CZ-4 DEB, 27536

Orbit data source: Space-Track

CZ-4 DEB, 27536 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/27536?theme=dark&initialShowStats=false

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Identifier

27536, 1999-057MP

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: 12 hours ago

TLE from 12 hours ago

0 CZ-4 DEB
1 27536U 99057MP  26139.60260889  .00002106  00000-0  37063-3 0  9994
2 27536  98.4619 176.1135 0026917 169.4430 342.3187 14.68485442280530

Epoch: 2026-05-19T14:27Z

TLE epoch observation values (Epoch: 2026-05-19T14:27:45.408Z)

Latitude

28.04109°

Longitude

-93.57962°

Altitude

651.346 km

Speed

7.544 km/s

True Right ascension

00h 02m 32s

True Declination

27° 53' 47"

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

11:21:19

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

681.942 km

Perigee altitude

644.037 km

Semi-major axis

7,041.126 km

Eccentricity

0.00269

Inclination

98.4619°

RAAN

176.1135°

Arg. of periapsis

169.443°

True anomaly

342.22472°

Mean anomaly

342.3187°

Eccentric anomaly

342.27174°

Mean motion

3.6735 °/min

Orbital period

98 mins

BSTAR

0.00037063

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

CZ-4 DEB, 26338

CZ-4 DEB, 26442

CZ-4 DEB, 26446

CZ-4 DEB, 26229 (Decayed)

CZ-4 DEB, 26324 (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.
7 mins	2026-05-20 02:58:43.601Z	198.676° SSW	2026-05-20 03:01:43.601Z	250.375° W	31.279°	2026-05-20 03:05:43.601Z	326.458° NNW
7 mins	2026-05-20 14:53:43.601Z	35.756° NE	2026-05-20 14:56:43.601Z	107.024° ESE	34.448°	2026-05-20 15:00:43.601Z	171.741° S
4 mins	2026-05-20 16:31:43.601Z	318.517° NNW	2026-05-20 16:32:43.601Z	302.72° NW	16.497°	2026-05-20 16:35:43.601Z	257.761° W
7 mins	2026-05-21 01:53:43.601Z	132.002° SE	2026-05-21 01:56:43.601Z	64.541° ENE	33.681°	2026-05-21 02:00:43.601Z	1.741° NNE

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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, 27536 on other resources

View CZ-4 DEB, 27536 on Heavens-Above

View CZ-4 DEB, 27536 on Keep Track

View CZ-4 DEB, 27536 on Celestrak

View CZ-4 DEB, 27536 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, 27536

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-05-19T14:27:45.408Z)

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, 27536 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago