OPS 4682 DEB, 29059

Orbit data source: Space-Track

OPS 4682 DEB, 29059 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/29059?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29059, 1965-027BJ

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, 0.094 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

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

TLE from 2 days ago

0 OPS 4682 DEB
1 29059U 65027BJ  26296.67290743  .00000176  00000-0  60776-3 0  9991
2 29059  90.2464   9.1294 0029322 247.9133 265.8884 12.94379072172234

Epoch: 2026-10-23T16:08Z

TLE epoch observation values (Epoch: 2026-10-23T16:08:59.201Z)

Latitude

26.56507°

Longitude

-85.08477°

Altitude

1,289.094 km

Speed

7.213 km/s

True Right ascension

12h 37m 00s

True Declination

26° 26' 14"

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

01:01:38

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,303.784 km

Perigee altitude

1,258.866 km

Semi-major axis

7,659.462 km

Eccentricity

0.00293

Inclination

90.2464°

RAAN

9.1294°

Arg. of periapsis

247.9133°

True anomaly

265.55335°

Mean anomaly

265.8884°

Eccentric anomaly

265.72087°

Mean motion

3.23777 °/min

Orbital period

111.19 mins

BSTAR

0.00060776

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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.
12 mins	2026-10-25 06:25:34.614Z	221.073° SW	2026-10-25 06:31:34.614Z	279.805° WNW	31.865°	2026-10-25 06:37:34.614Z	335.758° NNW
12 mins	2026-10-25 16:13:34.614Z	26.772° NE	2026-10-25 16:18:34.614Z	78.337° E	35.064°	2026-10-25 16:25:34.614Z	146.533° SSE
12 mins	2026-10-25 18:04:34.614Z	343.404° N	2026-10-25 18:09:34.614Z	288.662° WNW	43.703°	2026-10-25 18:16:34.614Z	214.606° SW
13 mins	2026-10-26 04:41:34.614Z	153.205° SSE	2026-10-26 04:47:34.614Z	70.696° E	57.54°	2026-10-26 04:54:34.614Z	5.871° NNE

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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, 29059 on other resources

View OPS 4682 DEB, 29059 on Heavens-Above

View OPS 4682 DEB, 29059 on Keep Track

View OPS 4682 DEB, 29059 on Celestrak

View OPS 4682 DEB, 29059 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, 29059

Orbit data source: Space-Track

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

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-10-23T16:08:59.201Z)

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, 29059 on other resources

Documentation

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