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

8 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 (60 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 8 hours ago

0 SCOUT A R/B
1 01865U 65109B   25182.57409573  .00000090  00000-0  76478-4 0  9994
2 01865  89.0663 283.6795 0110156 325.6825  33.7256 13.76734970985385

Epoch: 2025-07-01T13:46Z

TLE epoch observation values (Epoch: 2025-07-01T13:46:41.871Z)

Latitude

-0.00007°

Longitude

157.13744°

Altitude

911.375 km

Speed

7.43 km/s

True Right ascension

18h 54m 43s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

-66.68544°

Longitude

154.94706°

Altitude

931.273 km

Speed

7.42 km/s

Apparent Right ascension

20h 43m 43s

Apparent Declination

-56° 10' 06"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

09:51:23

Azimuth

151.252° SSE

Elevation

-70.315°

Doppler factor

Orbital elements

Apogee altitude

1,053.475 km

Perigee altitude

891.531 km

Semi-major axis

7,350.64 km

Eccentricity

0.01102

Inclination

89.0663°

RAAN

283.6795°

Arg. of periapsis

325.6825°

True anomaly

Unknown

Mean anomaly

33.7256°

Eccentric anomaly

Unknown

Mean motion

3.44394 °/min

Orbital period

104.53 mins

BSTAR

0.000076478

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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.
6 mins	2025-07-02 05:38:00.749Z	102.267° ESE	2025-07-02 05:41:00.749Z	71.639° E	14.27°	2025-07-02 05:44:00.749Z	41.467° NE
10 mins	2025-07-02 07:20:00.749Z	184.757° SSW	2025-07-02 07:25:00.749Z	301.334° NW	43.96°	2025-07-02 07:30:00.749Z	355.189° N
11 mins	2025-07-02 18:17:00.749Z	20.321° NNE	2025-07-02 18:22:00.749Z	83.838° E	33.214°	2025-07-02 18:28:00.749Z	153.004° SSE
10 mins	2025-07-02 20:02:00.749Z	334.328° NNW	2025-07-02 20:06:00.749Z	287.981° WNW	27.742°	2025-07-02 20:12:00.749Z	222.053° SW

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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