026-02-16T11:50Z
TLE epoch observation values (Epoch: 2026-02-16T11:50:00.428Z)
Latitude
30.70058°
Longitude
-92.26898°
Altitude
1,153.818 km
Speed
7.498 km/s
True Right ascension
15h 26m 52s
True Declination
30° 33' 28"
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
09:18:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,216.968 km
Perigee altitude
1,063.509 km
Semi-major axis
8,018.376 km
Eccentricity
0.07193
Inclination
59.5935°
RAAN
211.4364°
Arg. of periapsis
1.9993°
True anomaly
34.19917°
Mean anomaly
29.7666°
Eccentric anomaly
31.94721°
Mean motion
3.02283 °/min
Orbital period
119.09 mins
BSTAR
0.0011611
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