OPS 4682 DEB, 18675

Orbit data source: Space-Track

OPS 4682 DEB, 18675 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/18675?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

18675, 1965-027AH

Orbit

LEO

Last TLE update

11 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 11 hours ago

0 OPS 4682 DEB
1 18675U 65027AH  25222.30939248 -.00000647  00000-0 -21833-2 0  9996
2 18675  90.2468 347.5191 0025517  19.0853   9.2591 12.99675571818212

Epoch: 2025-08-10T07:25Z

TLE epoch observation values (Epoch: 2025-08-10T07:25:31.51Z)

Latitude

28.43143°

Longitude

-83.02773°

Altitude

1,247.622 km

Speed

7.243 km/s

True Right ascension

23h 09m 32s

True Declination

28° 17' 49"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

62.29763°

Longitude

-83.35178°

Altitude

1,260.149 km

Speed

7.238 km/s

Apparent Right ascension

21h 52m 51s

Apparent Declination

18° 10' 27"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

08:58:33

Azimuth

344.994° N

Elevation

-30.546°

Doppler factor

Orbital elements

Apogee altitude

1,279.977 km

Perigee altitude

1,240.994 km

Semi-major axis

7,638.622 km

Eccentricity

0.00255

Inclination

90.2468°

RAAN

347.5191°

Arg. of periapsis

19.0853°

True anomaly

9.3063°

Mean anomaly

9.2591°

Eccentric anomaly

9.28268°

Mean motion

3.25103 °/min

Orbital period

110.73 mins

BSTAR

-0.0021833

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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.
8 mins	2025-08-10 19:00:02.984Z	39.754° NE	2025-08-10 19:04:02.984Z	72.328° E	15.568°	2025-08-10 19:08:02.984Z	106.488° ESE
13 mins	2025-08-10 20:50:02.984Z	1.538° NNE	2025-08-10 20:56:02.984Z	225.737° WSW	44.898°	2025-08-10 21:03:02.984Z	186.373° SSW
6 mins	2025-08-10 22:43:02.984Z	311.453° NW	2025-08-10 22:45:02.984Z	294.149° NW	14.744°	2025-08-10 22:49:02.984Z	261.418° W
9 mins	2025-08-11 07:27:02.984Z	115.037° SE	2025-08-11 07:31:02.984Z	73.301° E	24.132°	2025-08-11 07:36:02.984Z	25.273° NE
13 mins	2025-08-11 09:15:02.984Z	197.115° SSW	2025-08-11 09:21:02.984Z	271.364° WNW	39.724°	2025-08-11 09:28:02.984Z	348.518° N

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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Authenticating...

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Check out OPS 4682 DEB, 18675 on other resources

View OPS 4682 DEB, 18675 on Heavens-Above

View OPS 4682 DEB, 18675 on Keep Track

View OPS 4682 DEB, 18675 on Celestrak

View OPS 4682 DEB, 18675 on Gunter's Space Page

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