OPS 4682 DEB, 38388

Orbit data source: Space-Track

OPS 4682 DEB, 38388 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/38388?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38388, 1965-027CR

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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago

0 OPS 4682 DEB
1 38388U 65027CR  26174.80861935  .00000425  00000-0  13739-2 0  9996
2 38388  90.2718  23.2037 0036817 336.4886  23.4552 13.00591340664923

Epoch: 2026-06-23T19:24Z

TLE epoch observation values (Epoch: 2026-06-23T19:24:24.711Z)

Latitude

-0.00004°

Longitude

-179.87413°

Altitude

1,236.87 km

Speed

7.249 km/s

True Right ascension

01h 32m 48s

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

21:07:33

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,285.007 km

Perigee altitude

1,228.787 km

Semi-major axis

7,635.034 km

Eccentricity

0.00368

Inclination

90.2718°

RAAN

23.2037°

Arg. of periapsis

336.4886°

True anomaly

23.62384°

Mean anomaly

23.4552°

Eccentric anomaly

23.53945°

Mean motion

3.25332 °/min

Orbital period

110.66 mins

BSTAR

0.0013739

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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	2026-06-24 13:58:44.118Z	163.31° S	2026-06-24 14:04:44.118Z	70.237° E	43.247°	2026-06-24 14:11:44.118Z	2.306° NNE
9 mins	2026-06-24 15:51:44.118Z	245.634° WSW	2026-06-24 15:55:44.118Z	283.364° WNW	19.314°	2026-06-24 16:00:44.118Z	326.664° NNW
13 mins	2026-06-25 01:33:44.118Z	16.537° NNE	2026-06-25 01:39:44.118Z	80.257° E	36.907°	2026-06-25 01:46:44.118Z	158.77° S
11 mins	2026-06-25 03:24:44.118Z	338.427° N	2026-06-25 03:29:44.118Z	290.533° WNW	27.753°	2026-06-25 03:35:44.118Z	230.333° WSW

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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, 38388 on other resources

View OPS 4682 DEB, 38388 on Heavens-Above

View OPS 4682 DEB, 38388 on Keep Track

View OPS 4682 DEB, 38388 on Celestrak

View OPS 4682 DEB, 38388 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, 38388

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2026-06-23T19:24:24.711Z)

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, 38388 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 15 hours ago