CZ-4 DEB, 26200

Orbit data source: Space-Track

CZ-4 DEB, 26200 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/26200?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26200, 1999-057CN

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)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 CZ-4 DEB
1 26200U 99057CN  25348.89742324  .00002961  00000-0  42228-3 0  9990
2 26200  98.2774 325.4565 0042115 173.4191 186.7580 14.76957179369300

Epoch: 2025-12-14T21:32Z

TLE epoch observation values (Epoch: 2025-12-14T21:32:17.367Z)

Latitude

-0.00007°

Longitude

-81.4196°

Altitude

671.306 km

Speed

7.506 km/s

True Right ascension

21h 41m 49s

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

01:19:13

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

665.548 km

Perigee altitude

606.467 km

Semi-major axis

7,014.144 km

Eccentricity

0.00421

Inclination

98.2774°

RAAN

325.4565°

Arg. of periapsis

173.4191°

True anomaly

186.7015°

Mean anomaly

186.758°

Eccentric anomaly

186.72972°

Mean motion

3.69472 °/min

Orbital period

97.44 mins

BSTAR

0.00042228

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

CZ-4 DEB, 26426 (Decayed)

CBERS 1 DEB, 32073 (Decayed)

CZ-4 DEB, 26290 (Decayed)

CZ-4 DEB, 26336

CZ-4 DEB, 26654

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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.
8 mins	2025-12-16 11:29:42.266Z	13.592° NNE	2025-12-16 11:33:42.266Z	29.272° NE	44.55°	2025-12-16 11:37:42.266Z	193.053° SSW
7 mins	2025-12-16 22:26:42.266Z	156.434° SSE	2025-12-16 22:29:42.266Z	114.689° SE	42.524°	2025-12-16 22:33:42.266Z	352.805° 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, 26200 on other resources

View CZ-4 DEB, 26200 on Heavens-Above

View CZ-4 DEB, 26200 on Keep Track

View CZ-4 DEB, 26200 on Celestrak

View CZ-4 DEB, 26200 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, 26200

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: 2025-12-14T21:32:17.367Z)

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, 26200 on other resources

Documentation

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