OPS 0856 DEB, 23820

Orbit data source: Space-Track

OPS 0856 DEB, 23820 is space debris in LEO originally from a launch on Fri, 19 Aug 1966 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/23820?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

23820, 1966-077D

Orbit

LEO

Last TLE update

6 months ago

Origin

United States Space Force (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-08-19 (59 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 6 months ago

0 OPS 0856 DEB
1 23820U 66077D   25018.85178970 -.00005976  00000-0 -35790+0 0  9994
2 23820  88.4548 332.4245 1835539 297.3742  45.2216  8.91045185 44048

Epoch: 2025-01-18T20:26Z

TLE epoch observation values (Epoch: 2025-01-18T20:26:34.63Z)

Latitude

-0.00004°

Longitude

-92.71493°

Altitude

2,384.203 km

Speed

7.103 km/s

True Right ascension

22h 09m 41s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-81.1936°

Longitude

-113.47255°

Altitude

5,310.632 km

Speed

5.272 km/s

Apparent Right ascension

07h 51m 15s

Apparent Declination

-78° 37' 20"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

20:11:21

Azimuth

178.418° S

Elevation

-51.241°

Doppler factor

Orbital elements

Apogee altitude

5,251.148 km

Perigee altitude

1,644.044 km

Semi-major axis

9,825.733 km

Eccentricity

0.18355

Inclination

88.4548°

RAAN

332.4245°

Arg. of periapsis

297.3742°

True anomaly

Unknown

Mean anomaly

45.2216°

Eccentric anomaly

Unknown

Mean motion

2.22841 °/min

Orbital period

161.55 mins

BSTAR

-0.3579

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Other satellites on launch #77 in the year 1966 (1966-08-19 UTC)

SECOR 7 (EGRS 7), 2411

OPS 0856 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.
24 mins	2025-07-08 08:52:42.250Z	168.498° S	2025-07-08 09:07:42.250Z	83.834° E	44.23°	2025-07-08 09:16:42.250Z	3.962° NNE
14 mins	2025-07-08 11:42:42.250Z	248.485° W	2025-07-08 11:49:42.250Z	282.275° WNW	17.261°	2025-07-08 11:56:42.250Z	325.363° NNW
20 mins	2025-07-08 20:19:42.250Z	11.756° NNE	2025-07-08 20:27:42.250Z	90.623° ESE	39.572°	2025-07-08 20:39:42.250Z	163.21° S
13 mins	2025-07-08 23:03:42.250Z	323.947° NNW	2025-07-08 23:08:42.250Z	285.828° WNW	21.833°	2025-07-08 23:16:42.250Z	240.12° WSW
9 mins	2025-07-09 06:40:42.250Z	92.093° ESE	2025-07-09 06:44:42.250Z	71.813° E	13.972°	2025-07-09 06:49:42.250Z	42.059° NE

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Check out OPS 0856 DEB, 23820 on other resources

View OPS 0856 DEB, 23820 on Heavens-Above

View OPS 0856 DEB, 23820 on Keep Track

View OPS 0856 DEB, 23820 on Celestrak

View OPS 0856 DEB, 23820 on Gunter's Space Page

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