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

3 days 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 3 days ago

0 SCOUT A DEB
1 02580U 66076C   25118.08559062  .00000475  00000-0  44079-3 0  9995
2 02580  89.1464 324.3846 0096179 142.0234 347.9955 13.78511178934715

Epoch: 2025-04-28T02:03Z

Definitive object data (Epoch: 2025-04-28T02:03:15.029Z)

Latitude

50.30176°

Longitude

-103.75565°

Altitude

908.177 km

Speed

7.437 km/s

True Right ascension

09h 33m 26s

True Declination

50° 08' 10"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-18.89892°

Longitude

-102.70552°

Altitude

946.616 km

Speed

7.392 km/s

Apparent Right ascension

12h 25m 53s

Apparent Declination

-60° 50' 29"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

07:40:06

Azimuth

149.018° SSE

Elevation

-26.196°

Doppler factor

Orbital elements

Apogee altitude

1,036.819 km

Perigee altitude

895.545 km

Semi-major axis

7,344.319 km

Eccentricity

0.0096179

Inclination

89.1464°

RAAN

324.3846°

Arg. of periapsis

142.0234°

True anomaly

347.76354°

Mean anomaly

347.9955°

Eccentric anomaly

347.8798°

Mean motion

3.44839 °/min

BSTAR

0.00044079

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	2025-05-01 01:26:52.097Z	12.99° NNE	2025-05-01 01:31:52.097Z	97.79° ESE	39.045°	2025-05-01 01:36:52.097Z	164.26° S
6 mins	2025-05-01 03:12:52.097Z	317.09° NNW	2025-05-01 03:15:52.097Z	280.174° WNW	17.987°	2025-05-01 03:18:52.097Z	246.311° WSW
9 mins	2025-05-01 13:10:52.097Z	137.863° SSE	2025-05-01 13:14:52.097Z	79.733° E	31.715°	2025-05-01 13:19:52.097Z	17.28° NNE
9 mins	2025-05-01 14:54:52.097Z	222.891° SW	2025-05-01 14:58:52.097Z	270.643° WNW	26.511°	2025-05-01 15:03:52.097Z	333.722° NNW

Authenticating...

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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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