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 day ago

TLE from 1 day ago
0 DELTA 1 DEB
1 02700U 65089C   26034.59083125 -.00000037  00000-0  19893-3 0  9999
2 02700  59.5942 240.9334 0718558 353.8540  34.8613 12.08981914695303
Epoch: 2026-02-03T14:10Z
TLE epoch observation values (Epoch: 2026-02-03T14:10:47.820Z)
Latitude
28.73318°
Longitude
-86.86809°
Altitude
1,184.934 km
Speed
7.469 km/s
True Right ascension
17h 18m 24s
True Declination
28° 35' 48"
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
23:43:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,216.428 km
Perigee altitude
1,064.091 km
Semi-major axis
8,018.397 km
Eccentricity
0.07186
Inclination
59.5942°
RAAN
240.9334°
Arg. of periapsis
353.854°
True anomaly
39.93429°
Mean anomaly
34.8613°
Eccentric anomaly
37.35958°
Mean motion
3.02282 °/min
Orbital period
119.09 mins
BSTAR
0.00019893
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