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   25299.35823458  .00009872  00000-0  26070-2 0  9997
2 02643  25.8434  24.8485 5943713  58.1317 346.3258  4.11092975746636
Epoch: 2025-10-26T08:35Z
TLE epoch observation values (Epoch: 2025-10-26T08:35:51.467Z)
Latitude
-0.00019°
Longitude
-139.09627°
Altitude
1,717.458 km
Speed
8.617 km/s
True Right ascension
01h 39m 22s
True Declination
0° 00' 01"
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
09:11:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,871.82 km
Perigee altitude
300.192 km
Semi-major axis
16,464.143 km
Eccentricity
0.59437
Inclination
25.8434°
RAAN
24.8485°
Arg. of periapsis
58.1317°
True anomaly
301.68325°
Mean anomaly
346.3258°
Eccentric anomaly
328.56516°
Mean motion
1.02739 °/min
Orbital period
350.4 mins
BSTAR
0.002607
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