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: 2 days ago

TLE from 2 days ago
0 DELTA 1 R/B(2)
1  2643U 67001D   25312.48531978  .00012819  00000-0  32178-2 0  9991
2  2643  25.8469  14.6292 5943050  75.4512 340.3865  4.11401047747172
Epoch: 2025-11-08T11:38Z
TLE epoch observation values (Epoch: 2025-11-08T11:38:51.628Z)
Latitude
-0.00005°
Longitude
152.00353°
Altitude
2,868.178 km
Speed
7.873 km/s
True Right ascension
00h 58m 31s
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
09:53:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,857.626 km
Perigee altitude
297.949 km
Semi-major axis
16,455.925 km
Eccentricity
0.59431
Inclination
25.8469°
RAAN
14.6292°
Arg. of periapsis
75.4512°
True anomaly
284.44228°
Mean anomaly
340.3865°
Eccentric anomaly
317.29001°
Mean motion
1.02816 °/min
Orbital period
350.14 mins
BSTAR
0.0032178
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