OPS 4682 DEB, 38436

Orbit data source: Space-Track

OPS 4682 DEB, 38436 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/38436?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38436, 1965-027ER

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: 4 days ago

TLE from 4 days ago

0 OPS 4682 DEB
1 38436U 65027ER  26147.54809523 -.00000513  00000-0 -17279-2 0  9999
2 38436  90.2405   2.4236 0025120 352.6502   7.4248 12.99946229612744

Epoch: 2026-05-27T13:09Z

TLE epoch observation values (Epoch: 2026-05-27T13:09:15.427Z)

Latitude

-0.00008°

Longitude

-79.99628°

Altitude

1,246.146 km

Speed

7.241 km/s

True Right ascension

00h 09m 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

18:34:21

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,278.61 km

Perigee altitude

1,240.239 km

Semi-major axis

7,637.561 km

Eccentricity

0.00251

Inclination

90.2405°

RAAN

2.4236°

Arg. of periapsis

352.6502°

True anomaly

7.46211°

Mean anomaly

7.4248°

Eccentric anomaly

7.44345°

Mean motion

3.2517 °/min

Orbital period

110.71 mins

BSTAR

-0.0017279

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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	2026-05-31 13:19:19.109Z	133.66° SE	2026-05-31 13:25:19.109Z	79.272° E	27.704°	2026-05-31 13:31:19.109Z	19.553° NNE
12 mins	2026-05-31 15:10:19.109Z	206.316° SW	2026-05-31 15:15:19.109Z	262.641° W	36.083°	2026-05-31 15:22:19.109Z	344.196° N
9 mins	2026-06-01 00:56:19.109Z	39.826° NE	2026-06-01 01:00:19.109Z	76.753° E	20.255°	2026-06-01 01:05:19.109Z	121.626° SE
13 mins	2026-06-01 02:45:19.109Z	356.009° N	2026-06-01 02:51:19.109Z	290.784° WNW	42.972°	2026-06-01 02:58:19.109Z	196.488° 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, 38436 on other resources

View OPS 4682 DEB, 38436 on Heavens-Above

View OPS 4682 DEB, 38436 on Keep Track

View OPS 4682 DEB, 38436 on Celestrak

View OPS 4682 DEB, 38436 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, 38436

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 4 days ago

TLE from 4 days ago

TLE epoch observation values (Epoch: 2026-05-27T13:09:15.427Z)

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, 38436 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 4 days ago