SCOUT A R/B, 2180

Orbit data source: Space-Track

SCOUT A R/B, 2180 is space debris in LEO originally from a launch on Thu, 19 May 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
2180, 1966-041B
Orbit
LEO
Last TLE update
13 hours ago
Origin
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
1966-05-19 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 13 hours ago
0 SCOUT A R/B
1 02180U 66041B   25199.39465275  .00000077  00000-0  44322-4 0  9998
2 02180  90.2221  74.3816 0076410 294.6016  64.7216 14.00960998 16531
Epoch: 2025-07-18T09:28Z
TLE epoch observation values (Epoch: 2025-07-18T09:28:17.997Z)
Latitude
-0.00002°
Longitude
-4.14012°
Altitude
870.124 km
Speed
7.429 km/s
True Right ascension
04h 57m 31s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-58.99096°
Longitude
-3.7589°
Altitude
858.398 km
Speed
7.45 km/s
Apparent Right ascension
01h 55m 04s
Apparent Declination
-56° 51' 46"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
11:41:59
Azimuth
220.673° SW
Elevation
-62.605°
Doppler factor
1
Orbital elements
Apogee altitude
942.961 km
Perigee altitude
831.929 km
Semi-major axis
7,265.582 km
Eccentricity
0.00764
Inclination
90.2221°
RAAN
74.3816°
Arg. of periapsis
294.6016°
True anomaly
65.51657°
Mean anomaly
64.7216°
Eccentric anomaly
65.11876°
Mean motion
3.50459 °/min
Orbital period
102.72 mins
BSTAR
0.000044322
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