OPS 4682 DEB, 38429

Orbit data source: Space-Track

OPS 4682 DEB, 38429 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/38429?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38429, 1965-027EJ

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: 6 days ago

TLE from 6 days ago

0 OPS 4682 DEB
1 38429U 65027EJ  26202.15238660 -.00000157  00000-0 -56080-3 0  9996
2 38429  90.2347   1.4601 0039791 306.1907  53.5536 12.98007719593828

Epoch: 2026-07-21T03:39Z

TLE epoch observation values (Epoch: 2026-07-21T03:39:26.202Z)

Latitude

-0.00007°

Longitude

7.67475°

Altitude

1,254.78 km

Speed

7.236 km/s

True Right ascension

00h 05m 50s

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

00:02:04

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,297.453 km

Perigee altitude

1,236.611 km

Semi-major axis

7,645.169 km

Eccentricity

0.00398

Inclination

90.2347°

RAAN

1.4601°

Arg. of periapsis

306.1907°

True anomaly

53.92147°

Mean anomaly

53.5536°

Eccentric anomaly

53.73743°

Mean motion

3.24685 °/min

Orbital period

110.88 mins

BSTAR

-0.0005608

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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.
14 mins	2026-07-27 11:27:01.751Z	204.86° SW	2026-07-27 11:34:01.751Z	277.393° WNW	34.619°	2026-07-27 11:41:01.751Z	344.599° N
10 mins	2026-07-27 21:15:01.751Z	35.812° NE	2026-07-27 21:20:01.751Z	83.943° E	22.525°	2026-07-27 21:25:01.751Z	128.14° SE
13 mins	2026-07-27 23:05:01.751Z	352.551° N	2026-07-27 23:11:01.751Z	269.437° W	41.51°	2026-07-27 23:18:01.751Z	200.026° SSW
12 mins	2026-07-28 09:41:01.751Z	136.093° SSE	2026-07-28 09:46:01.751Z	82.948° E	32.213°	2026-07-28 09:53:01.751Z	13.268° NNE

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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, 38429 on other resources

View OPS 4682 DEB, 38429 on Heavens-Above

View OPS 4682 DEB, 38429 on Keep Track

View OPS 4682 DEB, 38429 on Celestrak

View OPS 4682 DEB, 38429 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, 38429

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 days ago

TLE from 6 days ago

TLE epoch observation values (Epoch: 2026-07-21T03:39:26.202Z)

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, 38429 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 6 days ago