CZ-4 DEB, 27806

Orbit data source: Space-Track

CZ-4 DEB, 27806 is space debris in SSO originally from a launch on Thu, 14 Oct 1999 UTC launched from the Taiyaun Space Center, China (TSC). 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/27806?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

27806, 1999-057MW

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1999-10-14 (26 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

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: 1 week ago

TLE from 1 week ago

0 CZ-4 DEB
1 27806U 99057MW  26077.33459907  .00000142  00000-0  66466-4 0  9994
2 27806  98.9019 107.0153 0108651 358.9374   1.1562 14.32055988269410

Epoch: 2026-03-18T08:01Z

TLE epoch observation values (Epoch: 2026-03-18T08:01:49.359Z)

Latitude

0.00001°

Longitude

170.65978°

Altitude

709.966 km

Speed

7.541 km/s

True Right ascension

07h 08m 03s

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

19:30:21

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

859.814 km

Perigee altitude

704.222 km

Semi-major axis

7,160.155 km

Eccentricity

0.01087

Inclination

98.9019°

RAAN

107.0153°

Arg. of periapsis

358.9374°

True anomaly

1.18167°

Mean anomaly

1.1562°

Eccentric anomaly

1.1689°

Mean motion

3.58228 °/min

Orbital period

100.49 mins

BSTAR

0.000066466

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Other satellites on launch #57 in the year 1999 (1999-10-14 UTC)

CZ-4 DEB, 26458 (Decayed)

CZ-4 DEB, 26343 (Decayed)

CZ-4 DEB, 26651 (Decayed)

CZ-4 DEB, 35328 (Decayed)

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CZ-4 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.
10 mins	2026-03-25 14:59:36.264Z	9.971° NNE	2026-03-25 15:04:36.264Z	240.216° WSW	43.616°	2026-03-25 15:09:36.264Z	200.988° SSW
5 mins	2026-03-26 00:39:36.264Z	90.123° ESE	2026-03-26 00:41:36.264Z	61.237° ENE	17.466°	2026-03-26 00:44:36.264Z	22.815° NE
7 mins	2026-03-26 02:17:36.264Z	192.702° SSW	2026-03-26 02:20:36.264Z	267.933° W	38.065°	2026-03-26 02:24:36.264Z	333.565° NNW

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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 CZ-4 DEB, 27806 on other resources

View CZ-4 DEB, 27806 on Heavens-Above

View CZ-4 DEB, 27806 on Keep Track

View CZ-4 DEB, 27806 on Celestrak

View CZ-4 DEB, 27806 on Gunter's Space Page

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

CZ-4 DEB, 27806

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 week ago

TLE from 1 week ago

TLE epoch observation values (Epoch: 2026-03-18T08:01:49.359Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #57 in the year 1999 (1999-10-14 UTC)

CZ-4 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4 DEB, 27806 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 week ago