SCOUT A DEB, 31407

Orbit data source: Space-Track

SCOUT A DEB, 31407 is space debris in LEO originally from a launch on Thu, 19 May 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/31407?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

31407, 1966-041H

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)

1966-05-19 (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 31407U 66041H   25199.34238380  .00001577  00000-0  59170-3 0  9994
2 31407  90.1980  67.2201 0053296 276.9793  82.5343 14.30601868452395

Epoch: 2025-07-18T08:13Z

TLE epoch observation values (Epoch: 2025-07-18T08:13:01.96Z)

Latitude

-0.00001°

Longitude

7.56672°

Altitude

788.025 km

Speed

7.462 km/s

True Right ascension

04h 28m 52s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-14.55452°

Longitude

-172.46118°

Altitude

788.483 km

Speed

7.462 km/s

Apparent Right ascension

13h 48m 52s

Apparent Declination

-38° 34' 25"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

21:26:55

Azimuth

249.209° W

Elevation

-40.458°

Doppler factor

Orbital elements

Apogee altitude

824.838 km

Perigee altitude

748.467 km

Semi-major axis

7,164.79 km

Eccentricity

0.00533

Inclination

90.198°

RAAN

67.2201°

Arg. of periapsis

276.9793°

True anomaly

83.14036°

Mean anomaly

82.5343°

Eccentric anomaly

82.83728°

Mean motion

3.5788 °/min

Orbital period

100.59 mins

BSTAR

0.0005917

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Other satellites on launch #41 in the year 1966 (1966-05-19 UTC)

OPS 0082 (TRANSIT 13), 2176

SCOUT A R/B, 2180

SCOUT A DEB, 2225 (Decayed)

SCOUT A DEB, 2644

SCOUT A DEB, 3591

SCOUT A DEB, 4555

SCOUT A DEB, 28210 (Decayed)

TRANSIT 13 DEB, 42667 (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.
8 mins	2025-07-19 14:33:48.868Z	126.997° SE	2025-07-19 14:37:48.868Z	74.031° E	22.778°	2025-07-19 14:41:48.868Z	24.543° NE
8 mins	2025-07-19 16:14:48.868Z	217.166° SW	2025-07-19 16:17:48.868Z	270.67° WNW	31.621°	2025-07-19 16:22:48.868Z	340.823° N
8 mins	2025-07-20 02:46:48.868Z	29.269° NE	2025-07-20 02:50:48.868Z	92.711° ESE	28.282°	2025-07-20 02:54:48.868Z	146.491° SSE
7 mins	2025-07-20 04:27:48.868Z	328.833° NNW	2025-07-20 04:30:48.868Z	282.974° WNW	25.689°	2025-07-20 04:34:48.868Z	227.753° WSW

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, 31407 on other resources

View SCOUT A DEB, 31407 on Heavens-Above

View SCOUT A DEB, 31407 on Keep Track

View SCOUT A DEB, 31407 on Celestrak

View SCOUT A DEB, 31407 on Gunter's Space Page

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