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
Last TLE update
20 hours ago
Origin
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

TLE from 20 hours ago
0 DELTA 1 R/B
1 02436U 66087B   25198.50808695 -.00000025  00000-0  95342-4 0  9993
2 02436 100.9892 168.0434 0065304 339.4629  20.3826 12.57660137698031
Epoch: 2025-07-17T12:11Z
TLE epoch observation values (Epoch: 2025-07-17T12:11:38.712Z)
Latitude
-0.00004°
Longitude
49.55921°
Altitude
1,387.449 km
Speed
7.188 km/s
True Right ascension
11h 12m 10s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
67.62082°
Longitude
-101.68658°
Altitude
1,478.057 km
Speed
7.115 km/s
Apparent Right ascension
06h 11m 14s
Apparent Declination
34° 12' 00"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
20:36:57
Azimuth
29.787° NE
Elevation
-8.61°
Doppler factor
1
Orbital elements
Apogee altitude
1,481.102 km
Perigee altitude
1,379.12 km
Semi-major axis
7,808.248 km
Eccentricity
0.00653
Inclination
100.9892°
RAAN
168.0434°
Arg. of periapsis
339.4629°
True anomaly
20.64524°
Mean anomaly
20.3826°
Eccentric anomaly
20.51372°
Mean motion
3.14567 °/min
Orbital period
114.44 mins
BSTAR
0.000095342
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