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 (26 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: 19 hours ago

TLE from 19 hours ago

0 CZ-4 DEB
1 26262U 99057EY  26083.71433075  .00009192  00000-0  11633-2 0  9994
2 26262  98.3315 180.2881 0039039  57.1989  99.0614 14.81506809375297

Epoch: 2026-03-24T17:08Z

TLE epoch observation values (Epoch: 2026-03-24T17:08:38.176Z)

Latitude

23.05835°

Longitude

-75.50433°

Altitude

631.86 km

Speed

7.542 km/s

True Right ascension

00h 15m 22s

True Declination

22° 55' 57"

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

17:05:11

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

648.957 km

Perigee altitude

594.304 km

Semi-major axis

6,999.768 km

Eccentricity

0.0039

Inclination

98.3315°

RAAN

180.2881°

Arg. of periapsis

57.1989°

True anomaly

99.50283°

Mean anomaly

99.0614°

Eccentric anomaly

99.28215°

Mean motion

3.70611 °/min

Orbital period

97.14 mins

BSTAR

0.0011633

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

CBERS 1 DEB, 32468 (Decayed)

CZ-4 DEB, 26442

CBERS 1 DEB, 32080 (Decayed)

CZ-4 DEB, 26426 (Decayed)

CZ-4 DEB, 26269 (Decayed)

CZ-4 DEB, 26429 (Decayed)

CZ-4 DEB, 26325 (Decayed)

CZ-4 DEB, 26431 (Decayed)

CZ-4 DEB, 26458 (Decayed)

CZ-4 DEB, 26238 (Decayed)

CZ-4 DEB, 26657 (Decayed)

CZ-4 DEB, 26693 (Decayed)

CZ-4 DEB, 26757 (Decayed)

CZ-4 DEB, 26131 (Decayed)

CZ-4 DEB, 27008 (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	2026-03-25 18:56:49.663Z	26.368° NE	2026-03-25 19:00:49.663Z	125.528° SE	36.891°	2026-03-25 19:03:49.663Z	174.412° S
6 mins	2026-03-26 05:51:49.663Z	133.599° SE	2026-03-26 05:54:49.663Z	66.24° ENE	32.249°	2026-03-26 05:57:49.663Z	7.13° 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: 19 hours ago

TLE from 19 hours ago

TLE epoch observation values (Epoch: 2026-03-24T17:08:38.176Z)

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: 19 hours ago