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: 9 hours ago

TLE from 9 hours ago
0 SCOUT A R/B
1  2120U 66024B   26001.01461114  .00000160  00000-0  15094-3 0  9999
2  2120  89.8151 175.0474 0151850 358.7780   1.2991 13.72605606988985
Epoch: 2026-01-01T00:21Z
TLE epoch observation values (Epoch: 2026-01-01T00:21:02.402Z)
Latitude
0.00003°
Longitude
69.11213°
Altitude
881.337 km
Speed
7.468 km/s
True Right ascension
11h 40m 11s
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
09:21:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,099.091 km
Perigee altitude
875.404 km
Semi-major axis
7,365.384 km
Eccentricity
0.01519
Inclination
89.8151°
RAAN
175.0474°
Arg. of periapsis
358.778°
True anomaly
1.33931°
Mean anomaly
1.2991°
Eccentric anomaly
1.31913°
Mean motion
3.4336 °/min
Orbital period
104.85 mins
BSTAR
0.00015094
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