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: 20 hours ago

TLE from 20 hours ago
0 DELTA 1 R/B
1 02436U 66087B   25355.13763344 -.00000027  00000-0  84863-4 0  9996
2 02436 101.0190 314.5088 0065706  24.7919 335.6293 12.57669675717723
Epoch: 2025-12-21T03:18Z
TLE epoch observation values (Epoch: 2025-12-21T03:18:11.529Z)
Latitude
0.00002°
Longitude
175.00636°
Altitude
1,388.491 km
Speed
7.187 km/s
True Right ascension
20h 58m 02s
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
22:43:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,481.377 km
Perigee altitude
1,378.768 km
Semi-major axis
7,808.21 km
Eccentricity
0.00657
Inclination
101.019°
RAAN
314.5088°
Arg. of periapsis
24.7919°
True anomaly
335.31627°
Mean anomaly
335.6293°
Eccentric anomaly
335.47302°
Mean motion
3.14569 °/min
Orbital period
114.44 mins
BSTAR
0.000084863
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Other satellites on launch #87 in the year 1966 (1966-10-02 UTC)

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