CZ-4 DEB, 26272

Orbit data source: Space-Track

CZ-4 DEB, 26272 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/26272?theme=dark&initialShowStats=false

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Identifier

26272, 1999-057FJ

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: 23 hours ago

TLE from 23 hours ago

0 CZ-4 DEB
1 26272U 99057FJ  25357.18985086  .00008298  00000-0  10979-2 0  9991
2 26272  98.2758  78.6935 0051211 290.8159 128.8995 14.79290318362818

Epoch: 2025-12-23T04:33Z

TLE epoch observation values (Epoch: 2025-12-23T04:33:23.114Z)

Latitude

59.24512°

Longitude

-95.70061°

Altitude

664.264 km

Speed

7.519 km/s

True Right ascension

04h 18m 29s

True Declination

59° 05' 30"

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

02:53:01

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

664.506 km

Perigee altitude

592.742 km

Semi-major axis

7,006.761 km

Eccentricity

0.00512

Inclination

98.2758°

RAAN

78.6935°

Arg. of periapsis

290.8159°

True anomaly

129.35437°

Mean anomaly

128.8995°

Eccentric anomaly

129.12712°

Mean motion

3.70056 °/min

Orbital period

97.28 mins

BSTAR

0.0010979

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

CBERS 1 DEB, 31868 (Decayed)

CZ-4 DEB, 26138 (Decayed)

CZ-4 DEB, 34211 (Decayed)

CZ-4 DEB, 26177 (Decayed)

CZ-4 DEB, 26422 (Decayed)

CBERS 1 DEB, 31593 (Decayed)

CZ-4 DEB, 26135 (Decayed)

CZ-4 DEB, 26133 (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.
6 mins	2025-12-24 04:46:46.996Z	119.362° SE	2025-12-24 04:49:46.996Z	69.508° E	23.889°	2025-12-24 04:52:46.996Z	18.18° NNE
6 mins	2025-12-24 06:23:46.996Z	219.66° SW	2025-12-24 06:25:46.996Z	257.675° W	24.675°	2025-12-24 06:29:46.996Z	322.329° NNW
7 mins	2025-12-24 18:12:46.996Z	30.263° NE	2025-12-24 18:15:46.996Z	113.826° SE	38.806°	2025-12-24 18:19:46.996Z	177.964° S

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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, 26272 on other resources

View CZ-4 DEB, 26272 on Heavens-Above

View CZ-4 DEB, 26272 on Keep Track

View CZ-4 DEB, 26272 on Celestrak

View CZ-4 DEB, 26272 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, 26272

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 23 hours ago

TLE from 23 hours ago

TLE epoch observation values (Epoch: 2025-12-23T04:33:23.114Z)

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, 26272 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 23 hours ago