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

5 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 5 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

43.71953°

Longitude

-101.57035°

Altitude

2,385.762 km

Speed

7.111 km/s

Apparent Right ascension

22h 14m 04s

Apparent Declination

53° 09' 19"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:22:22

Azimuth

29.327° NE

Elevation

74.105°

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.
9 mins	2025-07-01 09:44:02.516Z	29.772° NE	2025-07-01 09:44:02.516Z	29.772° NE	43.909°	2025-07-01 09:53:02.516Z	2.378° NNE
15 mins	2025-07-01 12:17:02.516Z	248.589° W	2025-07-01 12:25:02.516Z	284.29° WNW	17.379°	2025-07-01 12:32:02.516Z	324.801° NNW
18 mins	2025-07-01 20:56:02.516Z	12.818° NNE	2025-07-01 21:03:02.516Z	92.667° ESE	40.407°	2025-07-01 21:14:02.516Z	164.959° S
12 mins	2025-07-01 23:39:02.516Z	323.493° NNW	2025-07-01 23:44:02.516Z	285.806° WNW	19.191°	2025-07-01 23:51:02.516Z	244.38° WSW
12 mins	2025-07-02 07:14:02.516Z	98.994° ESE	2025-07-02 07:20:02.516Z	70.238° E	16.751°	2025-07-02 07:26:02.516Z	35.364° NE

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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