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

Last TLE update

1 day ago

Origin

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

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 SCOUT B DEB
1 02800U 66070D   25220.81574705  .00011055  00000-0  14265-2 0  9999
2 02800  81.4042 115.3978 1412602  15.5373 348.4781 12.37698988546039

Epoch: 2025-08-08T19:34Z

TLE epoch observation values (Epoch: 2025-08-08T19:34:40.545Z)

Latitude

-0.00006°

Longitude

-135.83153°

Altitude

434.04 km

Speed

8.16 km/s

True Right ascension

07h 41m 35s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

68.61451°

Longitude

20.79314°

Altitude

1,497.043 km

Speed

7.136 km/s

Apparent Right ascension

21h 39m 13s

Apparent Declination

28° 05' 15"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

11:30:48

Azimuth

25.605° NE

Elevation

-17.212°

Doppler factor

Orbital elements

Apogee altitude

2,628.498 km

Perigee altitude

398.894 km

Semi-major axis

7,891.833 km

Eccentricity

0.14126

Inclination

81.4042°

RAAN

115.3978°

Arg. of periapsis

15.5373°

True anomaly

344.57847°

Mean anomaly

348.4781°

Eccentric anomaly

346.60281°

Mean motion

3.09582 °/min

Orbital period

116.29 mins

BSTAR

0.0014265

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

OV3-3, 2389

SCOUT B R/B, 2404 (Decayed)

SCOUT B DEB, 2521 (Decayed)

SCOUT B 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.
18 mins	2025-08-10 03:07:49.480Z	16.824° NNE	2025-08-10 03:14:49.480Z	68.488° E	27.676°	2025-08-10 03:25:49.480Z	127.786° SE
22 mins	2025-08-10 05:04:49.480Z	345.471° N	2025-08-10 05:12:49.480Z	272.689° WNW	43.987°	2025-08-10 05:26:49.480Z	183.483° SSW
12 mins	2025-08-10 07:04:49.480Z	307.524° NW	2025-08-10 07:09:49.480Z	277.802° WNW	17.424°	2025-08-10 07:16:49.480Z	244.603° WSW
5 mins	2025-08-10 18:16:49.480Z	243.673° WSW	2025-08-10 18:17:49.480Z	276.261° WNW	29.662°	2025-08-10 18:21:49.480Z	353.601° N

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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Authenticating...

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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

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