DELTA 1 R/B, 2436

Orbit data source: Space-Track

DELTA 1 R/B, 2436 is space debris in SSO originally from a launch on Sun, 02 Oct 1966 UTC launched from the Air Force Western Test Range (AFWTR). 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
2436, 1966-087B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
1966-10-02 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
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 day ago

TLE from 1 day ago
0 DELTA 1 R/B
1  2436U 66087B   25324.83016975 -.00000016  00000-0  14370-3 0  9993
2  2436 101.0139 286.1413 0065690  85.1622 275.6952 12.57667661713911
Epoch: 2025-11-20T19:55Z
TLE epoch observation values (Epoch: 2025-11-20T19:55:26.666Z)
Latitude
-0.00003°
Longitude
-72.80173°
Altitude
1,430.439 km
Speed
7.148 km/s
True Right ascension
19h 04m 33s
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
17:10:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,481.373 km
Perigee altitude
1,378.789 km
Semi-major axis
7,808.218 km
Eccentricity
0.00657
Inclination
101.0139°
RAAN
286.1413°
Arg. of periapsis
85.1622°
True anomaly
274.94557°
Mean anomaly
275.6952°
Eccentric anomaly
275.32045°
Mean motion
3.14569 °/min
Orbital period
114.44 mins
BSTAR
0.0001437
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Other satellites on launch #87 in the year 1966 (1966-10-02 UTC)

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