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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ISO8601 Format

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, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 CZ-4 DEB
1 26175U 99057BM  26139.53780235  .00000210  00000-0  16102-3 0  9991
2 26175  98.7403 354.4956 0331226 196.8634 162.1296 13.79351004315104

Epoch: 2026-05-19T12:54Z

TLE epoch observation values (Epoch: 2026-05-19T12:54:26.123Z)

Latitude

0.00006°

Longitude

-76.32353°

Altitude

1,201.344 km

Speed

7.138 km/s

True Right ascension

23h 37m 58s

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

09:30:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,206.57 km

Perigee altitude

720.229 km

Semi-major axis

7,341.537 km

Eccentricity

0.03312

Inclination

98.7403°

RAAN

354.4956°

Arg. of periapsis

196.8634°

True anomaly

163.25004°

Mean anomaly

162.1296°

Eccentric anomaly

162.69414°

Mean motion

3.45035 °/min

Orbital period

104.34 mins

BSTAR

0.00016102

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

CZ-4 DEB, 26306

CZ-4 DEB, 26152

CZ-4 DEB, 26241

CZ-4 DEB, 26229 (Decayed)

CZ-4 DEB, 26446

CBERS 1 DEB, 32079

CZ-4 DEB, 26200

CZ-4 DEB, 26324 (Decayed)

CBERS 1 DEB, 34217 (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	2026-05-20 03:27:13.020Z	7.264° NNE	2026-05-20 03:31:13.020Z	313.843° NW	42.807°	2026-05-20 03:36:13.020Z	204.707° SW
11 mins	2026-05-20 13:25:13.020Z	128.485° SE	2026-05-20 13:30:13.020Z	68.162° E	33.728°	2026-05-20 13:36:13.020Z	2.115° NNE
11 mins	2026-05-20 15:08:13.020Z	204.127° SW	2026-05-20 15:13:13.020Z	263.926° W	31.997°	2026-05-20 15:19:13.020Z	328.524° 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: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-05-19T12:54:26.123Z)

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: 12 hours ago