CZ-4 DEB, 26333

Orbit data source: Space-Track

CZ-4 DEB, 26333 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/26333?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26333, 1999-057HS

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: 11 hours ago

TLE from 11 hours ago

0 CZ-4 DEB
1 26333U 99057HS  25345.20556046  .00435592  00000-0  64691-2 0  9990
2 26333  98.1166  69.2558 0014524 254.3891 105.5757 15.53564906368194

Epoch: 2025-12-11T04:56Z

TLE epoch observation values (Epoch: 2025-12-11T04:56:00.423Z)

Latitude

-0.00008°

Longitude

-84.91082°

Altitude

412.101 km

Speed

7.662 km/s

True Right ascension

04h 37m 01s

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

14:06:26

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

413.13 km

Perigee altitude

393.432 km

Semi-major axis

6,781.418 km

Eccentricity

0.00145

Inclination

98.1166°

RAAN

69.2558°

Arg. of periapsis

254.3891°

True anomaly

105.73594°

Mean anomaly

105.5757°

Eccentric anomaly

105.65583°

Mean motion

3.88653 °/min

Orbital period

92.63 mins

BSTAR

0.0064691

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

CBERS 1 DEB, 36317 (Decayed)

CZ-4 DEB, 26255 (Decayed)

CZ-4 DEB, 26426 (Decayed)

CZ-4 DEB, 26120 (Decayed)

CZ-4 DEB, 27008 (Decayed)

CBERS 1 DEB, 34212 (Decayed)

CZ-4 DEB, 26317 (Decayed)

CBERS 1 DEB, 30788 (Decayed)

CZ-4 DEB, 26225 (Decayed)

CZ-4 DEB, 26326 (Decayed)

CZ-4 DEB, 26252 (Decayed)

CZ-4 DEB, 26269 (Decayed)

CZ-4 DEB, 26180 (Decayed)

CBERS 1 DEB, 32072 (Decayed)

CZ-4 DEB, 26179 (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.
4 mins	2025-12-12 05:48:28.679Z	166.184° S	2025-12-12 05:50:28.679Z	347.34° N	41.163°	2025-12-12 05:52:28.679Z	347.171° N

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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, 26333 on other resources

View CZ-4 DEB, 26333 on Heavens-Above

View CZ-4 DEB, 26333 on Keep Track

View CZ-4 DEB, 26333 on Celestrak

View CZ-4 DEB, 26333 on Gunter's Space Page

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

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