CZ-4 DEB, 26158

Orbit data source: Space-Track

CZ-4 DEB, 26158 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/26158?theme=dark&initialShowStats=false

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Identifier

26158, 1999-057AU

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, 0.2 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago

0 CZ-4 DEB
1 26158U 99057AU  26100.13215132  .00001616  00000-0  54974-3 0  9995
2 26158  98.9588 167.1668 0177186 197.5102 192.7267 14.29591387344027

Epoch: 2026-04-10T03:10Z

TLE epoch observation values (Epoch: 2026-04-10T03:10:17.874Z)

Latitude

29.44798°

Longitude

-83.8575°

Altitude

920.834 km

Speed

7.33 km/s

True Right ascension

10h 48m 20s

True Declination

29° 18' 15"

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

18:04:03

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

917.267 km

Perigee altitude

663.24 km

Semi-major axis

7,168.391 km

Eccentricity

0.01772

Inclination

98.9588°

RAAN

167.1668°

Arg. of periapsis

197.5102°

True anomaly

192.28887°

Mean anomaly

192.7267°

Eccentric anomaly

192.50685°

Mean motion

3.57611 °/min

Orbital period

100.67 mins

BSTAR

0.00054974

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

CZ-4 DEB, 26238 (Decayed)

CBERS 1 DEB, 32064 (Decayed)

CZ-4 DEB, 26176 (Decayed)

CZ-4 DEB, 26133 (Decayed)

CZ-4 DEB, 26753 (Decayed)

CZ-4 DEB, 26129

CZ-4 DEB, 26436

CZ-4 DEB, 26185 (Decayed)

CZ-4B R/B, 25942

CZ-4 DEB, 26759 (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.
8 mins	2026-04-10 17:03:37.757Z	23.238° NE	2026-04-10 17:07:37.757Z	88.285° E	40.409°	2026-04-10 17:11:37.757Z	178.767° S
10 mins	2026-04-11 04:20:37.757Z	164.248° S	2026-04-11 04:25:37.757Z	348.049° N	44.385°	2026-04-11 04:30:37.757Z	346.361° N

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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, 26158 on other resources

View CZ-4 DEB, 26158 on Heavens-Above

View CZ-4 DEB, 26158 on Keep Track

View CZ-4 DEB, 26158 on Celestrak

View CZ-4 DEB, 26158 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, 26158

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-04-10T03:10:17.874Z)

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, 26158 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 9 hours ago