CZ-4 DEB, 26175

Orbit data source: Space-Track

CZ-4 DEB, 26175 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/26175?theme=dark&initialShowStats=false

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Identifier

26175, 1999-057BM

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, 0.081 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 CZ-4 DEB
1 26175U 99057BM  26276.99152647  .00000205  00000-0  15744-3 0  9998
2 26175  98.7239 121.5450 0331155 186.2605 173.4362 13.79434117334056

Epoch: 2026-10-03T23:47Z

TLE epoch observation values (Epoch: 2026-10-03T23:47:47.887Z)

Latitude

0.00002°

Longitude

111.90429°

Altitude

1,210.51 km

Speed

7.129 km/s

True Right ascension

08h 06m 10s

True Declination

0° 00' 00"

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

19:27:30

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,206.213 km

Perigee altitude

719.995 km

Semi-major axis

7,341.241 km

Eccentricity

0.03312

Inclination

98.7239°

RAAN

121.545°

Arg. of periapsis

186.2605°

True anomaly

173.85281°

Mean anomaly

173.4362°

Eccentric anomaly

173.64618°

Mean motion

3.45056 °/min

Orbital period

104.33 mins

BSTAR

0.00015744

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

CZ-4 DEB, 26285 (Decayed)

CZ-4 DEB, 26650 (Decayed)

CZ-4 DEB, 26658

CBERS 1 DEB, 30792

CBERS 1 DEB, 32082 (Decayed)

CZ-4 DEB, 26329

CBERS 1 DEB, 30780 (Decayed)

CZ-4 DEB, 26344 (Decayed)

CZ-4 DEB, 26423 (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.
9 mins	2026-10-05 02:30:58.887Z	17.237° NNE	2026-10-05 02:35:58.887Z	105.608° ESE	74.873°	2026-10-05 02:39:58.887Z	187.069° SSW
9 mins	2026-10-05 12:30:58.887Z	110.78° ESE	2026-10-05 12:34:58.887Z	66.095° ENE	29.368°	2026-10-05 12:39:58.887Z	11.994° NNE
12 mins	2026-10-05 14:11:58.887Z	186.44° SSW	2026-10-05 14:17:58.887Z	267.492° W	54.595°	2026-10-05 14:23:58.887Z	335.974° NNW

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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, 26175 on other resources

View CZ-4 DEB, 26175 on Heavens-Above

View CZ-4 DEB, 26175 on Keep Track

View CZ-4 DEB, 26175 on Celestrak

View CZ-4 DEB, 26175 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, 26175

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-10-03T23:47:47.887Z)

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, 26175 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago