SCOUT A DEB, 2580

Orbit data source: Space-Track

SCOUT A DEB, 2580 is space debris in LEO originally from a launch on Thu, 18 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/2580?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2580, 1966-076C

Orbit

LEO

Last TLE update

7 hours ago

Origin

United States Navy (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-08-18 (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 7 hours ago

0 SCOUT A DEB
1 02580U 66076C   25128.97845921  .00000365  00000-0  33494-3 0  9993
2 02580  89.1457 323.3982 0097038 109.6268  44.9365 13.78519890936213

Epoch: 2025-05-08T23:28Z

Definitive object data (Epoch: 2025-05-08T23:28:58.875Z)

Latitude

24.66682°

Longitude

-76.27862°

Altitude

922.082 km

Speed

7.418 km/s

True Right ascension

09h 32m 01s

True Declination

24° 32' 23"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

40.73136°

Longitude

-76.64612°

Altitude

913.505 km

Speed

7.43 km/s

Apparent Right ascension

06h 18m 59s

Apparent Declination

5° 56' 53"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

14:31:19

Azimuth

297.176° NW

Elevation

-20.482°

Doppler factor

Orbital elements

Apogee altitude

1,037.419 km

Perigee altitude

894.884 km

Semi-major axis

7,344.288 km

Eccentricity

0.0097038

Inclination

89.1457°

RAAN

323.3982°

Arg. of periapsis

109.6268°

True anomaly

45.72869°

Mean anomaly

44.9365°

Eccentric anomaly

45.33191°

Mean motion

3.44841 °/min

BSTAR

0.00033494

Orbital period

104.4 mins

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Other satellites on launch #76 in the year 1966 (1966-08-18 UTC)

OPS 2366 (TRANSIT 14), 2401

SCOUT A R/B, 2413

SCOUT A DEB, 2702

TRANSIT 14 DEB, 7558 (Decayed)

TRANSIT 14 DEB, 8000 (Decayed)

TRANSIT 14 DEB, 9401 (Decayed)

TRANSIT 14 DEB, 26817

TRANSIT 14 DEB, 29138 (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.
10 mins	2025-05-09 12:47:29.683Z	151.219° SSE	2025-05-09 12:52:29.683Z	77.798° E	36.159°	2025-05-09 12:57:29.683Z	12.66° NNE
8 mins	2025-05-09 14:33:29.683Z	236.887° WSW	2025-05-09 14:36:29.683Z	272.554° WNW	21.513°	2025-05-09 14:41:29.683Z	330.402° NNW
5 mins	2025-05-09 23:45:29.683Z	54.933° ENE	2025-05-09 23:47:29.683Z	77.547° E	14.522°	2025-05-09 23:50:29.683Z	109.494° ESE
9 mins	2025-05-10 01:28:29.683Z	352.716° N	2025-05-10 01:32:29.683Z	268.011° W	43.049°	2025-05-10 01:37:29.683Z	193.33° SSW

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Check out SCOUT A DEB, 2580 on other resources

View SCOUT A DEB, 2580 on Heavens-Above

View SCOUT A DEB, 2580 on Keep Track

View SCOUT A DEB, 2580 on Celestrak

View SCOUT A DEB, 2580 on Gunter's Space Page

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