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
CYL, 1.1 m
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 02120U 66024B   26262.13075700  .00000058  00000-0  49069-4 0  9999
2 02120  89.8197 170.1043 0150197 293.8288  64.7193 13.72660480 24797
Epoch: 2026-09-19T03:08Z
TLE epoch observation values (Epoch: 2026-09-19T03:08:17.404Z)
Latitude
-0.00003°
Longitude
124.98808°
Altitude
947.124 km
Speed
7.401 km/s
True Right ascension
11h 20m 25s
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
09:01:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,097.674 km
Perigee altitude
876.428 km
Semi-major axis
7,365.188 km
Eccentricity
0.01502
Inclination
89.8197°
RAAN
170.1043°
Arg. of periapsis
293.8288°
True anomaly
66.28797°
Mean anomaly
64.7193°
Eccentric anomaly
65.5024°
Mean motion
3.43374 °/min
Orbital period
104.84 mins
BSTAR
0.000049069
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