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

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 38388U 65027CR  26116.72575693  .00000367  00000-0  11806-2 0  9994
2 38388  90.2726  21.7492 0036134 120.0725 240.3988 13.00613735657378

Epoch: 2026-04-26T17:25Z

TLE epoch observation values (Epoch: 2026-04-26T17:25:05.398Z)

Latitude

-0.00011°

Longitude

-94.24894°

Altitude

1,276.278 km

Speed

7.211 km/s

True Right ascension

01h 26m 59s

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

05:44:26

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,284.397 km

Perigee altitude

1,229.221 km

Semi-major axis

7,634.946 km

Eccentricity

0.00361

Inclination

90.2726°

RAAN

21.7492°

Arg. of periapsis

120.0725°

True anomaly

240.03958°

Mean anomaly

240.3988°

Eccentric anomaly

240.21911°

Mean motion

3.25338 °/min

Orbital period

110.65 mins

BSTAR

0.0011806

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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	2026-04-30 05:06:24.153Z	15.362° NNE	2026-04-30 05:13:24.153Z	94.151° ESE	35.927°	2026-04-30 05:19:24.153Z	156.818° SSE
11 mins	2026-04-30 06:58:24.153Z	335.923° NNW	2026-04-30 07:03:24.153Z	281.954° WNW	27.651°	2026-04-30 07:09:24.153Z	226.438° WSW
12 mins	2026-04-30 17:32:24.153Z	164.884° S	2026-04-30 17:38:24.153Z	55.951° ENE	43.483°	2026-04-30 17:44:24.153Z	2.246° NNE
8 mins	2026-04-30 19:25:24.153Z	248.088° W	2026-04-30 19:29:24.153Z	285.456° WNW	18.487°	2026-04-30 19:33:24.153Z	320.973° 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, 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: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-04-26T17:25:05.398Z)

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: 3 days ago