OPS 4682 DEB, 18783

Orbit data source: Space-Track

OPS 4682 DEB, 18783 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/18783?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

18783, 1965-027AK

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 18783U 65027AK  25127.15011139  .00000063  00000-0  18233-3 0  9994
2 18783  90.2569  16.5321 0025577 198.7034 316.7588 13.00586167527690

Epoch: 2025-05-07T03:36Z

Definitive object data (Epoch: 2025-05-07T03:36:09.624Z)

Latitude

24.76294°

Longitude

-82.62919°

Altitude

1,248.575 km

Speed

7.24 km/s

True Right ascension

13h 06m 36s

True Declination

24° 38' 27"

Sunlit

Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude

53.79654°

Longitude

96.95432°

Altitude

1,283.475 km

Speed

7.212 km/s

Apparent Right ascension

02h 02m 29s

Apparent Declination

12° 50' 39"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

14:55:41

Azimuth

16.054° NNE

Elevation

-35.81°

Doppler factor

Orbital elements

Apogee altitude

1,276.445 km

Perigee altitude

1,237.389 km

Semi-major axis

7,635.054 km

Eccentricity

0.0025577

Inclination

90.2569°

RAAN

16.5321°

Arg. of periapsis

198.7034°

True anomaly

316.55754°

Mean anomaly

316.7588°

Eccentric anomaly

316.65822°

Mean motion

3.25331 °/min

BSTAR

0.00018233

Orbital period

110.66 mins

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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	2025-05-09 15:50:48.095Z	138.199° SSE	2025-05-09 15:56:48.095Z	79.461° E	31.33°	2025-05-09 16:02:48.095Z	16.964° NNE
12 mins	2025-05-09 17:41:48.095Z	212.771° SW	2025-05-09 17:46:48.095Z	266.226° W	33.077°	2025-05-09 17:53:48.095Z	341.505° N
9 mins	2025-05-10 03:27:48.095Z	40.048° NE	2025-05-10 03:31:48.095Z	80.998° E	22.674°	2025-05-10 03:36:48.095Z	127.981° SE
13 mins	2025-05-10 05:16:48.095Z	351.985° N	2025-05-10 05:22:48.095Z	271.377° WNW	40.728°	2025-05-10 05:29:48.095Z	201.217° SSW

Authenticating...

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Check out OPS 4682 DEB, 18783 on other resources

View OPS 4682 DEB, 18783 on Heavens-Above

View OPS 4682 DEB, 18783 on Keep Track

View OPS 4682 DEB, 18783 on Celestrak

View OPS 4682 DEB, 18783 on Gunter's Space Page

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