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

9 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 9 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

Definitive object data (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 TLE epoch

Visualization TLE readout

Latitude

79.01013°

Longitude

87.47238°

Altitude

2,982.911 km

Speed

6.716 km/s

Apparent Right ascension

12h 10m 27s

Apparent Declination

57° 20' 04"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

00:52:33

Azimuth

5.709° NNE

Elevation

7.653°

Doppler factor

Orbital elements

Apogee altitude

4,825.846 km

Perigee altitude

2,242.266 km

Semi-major axis

9,912.193 km

Eccentricity

0.1303233

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

BSTAR

0.05422

Orbital period

163.69 mins

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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.
39 mins	2025-05-09 16:43:02.522Z	7.395° NNE	2025-05-09 17:00:02.522Z	89.857° E	39.859°	2025-05-09 17:22:02.522Z	162.539° S
34 mins	2025-05-09 19:28:02.522Z	349.74° N	2025-05-09 19:42:02.522Z	285.445° WNW	35.998°	2025-05-09 20:02:02.522Z	222.543° SW
6 mins	2025-05-10 03:16:02.522Z	67.127° ENE	2025-05-10 03:19:02.522Z	51.008° ENE	12.22°	2025-05-10 03:22:02.522Z	35.711° NE
22 mins	2025-05-10 05:48:02.522Z	169.731° S	2025-05-10 05:58:02.522Z	98.557° ESE	44.668°	2025-05-10 06:10:02.522Z	0.617° NNE
12 mins	2025-05-10 08:39:02.522Z	266.547° W	2025-05-10 08:44:02.522Z	295.063° NW	15.866°	2025-05-10 08:51:02.522Z	331.938° NNW
20 mins	2025-05-10 14:38:02.522Z	32.038° NE	2025-05-10 14:47:02.522Z	64.853° ENE	15.916°	2025-05-10 14:58:02.522Z	98.446° ESE

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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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