CZ-4 DEB, 26205

Orbit data source: Space-Track

CZ-4 DEB, 26205 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/26205?theme=dark&initialShowStats=false

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Identifier

26205, 1999-057CT

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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago

0 CZ-4 DEB
1 26205U 99057CT  26226.17863881  .00000025  00000-0  55075-4 0  9998
2 26205  99.1560 197.4058 0641066  77.1807 290.0115 13.13004049260678

Epoch: 2026-08-14T04:17Z

TLE epoch observation values (Epoch: 2026-08-14T04:17:14.393Z)

Latitude

-0.00002°

Longitude

170.48824°

Altitude

1,076.195 km

Speed

7.38 km/s

True Right ascension

13h 09m 37s

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

05:23:33

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,695.245 km

Perigee altitude

722.491 km

Semi-major axis

7,587.005 km

Eccentricity

0.06411

Inclination

99.156°

RAAN

197.4058°

Arg. of periapsis

77.1807°

True anomaly

282.93267°

Mean anomaly

290.0115°

Eccentric anomaly

286.48953°

Mean motion

3.28426 °/min

Orbital period

109.61 mins

BSTAR

0.000055075

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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.
6 mins	2026-08-14 20:53:51.352Z	109.95° ESE	2026-08-14 20:56:51.352Z	73.906° E	19.169°	2026-08-14 20:59:51.352Z	28.82° NE
8 mins	2026-08-14 22:41:51.352Z	197.795° SSW	2026-08-14 22:45:51.352Z	271.512° WNW	32.675°	2026-08-14 22:49:51.352Z	328.767° NNW
9 mins	2026-08-15 10:08:51.352Z	51.955° ENE	2026-08-15 10:11:51.352Z	97.07° ESE	27.462°	2026-08-15 10:17:51.352Z	159.85° S
9 mins	2026-08-15 11:56:51.352Z	344.224° N	2026-08-15 11:59:51.352Z	297.039° NW	30.557°	2026-08-15 12:05:51.352Z	227.418° WSW

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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, 26205 on other resources

View CZ-4 DEB, 26205 on Heavens-Above

View CZ-4 DEB, 26205 on Keep Track

View CZ-4 DEB, 26205 on Celestrak

View CZ-4 DEB, 26205 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, 26205

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-08-14T04:17:14.393Z)

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, 26205 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago