CZ-4 DEB, 26143

Orbit data source: Space-Track

CZ-4 DEB, 26143 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/26143?theme=dark&initialShowStats=false

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Identifier

26143, 1999-057AF

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: 21 hours ago

TLE from 21 hours ago

0 CZ-4 DEB
1 26143U 99057AF  26083.83920073  .00000528  00000-0  46299-3 0  9995
2 26143  98.9895  52.9900 0475977 339.4753  45.5877 13.47567057276369

Epoch: 2026-03-24T20:08Z

TLE epoch observation values (Epoch: 2026-03-24T20:08:26.943Z)

Latitude

28.78068°

Longitude

-76.39206°

Altitude

845.256 km

Speed

7.551 km/s

True Right ascension

03h 12m 07s

True Declination

28° 38' 15"

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

22:40:14

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,433.401 km

Perigee altitude

723.565 km

Semi-major axis

7,456.62 km

Eccentricity

0.0476

Inclination

98.9895°

RAAN

52.99°

Arg. of periapsis

339.4753°

True anomaly

49.64936°

Mean anomaly

45.5877°

Eccentric anomaly

47.60163°

Mean motion

3.37078 °/min

Orbital period

106.8 mins

BSTAR

0.00046299

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

CZ-4 DEB, 26343 (Decayed)

CZ-4 DEB, 26651 (Decayed)

CZ-4 DEB, 26657 (Decayed)

CZ-4 DEB, 26173 (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.
10 mins	2026-03-25 21:04:58.133Z	130.314° SE	2026-03-25 21:08:58.133Z	73.106° E	32.585°	2026-03-25 21:14:58.133Z	359.77° N
7 mins	2026-03-25 22:51:58.133Z	224.162° SW	2026-03-25 22:54:58.133Z	268.817° W	24.072°	2026-03-25 22:58:58.133Z	317.762° NNW
13 mins	2026-03-26 10:01:58.133Z	31.821° NE	2026-03-26 10:07:58.133Z	102.454° ESE	36.963°	2026-03-26 10:14:58.133Z	169.064° S
13 mins	2026-03-26 11:46:58.133Z	354.376° N	2026-03-26 11:52:58.133Z	292.71° NW	33.013°	2026-03-26 11:59:58.133Z	230.857° WSW

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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, 26143 on other resources

View CZ-4 DEB, 26143 on Heavens-Above

View CZ-4 DEB, 26143 on Keep Track

View CZ-4 DEB, 26143 on Celestrak

View CZ-4 DEB, 26143 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, 26143

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: 2026-03-24T20:08:26.943Z)

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, 26143 on other resources

Documentation

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