OPS 4682 DEB, 18269

Orbit data source: Space-Track

OPS 4682 DEB, 18269 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/18269?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

18269, 1965-027Y

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: 2 weeks ago

TLE from 2 weeks ago

0 OPS 4682 DEB
1 18269U 65027Y   26026.22750212  .00000351  00000-0  12083-2 0  9998
2 18269  90.2560  10.2088 0030801 191.4153 168.6272 12.95879205551501

Epoch: 2026-01-26T05:27Z

TLE epoch observation values (Epoch: 2026-01-26T05:27:36.183Z)

Latitude

0.00003°

Longitude

162.78176°

Altitude

1,304.279 km

Speed

7.194 km/s

True Right ascension

00h 40m 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

14:10:10

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,298.982 km

Perigee altitude

1,251.834 km

Semi-major axis

7,653.545 km

Eccentricity

0.00308

Inclination

90.256°

RAAN

10.2088°

Arg. of periapsis

191.4153°

True anomaly

168.69654°

Mean anomaly

168.6272°

Eccentric anomaly

168.6619°

Mean motion

3.24152 °/min

Orbital period

111.06 mins

BSTAR

0.0012083

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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	2026-02-11 21:49:25.906Z	163.156° S	2026-02-11 21:55:25.906Z	100.921° ESE	42.983°	2026-02-11 22:02:25.906Z	3.368° NNE
9 mins	2026-02-11 23:43:25.906Z	245.732° WSW	2026-02-11 23:47:25.906Z	283.583° WNW	20.118°	2026-02-11 23:52:25.906Z	326.805° NNW
13 mins	2026-02-12 09:27:25.906Z	16.282° NNE	2026-02-12 09:33:25.906Z	82.234° E	37.036°	2026-02-12 09:40:25.906Z	159.804° S
10 mins	2026-02-12 11:19:25.906Z	334.383° NNW	2026-02-12 11:24:25.906Z	280.85° WNW	26.874°	2026-02-12 11:29:25.906Z	232.345° WSW

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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, 18269 on other resources

View OPS 4682 DEB, 18269 on Heavens-Above

View OPS 4682 DEB, 18269 on Keep Track

View OPS 4682 DEB, 18269 on Celestrak

View OPS 4682 DEB, 18269 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, 18269

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 weeks ago

TLE from 2 weeks ago

TLE epoch observation values (Epoch: 2026-01-26T05:27:36.183Z)

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, 18269 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 weeks ago