OPS 4682 DEB, 19950

Orbit data source: Space-Track

OPS 4682 DEB, 19950 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/19950?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

19950, 1965-027AY

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: 6 days ago

TLE from 6 days ago

0 OPS 4682 DEB
1 19950U 65027AY  26060.82341858 -.00000079  00000-0 -30973-3 0  9990
2 19950  90.2442   6.9282 0031630 109.1797 251.2750 12.95020872538757

Epoch: 2026-03-01T19:45Z

TLE epoch observation values (Epoch: 2026-03-01T19:45:43.365Z)

Latitude

-0.00001°

Longitude

-89.12814°

Altitude

1,292.382 km

Speed

7.206 km/s

True Right ascension

00h 27m 42s

True Declination

0° 00' 00"

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

11:45:53

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,303.011 km

Perigee altitude

1,254.573 km

Semi-major axis

7,656.929 km

Eccentricity

0.00316

Inclination

90.2442°

RAAN

6.9282°

Arg. of periapsis

109.1797°

True anomaly

250.93217°

Mean anomaly

251.275°

Eccentric anomaly

251.10354°

Mean motion

3.23938 °/min

Orbital period

111.13 mins

BSTAR

-0.00030973

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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.
14 mins	2026-03-07 08:01:11.003Z	8.677° NNE	2026-03-07 08:08:11.003Z	92.338° ESE	42.534°	2026-03-07 08:15:11.003Z	171.766° S
9 mins	2026-03-07 09:54:11.003Z	327.702° NNW	2026-03-07 09:58:11.003Z	290.226° WNW	21.059°	2026-03-07 10:03:11.003Z	244.76° WSW
7 mins	2026-03-07 18:43:11.003Z	96.745° ESE	2026-03-07 18:46:11.003Z	68.657° E	18.064°	2026-03-07 18:50:11.003Z	33.691° NE
13 mins	2026-03-07 20:30:11.003Z	182.911° SSW	2026-03-07 20:36:11.003Z	277.166° WNW	44.351°	2026-03-07 20:43:11.003Z	354.587° N

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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, 19950 on other resources

View OPS 4682 DEB, 19950 on Heavens-Above

View OPS 4682 DEB, 19950 on Keep Track

View OPS 4682 DEB, 19950 on Celestrak

View OPS 4682 DEB, 19950 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, 19950

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 days ago

TLE from 6 days ago

TLE epoch observation values (Epoch: 2026-03-01T19:45:43.365Z)

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, 19950 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 6 days ago