OPS 4682 DEB, 1389

Orbit data source: Space-Track

OPS 4682 DEB, 1389 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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https://www.satcat.com/sats-embedded/1389?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

1389, 1965-027D

Orbit

LEO

Country

Related business

United States Space Force (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

7 kg wet, 7 kg dry

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

Radar Cross Section

Medium (>0.1 m² and <1 m²)

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Last TLE update: 7 hours ago

TLE from 7 hours ago

0 OPS 4682 DEB
1  1389U 65027D   26130.49962045  .00000482  00000-0  12710-2 0  9999
2  1389  89.8675 220.1684 0022374 230.1110 141.1965 13.14730861905730

Epoch: 2026-05-10T11:59Z

TLE epoch observation values (Epoch: 2026-05-10T11:59:27.206Z)

Latitude

11.42164°

Longitude

172.02986°

Altitude

1,220.301 km

Speed

7.239 km/s

True Right ascension

14h 40m 46s

True Declination

11° 21' 33"

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

03:40:36

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,218.975 km

Perigee altitude

1,185.055 km

Semi-major axis

7,580.152 km

Eccentricity

0.00224

Inclination

89.8675°

RAAN

220.1684°

Arg. of periapsis

230.111°

True anomaly

141.35682°

Mean anomaly

141.1965°

Eccentric anomaly

141.27669°

Mean motion

3.28872 °/min

Orbital period

109.47 mins

BSTAR

0.001271

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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.
9 mins	2026-05-10 19:51:38.941Z	329.488° NNW	2026-05-10 19:55:38.941Z	293.42° NW	19.887°	2026-05-10 20:00:38.941Z	246.238° WSW
5 mins	2026-05-11 04:33:38.941Z	88.033° E	2026-05-11 04:35:38.941Z	70.274° E	14.649°	2026-05-11 04:38:38.941Z	44.008° NE
12 mins	2026-05-11 06:18:38.941Z	175.095° S	2026-05-11 06:23:38.941Z	166.569° S	44.677°	2026-05-11 06:30:38.941Z	358.434° N
6 mins	2026-05-11 08:11:38.941Z	261.341° W	2026-05-11 08:14:38.941Z	288.039° WNW	14.773°	2026-05-11 08:17:38.941Z	313.772° NW
12 mins	2026-05-11 17:46:38.941Z	14.447° NNE	2026-05-11 17:52:38.941Z	102.247° ESE	39.583°	2026-05-11 17:58:38.941Z	164.506° S

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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, 1389 on other resources

View OPS 4682 DEB, 1389 on Heavens-Above

View OPS 4682 DEB, 1389 on Keep Track

View OPS 4682 DEB, 1389 on Celestrak

View OPS 4682 DEB, 1389 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, 1389

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 7 hours ago

TLE from 7 hours ago

TLE epoch observation values (Epoch: 2026-05-10T11:59:27.206Z)

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, 1389 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 7 hours ago