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

19 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 19 hours ago

0 OPS 4682 DEB
1 18691U 65027AJ  25169.44618541 -.00000083  00000-0 -31418-3 0  9994
2 18691  90.2257 349.1992 0024788 348.2689  41.3318 12.96600250777954

Epoch: 2025-06-18T10:42Z

TLE epoch observation values (Epoch: 2025-06-18T10:42:30.419Z)

Latitude

29.83407°

Longitude

-78.48444°

Altitude

1,264.94 km

Speed

7.232 km/s

True Right ascension

23h 16m 16s

True Declination

29° 41' 45"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

27.66085°

Longitude

101.77858°

Altitude

1,297.252 km

Speed

7.201 km/s

Apparent Right ascension

08h 42m 40s

Apparent Declination

-3° 52' 44"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

16:41:59

Azimuth

287.117° WNW

Elevation

-25.09°

Doppler factor

Orbital elements

Apogee altitude

1,291.533 km

Perigee altitude

1,253.604 km

Semi-major axis

7,650.705 km

Eccentricity

0.00248

Inclination

90.2257°

RAAN

349.1992°

Arg. of periapsis

348.2689°

True anomaly

Unknown

Mean anomaly

41.3318°

Eccentric anomaly

Unknown

Mean motion

3.24333 °/min

Orbital period

111 mins

BSTAR

-0.00031418

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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	2025-06-19 10:46:36.380Z	112.406° ESE	2025-06-19 10:51:36.380Z	67.592° E	19.804°	2025-06-19 10:55:36.380Z	31.869° NE
13 mins	2025-06-19 12:35:36.380Z	187.672° SSW	2025-06-19 12:41:36.380Z	286.716° WNW	43.276°	2025-06-19 12:48:36.380Z	353.106° N
6 mins	2025-06-19 22:24:36.380Z	53.102° ENE	2025-06-19 22:27:36.380Z	78.045° E	13.64°	2025-06-19 22:30:36.380Z	101.876° ESE
14 mins	2025-06-20 00:12:36.380Z	4.33° NNE	2025-06-20 00:18:36.380Z	38.56° NE	44.552°	2025-06-20 00:26:36.380Z	181.67° SSW
7 mins	2025-06-20 02:05:36.380Z	319.335° NNW	2025-06-20 02:08:36.380Z	293.058° NW	17.046°	2025-06-20 02:12:36.380Z	258.63° W

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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