SCOUT B R/B, 1502

Orbit data source: Space-Track

SCOUT B R/B, 1502 is space debris in LEO originally from a launch on Tue, 10 Aug 1965 UTC via an SCOUT B launch vehicle from the Wallops Island (WLPIS). 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
1502, 1965-063B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NASA LaRC
Mission
Spacecraft
Bus & Motor
ESEC, Unknown motor
Mass
47 kg wet, 4 kg dry
Launch date (UTC)
1965-08-10 (61 years ago)
Launch vehicle
SCOUT B
Launch site
Wallops Island (WLPIS)
Object type
Payload
Rocket body
Debris
Shape & HBR
FRUST, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 SCOUT B R/B
1  1502U 65063B   26306.76210882 -.00000062  00000-0 -22529-3 0  9992
2  1502  69.2334  44.4230 0783701  61.9476  87.2937 11.78606193634723
Epoch: 2026-11-02T18:17Z
TLE epoch observation values (Epoch: 2026-11-02T18:17:26.202Z)
Latitude
20.31644°
Longitude
-100.00289°
Altitude
1,799.665 km
Speed
6.976 km/s
True Right ascension
14h 25m 33s
True Declination
20° 13' 08"
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
04:53:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,415.471 km
Perigee altitude
1,137.327 km
Semi-major axis
8,154.536 km
Eccentricity
0.07837
Inclination
69.2334°
RAAN
44.423°
Arg. of periapsis
61.9476°
True anomaly
96.26905°
Mean anomaly
87.2937°
Eccentric anomaly
91.7818°
Mean motion
2.94744 °/min
Orbital period
122.14 mins
BSTAR
-0.00022529
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