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

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ISO8601 Format

Identifier

1502, 1965-063B

Orbit

LEO

Last TLE update

2 days 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 2 days ago

0 SCOUT B R/B
1 01502U 65063B   25118.54319946  .00000013  00000-0  30809-3 0  9993
2 01502  69.2295 160.8126 0781162 141.1905   7.4865 11.78588046569539

Epoch: 2025-04-28T13:02Z

Definitive object data (Epoch: 2025-04-28T13:02:12.433Z)

Latitude

27.95759°

Longitude

-83.04726°

Altitude

1,149.951 km

Speed

7.557 km/s

True Right ascension

21h 57m 02s

True Declination

27° 49' 22"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

28.39434°

Longitude

-86.08531°

Altitude

1,151.563 km

Speed

7.555 km/s

Apparent Right ascension

00h 41m 44s

Apparent Declination

-4° 33' 33"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

17:24:22

Azimuth

80.885° E

Elevation

-17.714°

Doppler factor

Orbital elements

Apogee altitude

2,413.491 km

Perigee altitude

1,139.475 km

Semi-major axis

8,154.62 km

Eccentricity

0.0781162

Inclination

69.2295°

RAAN

160.8126°

Arg. of periapsis

141.1905°

True anomaly

8.77711°

Mean anomaly

7.4865°

Eccentric anomaly

8.11857°

Mean motion

2.94739 °/min

BSTAR

0.00030809

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.
9 mins	2025-04-30 11:40:27.655Z	1.178° NNE	2025-04-30 11:44:27.655Z	36.74° NE	18.041°	2025-04-30 11:49:27.655Z	84.382° E
12 mins	2025-04-30 13:45:27.655Z	331.595° NNW	2025-04-30 13:51:27.655Z	232.718° WSW	44.548°	2025-04-30 13:57:27.655Z	161.68° S
7 mins	2025-05-01 01:29:27.655Z	112.784° SE	2025-05-01 01:32:27.655Z	96.206° ESE	13.019°	2025-05-01 01:36:27.655Z	72.624° E
19 mins	2025-05-01 03:26:27.655Z	189.65° SSW	2025-05-01 03:37:27.655Z	97.64° ESE	42.964°	2025-05-01 03:45:27.655Z	31.546° NE
15 mins	2025-05-01 05:35:27.655Z	253.562° W	2025-05-01 05:43:27.655Z	311.312° NW	28.485°	2025-05-01 05:50:27.655Z	8.332° NNE

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

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.