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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

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   26135.28139567  .00005444  00000-0  13396-2 0  9998
2 02643  25.7165 226.2912 5907303 326.9870   7.2257  4.16768061754962
Epoch: 2026-05-15T06:45Z
TLE epoch observation values (Epoch: 2026-05-15T06:45:12.585Z)
Latitude
0.00001°
Longitude
-108.04045°
Altitude
719.774 km
Speed
9.374 km/s
True Right ascension
15h 05m 06s
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
19:29:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,573.649 km
Perigee altitude
298.846 km
Semi-major axis
16,314.385 km
Eccentricity
0.59073
Inclination
25.7165°
RAAN
226.2912°
Arg. of periapsis
326.987°
True anomaly
33.35074°
Mean anomaly
7.2257°
Eccentric anomaly
17.27879°
Mean motion
1.04157 °/min
Orbital period
345.63 mins
BSTAR
0.0013396
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