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

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ISO8601 Format

Identifier

23820, 1966-077D

Orbit

LEO

Last TLE update

4 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 4 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

Definitive object data (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 TLE epoch

Visualization TLE readout

Latitude

14.62923°

Longitude

79.87975°

Altitude

1,649.485 km

Speed

7.67 km/s

Apparent Right ascension

10h 49m 03s

Apparent Declination

-9° 55' 14"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

00:41:15

Azimuth

47.414° ENE

Elevation

-51.018°

Doppler factor

Orbital elements

Apogee altitude

5,251.148 km

Perigee altitude

1,644.044 km

Semi-major axis

9,825.733 km

Eccentricity

0.1835539

Inclination

88.4548°

RAAN

332.4245°

Arg. of periapsis

297.3742°

True anomaly

62.72218°

Mean anomaly

45.2216°

Eccentric anomaly

53.69713°

Mean motion

2.22841 °/min

BSTAR

-0.3579

Orbital period

161.55 mins

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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.
18 mins	2025-05-10 00:17:45.810Z	7.203° NNE	2025-05-10 00:28:45.810Z	87.724° E	36.228°	2025-05-10 00:35:45.810Z	150.153° SSE
13 mins	2025-05-10 03:01:45.810Z	339.324° N	2025-05-10 03:08:45.810Z	294.678° NW	23.294°	2025-05-10 03:14:45.810Z	247.1° WSW
26 mins	2025-05-10 10:24:45.810Z	101.734° ESE	2025-05-10 10:38:45.810Z	64.687° ENE	22.124°	2025-05-10 10:50:45.810Z	21.795° NNE
45 mins	2025-05-10 12:50:45.810Z	167.257° S	2025-05-10 13:17:45.810Z	80.188° E	44.772°	2025-05-10 13:35:45.810Z	1.749° NNE
36 mins	2025-05-10 15:39:45.810Z	230.24° WSW	2025-05-10 15:59:45.810Z	283.286° WNW	27.458°	2025-05-10 16:15:45.810Z	343.724° N

Authenticating...

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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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