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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 SCOUT B R/B
1 01502U 65063B   26104.11755763 -.00000045  00000-0 -82754-4 0  9997
2 01502  69.2354 350.8000 0786341 222.9628 312.2251 11.78597861610843
Epoch: 2026-04-14T02:49Z
TLE epoch observation values (Epoch: 2026-04-14T02:49:16.979Z)
Latitude
11.11975°
Longitude
-78.07157°
Altitude
1,378.312 km
Speed
7.345 km/s
True Right ascension
11h 06m 11s
True Declination
11° 03' 36"
Sunlit
Object was in full shadow 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
19:33:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,417.665 km
Perigee altitude
1,135.21 km
Semi-major axis
8,154.574 km
Eccentricity
0.07863
Inclination
69.2354°
RAAN
350.8°
Arg. of periapsis
222.9628°
True anomaly
305.10056°
Mean anomaly
312.2251°
Eccentric anomaly
308.70941°
Mean motion
2.94741 °/min
Orbital period
122.14 mins
BSTAR
-0.000082754
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