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
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 DELTA 1 R/B
1 02436U 66087B   25241.14567949 -.00000014  00000-0  16392-3 0  9991
2 02436 100.9956 207.8788 0064614 253.3502 106.0474 12.57661693703398
Epoch: 2025-08-29T03:29Z
TLE epoch observation values (Epoch: 2025-08-29T03:29:46.707Z)
Latitude
-0.00011°
Longitude
177.83568°
Altitude
1,449.476 km
Speed
7.131 km/s
True Right ascension
13h 51m 30s
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
13:52:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,480.557 km
Perigee altitude
1,379.652 km
Semi-major axis
7,808.242 km
Eccentricity
0.00646
Inclination
100.9956°
RAAN
207.8788°
Arg. of periapsis
253.3502°
True anomaly
106.75737°
Mean anomaly
106.0474°
Eccentric anomaly
106.40254°
Mean motion
3.14567 °/min
Orbital period
114.44 mins
BSTAR
0.00016392
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Other satellites on launch #87 in the year 1966 (1966-10-02 UTC)

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