OPS 0856 DEB, 24676

Orbit data source: Space-Track

OPS 0856 DEB, 24676 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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https://www.satcat.com/sats-embedded/24676?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

24676, 1966-077Q

Orbit

LEO

Country

Related business

United States Space Force (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-08-19 (60 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago

0 OPS 0856 DEB
1 24676U 66077Q   26300.69022100 -.00017090  00000-0 -60688+0 0  9998
2 24676  88.4639  38.2295 1989635 111.5802 270.8130  9.02472093567435

Epoch: 2026-10-27T16:33Z

TLE epoch observation values (Epoch: 2026-10-27T16:33:55.094Z)

Latitude

-0.00002°

Longitude

113.7002°

Altitude

3,719.324 km

Speed

6.17 km/s

True Right ascension

02h 32m 55s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

18:04:11

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

5,302.83 km

Perigee altitude

1,426.004 km

Semi-major axis

9,742.554 km

Eccentricity

0.19896

Inclination

88.4639°

RAAN

38.2295°

Arg. of periapsis

111.5802°

True anomaly

248.51129°

Mean anomaly

270.813°

Eccentric anomaly

259.60049°

Mean motion

2.25701 °/min

Orbital period

159.5 mins

BSTAR

-0.60688

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

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OPS 0856 DEB Visibility forecast

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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	2026-10-31 05:43:40.516Z	151.883° SSE	2026-10-31 05:58:40.516Z	85.194° E	50.699°	2026-10-31 06:07:40.516Z	12.733° NNE
21 mins	2026-10-31 08:25:40.516Z	218.855° SW	2026-10-31 08:37:40.516Z	272.729° WNW	32.98°	2026-10-31 08:46:40.516Z	337.903° N
13 mins	2026-10-31 17:02:40.516Z	33.797° NE	2026-10-31 17:07:40.516Z	78.622° E	24.999°	2026-10-31 17:15:40.516Z	132.292° SE
15 mins	2026-10-31 19:41:40.516Z	339.566° N	2026-10-31 19:47:40.516Z	274.304° WNW	42.451°	2026-10-31 19:56:40.516Z	212.343° SW

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out OPS 0856 DEB, 24676 on other resources

View OPS 0856 DEB, 24676 on Heavens-Above

View OPS 0856 DEB, 24676 on Keep Track

View OPS 0856 DEB, 24676 on Celestrak

View OPS 0856 DEB, 24676 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

OPS 0856 DEB, 24676

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-10-27T16:33:55.094Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

OPS 0856 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out OPS 0856 DEB, 24676 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago