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: 8 hours ago

TLE from 8 hours ago
0 SCOUT A R/B
1 02120U 66024B   26070.85102737  .00000139  00000-0  12743-3 0  9994
2 02120  89.8218 173.7341 0153309 147.6117 213.4572 13.72626948998566
Epoch: 2026-03-11T20:25Z
TLE epoch observation values (Epoch: 2026-03-11T20:25:28.764Z)
Latitude
-0.00003°
Longitude
57.85491°
Altitude
1,087.924 km
Speed
7.261 km/s
True Right ascension
11h 34m 56s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
08:41:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,100.088 km
Perigee altitude
874.254 km
Semi-major axis
7,365.308 km
Eccentricity
0.01533
Inclination
89.8218°
RAAN
173.7341°
Arg. of periapsis
147.6117°
True anomaly
212.50395°
Mean anomaly
213.4572°
Eccentric anomaly
212.97906°
Mean motion
3.43366 °/min
Orbital period
104.84 mins
BSTAR
0.00012743
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