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 week ago

TLE from 1 week ago
0 DELTA 1 R/B(2)
1 02643U 67001D   26075.72493609  .00014037  00000-0  27266-2 0  9999
2 02643  25.7751 273.6330 5924568 246.6590  42.2827  4.15549131752483
Epoch: 2026-03-16T17:23Z
TLE epoch observation values (Epoch: 2026-03-16T17:23:54.478Z)
Latitude
-0.00012°
Longitude
-161.67543°
Altitude
7,474.052 km
Speed
5.759 km/s
True Right ascension
18h 14m 27s
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
11:31:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,652.591 km
Perigee altitude
283.674 km
Semi-major axis
16,346.269 km
Eccentricity
0.59246
Inclination
25.7751°
RAAN
273.633°
Arg. of periapsis
246.659°
True anomaly
113.28762°
Mean anomaly
42.2827°
Eccentric anomaly
75.08419°
Mean motion
1.03852 °/min
Orbital period
346.65 mins
BSTAR
0.0027266
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