OPS 4682 DEB, 19576

Orbit data source: Space-Track

OPS 4682 DEB, 19576 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/19576?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

19576, 1965-027AV

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: 8 hours ago

TLE from 8 hours ago

0 OPS 4682 DEB
1 19576U 65027AV  26036.36864947 -.00000163  00000-0 -55952-3 0  9993
2 19576  90.2392   6.1534 0024830 202.9071 311.8320 13.00673674781216

Epoch: 2026-02-05T08:50Z

TLE epoch observation values (Epoch: 2026-02-05T08:50:51.314Z)

Latitude

25.5006°

Longitude

-81.96876°

Altitude

1,249.914 km

Speed

7.238 km/s

True Right ascension

12h 25m 04s

True Declination

25° 22' 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

18:28:38

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,275.531 km

Perigee altitude

1,237.617 km

Semi-major axis

7,634.711 km

Eccentricity

0.00248

Inclination

90.2392°

RAAN

6.1534°

Arg. of periapsis

202.9071°

True anomaly

311.61956°

Mean anomaly

311.832°

Eccentric anomaly

311.72582°

Mean motion

3.25353 °/min

Orbital period

110.65 mins

BSTAR

-0.00055952

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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.
12 mins	2026-02-05 21:05:46.848Z	131.145° SE	2026-02-05 21:11:46.848Z	72.945° E	27.84°	2026-02-05 21:17:46.848Z	17.89° NNE
13 mins	2026-02-05 22:55:46.848Z	204.002° SW	2026-02-05 23:01:46.848Z	274.111° WNW	36.793°	2026-02-05 23:08:46.848Z	345.859° N
9 mins	2026-02-06 08:41:46.848Z	38.633° NE	2026-02-06 08:45:46.848Z	74.886° E	19.465°	2026-02-06 08:50:46.848Z	120.335° SE
13 mins	2026-02-06 10:30:46.848Z	356.585° N	2026-02-06 10:36:46.848Z	297.357° NW	42.997°	2026-02-06 10:43:46.848Z	195.801° SSW

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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, 19576 on other resources

View OPS 4682 DEB, 19576 on Heavens-Above

View OPS 4682 DEB, 19576 on Keep Track

View OPS 4682 DEB, 19576 on Celestrak

View OPS 4682 DEB, 19576 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, 19576

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-02-05T08:50:51.314Z)

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, 19576 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago