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: 16 hours ago

TLE from 16 hours ago
0 DELTA 1 R/B(2)
1 02643U 67001D   26038.91167366  .00018644  00000-0  35784-2 0  9999
2 02643  25.8000 302.8575 5932572 197.1213 128.2832  4.14376014750951
Epoch: 2026-02-07T21:52Z
TLE epoch observation values (Epoch: 2026-02-07T21:52:48.604Z)
Latitude
0.00007°
Longitude
-163.36225°
Altitude
18,133.972 km
Speed
2.86 km/s
True Right ascension
20h 11m 28s
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
15:54:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,714.792 km
Perigee altitude
283.13 km
Semi-major axis
16,377.098 km
Eccentricity
0.59326
Inclination
25.8°
RAAN
302.8575°
Arg. of periapsis
197.1213°
True anomaly
162.90272°
Mean anomaly
128.2832°
Eccentric anomaly
146.86381°
Mean motion
1.03559 °/min
Orbital period
347.63 mins
BSTAR
0.0035784
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