OPS 4682 DEB, 38382

Orbit data source: Space-Track

OPS 4682 DEB, 38382 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/38382?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38382, 1965-027CK

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: 19 hours ago

TLE from 19 hours ago

0 OPS 4682 DEB
1 38382U 65027CK  26100.01768213  .00000372  00000-0  12693-2 0  9996
2 38382  90.2547   7.4055 0027026 348.5992  11.4513 12.96761282 53592

Epoch: 2026-04-10T00:25Z

TLE epoch observation values (Epoch: 2026-04-10T00:25:27.736Z)

Latitude

0.00002°

Longitude

162.78256°

Altitude

1,257.409 km

Speed

7.236 km/s

True Right ascension

00h 29m 37s

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

01:42:48

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,292.609 km

Perigee altitude

1,251.259 km

Semi-major axis

7,650.071 km

Eccentricity

0.0027

Inclination

90.2547°

RAAN

7.4055°

Arg. of periapsis

348.5992°

True anomaly

11.51299°

Mean anomaly

11.4513°

Eccentric anomaly

11.48212°

Mean motion

3.24373 °/min

Orbital period

110.98 mins

BSTAR

0.0012693

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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.
12 mins	2026-04-11 04:49:07.842Z	26.905° NE	2026-04-11 04:55:07.842Z	81.997° E	24.887°	2026-04-11 05:01:07.842Z	135.732° SSE
13 mins	2026-04-11 06:40:07.842Z	350.688° N	2026-04-11 06:46:07.842Z	279.802° WNW	39.582°	2026-04-11 06:53:07.842Z	204.869° SW
12 mins	2026-04-11 17:17:07.842Z	141.299° SSE	2026-04-11 17:22:07.842Z	85.016° E	34.802°	2026-04-11 17:29:07.842Z	11.215° NNE
11 mins	2026-04-11 19:08:07.842Z	221.204° SW	2026-04-11 19:13:07.842Z	274.349° WNW	29.19°	2026-04-11 19:19:07.842Z	335.857° 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, 38382 on other resources

View OPS 4682 DEB, 38382 on Heavens-Above

View OPS 4682 DEB, 38382 on Keep Track

View OPS 4682 DEB, 38382 on Celestrak

View OPS 4682 DEB, 38382 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, 38382

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 19 hours ago

TLE from 19 hours ago

TLE epoch observation values (Epoch: 2026-04-10T00:25:27.736Z)

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, 38382 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 19 hours ago