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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Iframe URL

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 (59 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

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 weeks ago

TLE from 2 weeks ago

0 OPS 0856 DEB
1 24676U 66077Q   26014.09731393 -.00006629  00000-0 -12555+0 0  9991
2 24676  87.9142  60.5497 2209527 102.4032 283.1271  9.04968358541532

Epoch: 2026-01-14T02:20Z

TLE epoch observation values (Epoch: 2026-01-14T02:20:07.923Z)

Latitude

-0.00006°

Longitude

-88.05351°

Altitude

3,333.816 km

Speed

6.413 km/s

True Right ascension

04h 02m 11s

True Declination

0° 00' 00"

Sunlit

Object was in daylight 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

22:52:32

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

5,495.128 km

Perigee altitude

1,197.779 km

Semi-major axis

9,724.591 km

Eccentricity

0.22095

Inclination

87.9142°

RAAN

60.5497°

Arg. of periapsis

102.4032°

True anomaly

257.69172°

Mean anomaly

283.1271°

Eccentric anomaly

270.46786°

Mean motion

2.26327 °/min

Orbital period

159.06 mins

BSTAR

-0.12555

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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, 25828

OPS 0856 DEB, 25826

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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.
14 mins	2026-01-25 01:06:08.056Z	132.272° SE	2026-01-25 01:14:08.056Z	85.145° E	24.908°	2026-01-25 01:20:08.056Z	30.246° NE
16 mins	2026-01-25 03:44:08.056Z	210.28° SW	2026-01-25 03:53:08.056Z	268.726° W	32.885°	2026-01-25 04:00:08.056Z	341.381° N
8 mins	2026-01-25 12:17:08.056Z	57.344° ENE	2026-01-25 12:20:08.056Z	80.131° E	15.324°	2026-01-25 12:25:08.056Z	109.562° ESE
18 mins	2026-01-25 14:53:08.056Z	349.658° N	2026-01-25 14:59:08.056Z	274.479° WNW	42.558°	2026-01-25 15:11:08.056Z	194.726° SSW

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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: 2 weeks ago

TLE from 2 weeks ago

TLE epoch observation values (Epoch: 2026-01-14T02:20:07.923Z)

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: 2 weeks ago