OPS 4682 DEB, 38405

Orbit data source: Space-Track

OPS 4682 DEB, 38405 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/38405?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38405, 1965-027DJ

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: 8 hours ago

TLE from 8 hours ago

0 OPS 4682 DEB
1 38405U 65027DJ  26119.48981585  .00001951  00000-0  64868-2 0  9997
2 38405  90.2709  21.0288 0014956 280.2737  79.6698 12.99695162658738

Epoch: 2026-04-29T11:45Z

TLE epoch observation values (Epoch: 2026-04-29T11:45:20.089Z)

Latitude

-0.00007°

Longitude

-12.75494°

Altitude

1,264.131 km

Speed

7.224 km/s

True Right ascension

01h 24m 06s

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

03:42:59

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,271.833 km

Perigee altitude

1,248.985 km

Semi-major axis

7,638.546 km

Eccentricity

0.0015

Inclination

90.2709°

RAAN

21.0288°

Arg. of periapsis

280.2737°

True anomaly

79.83846°

Mean anomaly

79.6698°

Eccentric anomaly

79.75413°

Mean motion

3.25108 °/min

Orbital period

110.73 mins

BSTAR

0.0064868

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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	2026-04-30 04:59:16.462Z	15.588° NNE	2026-04-30 05:06:16.462Z	86.889° E	35.149°	2026-04-30 05:13:16.462Z	156.826° SSE
11 mins	2026-04-30 06:51:16.462Z	338.854° N	2026-04-30 06:56:16.462Z	287.825° WNW	29.314°	2026-04-30 07:02:16.462Z	226.683° WSW
13 mins	2026-04-30 17:25:16.462Z	163.333° S	2026-04-30 17:31:16.462Z	91.213° ESE	43.217°	2026-04-30 17:38:16.462Z	2.909° NNE
9 mins	2026-04-30 19:18:16.462Z	242.319° WSW	2026-04-30 19:22:16.462Z	278.541° WNW	19.778°	2026-04-30 19:27:16.462Z	323.799° 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, 38405 on other resources

View OPS 4682 DEB, 38405 on Heavens-Above

View OPS 4682 DEB, 38405 on Keep Track

View OPS 4682 DEB, 38405 on Celestrak

View OPS 4682 DEB, 38405 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, 38405

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-04-29T11:45:20.089Z)

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, 38405 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago