OPS 4682 DEB, 18965

Orbit data source: Space-Track

OPS 4682 DEB, 18965 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/18965?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

18965, 1965-027AN

Orbit

LEO

Last TLE update

1 day ago

Origin

United States Air Force (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1965-04-03 (60 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 OPS 4682 DEB
1 18965U 65027AN  25181.26764513 -.00000303  00000-0 -10338-2 0  9995
2 18965  90.2615  17.2980 0041747 288.7450 133.9046 12.99450625904785

Epoch: 2025-06-30T06:25Z

TLE epoch observation values (Epoch: 2025-06-30T06:25:24.539Z)

Latitude

63.07462°

Longitude

1.85354°

Altitude

1,297.351 km

Speed

7.203 km/s

True Right ascension

01h 07m 08s

True Declination

62° 56' 43"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

12.1278°

Longitude

2.33753°

Altitude

1,264.264 km

Speed

7.225 km/s

Apparent Right ascension

03h 52m 05s

Apparent Declination

-22° 03' 28"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:31:15

Azimuth

104.227° ESE

Elevation

-17.791°

Doppler factor

Orbital elements

Apogee altitude

1,293.26 km

Perigee altitude

1,229.475 km

Semi-major axis

7,639.505 km

Eccentricity

0.00417

Inclination

90.2615°

RAAN

17.298°

Arg. of periapsis

288.745°

True anomaly

Unknown

Mean anomaly

133.9046°

Eccentric anomaly

Unknown

Mean motion

3.25046 °/min

Orbital period

110.75 mins

BSTAR

-0.0010338

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

OPS 4682 (SNAPSHOT), 1314

OPS 4682 DEB Visibility forecast

Observer location: undefined°, undefined°

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.
9 mins	2025-07-01 11:48:53.745Z	110.393° ESE	2025-07-01 11:53:53.745Z	66.109° ENE	19.219°	2025-07-01 11:57:53.745Z	31.528° NE
13 mins	2025-07-01 13:36:53.745Z	184.655° SSW	2025-07-01 13:42:53.745Z	249.459° W	43.818°	2025-07-01 13:49:53.745Z	353.101° N
5 mins	2025-07-01 23:25:53.745Z	57.458° ENE	2025-07-01 23:27:53.745Z	73.709° E	12.59°	2025-07-01 23:30:53.745Z	97.401° ESE
14 mins	2025-07-02 01:12:53.745Z	5.69° NNE	2025-07-02 01:19:53.745Z	120.267° SE	44.317°	2025-07-02 01:26:53.745Z	178.891° S
8 mins	2025-07-02 03:05:53.745Z	320.318° NNW	2025-07-02 03:08:53.745Z	293.353° NW	18.319°	2025-07-02 03:13:53.745Z	250.769° W

Authenticating...

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Check out OPS 4682 DEB, 18965 on other resources

View OPS 4682 DEB, 18965 on Heavens-Above

View OPS 4682 DEB, 18965 on Keep Track

View OPS 4682 DEB, 18965 on Celestrak

View OPS 4682 DEB, 18965 on Gunter's Space Page

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