CZ-4 DEB, 27492

Orbit data source: Space-Track

CZ-4 DEB, 27492 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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https://www.satcat.com/sats-embedded/27492?theme=dark&initialShowStats=false

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Identifier

27492, 1999-057MM

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 (27 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 day ago

TLE from 1 day ago

0 CZ-4 DEB
1 27492U 99057MM  26225.60450823  .00001487  00000-0  29523-3 0  9993
2 27492  98.3863 284.2083 0075667 201.4527 158.3498 14.61967741331812

Epoch: 2026-08-13T14:30Z

TLE epoch observation values (Epoch: 2026-08-13T14:30:29.511Z)

Latitude

0.00004°

Longitude

104.54363°

Altitude

739.562 km

Speed

7.459 km/s

True Right ascension

18h 56m 49s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

13:48:33

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

737.351 km

Perigee altitude

630.478 km

Semi-major axis

7,062.051 km

Eccentricity

0.00757

Inclination

98.3863°

RAAN

284.2083°

Arg. of periapsis

201.4527°

True anomaly

158.66691°

Mean anomaly

158.3498°

Eccentric anomaly

158.50863°

Mean motion

3.65718 °/min

Orbital period

98.44 mins

BSTAR

0.00029523

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

CZ-4B DEB, 44589

CZ-4 DEB, 35323 (Decayed)

CZ-4 DEB, 36304 (Decayed)

CZ-4 DEB, 26149 (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.
6 mins	2026-08-15 02:48:28.869Z	102.398° ESE	2026-08-15 02:51:28.869Z	59.652° ENE	18.315°	2026-08-15 02:54:28.869Z	20.985° NNE
8 mins	2026-08-15 04:24:28.869Z	190.351° SSW	2026-08-15 04:28:28.869Z	271.902° WNW	36.321°	2026-08-15 04:32:28.869Z	333.244° NNW
6 mins	2026-08-15 16:23:28.869Z	41.667° NE	2026-08-15 16:25:28.869Z	83.03° E	32.053°	2026-08-15 16:29:28.869Z	165.234° S
4 mins	2026-08-15 18:01:28.869Z	320.651° NNW	2026-08-15 18:03:28.869Z	286.912° WNW	17.8°	2026-08-15 18:05:28.869Z	257.312° W

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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, 27492 on other resources

View CZ-4 DEB, 27492 on Heavens-Above

View CZ-4 DEB, 27492 on Keep Track

View CZ-4 DEB, 27492 on Celestrak

View CZ-4 DEB, 27492 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, 27492

Orbit data source: Space-Track

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

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-08-13T14:30:29.511Z)

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, 27492 on other resources

Documentation

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