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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago

0 CZ-4 DEB
1 26152U 99057AN  26226.25674950  .00000069  00000-0  90387-4 0  9998
2 26152  99.1355 228.9014 0519567 165.8112 265.4525 13.38563169285877

Epoch: 2026-08-14T06:09Z

TLE epoch observation values (Epoch: 2026-08-14T06:09:43.156Z)

Latitude

63.91645°

Longitude

154.71065°

Altitude

1,176.394 km

Speed

7.247 km/s

True Right ascension

13h 59m 18s

True Declination

63° 47' 17"

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

06:21:39

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,501.072 km

Perigee altitude

722.756 km

Semi-major axis

7,490.051 km

Eccentricity

0.05196

Inclination

99.1355°

RAAN

228.9014°

Arg. of periapsis

165.8112°

True anomaly

259.55826°

Mean anomaly

265.4525°

Eccentric anomaly

262.50106°

Mean motion

3.34824 °/min

Orbital period

107.52 mins

BSTAR

0.000090387

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

CZ-4 DEB, 26275 (Decayed)

CBERS 1 DEB, 32076 (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	2026-08-14 22:09:48.234Z	86.434° E	2026-08-14 22:13:48.234Z	54.514° ENE	14.375°	2026-08-14 22:16:48.234Z	28.91° NE
13 mins	2026-08-14 23:51:48.234Z	153.983° SSE	2026-08-14 23:58:48.234Z	62.84° ENE	43.723°	2026-08-15 00:04:48.234Z	351.305° N
10 mins	2026-08-15 01:39:48.234Z	222.561° SW	2026-08-15 01:44:48.234Z	264.401° W	21.366°	2026-08-15 01:49:48.234Z	310.802° NW
8 mins	2026-08-15 12:56:48.234Z	22.546° NE	2026-08-15 13:00:48.234Z	107.018° ESE	42.081°	2026-08-15 13:04:48.234Z	182.699° SSW

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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: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-08-14T06:09:43.156Z)

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: 10 hours ago