OPS 4682 DEB, 18691

Orbit data source: Space-Track

OPS 4682 DEB, 18691 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/18691?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

18691, 1965-027AJ

Orbit

LEO

Last TLE update

5 hours 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 5 hours ago

0 OPS 4682 DEB
1 18691U 65027AJ  25182.21049786 -.00000056  00000-0 -21877-3 0  9991
2 18691  90.2271 349.4624 0023658 312.4710 224.3655 12.96604290779674

Epoch: 2025-07-01T05:03Z

TLE epoch observation values (Epoch: 2025-07-01T05:03:07.015Z)

Latitude

3.25962°

Longitude

174.18682°

Altitude

1,290.903 km

Speed

7.205 km/s

True Right ascension

11h 17m 54s

True Declination

3° 14' 29"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-12.46236°

Longitude

-5.77213°

Altitude

1,266.049 km

Speed

7.229 km/s

Apparent Right ascension

01h 47m 47s

Apparent Declination

-54° 27' 06"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:16:22

Azimuth

144.846° SSE

Elevation

-20.731°

Doppler factor

Orbital elements

Apogee altitude

1,290.652 km

Perigee altitude

1,254.452 km

Semi-major axis

7,650.689 km

Eccentricity

0.00237

Inclination

90.2271°

RAAN

349.4624°

Arg. of periapsis

312.471°

True anomaly

Unknown

Mean anomaly

224.3655°

Eccentric anomaly

Unknown

Mean motion

3.24334 °/min

Orbital period

111 mins

BSTAR

-0.00021877

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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 09:51:03.479Z	106.003° ESE	2025-07-01 09:55:03.479Z	72.757° E	17.183°	2025-07-01 10:00:03.479Z	30.73° NE
13 mins	2025-07-01 11:39:03.479Z	180.109° SSW	2025-07-01 11:45:03.479Z	243.452° WSW	44.683°	2025-07-01 11:52:03.479Z	355.448° N
5 mins	2025-07-01 13:35:03.479Z	268.778° W	2025-07-01 13:37:03.479Z	285.35° WNW	13.062°	2025-07-01 13:40:03.479Z	309.758° NW
13 mins	2025-07-01 23:17:03.479Z	8.413° NNE	2025-07-01 23:23:03.479Z	92.164° ESE	43.755°	2025-07-01 23:30:03.479Z	175.35° S
9 mins	2025-07-02 01:09:03.479Z	325.297° NNW	2025-07-02 01:13:03.479Z	288.795° WNW	19.79°	2025-07-02 01:18:03.479Z	246.35° WSW

Authenticating...

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Check out OPS 4682 DEB, 18691 on other resources

View OPS 4682 DEB, 18691 on Heavens-Above

View OPS 4682 DEB, 18691 on Keep Track

View OPS 4682 DEB, 18691 on Celestrak

View OPS 4682 DEB, 18691 on Gunter's Space Page

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