OPS 4682 DEB, 38384

Orbit data source: Space-Track

OPS 4682 DEB, 38384 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/38384?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38384, 1965-027CM

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: 22 hours ago

TLE from 22 hours ago

0 OPS 4682 DEB
1 38384U 65027CM  26105.47890413 -.00000178  00000-0 -62956-3 0  9995
2 38384  90.2664  15.6039 0015983 150.2426 209.9608 12.98510921656194

Epoch: 2026-04-15T11:29Z

TLE epoch observation values (Epoch: 2026-04-15T11:29:37.316Z)

Latitude

0°

Longitude

-0.4418°

Altitude

1,281.402 km

Speed

7.21 km/s

True Right ascension

01h 02m 24s

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

16:26:36

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,277.272 km

Perigee altitude

1,252.84 km

Semi-major axis

7,643.193 km

Eccentricity

0.0016

Inclination

90.2664°

RAAN

15.6039°

Arg. of periapsis

150.2426°

True anomaly

209.86949°

Mean anomaly

209.9608°

Eccentric anomaly

209.91513°

Mean motion

3.24811 °/min

Orbital period

110.83 mins

BSTAR

-0.00062956

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

OPS 4682 (SNAPSHOT), 1314

OPS 4682 DEB, 19113

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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	2026-04-16 17:11:51.483Z	133.909° SE	2026-04-16 17:17:51.483Z	75.734° E	29.04°	2026-04-16 17:23:51.483Z	17.71° NNE
12 mins	2026-04-16 19:02:51.483Z	208.997° SW	2026-04-16 19:07:51.483Z	266.055° W	35.292°	2026-04-16 19:14:51.483Z	343.57° N
9 mins	2026-04-17 04:49:51.483Z	43.048° NE	2026-04-17 04:53:51.483Z	83.061° E	20.944°	2026-04-17 04:58:51.483Z	126.717° SE
13 mins	2026-04-17 06:38:51.483Z	353.993° N	2026-04-17 06:44:51.483Z	269.144° W	42.168°	2026-04-17 06:51:51.483Z	198.046° SSW

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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, 38384 on other resources

View OPS 4682 DEB, 38384 on Heavens-Above

View OPS 4682 DEB, 38384 on Keep Track

View OPS 4682 DEB, 38384 on Celestrak

View OPS 4682 DEB, 38384 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, 38384

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 22 hours ago

TLE from 22 hours ago

TLE epoch observation values (Epoch: 2026-04-15T11:29:37.316Z)

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, 38384 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 22 hours ago