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 (61 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 SCOUT A R/B
1 02120U 66024B   26270.14923668  .00000086  00000-0  77889-4 0  9996
2 02120  89.8192 169.9538 0149965 269.4146  88.9833 13.72661533 25891
Epoch: 2026-09-27T03:34Z
TLE epoch observation values (Epoch: 2026-09-27T03:34:54.049Z)
Latitude
0.00001°
Longitude
110.2815°
Altitude
992.715 km
Speed
7.355 km/s
True Right ascension
11h 19m 48s
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
03:22:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,097.499 km
Perigee altitude
876.595 km
Semi-major axis
7,365.184 km
Eccentricity
0.015
Inclination
89.8192°
RAAN
169.9538°
Arg. of periapsis
269.4146°
True anomaly
90.70182°
Mean anomaly
88.9833°
Eccentric anomaly
89.84253°
Mean motion
3.43374 °/min
Orbital period
104.84 mins
BSTAR
0.000077889
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