CZ-4 DEB, 26209

Orbit data source: Space-Track

CZ-4 DEB, 26209 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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Iframe URL

https://www.satcat.com/sats-embedded/26209?theme=dark&initialShowStats=false

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Identifier

26209, 1999-057CX

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: 9 hours ago

TLE from 9 hours ago

0 CZ-4 DEB
1 26209U 99057CX  26139.73244161  .00000481  00000-0  97199-4 0  9990
2 26209  98.6461 308.4177 0028201 173.0142 198.4278 14.65998414393168

Epoch: 2026-05-19T17:34Z

TLE epoch observation values (Epoch: 2026-05-19T17:34:42.955Z)

Latitude

11.1612°

Longitude

165.62663°

Altitude

694.968 km

Speed

7.5 km/s

True Right ascension

20h 26m 49s

True Declination

11° 05' 44"

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

11:21:12

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

690.845 km

Perigee altitude

651.087 km

Semi-major axis

7,049.103 km

Eccentricity

0.00282

Inclination

98.6461°

RAAN

308.4177°

Arg. of periapsis

173.0142°

True anomaly

198.32599°

Mean anomaly

198.4278°

Eccentric anomaly

198.37686°

Mean motion

3.66727 °/min

Orbital period

98.17 mins

BSTAR

0.000097199

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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.
5 mins	2026-05-20 10:04:35.930Z	97.266° ESE	2026-05-20 10:06:35.930Z	67.478° ENE	17.58°	2026-05-20 10:09:35.930Z	24.535° NE
7 mins	2026-05-20 11:40:35.930Z	195.624° SSW	2026-05-20 11:43:35.930Z	262.935° W	35.348°	2026-05-20 11:47:35.930Z	331.816° NNW
6 mins	2026-05-20 23:36:35.930Z	42.323° NE	2026-05-20 23:39:35.930Z	111.088° ESE	30.608°	2026-05-20 23:42:35.930Z	161.906° S
4 mins	2026-05-21 01:14:35.930Z	320.156° NNW	2026-05-21 01:15:35.930Z	303.138° NW	19.002°	2026-05-21 01:18:35.930Z	254.54° W

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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, 26209 on other resources

View CZ-4 DEB, 26209 on Heavens-Above

View CZ-4 DEB, 26209 on Keep Track

View CZ-4 DEB, 26209 on Celestrak

View CZ-4 DEB, 26209 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, 26209

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-05-19T17:34:42.955Z)

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, 26209 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 9 hours ago