OPS 4682 DEB, 38363

Orbit data source: Space-Track

OPS 4682 DEB, 38363 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/38363?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38363, 1965-027BQ

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: 15 hours ago

TLE from 15 hours ago

0 OPS 4682 DEB
1 38363U 65027BQ  26107.18371696  .00000791  00000-0  25515-2 0  9997
2 38363  90.2468   8.2362 0032026   9.5799 350.5928 13.01265422544222

Epoch: 2026-04-17T04:24Z

TLE epoch observation values (Epoch: 2026-04-17T04:24:33.145Z)

Latitude

-0°

Longitude

96.77754°

Altitude

1,235.892 km

Speed

7.248 km/s

True Right ascension

00h 32m 56s

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

01:51:20

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,278.701 km

Perigee altitude

1,229.814 km

Semi-major axis

7,632.395 km

Eccentricity

0.0032

Inclination

90.2468°

RAAN

8.2362°

Arg. of periapsis

9.5799°

True anomaly

350.53258°

Mean anomaly

350.5928°

Eccentric anomaly

350.56271°

Mean motion

3.25501 °/min

Orbital period

110.6 mins

BSTAR

0.0025515

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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.
10 mins	2026-04-17 19:18:06.886Z	238.948° WSW	2026-04-17 19:23:06.886Z	284.019° WNW	19.242°	2026-04-17 19:28:06.886Z	327.241° NNW
13 mins	2026-04-18 05:01:06.886Z	18.377° NNE	2026-04-18 05:07:06.886Z	91.225° ESE	36.648°	2026-04-18 05:14:06.886Z	159.793° S
11 mins	2026-04-18 06:52:06.886Z	335.803° NNW	2026-04-18 06:57:06.886Z	283.028° WNW	27.894°	2026-04-18 07:03:06.886Z	227.429° WSW
13 mins	2026-04-18 17:25:06.886Z	165.899° S	2026-04-18 17:31:06.886Z	94.354° ESE	43.786°	2026-04-18 17:38:06.886Z	1.846° 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, 38363 on other resources

View OPS 4682 DEB, 38363 on Heavens-Above

View OPS 4682 DEB, 38363 on Keep Track

View OPS 4682 DEB, 38363 on Celestrak

View OPS 4682 DEB, 38363 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, 38363

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2026-04-17T04:24:33.145Z)

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, 38363 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 15 hours ago