SCOUT A R/B, 2120

Orbit data source: Space-Track

SCOUT A R/B, 2120 is space debris in LEO originally from a launch on Sat, 26 Mar 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
2120, 1966-024B
Orbit
LEO
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)
1966-03-26 (60 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: 13 hours ago

TLE from 13 hours ago
0 SCOUT A R/B
1  2120U 66024B   25304.70659830  .00000123  00000-0  11255-3 0  9998
2  2120  89.8187 176.2172 0151672 181.5226 178.5498 13.72587042980571
Epoch: 2025-10-31T16:57Z
TLE epoch observation values (Epoch: 2025-10-31T16:57:30.093Z)
Latitude
0.00006°
Longitude
-118.40537°
Altitude
1,105.032 km
Speed
7.244 km/s
True Right ascension
11h 44m 52s
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
01:52:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,099.027 km
Perigee altitude
875.6 km
Semi-major axis
7,365.451 km
Eccentricity
0.01517
Inclination
89.8187°
RAAN
176.2172°
Arg. of periapsis
181.5226°
True anomaly
178.59297°
Mean anomaly
178.5498°
Eccentric anomaly
178.57146°
Mean motion
3.43356 °/min
Orbital period
104.85 mins
BSTAR
0.00011255
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