CZ-4 DEB, 26262

Orbit data source: Space-Track

CZ-4 DEB, 26262 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/26262?theme=dark&initialShowStats=false

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Identifier

26262, 1999-057EY

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: 21 hours ago

TLE from 21 hours ago

0 CZ-4 DEB
1 26262U 99057EY  26263.52797632  .00005901  00000-0  70761-3 0  9997
2 26262  98.3384   7.7247 0036991 194.0713 227.7854 14.83973613401943

Epoch: 2026-09-20T12:40Z

TLE epoch observation values (Epoch: 2026-09-20T12:40:17.154Z)

Latitude

60.54384°

Longitude

163.2739°

Altitude

644.567 km

Speed

7.532 km/s

True Right ascension

23h 31m 03s

True Declination

60° 23' 38"

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

02:49:27

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

639.729 km

Perigee altitude

588.001 km

Semi-major axis

6,992.002 km

Eccentricity

0.0037

Inclination

98.3384°

RAAN

7.7247°

Arg. of periapsis

194.0713°

True anomaly

227.47243°

Mean anomaly

227.7854°

Eccentric anomaly

227.62882°

Mean motion

3.71228 °/min

Orbital period

96.98 mins

BSTAR

0.00070761

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

CBERS 1 DEB, 31592 (Decayed)

CZ-4 DEB, 26423 (Decayed)

CZ-4 DEB, 26304 (Decayed)

CBERS 1 DEB, 31594 (Decayed)

CBERS 1 DEB, 32078 (Decayed)

CZ-4 DEB, 26289 (Decayed)

CZ-4 DEB, 26215 (Decayed)

CZ-4 DEB, 26175

CZ-4 DEB, 26445 (Decayed)

CZ-4 DEB, 28490 (Decayed)

CZ-4 DEB, 26126

CZ-4 DEB, 26127

CZ-4 DEB, 26185 (Decayed)

CZ-4 DEB, 26119

CBERS 1 DEB, 32079

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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	2026-09-21 19:42:46.300Z	22.952° NE	2026-09-21 19:46:46.300Z	130.231° SE	55.107°	2026-09-21 19:49:46.300Z	179.05° S
6 mins	2026-09-22 06:36:46.300Z	134.732° SE	2026-09-22 06:39:46.300Z	55.953° ENE	44.044°	2026-09-22 06:42:46.300Z	3.737° NNE

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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, 26262 on other resources

View CZ-4 DEB, 26262 on Heavens-Above

View CZ-4 DEB, 26262 on Keep Track

View CZ-4 DEB, 26262 on Celestrak

View CZ-4 DEB, 26262 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, 26262

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 21 hours ago

TLE from 21 hours ago

TLE epoch observation values (Epoch: 2026-09-20T12:40:17.154Z)

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, 26262 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 21 hours ago