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

16.42993°

Longitude

88.68929°

Altitude

4,700.431 km

Speed

5.637 km/s

Apparent Right ascension

03h 39m 03s

Apparent Declination

-7° 54' 46"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

00:16:06

Azimuth

123.514° SE

Elevation

23.109°

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

Unknown

Mean anomaly

53.8356°

Eccentric anomaly

Unknown

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.
7 mins	2025-07-11 11:57:59.340Z	123.594° SE	2025-07-11 11:57:59.340Z	123.594° SE	21.387°	2025-07-11 12:04:59.340Z	137.274° SSE
47 mins	2025-07-11 14:04:59.340Z	358.758° N	2025-07-11 14:27:59.340Z	274.471° WNW	44.112°	2025-07-11 14:51:59.340Z	199.987° SSW
31 mins	2025-07-11 16:49:59.340Z	347.399° N	2025-07-11 17:03:59.340Z	309.167° NW	22.179°	2025-07-11 17:20:59.340Z	265.966° W
29 mins	2025-07-12 00:20:59.340Z	133.761° SE	2025-07-12 00:32:59.340Z	67.771° E	36.015°	2025-07-12 00:49:59.340Z	4.796° NNE
30 mins	2025-07-12 03:03:59.340Z	213.583° SW	2025-07-12 03:15:59.340Z	286.087° WNW	37.109°	2025-07-12 03:33:59.340Z	355.011° N
5 mins	2025-07-12 09:20:59.340Z	35.913° NE	2025-07-12 09:22:59.340Z	40.837° NE	10.309°	2025-07-12 09:25:59.340Z	48.133° ENE

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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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