OPS 4682 DEB, 18479

Orbit data source: Space-Track

OPS 4682 DEB, 18479 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/18479?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

18479, 1965-027AC

Orbit

LEO

Last TLE update

2 days 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 2 days ago

0 OPS 4682 DEB
1 18479U 65027AC  25220.85983694  .00000337  00000-0  11334-2 0  9999
2 18479  90.2386 359.0038 0030655 162.8577 358.1403 12.97432442907257

Epoch: 2025-08-08T20:38Z

TLE epoch observation values (Epoch: 2025-08-08T20:38:09.911Z)

Latitude

19.00928°

Longitude

-88.05955°

Altitude

1,251.127 km

Speed

7.242 km/s

True Right ascension

11h 56m 20s

True Declination

18° 54' 38"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

30.04301°

Longitude

91.76471°

Altitude

1,290.209 km

Speed

7.207 km/s

Apparent Right ascension

23h 16m 22s

Apparent Declination

-1° 16' 05"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

10:22:54

Azimuth

339.159° N

Elevation

-49.484°

Doppler factor

Orbital elements

Apogee altitude

1,292.737 km

Perigee altitude

1,245.851 km

Semi-major axis

7,647.431 km

Eccentricity

0.00307

Inclination

90.2386°

RAAN

359.0038°

Arg. of periapsis

162.8577°

True anomaly

358.12886°

Mean anomaly

358.1403°

Eccentric anomaly

358.13458°

Mean motion

3.24541 °/min

Orbital period

110.93 mins

BSTAR

0.0011334

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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.
12 mins	2025-08-10 20:33:10.030Z	23.209° NE	2025-08-10 20:39:10.030Z	86.72° E	30.296°	2025-08-10 20:45:10.030Z	146.114° SSE
12 mins	2025-08-10 22:24:10.030Z	343.795° N	2025-08-10 22:30:10.030Z	273.28° WNW	33.326°	2025-08-10 22:36:10.030Z	216.327° SW
13 mins	2025-08-11 09:00:10.030Z	153.925° SSE	2025-08-11 09:06:10.030Z	69.203° E	40.258°	2025-08-11 09:13:10.030Z	5.47° NNE
10 mins	2025-08-11 10:52:10.030Z	233.638° WSW	2025-08-11 10:57:10.030Z	282.854° WNW	23.638°	2025-08-11 11:02:10.030Z	329.032° NNW

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, 18479 on other resources

View OPS 4682 DEB, 18479 on Heavens-Above

View OPS 4682 DEB, 18479 on Keep Track

View OPS 4682 DEB, 18479 on Celestrak

View OPS 4682 DEB, 18479 on Gunter's Space Page

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