CZ-4 DEB, 26134

Orbit data source: Space-Track

CZ-4 DEB, 26134 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/26134?theme=dark&initialShowStats=false

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Identifier

26134, 1999-057W

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, 0.082 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago

0 CZ-4 DEB
1 26134U 99057W   26277.21097492  .00000376  00000-0  27425-3 0  9993
2 26134  98.9881  67.7901 0417222  44.2173 129.9682 13.66449297315973

Epoch: 2026-10-04T05:03Z

TLE epoch observation values (Epoch: 2026-10-04T05:03:48.233Z)

Latitude

2.14457°

Longitude

159.26932°

Altitude

1,220.305 km

Speed

7.143 km/s

True Right ascension

16h 32m 30s

True Declination

2° 07' 57"

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

21:46:40

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,317.815 km

Perigee altitude

701.351 km

Semi-major axis

7,387.72 km

Eccentricity

0.04172

Inclination

98.9881°

RAAN

67.7901°

Arg. of periapsis

44.2173°

True anomaly

133.5112°

Mean anomaly

129.9682°

Eccentric anomaly

131.75161°

Mean motion

3.41804 °/min

Orbital period

105.32 mins

BSTAR

0.00027425

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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, 26287 (Decayed)

CZ-4 DEB, 26650 (Decayed)

CZ-4 DEB, 35320

CBERS 1 DEB, 32082 (Decayed)

CZ-4 DEB, 26344 (Decayed)

CZ-4 DEB, 26423 (Decayed)

CZ-4 DEB, 26292 (Decayed)

CZ-4 DEB, 26338

CBERS 1 DEB, 30781 (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	2026-10-05 10:13:45.942Z	172.662° S	2026-10-05 10:16:45.942Z	224.04° SW	73.596°	2026-10-05 10:20:45.942Z	341.618° N
11 mins	2026-10-05 22:58:45.942Z	18.188° NNE	2026-10-05 23:02:45.942Z	83.644° E	80.226°	2026-10-05 23:09:45.942Z	191.667° SSW
6 mins	2026-10-06 00:43:45.942Z	326.802° NNW	2026-10-06 00:46:45.942Z	293.755° NW	17.239°	2026-10-06 00:49:45.942Z	264.812° W

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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, 26134 on other resources

View CZ-4 DEB, 26134 on Heavens-Above

View CZ-4 DEB, 26134 on Keep Track

View CZ-4 DEB, 26134 on Celestrak

View CZ-4 DEB, 26134 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, 26134

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 23 hours ago

TLE from 23 hours ago

TLE epoch observation values (Epoch: 2026-10-04T05:03:48.233Z)

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, 26134 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 23 hours ago