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: 1 day ago

TLE from 1 day ago
0 DELTA 1 R/B(2)
1 02643U 67001D   25259.67527887  .00007932  00000-0  21387-2 0  9996
2 02643  25.8202  55.6290 5947107   5.9732 358.7401  4.10254954745000
Epoch: 2025-09-16T16:12Z
TLE epoch observation values (Epoch: 2025-09-16T16:12:24.094Z)
Latitude
0.00003°
Longitude
176.66487°
Altitude
321.175 km
Speed
9.737 km/s
True Right ascension
03h 42m 30s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
15:38:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,913.143 km
Perigee altitude
303.686 km
Semi-major axis
16,486.552 km
Eccentricity
0.59471
Inclination
25.8202°
RAAN
55.629°
Arg. of periapsis
5.9732°
True anomaly
353.84249°
Mean anomaly
358.7401°
Eccentric anomaly
356.89359°
Mean motion
1.02529 °/min
Orbital period
351.12 mins
BSTAR
0.0021387
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