CZ-4 DEB, 26162

Orbit data source: Space-Track

CZ-4 DEB, 26162 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/26162?theme=dark&initialShowStats=false

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Identifier

26162, 1999-057AY

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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago

0 CZ-4 DEB
1 26162U 99057AY  26085.14176343  .00002288  00000-0  90122-3 0  9994
2 26162  99.0865 146.9183 0253127 212.4643 146.0743 14.14202003330727

Epoch: 2026-03-26T03:24Z

TLE epoch observation values (Epoch: 2026-03-26T03:24:08.360Z)

Latitude

-0.00001°

Longitude

-87.7115°

Altitude

1,001.062 km

Speed

7.273 km/s

True Right ascension

09h 47m 40s

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

00:36:00

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,024.977 km

Perigee altitude

659.444 km

Semi-major axis

7,220.347 km

Eccentricity

0.02531

Inclination

99.0865°

RAAN

146.9183°

Arg. of periapsis

212.4643°

True anomaly

147.65153°

Mean anomaly

146.0743°

Eccentric anomaly

146.86702°

Mean motion

3.53758 °/min

Orbital period

101.76 mins

BSTAR

0.00090122

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

CZ-4 DEB, 26322 (Decayed)

CBERS 1 DEB, 31586 (Decayed)

CZ-4 DEB, 26305 (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.
11 mins	2026-03-27 03:17:29.103Z	137.808° SSE	2026-03-27 03:23:29.103Z	61.573° ENE	35.247°	2026-03-27 03:28:29.103Z	1.014° NNE
9 mins	2026-03-27 04:59:29.103Z	211.554° SW	2026-03-27 05:03:29.103Z	259.592° W	26.939°	2026-03-27 05:08:29.103Z	320.239° NNW
4 mins	2026-03-27 15:43:29.103Z	73.172° E	2026-03-27 15:44:29.103Z	86.411° E	14.895°	2026-03-27 15:47:29.103Z	124.801° SE
8 mins	2026-03-27 17:22:29.103Z	359.919° N	2026-03-27 17:25:29.103Z	305.961° NW	39.602°	2026-03-27 17:30:29.103Z	211.486° SW

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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, 26162 on other resources

View CZ-4 DEB, 26162 on Heavens-Above

View CZ-4 DEB, 26162 on Keep Track

View CZ-4 DEB, 26162 on Celestrak

View CZ-4 DEB, 26162 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, 26162

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2026-03-26T03:24:08.360Z)

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, 26162 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago