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   26025.65249213  .00000192  00000-0  17300-3 0  9994
2 01865  89.0638 263.1001 0113182  56.6811 304.5131 13.76800402 14027

Epoch: 2026-01-25T15:39Z

TLE epoch observation values (Epoch: 2026-01-25T15:39:35.320Z)

Latitude

-0.00003°

Longitude

-96.75659°

Altitude

931.729 km

Speed

7.409 km/s

True Right ascension

17h 32m 24s

True Declination

0° 00' 00"

Sunlit

Object was in daylight 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

00:53:46

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,055.463 km

Perigee altitude

889.076 km

Semi-major axis

7,350.407 km

Eccentricity

0.01132

Inclination

89.0638°

RAAN

263.1001°

Arg. of periapsis

56.6811°

True anomaly

303.43583°

Mean anomaly

304.5131°

Eccentric anomaly

303.97533°

Mean motion

3.4441 °/min

Orbital period

104.53 mins

BSTAR

0.000173

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

OPS 1509 (TRANSIT 10), 1864

TRANSIT 10 DEB, 25576 (Decayed)

SCOUT A DEB, 2226

TRANSIT 10 DEB, 24705

SCOUT A DEB, 2086 (Decayed)

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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.
8 mins	2026-01-26 02:43:07.123Z	35.228° NE	2026-01-26 02:47:07.123Z	78.39° E	18.828°	2026-01-26 02:51:07.123Z	121.625° SE
10 mins	2026-01-26 04:28:07.123Z	346.646° N	2026-01-26 04:32:07.123Z	273.961° WNW	40.119°	2026-01-26 04:38:07.123Z	198.902° SSW
9 mins	2026-01-26 16:12:07.123Z	181.587° SSW	2026-01-26 16:16:07.123Z	276.293° WNW	44.794°	2026-01-26 16:21:07.123Z	357.067° N

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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: 2026-01-25T15:39:35.320Z)

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