SCOUT A R/B, 1865

Orbit data source: Space-Track

SCOUT A R/B, 1865 is space debris in LEO originally from a launch on Wed, 22 Dec 1965 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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<iframe src="https://www.satcat.com/sats-embedded/1865?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/1865?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

1865, 1965-109B

Orbit

LEO

Last TLE update

17 hours ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

ABL

Mission

Spacecraft

Bus & Motor

ALTAIR, Unknown motor

Mass

33 kg wet, 33 kg dry

Launch date (UTC)

1965-12-22 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

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 17 hours ago

0 SCOUT A R/B
1 01865U 65109B   25114.90895355  .00000270  00000-0  24942-3 0  9991
2 01865  89.0603 290.3720 0112086 168.1972 192.1862 13.76718022976078

Epoch: 2025-04-24T21:48Z

Definitive object data (Epoch: 2025-04-24T21:48:53.586Z)

Latitude

-0.00005°

Longitude

109.9751°

Altitude

1,059.166 km

Speed

7.282 km/s

True Right ascension

19h 21m 29s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-29.23998°

Longitude

109.38022°

Altitude

1,066.109 km

Speed

7.278 km/s

Apparent Right ascension

16h 04m 15s

Apparent Declination

-58° 44' 49"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

22:21:55

Azimuth

219.386° SW

Elevation

-35.393°

Doppler factor

Orbital elements

Apogee altitude

1,054.954 km

Perigee altitude

890.172 km

Semi-major axis

7,350.7 km

Eccentricity

0.0112086

Inclination

89.0603°

RAAN

290.372°

Arg. of periapsis

168.1972°

True anomaly

191.91874°

Mean anomaly

192.1862°

Eccentric anomaly

192.05211°

Mean motion

3.4439 °/min

BSTAR

0.00024942

Orbital period

104.53 mins

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Other satellites on launch #109 in the year 1965 (1965-12-22 UTC)

OPS 1509 (TRANSIT 10), 1864

SCOUT A DEB, 2086 (Decayed)

SCOUT A DEB, 2226

TRANSIT 10 DEB, 24705

TRANSIT 10 DEB, 25576 (Decayed)

SCOUT A 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.
8 mins	2025-04-25 22:50:51.464Z	33.456° NE	2025-04-25 22:54:51.464Z	83.849° E	22.273°	2025-04-25 22:58:51.464Z	131.287° SE
8 mins	2025-04-26 00:35:51.464Z	337.465° NNW	2025-04-26 00:39:51.464Z	265.227° W	33.495°	2025-04-26 00:43:51.464Z	212.895° SW
6 mins	2025-04-26 10:36:51.464Z	101.315° ESE	2025-04-26 10:38:51.464Z	79.55° E	17.786°	2025-04-26 10:42:51.464Z	37.164° NE
11 mins	2025-04-26 12:17:51.464Z	190.369° SSW	2025-04-26 12:22:51.464Z	250.993° W	42.206°	2025-04-26 12:28:51.464Z	352.155° N

Authenticating...

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Check out SCOUT A R/B, 1865 on other resources

View SCOUT A R/B, 1865 on Heavens-Above

View SCOUT A R/B, 1865 on Keep Track

View SCOUT A R/B, 1865 on Celestrak

View SCOUT A R/B, 1865 on Gunter's Space Page

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