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 src="https://www.satcat.com/sats-embedded/18691?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

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

3 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 3 days ago

0 OPS 4682 DEB
1 18691U 65027AJ  25126.40599718  .00000641  00000-0  22072-2 0  9990
2 18691  90.2301 348.3115 0026974  94.8323  28.0586 12.96583186772378

Epoch: 2025-05-06T09:44Z

Definitive object data (Epoch: 2025-05-06T09:44:38.156Z)

Latitude

57.05299°

Longitude

158.00012°

Altitude

1,266.916 km

Speed

7.236 km/s

True Right ascension

11h 14m 39s

True Declination

56° 54' 23"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

27.94588°

Longitude

157.82872°

Altitude

1,270.079 km

Speed

7.227 km/s

Apparent Right ascension

08h 09m 35s

Apparent Declination

-5° 31' 55"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

14:33:58

Azimuth

269.645° W

Elevation

-8.217°

Doppler factor

Orbital elements

Apogee altitude

1,293.273 km

Perigee altitude

1,251.998 km

Semi-major axis

7,650.772 km

Eccentricity

0.0026974

Inclination

90.2301°

RAAN

348.3115°

Arg. of periapsis

94.8323°

True anomaly

28.20443°

Mean anomaly

28.0586°

Eccentric anomaly

28.13147°

Mean motion

3.24329 °/min

BSTAR

0.0022072

Orbital period

111 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.
7 mins	2025-05-09 13:13:08.203Z	98.012° ESE	2025-05-09 13:16:08.203Z	72.201° E	16.155°	2025-05-09 13:20:08.203Z	37.436° NE
13 mins	2025-05-09 15:00:08.203Z	178.07° S	2025-05-09 15:06:08.203Z	235.895° WSW	44.886°	2025-05-09 15:13:08.203Z	356.435° N
5 mins	2025-05-09 16:56:08.203Z	268.647° W	2025-05-09 16:58:08.203Z	285.718° WNW	13.622°	2025-05-09 17:01:08.203Z	310.626° NW
14 mins	2025-05-10 02:37:08.203Z	8.256° NNE	2025-05-10 02:44:08.203Z	106.269° ESE	42.978°	2025-05-10 02:51:08.203Z	173.777° S
9 mins	2025-05-10 04:30:08.203Z	324.281° NNW	2025-05-10 04:34:08.203Z	285.869° WNW	20.247°	2025-05-10 04:39:08.203Z	243.416° 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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