OPS 4682 DEB, 17666

Orbit data source: Space-Track

OPS 4682 DEB, 17666 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/17666?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

17666, 1965-027V

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 17666U 65027V   26103.73135163  .00000684  00000-0  23306-2 0  9991
2 17666  90.2504  10.5557 0038593 258.6397 127.6686 12.97285663941457

Epoch: 2026-04-13T17:33Z

TLE epoch observation values (Epoch: 2026-04-13T17:33:08.780Z)

Latitude

26.68936°

Longitude

-94.77388°

Altitude

1,294.108 km

Speed

7.203 km/s

True Right ascension

00h 41m 43s

True Declination

26° 33' 40"

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

14:57:03

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,299.387 km

Perigee altitude

1,240.355 km

Semi-major axis

7,648.008 km

Eccentricity

0.00386

Inclination

90.2504°

RAAN

10.5557°

Arg. of periapsis

258.6397°

True anomaly

128.01763°

Mean anomaly

127.6686°

Eccentric anomaly

127.84322°

Mean motion

3.24504 °/min

Orbital period

110.94 mins

BSTAR

0.0023306

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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	2026-04-14 17:34:24.411Z	157.333° SSE	2026-04-14 17:41:24.411Z	77.187° E	40.704°	2026-04-14 17:48:24.411Z	5.749° NNE
11 mins	2026-04-14 19:27:24.411Z	232.332° WSW	2026-04-14 19:32:24.411Z	279.632° WNW	23.648°	2026-04-14 19:38:24.411Z	332.737° NNW
13 mins	2026-04-15 05:12:24.411Z	19.901° NNE	2026-04-15 05:18:24.411Z	82.625° E	33.627°	2026-04-15 05:25:24.411Z	153.44° SSE
12 mins	2026-04-15 07:03:24.411Z	342.114° N	2026-04-15 07:09:24.411Z	278.632° WNW	30.997°	2026-04-15 07:15:24.411Z	221.9° 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, 17666 on other resources

View OPS 4682 DEB, 17666 on Heavens-Above

View OPS 4682 DEB, 17666 on Keep Track

View OPS 4682 DEB, 17666 on Celestrak

View OPS 4682 DEB, 17666 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, 17666

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: 2026-04-13T17:33:08.780Z)

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, 17666 on other resources

Documentation

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