DELTA 1 R/B(1), 11636

Orbit data source: Space-Track

DELTA 1 R/B(1), 11636 is space debris in LEO originally from a launch on Fri, 07 Dec 1979 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
11636, 1979-101B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
MDAC-HB
Mission
Spacecraft
Bus & Motor
DELTA/TR-201, Unknown motor
Mass
845 kg wet, 845 kg dry
Launch date (UTC)
1979-12-07 (46 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 3.2 m
Radar Cross Section
7.796 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 DELTA 1 R/B(1)
1 11636U 79101B   25264.50785088  .00000545  00000-0  29347-3 0  9997
2 11636  28.2123  83.9146 1261501  76.7911 296.9980 12.21046921964308
Epoch: 2025-09-21T12:11Z
TLE epoch observation values (Epoch: 2025-09-21T12:11:18.316Z)
Latitude
Longitude
-99.5371°
Altitude
1,239.23 km
Speed
7.393 km/s
True Right ascension
05h 35m 39s
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
13:44:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,597.159 km
Perigee altitude
586.353 km
Semi-major axis
7,969.893 km
Eccentricity
0.12615
Inclination
28.2123°
RAAN
83.9146°
Arg. of periapsis
76.7911°
True anomaly
283.26172°
Mean anomaly
296.998°
Eccentric anomaly
290.21537°
Mean motion
3.05045 °/min
Orbital period
118.02 mins
BSTAR
0.00029347
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