DELTA 1 R/B(2), 2643

Orbit data source: Space-Track

DELTA 1 R/B(2), 2643 is space debris in HEO originally from a launch on Wed, 11 Jan 1967 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
2643, 1967-001D
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
UTC
Mission
Spacecraft
Bus & Motor
FW4, Unknown motor
Mass
34 kg wet, 34 kg dry
Launch date (UTC)
1967-01-11 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 DELTA 1 R/B(2)
1 02643U 67001D   25241.39098074  .00007967  00000-0  22045-2 0  9997
2 02643  25.7978  69.7904 5949025 341.9864   3.7082  4.09956676744253
Epoch: 2025-08-29T09:23Z
TLE epoch observation values (Epoch: 2025-08-29T09:23:00.735Z)
Latitude
0.00012°
Longitude
-48.7886°
Altitude
433.751 km
Speed
9.636 km/s
True Right ascension
04h 39m 13s
True Declination
0° 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
15:50:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,929.059 km
Perigee altitude
303.763 km
Semi-major axis
16,494.548 km
Eccentricity
0.5949
Inclination
25.7978°
RAAN
69.7904°
Arg. of periapsis
341.9864°
True anomaly
17.94184°
Mean anomaly
3.7082°
Eccentric anomaly
9.09777°
Mean motion
1.02455 °/min
Orbital period
351.37 mins
BSTAR
0.0022045
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