OPS 4682 DEB, 38391

Orbit data source: Space-Track

OPS 4682 DEB, 38391 is space debris in LEO originally from a launch on Sat, 03 Apr 1965 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/38391?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38391, 1965-027CU

Orbit

LEO

Country

Related business

United States Air Force (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1965-04-03 (61 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: 5 days ago

TLE from 5 days ago

0 OPS 4682 DEB
1 38391U 65027CU  26114.41125813  .00000197  00000-0  64277-3 0  9999
2 38391  90.2238   6.7941 0039539 192.0727 167.9451 12.98390333592790

Epoch: 2026-04-24T09:52Z

TLE epoch observation values (Epoch: 2026-04-24T09:52:12.702Z)

Latitude

0.00005°

Longitude

6.29681°

Altitude

1,300.859 km

Speed

7.192 km/s

True Right ascension

00h 27m 10s

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

00:34:38

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,295.752 km

Perigee altitude

1,235.307 km

Semi-major axis

7,643.666 km

Eccentricity

0.00395

Inclination

90.2238°

RAAN

6.7941°

Arg. of periapsis

192.0727°

True anomaly

168.03927°

Mean anomaly

167.9451°

Eccentric anomaly

167.99223°

Mean motion

3.24781 °/min

Orbital period

110.84 mins

BSTAR

0.00064277

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Other satellites on launch #27 in the year 1965 (1965-04-03 UTC)

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OPS 4682 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.
14 mins	2026-04-29 17:34:26.566Z	202.355° SSW	2026-04-29 17:41:26.566Z	272.933° WNW	35.909°	2026-04-29 17:48:26.566Z	344.838° N
9 mins	2026-04-30 03:22:26.566Z	37.464° NE	2026-04-30 03:26:26.566Z	74.518° E	20.601°	2026-04-30 03:31:26.566Z	121.815° SE
12 mins	2026-04-30 05:12:26.566Z	353.706° N	2026-04-30 05:18:26.566Z	259.376° W	42.047°	2026-04-30 05:24:26.566Z	198.792° SSW
11 mins	2026-04-30 15:48:26.566Z	132.988° SE	2026-04-30 15:53:26.566Z	79.716° E	31.062°	2026-04-30 15:59:26.566Z	17.472° NNE

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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 OPS 4682 DEB, 38391 on other resources

View OPS 4682 DEB, 38391 on Heavens-Above

View OPS 4682 DEB, 38391 on Keep Track

View OPS 4682 DEB, 38391 on Celestrak

View OPS 4682 DEB, 38391 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

OPS 4682 DEB, 38391

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 5 days ago

TLE from 5 days ago

TLE epoch observation values (Epoch: 2026-04-24T09:52:12.702Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #27 in the year 1965 (1965-04-03 UTC)

OPS 4682 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out OPS 4682 DEB, 38391 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 5 days ago