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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ISO8601 Format

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

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago

0 CZ-4 DEB
1 26262U 99057EY  26139.52650251  .00004167  00000-0  52240-3 0  9999
2 26262  98.3352 238.3713 0037524 233.4123 144.9592 14.82307256383563

Epoch: 2026-05-19T12:38Z

TLE epoch observation values (Epoch: 2026-05-19T12:38:09.816Z)

Latitude

18.40818°

Longitude

168.85147°

Altitude

646.063 km

Speed

7.525 km/s

True Right ascension

15h 42m 21s

True Declination

18° 18' 14"

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

15:17:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

645.365 km

Perigee altitude

592.852 km

Semi-major axis

6,997.245 km

Eccentricity

0.00375

Inclination

98.3352°

RAAN

238.3713°

Arg. of periapsis

233.4123°

True anomaly

145.20514°

Mean anomaly

144.9592°

Eccentric anomaly

145.08226°

Mean motion

3.70811 °/min

Orbital period

97.08 mins

BSTAR

0.0005224

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

CZ-4 DEB, 26229 (Decayed)

CZ-4 DEB, 26112 (Decayed)

CZ-4 DEB, 26324 (Decayed)

CZ-4 DEB, 28067

CZ-4 DEB, 27762

CZ-4 DEB, 27493

CZ-4 DEB, 26430 (Decayed)

CZ-4 DEB, 26755 (Decayed)

CZ-4 DEB, 26179 (Decayed)

CZ-4 DEB, 26449

CZ-4 DEB, 26222

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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	2026-05-20 06:29:09.195Z	162.437° S	2026-05-20 06:33:09.195Z	126.627° SE	44.335°	2026-05-20 06:37:09.195Z	349.161° N
6 mins	2026-05-20 19:55:09.195Z	350.864° N	2026-05-20 19:57:09.195Z	305.809° NW	35.78°	2026-05-20 20:01:09.195Z	216.144° SW

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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: 18 hours ago

TLE from 18 hours ago

TLE epoch observation values (Epoch: 2026-05-19T12:38:09.816Z)

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: 18 hours ago