OPS 4682 DEB, 18784

Orbit data source: Space-Track

OPS 4682 DEB, 18784 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/18784?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

18784, 1965-027AL

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: 11 hours ago

TLE from 11 hours ago

0 OPS 4682 DEB
1 18784U 65027AL  26104.17141435  .00000661  00000-0  22576-2 0  9994
2 18784  90.2536   2.9255 0040369 288.7649 225.6897 12.97107432794087

Epoch: 2026-04-14T04:06Z

TLE epoch observation values (Epoch: 2026-04-14T04:06:50.199Z)

Latitude

25.90391°

Longitude

-81.01261°

Altitude

1,298.226 km

Speed

7.199 km/s

True Right ascension

12h 12m 11s

True Declination

25° 46' 43"

Sunlit

Object was in full shadow 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

21:30:43

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,301.449 km

Perigee altitude

1,239.695 km

Semi-major axis

7,648.709 km

Eccentricity

0.00404

Inclination

90.2536°

RAAN

2.9255°

Arg. of periapsis

288.7649°

True anomaly

225.35985°

Mean anomaly

225.6897°

Eccentric anomaly

225.52466°

Mean motion

3.2446 °/min

Orbital period

110.95 mins

BSTAR

0.0022576

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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	2026-04-14 16:23:59.911Z	128.997° SE	2026-04-14 16:29:59.911Z	69.274° E	27.303°	2026-04-14 16:35:59.911Z	17.228° NNE
13 mins	2026-04-14 18:13:59.911Z	202.953° SW	2026-04-14 18:19:59.911Z	273.321° WNW	37.331°	2026-04-14 18:26:59.911Z	346.076° N
9 mins	2026-04-15 04:01:59.911Z	40.41° NE	2026-04-15 04:05:59.911Z	77.101° E	20.274°	2026-04-15 04:10:59.911Z	121.401° SE
14 mins	2026-04-15 05:50:59.911Z	356.493° N	2026-04-15 05:56:59.911Z	301.199° NW	42.905°	2026-04-15 06:04:59.911Z	195.237° 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, 18784 on other resources

View OPS 4682 DEB, 18784 on Heavens-Above

View OPS 4682 DEB, 18784 on Keep Track

View OPS 4682 DEB, 18784 on Celestrak

View OPS 4682 DEB, 18784 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, 18784

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-04-14T04:06:50.199Z)

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, 18784 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago