OPS 4682 DEB, 38433

Orbit data source: Space-Track

OPS 4682 DEB, 38433 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/38433?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38433, 1965-027EN

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: 16 hours ago

TLE from 16 hours ago

0 OPS 4682 DEB
1 38433U 65027EN  26104.19731911  .00001175  00000-0  32473-2 0  9991
2 38433  90.2607  11.7115 0033237 355.2312   4.8496 13.12175873623451

Epoch: 2026-04-14T04:44Z

TLE epoch observation values (Epoch: 2026-04-14T04:44:08.371Z)

Latitude

0.00003°

Longitude

98.2996°

Altitude

1,192.501 km

Speed

7.269 km/s

True Right ascension

00h 46m 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

03:30:20

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,237.086 km

Perigee altitude

1,186.632 km

Semi-major axis

7,589.996 km

Eccentricity

0.00332

Inclination

90.2607°

RAAN

11.7115°

Arg. of periapsis

355.2312°

True anomaly

4.88193°

Mean anomaly

4.8496°

Eccentric anomaly

4.86575°

Mean motion

3.28232 °/min

Orbital period

109.68 mins

BSTAR

0.0032473

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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	2026-04-15 05:07:38.217Z	20.226° NNE	2026-04-15 05:14:38.217Z	91.654° ESE	29.814°	2026-04-15 05:20:38.217Z	147.192° SSE
11 mins	2026-04-15 06:58:38.217Z	341.887° N	2026-04-15 07:03:38.217Z	281.942° WNW	33.948°	2026-04-15 07:09:38.217Z	217.079° SW
11 mins	2026-04-15 17:27:38.217Z	145.729° SSE	2026-04-15 17:32:38.217Z	77.882° E	37.211°	2026-04-15 17:38:38.217Z	10.493° NNE
10 mins	2026-04-15 19:17:38.217Z	228.489° WSW	2026-04-15 19:22:38.217Z	283.396° WNW	25.663°	2026-04-15 19:27:38.217Z	332.186° 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, 38433 on other resources

View OPS 4682 DEB, 38433 on Heavens-Above

View OPS 4682 DEB, 38433 on Keep Track

View OPS 4682 DEB, 38433 on Celestrak

View OPS 4682 DEB, 38433 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, 38433

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2026-04-14T04:44:08.371Z)

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, 38433 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago