OPS 0856 DEB, 27724

Orbit data source: Space-Track

OPS 0856 DEB, 27724 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/27724?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

27724, 1966-077AC

Orbit

LEO

Last TLE update

11 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 11 months ago

0 OPS 0856 DEB
1 27724U 66077AC  24232.93446642  .00000319  00000-0  54220-1 0  9996
2 27724  89.4978 220.2823 1303233 319.0474  53.8356  8.79425084 92515

Epoch: 2024-08-19T22:25Z

TLE epoch observation values (Epoch: 2024-08-19T22:25:37.898Z)

Latitude

26.12028°

Longitude

-84.63863°

Altitude

2,899.242 km

Speed

6.765 km/s

True Right ascension

14h 42m 06s

True Declination

26° 00' 57"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-29.24379°

Longitude

88.9784°

Altitude

3,694.569 km

Speed

6.244 km/s

Apparent Right ascension

00h 06m 26s

Apparent Declination

-55° 38' 16"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

05:05:56

Azimuth

216.827° SW

Elevation

-24.629°

Doppler factor

Orbital elements

Apogee altitude

4,825.846 km

Perigee altitude

2,242.266 km

Semi-major axis

9,912.193 km

Eccentricity

0.13032

Inclination

89.4978°

RAAN

220.2823°

Arg. of periapsis

319.0474°

True anomaly

67.0489°

Mean anomaly

53.8356°

Eccentric anomaly

60.32314°

Mean motion

2.19932 °/min

Orbital period

163.69 mins

BSTAR

0.05422

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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.
27 mins	2025-07-18 22:53:30.498Z	104.72° ESE	2025-07-18 23:05:30.498Z	53.349° ENE	25.209°	2025-07-18 23:20:30.498Z	6.98° NNE
33 mins	2025-07-19 01:31:30.498Z	181.789° SSW	2025-07-19 01:44:30.498Z	286.696° WNW	44.659°	2025-07-19 02:04:30.498Z	358.846° N
22 mins	2025-07-19 04:24:30.498Z	271.514° WNW	2025-07-19 04:33:30.498Z	307.286° NW	18.296°	2025-07-19 04:46:30.498Z	347.845° N
41 mins	2025-07-19 10:25:30.498Z	9.773° NNE	2025-07-19 10:46:30.498Z	69.428° E	27.724°	2025-07-19 11:06:30.498Z	125.643° SE
48 mins	2025-07-19 13:08:30.498Z	0.206° NNE	2025-07-19 13:32:30.498Z	271.719° WNW	44.934°	2025-07-19 13:56:30.498Z	191.326° SSW
26 mins	2025-07-19 15:53:30.498Z	349.788° N	2025-07-19 16:09:30.498Z	306.13° NW	26.131°	2025-07-19 16:19:30.498Z	275.241° WNW

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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Check out OPS 0856 DEB, 27724 on other resources

View OPS 0856 DEB, 27724 on Heavens-Above

View OPS 0856 DEB, 27724 on Keep Track

View OPS 0856 DEB, 27724 on Celestrak

View OPS 0856 DEB, 27724 on Gunter's Space Page

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