CZ-4 DEB, 26236

Orbit data source: Space-Track

CZ-4 DEB, 26236 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/26236?theme=dark&initialShowStats=false

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Identifier

26236, 1999-057EA

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, 0.5 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

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

TLE from 12 hours ago

0 CZ-4 DEB
1 26236U 99057EA  26226.13181231  .00000114  00000-0  49653-4 0  9994
2 26236  98.7017 277.7016 0088414 327.2819  52.1582 14.39738859384881

Epoch: 2026-08-14T03:09Z

TLE epoch observation values (Epoch: 2026-08-14T03:09:48.583Z)

Latitude

20.00654°

Longitude

-95.48963°

Altitude

723.516 km

Speed

7.515 km/s

True Right ascension

18h 18m 05s

True Declination

19° 53' 45"

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

05:23:18

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

819.573 km

Perigee altitude

693.413 km

Semi-major axis

7,134.63 km

Eccentricity

0.00884

Inclination

98.7017°

RAAN

277.7016°

Arg. of periapsis

327.2819°

True anomaly

52.96373°

Mean anomaly

52.1582°

Eccentric anomaly

52.56042°

Mean motion

3.60152 °/min

Orbital period

99.96 mins

BSTAR

0.000049653

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

CZ-4 DEB, 26230 (Decayed)

CZ-4 DEB, 26250 (Decayed)

CZ-4 DEB, 35325 (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	2026-08-14 15:20:36.557Z	46.919° ENE	2026-08-14 15:24:36.557Z	99.584° ESE	20.765°	2026-08-14 15:27:36.557Z	138.355° SSE
8 mins	2026-08-14 16:59:36.557Z	354.415° N	2026-08-14 17:03:36.557Z	277.629° WNW	35.214°	2026-08-14 17:07:36.557Z	221.06° SW
6 mins	2026-08-15 02:34:36.557Z	112.184° ESE	2026-08-15 02:37:36.557Z	61.809° ENE	24.512°	2026-08-15 02:40:36.557Z	16.971° NNE
6 mins	2026-08-15 04:13:36.557Z	215.08° SW	2026-08-15 04:15:36.557Z	251.164° W	27.856°	2026-08-15 04:19:36.557Z	320.461° 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, 26236 on other resources

View CZ-4 DEB, 26236 on Heavens-Above

View CZ-4 DEB, 26236 on Keep Track

View CZ-4 DEB, 26236 on Celestrak

View CZ-4 DEB, 26236 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, 26236

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: 2026-08-14T03:09:48.583Z)

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, 26236 on other resources

Documentation

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