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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<iframe src="https://www.satcat.com/sats-embedded/1502?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/1502?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

1502, 1965-063B

Orbit

LEO

Last TLE update

1 day ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

NASA LaRC

Mission

Spacecraft

Bus & Motor

ESEC, Unknown motor

Mass

47 kg wet, 4 kg dry

Launch date (UTC)

1965-08-10 (60 years ago)

Launch vehicle

SCOUT B

Launch site

Wallops Island (WLPIS)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 1.5 m

Radar Cross Section

0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 1 day ago

0 SCOUT B R/B
1 01502U 65063B   25128.46351571 -.00000032  00000-0 -95732-5 0  9996
2 01502  69.2281 145.8172 0780799 133.2984 338.5913 11.78588211570709

Epoch: 2025-05-08T11:07Z

Definitive object data (Epoch: 2025-05-08T11:07:27.757Z)

Latitude

62.69337°

Longitude

-114.54448°

Altitude

1,202.723 km

Speed

7.515 km/s

True Right ascension

18h 35m 25s

True Declination

62° 33' 40"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-15.48787°

Longitude

-63.40195°

Altitude

1,466.093 km

Speed

7.267 km/s

Apparent Right ascension

19h 28m 12s

Apparent Declination

-54° 19' 15"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

00:14:45

Azimuth

216.763° SW

Elevation

-22.351°

Doppler factor

Orbital elements

Apogee altitude

2,413.195 km

Perigee altitude

1,139.771 km

Semi-major axis

8,154.62 km

Eccentricity

0.0780799

Inclination

69.2281°

RAAN

145.8172°

Arg. of periapsis

133.2984°

True anomaly

335.0028°

Mean anomaly

338.5913°

Eccentric anomaly

336.83118°

Mean motion

2.94739 °/min

BSTAR

-0.0000095732

Orbital period

122.14 mins

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Other satellites on launch #63 in the year 1965 (1965-08-10 UTC)

SECOR 5 (EGRS 5), 1506

SCOUT B R/B Visibility forecast

Observer location: undefined°, undefined°

Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
18 mins	2025-05-10 01:17:20.026Z	171.171° S	2025-05-10 01:27:20.026Z	107.946° ESE	34.287°	2025-05-10 01:35:20.026Z	41.059° NE
16 mins	2025-05-10 03:24:20.026Z	232.558° WSW	2025-05-10 03:33:20.026Z	308.317° NW	37.144°	2025-05-10 03:40:20.026Z	13.386° NNE
4 mins	2025-05-10 05:39:20.026Z	316.217° NNW	2025-05-10 05:40:20.026Z	323.116° NNW	11.882°	2025-05-10 05:43:20.026Z	344.792° N
7 mins	2025-05-10 09:59:20.026Z	13.548° NNE	2025-05-10 10:02:20.026Z	43.302° NE	17.156°	2025-05-10 10:06:20.026Z	80.671° E
12 mins	2025-05-10 12:03:20.026Z	332.516° NNW	2025-05-10 12:08:20.026Z	293.122° NW	44.678°	2025-05-10 12:15:20.026Z	159.353° S

Authenticating...

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Check out SCOUT B R/B, 1502 on other resources

View SCOUT B R/B, 1502 on Heavens-Above

View SCOUT B R/B, 1502 on Keep Track

View SCOUT B R/B, 1502 on Celestrak

View SCOUT B R/B, 1502 on Gunter's Space Page

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