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 (60 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 DELTA 1 R/B(2)
1 02643U 67001D   26307.64987724  .00011130  00000-0  22741-2 0  9998
2 02643  25.7521  88.2204 5889046 200.9087 118.5873  4.20488563762186
Epoch: 2026-11-03T15:35Z
TLE epoch observation values (Epoch: 2026-11-03T15:35:49.393Z)
Latitude
-0.00006°
Longitude
171.33533°
Altitude
17,166.109 km
Speed
3.046 km/s
True Right ascension
05h 52m 48s
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
05:14:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,390.766 km
Perigee altitude
289.021 km
Semi-major axis
16,218.03 km
Eccentricity
0.5889
Inclination
25.7521°
RAAN
88.2204°
Arg. of periapsis
200.9087°
True anomaly
159.12849°
Mean anomaly
118.5873°
Eccentric anomaly
140.19017°
Mean motion
1.05086 °/min
Orbital period
342.58 mins
BSTAR
0.0022741
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