SCOUT A DEB, 2140

Orbit data source: Space-Track

SCOUT A DEB, 2140 is space debris in LEO originally from a launch on Fri, 28 Jan 1966 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/2140?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2140, 1966-005C

Orbit

LEO

Last TLE update

1 day ago

Origin

United States Navy (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-01-28 (59 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

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 SCOUT A DEB
1 02140U 66005C   25199.01148918  .00000162  00000-0  17695-3 0  9992
2 02140  89.9468  52.1022 0318603  70.4612 293.0648 13.48253172913423

Epoch: 2025-07-18T00:16Z

TLE epoch observation values (Epoch: 2025-07-18T00:16:32.665Z)

Latitude

-0.00008°

Longitude

111.89702°

Altitude

995.078 km

Speed

7.397 km/s

True Right ascension

03h 28m 24s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-37.37699°

Longitude

111.84868°

Altitude

1,140.472 km

Speed

7.258 km/s

Apparent Right ascension

07h 04m 56s

Apparent Declination

-64° 03' 26"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

00:32:31

Azimuth

146.329° SSE

Elevation

-38.63°

Doppler factor

Orbital elements

Apogee altitude

1,313.223 km

Perigee altitude

838.257 km

Semi-major axis

7,453.877 km

Eccentricity

0.03186

Inclination

89.9468°

RAAN

52.1022°

Arg. of periapsis

70.4612°

True anomaly

289.65454°

Mean anomaly

293.0648°

Eccentric anomaly

291.36479°

Mean motion

3.37264 °/min

Orbital period

106.74 mins

BSTAR

0.00017695

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Other satellites on launch #5 in the year 1966 (1966-01-28 UTC)

OPS 1593 (TRANSIT 11), 1952

TRANSIT 11 DEB, 11990 (Decayed)

TRANSIT 11 DEB, 11991

TRANSIT 11 DEB, 14226 (Decayed)

TRANSIT 11 DEB, 15341 (Decayed)

TRANSIT 11 DEB, 19366 (Decayed)

TRANSIT 11 DEB, 24704 (Decayed)

TRANSIT 11 DEB, 38523 (Decayed)

SCOUT A DEB 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	2025-07-19 13:47:54.386Z	140.477° SSE	2025-07-19 13:51:54.386Z	89.518° E	29.496°	2025-07-19 13:56:54.386Z	17.824° NNE
7 mins	2025-07-19 15:35:54.386Z	232.265° WSW	2025-07-19 15:38:54.386Z	274.736° WNW	23.786°	2025-07-19 15:42:54.386Z	328.16° NNW
6 mins	2025-07-20 00:58:54.386Z	54.728° ENE	2025-07-20 01:00:54.386Z	75.909° E	15.058°	2025-07-20 01:04:54.386Z	114.695° SE
11 mins	2025-07-20 02:43:54.386Z	355.745° N	2025-07-20 02:47:54.386Z	305.346° NW	43.341°	2025-07-20 02:54:54.386Z	191.698° SSW

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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Check out SCOUT A DEB, 2140 on other resources

View SCOUT A DEB, 2140 on Heavens-Above

View SCOUT A DEB, 2140 on Keep Track

View SCOUT A DEB, 2140 on Celestrak

View SCOUT A DEB, 2140 on Gunter's Space Page

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