CZ-4 DEB, 26152

Orbit data source: Space-Track

CZ-4 DEB, 26152 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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Iframe URL

https://www.satcat.com/sats-embedded/26152?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26152, 1999-057AN

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: 8 hours ago

TLE from 8 hours ago

0 CZ-4 DEB
1 26152U 99057AN  26139.49260961  .00000413  00000-0  38530-3 0  9994
2 26152  99.1330 150.4491 0519760  22.2980 127.8704 13.38525561274267

Epoch: 2026-05-19T11:49Z

TLE epoch observation values (Epoch: 2026-05-19T11:49:21.470Z)

Latitude

24.99823°

Longitude

-79.77838°

Altitude

1,368.85 km

Speed

7.055 km/s

True Right ascension

22h 18m 54s

True Declination

24° 52' 38"

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

04:38:26

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,501.364 km

Perigee altitude

722.744 km

Semi-major axis

7,490.191 km

Eccentricity

0.05198

Inclination

99.133°

RAAN

150.4491°

Arg. of periapsis

22.298°

True anomaly

132.38684°

Mean anomaly

127.8704°

Eccentric anomaly

130.14677°

Mean motion

3.34814 °/min

Orbital period

107.52 mins

BSTAR

0.0003853

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

CZ-4 DEB, 26178 (Decayed)

CZ-4 DEB, 26323

CZ-4 DEB, 26306

CZ-4 DEB, 26240 (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	2026-05-19 23:46:56.303Z	119.908° SE	2026-05-19 23:49:56.303Z	75.722° E	25.298°	2026-05-19 23:53:56.303Z	12.283° NNE
6 mins	2026-05-20 01:33:56.303Z	219.067° SW	2026-05-20 01:36:56.303Z	271.218° WNW	23.802°	2026-05-20 01:39:56.303Z	315.252° NNW
12 mins	2026-05-20 12:46:56.303Z	35.969° NE	2026-05-20 12:51:56.303Z	93.955° ESE	33.76°	2026-05-20 12:58:56.303Z	164.594° S
12 mins	2026-05-20 14:32:56.303Z	353.608° N	2026-05-20 14:37:56.303Z	296.107° NW	33.367°	2026-05-20 14:44:56.303Z	228.026° 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, 26152 on other resources

View CZ-4 DEB, 26152 on Heavens-Above

View CZ-4 DEB, 26152 on Keep Track

View CZ-4 DEB, 26152 on Celestrak

View CZ-4 DEB, 26152 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, 26152

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-05-19T11:49:21.470Z)

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, 26152 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago