OPS 4682 DEB, 38380

Orbit data source: Space-Track

OPS 4682 DEB, 38380 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/38380?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38380, 1965-027CH

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: 3 days ago

TLE from 3 days ago

0 OPS 4682 DEB
1 38380U 65027CH  26104.35440239  .00001080  00000-0  35693-2 0  9992
2 38380  90.2626 319.7568 0023625 124.0247 236.3123 12.99809021569322

Epoch: 2026-04-14T08:30Z

TLE epoch observation values (Epoch: 2026-04-14T08:30:20.366Z)

Latitude

-0.00004°

Longitude

-10.35991°

Altitude

1,275.762 km

Speed

7.213 km/s

True Right ascension

21h 19m 01s

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

01:07:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,278.007 km

Perigee altitude

1,241.917 km

Semi-major axis

7,638.099 km

Eccentricity

0.00236

Inclination

90.2626°

RAAN

319.7568°

Arg. of periapsis

124.0247°

True anomaly

236.08741°

Mean anomaly

236.3123°

Eccentric anomaly

236.19982°

Mean motion

3.25136 °/min

Orbital period

110.72 mins

BSTAR

0.0035693

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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.
13 mins	2026-04-18 01:47:24.604Z	15.269° NNE	2026-04-18 01:54:24.604Z	95.508° ESE	36.357°	2026-04-18 02:00:24.604Z	157.578° S
11 mins	2026-04-18 03:39:24.604Z	335.589° NNW	2026-04-18 03:44:24.604Z	282.221° WNW	27.418°	2026-04-18 03:50:24.604Z	227.113° WSW
13 mins	2026-04-18 14:13:24.604Z	166.333° S	2026-04-18 14:19:24.604Z	75.829° E	44.018°	2026-04-18 14:26:24.604Z	1.289° NNE
8 mins	2026-04-18 16:07:24.604Z	253.187° W	2026-04-18 16:10:24.604Z	281.267° WNW	18.21°	2026-04-18 16:15:24.604Z	324.505° NNW

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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, 38380 on other resources

View OPS 4682 DEB, 38380 on Heavens-Above

View OPS 4682 DEB, 38380 on Keep Track

View OPS 4682 DEB, 38380 on Celestrak

View OPS 4682 DEB, 38380 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, 38380

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-04-14T08:30:20.366Z)

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, 38380 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago