CZ-4 DEB, 26266

Orbit data source: Space-Track

CZ-4 DEB, 26266 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/26266?theme=dark&initialShowStats=false

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Identifier

26266, 1999-057FC

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: 17 hours ago

TLE from 17 hours ago

0 CZ-4 DEB
1 26266U 99057FC  26028.81685703  .00013472  00000-0  20712-2 0  9999
2 26266  98.4199 123.9604 0072091 154.9045 205.5694 14.71884948362721

Epoch: 2026-01-28T19:36Z

TLE epoch observation values (Epoch: 2026-01-28T19:36:16.447Z)

Latitude

0.00007°

Longitude

61.81339°

Altitude

703.866 km

Speed

7.479 km/s

True Right ascension

08h 15m 50s

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

13:48:53

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

702.814 km

Perigee altitude

601.451 km

Semi-major axis

7,030.269 km

Eccentricity

0.00721

Inclination

98.4199°

RAAN

123.9604°

Arg. of periapsis

154.9045°

True anomaly

205.21573°

Mean anomaly

205.5694°

Eccentric anomaly

205.39228°

Mean motion

3.68201 °/min

Orbital period

97.77 mins

BSTAR

0.0020712

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

CZ-4 DEB, 26435 (Decayed)

CBERS 1 DEB, 32468 (Decayed)

CZ-4 DEB, 26242 (Decayed)

CZ-4 DEB, 26459 (Decayed)

CZ-4 DEB, 26217 (Decayed)

CBERS 1 DEB, 32072 (Decayed)

CZ-4 DEB, 26424 (Decayed)

CBERS 1 DEB, 37583 (Decayed)

CZ-4 DEB, 26172 (Decayed)

CZ-4 DEB, 26252 (Decayed)

CZ-4 DEB, 26136 (Decayed)

CZ-4 DEB, 26349 (Decayed)

CZ-4 DEB, 29040

CZ-4 DEB, 26280

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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	2026-01-29 19:01:18.994Z	18.55° NNE	2026-01-29 19:04:18.994Z	57.478° ENE	42.615°	2026-01-29 19:08:18.994Z	187.015° SSW
7 mins	2026-01-30 06:00:18.994Z	151.351° SSE	2026-01-30 06:03:18.994Z	66.446° ENE	42.434°	2026-01-30 06:07:18.994Z	353.498° N

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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, 26266 on other resources

View CZ-4 DEB, 26266 on Heavens-Above

View CZ-4 DEB, 26266 on Keep Track

View CZ-4 DEB, 26266 on Celestrak

View CZ-4 DEB, 26266 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, 26266

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2026-01-28T19:36:16.447Z)

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, 26266 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago