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 URL

https://www.satcat.com/sats-embedded/1865?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

1865, 1965-109B

Orbit

LEO

Country

Related business

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

Unknown

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago

0 SCOUT A R/B
1 01865U 65109B   26105.88653108  .00000100  00000-0  84632-4 0  9992
2 01865  89.0650 255.1598 0111914 172.6809 187.6024 13.76821698 25067

Epoch: 2026-04-15T21:16Z

TLE epoch observation values (Epoch: 2026-04-15T21:16:36.285Z)

Latitude

-0.00001°

Longitude

91.96662°

Altitude

1,059.776 km

Speed

7.281 km/s

True Right ascension

17h 00m 38s

True Declination

0° 00' 00"

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

12:22:30

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,054.455 km

Perigee altitude

889.934 km

Semi-major axis

7,350.331 km

Eccentricity

0.01119

Inclination

89.065°

RAAN

255.1598°

Arg. of periapsis

172.6809°

True anomaly

187.43506°

Mean anomaly

187.6024°

Eccentric anomaly

187.5185°

Mean motion

3.44416 °/min

Orbital period

104.52 mins

BSTAR

0.000084632

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

TRANSIT 10 DEB, 25576 (Decayed)

SCOUT A DEB, 2086 (Decayed)

SCOUT A DEB, 2226

OPS 1509 (TRANSIT 10), 1864

TRANSIT 10 DEB, 24705

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SCOUT A R/B Visibility forecast

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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.
11 mins	2026-04-16 09:35:25.510Z	147.454° SSE	2026-04-16 09:41:25.510Z	76.229° E	33.025°	2026-04-16 09:46:25.510Z	16.565° NNE
9 mins	2026-04-16 11:21:25.510Z	224.338° SW	2026-04-16 11:25:25.510Z	271.347° WNW	26.994°	2026-04-16 11:30:25.510Z	332.983° NNW
9 mins	2026-04-16 22:18:25.510Z	358.127° N	2026-04-16 22:22:25.510Z	295.919° NW	44.661°	2026-04-16 22:27:25.510Z	186.72° SSW

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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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

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

SCOUT A R/B, 1865

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-04-15T21:16:36.285Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

SCOUT A R/B Visibility forecast

Co-orbital & Co-planar RSOs

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

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago