OPS 4682 DEB, 26732

Orbit data source: Space-Track

OPS 4682 DEB, 26732 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/26732?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26732, 1965-027BF

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 (62 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.071 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

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

TLE from 15 hours ago

0 OPS 4682 DEB
1 26732U 65027BF  26310.47761325  .00001145  00000-0  39582-2 0  9997
2 26732  90.2623  14.5265 0064850 170.1870 205.8127 12.96106869513602

Epoch: 2026-11-06T11:27Z

TLE epoch observation values (Epoch: 2026-11-06T11:27:45.784Z)

Latitude

15.65607°

Longitude

156.81593°

Altitude

1,324.349 km

Speed

7.175 km/s

True Right ascension

00h 57m 48s

True Declination

15° 34' 25"

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

22:10:08

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,324.138 km

Perigee altitude

1,224.884 km

Semi-major axis

7,652.648 km

Eccentricity

0.00649

Inclination

90.2623°

RAAN

14.5265°

Arg. of periapsis

170.187°

True anomaly

205.49147°

Mean anomaly

205.8127°

Eccentric anomaly

205.65185°

Mean motion

3.24209 °/min

Orbital period

111.04 mins

BSTAR

0.0039582

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Other satellites on launch #27 in the year 1965 (1965-04-03 UTC)

SECOR 4 (EGRS 4), 1315

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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.
14 mins	2026-11-07 04:09:25.007Z	152.338° SSE	2026-11-07 04:16:25.007Z	70.394° E	53.033°	2026-11-07 04:23:25.007Z	7.043° NNE
11 mins	2026-11-07 06:02:25.007Z	230.522° WSW	2026-11-07 06:07:25.007Z	282.098° WNW	29.283°	2026-11-07 06:13:25.007Z	335.32° NNW
11 mins	2026-11-07 15:48:25.007Z	26° NE	2026-11-07 15:53:25.007Z	80.971° E	36.423°	2026-11-07 15:59:25.007Z	145.548° SSE
11 mins	2026-11-07 17:39:25.007Z	340.776° N	2026-11-07 17:44:25.007Z	282.095° WNW	40.108°	2026-11-07 17:50:25.007Z	218.874° SW

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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, 26732 on other resources

View OPS 4682 DEB, 26732 on Heavens-Above

View OPS 4682 DEB, 26732 on Keep Track

View OPS 4682 DEB, 26732 on Celestrak

View OPS 4682 DEB, 26732 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, 26732

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: 2026-11-06T11:27:45.784Z)

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, 26732 on other resources

Documentation

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