SCOUT B DEB, 2800

Orbit data source: Space-Track

SCOUT B DEB, 2800 is space debris in LEO originally from a launch on Thu, 04 Aug 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/2800?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2800, 1966-070D

Orbit

LEO

Country

Related business

United States Space Force (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-08-04 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago

0 SCOUT B DEB
1 02800U 66070D   25351.55839625  .00003852  00000-0  48943-3 0  9997
2 02800  81.4039  19.1890 1399938  89.4484 286.6326 12.40446429562220

Epoch: 2025-12-17T13:24Z

TLE epoch observation values (Epoch: 2025-12-17T13:24:05.435Z)

Latitude

-0.00006°

Longitude

91.73981°

Altitude

1,340.417 km

Speed

7.263 km/s

True Right ascension

01h 16m 45s

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

22:13:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

2,605.207 km

Perigee altitude

398.857 km

Semi-major axis

7,880.169 km

Eccentricity

0.13999

Inclination

81.4039°

RAAN

19.189°

Arg. of periapsis

89.4484°

True anomaly

270.6635°

Mean anomaly

286.6326°

Eccentric anomaly

278.70392°

Mean motion

3.1027 °/min

Orbital period

116.03 mins

BSTAR

0.00048943

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Other satellites on launch #70 in the year 1966 (1966-08-04 UTC)

SCOUT B R/B, 2404 (Decayed)

SCOUT B DEB, 2521 (Decayed)

OV3-3, 2389

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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

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SCOUT B DEB 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	2025-12-18 03:03:31.113Z	196.157° SSW	2025-12-18 03:08:31.113Z	269.577° W	42.702°	2025-12-18 03:11:31.113Z	359.526° N
7 mins	2025-12-18 13:11:31.113Z	32.47° NE	2025-12-18 13:13:31.113Z	78.781° E	29.298°	2025-12-18 13:18:31.113Z	143.357° SSE
4 mins	2025-12-18 15:09:31.113Z	282.424° WNW	2025-12-18 15:10:31.113Z	267.437° W	16.379°	2025-12-18 15:13:31.113Z	232.241° WSW

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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 B DEB, 2800 on other resources

View SCOUT B DEB, 2800 on Heavens-Above

View SCOUT B DEB, 2800 on Keep Track

View SCOUT B DEB, 2800 on Celestrak

View SCOUT B DEB, 2800 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 B DEB, 2800

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2025-12-17T13:24:05.435Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #70 in the year 1966 (1966-08-04 UTC)

SCOUT B DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out SCOUT B DEB, 2800 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago