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.

Loading next visibility...
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 (60 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
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 DELTA 1 R/B(2)
1 02643U 67001D   26251.78819939  .00011658  00000-0  23118-2 0  9997
2 02643  25.6454 133.1239 5899803 124.8152 305.4429  4.19053031759835
Epoch: 2026-09-08T18:55Z
TLE epoch observation values (Epoch: 2026-09-08T18:55:00.427Z)
Latitude
0.00003°
Longitude
-138.46612°
Altitude
9,595.201 km
Speed
5.038 km/s
True Right ascension
08h 52m 32s
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
06:40:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,467.077 km
Perigee altitude
286.755 km
Semi-major axis
16,255.053 km
Eccentricity
0.58998
Inclination
25.6454°
RAAN
133.1239°
Arg. of periapsis
124.8152°
True anomaly
235.19103°
Mean anomaly
305.4429°
Eccentric anomaly
271.6536°
Mean motion
1.04727 °/min
Orbital period
343.75 mins
BSTAR
0.0023118
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|