OPS 4682 DEB, 38390

Orbit data source: Space-Track

OPS 4682 DEB, 38390 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/38390?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38390, 1965-027CT

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 38390U 65027CT  26119.41384564  .00000740  00000-0  25103-2 0  9991
2 38390  90.2351 357.9232 0029463 184.9557 175.1276 12.97754545606379

Epoch: 2026-04-29T09:55Z

TLE epoch observation values (Epoch: 2026-04-29T09:55:56.263Z)

Latitude

-0.00006°

Longitude

-8.43638°

Altitude

1,296.237 km

Speed

7.198 km/s

True Right ascension

23h 51m 41s

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

01:45:51

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,290.555 km

Perigee altitude

1,245.5 km

Semi-major axis

7,646.164 km

Eccentricity

0.00295

Inclination

90.2351°

RAAN

357.9232°

Arg. of periapsis

184.9557°

True anomaly

175.15617°

Mean anomaly

175.1276°

Eccentric anomaly

175.1419°

Mean motion

3.24622 °/min

Orbital period

110.9 mins

BSTAR

0.0025103

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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	2026-04-30 03:12:28.070Z	23.742° NE	2026-04-30 03:18:28.070Z	86.133° E	29.609°	2026-04-30 03:24:28.070Z	144.831° SSE
12 mins	2026-04-30 05:03:28.070Z	344.463° N	2026-04-30 05:09:28.070Z	272.968° WNW	34.127°	2026-04-30 05:15:28.070Z	215.171° SW
13 mins	2026-04-30 15:38:28.070Z	154.404° SSE	2026-04-30 15:44:28.070Z	93.099° ESE	39.603°	2026-04-30 15:51:28.070Z	7.651° NNE
10 mins	2026-04-30 17:31:28.070Z	234.294° WSW	2026-04-30 17:35:28.070Z	273.661° WNW	24.453°	2026-04-30 17:41:28.070Z	331.051° 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, 38390 on other resources

View OPS 4682 DEB, 38390 on Heavens-Above

View OPS 4682 DEB, 38390 on Keep Track

View OPS 4682 DEB, 38390 on Celestrak

View OPS 4682 DEB, 38390 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, 38390

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: 2026-04-29T09:55:56.263Z)

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, 38390 on other resources

Documentation

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