CZ-4 DEB, 26222

Orbit data source: Space-Track

CZ-4 DEB, 26222 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/26222?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26222, 1999-057DL

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, 2.0 m

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago

0 CZ-4 DEB
1 26222U 99057DL  26085.40014364  .00001606  00000-0  37482-3 0  9997
2 26222  98.4858 145.3346 0067434 339.7711  20.0815 14.54795799371736

Epoch: 2026-03-26T09:36Z

TLE epoch observation values (Epoch: 2026-03-26T09:36:12.410Z)

Latitude

-0.00007°

Longitude

177.43326°

Altitude

668.134 km

Speed

7.547 km/s

True Right ascension

09h 41m 20s

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

23:11:52

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

754.908 km

Perigee altitude

659.35 km

Semi-major axis

7,085.266 km

Eccentricity

0.00674

Inclination

98.4858°

RAAN

145.3346°

Arg. of periapsis

339.7711°

True anomaly

20.34894°

Mean anomaly

20.0815°

Eccentric anomaly

20.21501°

Mean motion

3.63923 °/min

Orbital period

98.92 mins

BSTAR

0.00037482

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

CZ-4 DEB, 26322 (Decayed)

CZ-4 DEB, 26453 (Decayed)

CZ-4 DEB, 36304 (Decayed)

CBERS 1 DEB, 31586 (Decayed)

CZ-4 DEB, 26305 (Decayed)

CZ-4 DEB, 26212 (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	2026-03-27 03:53:34.775Z	164.195° S	2026-03-27 03:56:34.775Z	124.691° SE	44.942°	2026-03-27 04:00:34.775Z	347.389° N
6 mins	2026-03-27 15:55:34.775Z	57.837° ENE	2026-03-27 15:57:34.775Z	90.332° ESE	22.742°	2026-03-27 16:01:34.775Z	147.358° SSE
7 mins	2026-03-27 17:32:34.775Z	347.131° N	2026-03-27 17:35:34.775Z	294.27° NW	30.762°	2026-03-27 17:39:34.775Z	228.739° 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, 26222 on other resources

View CZ-4 DEB, 26222 on Heavens-Above

View CZ-4 DEB, 26222 on Keep Track

View CZ-4 DEB, 26222 on Celestrak

View CZ-4 DEB, 26222 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, 26222

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-03-26T09:36:12.410Z)

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, 26222 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago