CZ-4 DEB, 26338

Orbit data source: Space-Track

CZ-4 DEB, 26338 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/26338?theme=dark&initialShowStats=false

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Identifier

26338, 1999-057HX

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, 0.5 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago

0 CZ-4 DEB
1 26338U 99057HX  26036.98881437  .00000666  00000-0  21677-3 0  9991
2 26338  98.7121  86.2249 0089448 193.9673 238.9807 14.39875642357588

Epoch: 2026-02-05T23:43Z

TLE epoch observation values (Epoch: 2026-02-05T23:43:53.561Z)

Latitude

70.20969°

Longitude

-70.94363°

Altitude

804.33 km

Speed

7.44 km/s

True Right ascension

04h 04m 39s

True Declination

70° 06' 02"

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

07:38:43

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

819.855 km

Perigee altitude

692.227 km

Semi-major axis

7,134.178 km

Eccentricity

0.00894

Inclination

98.7121°

RAAN

86.2249°

Arg. of periapsis

193.9673°

True anomaly

238.10735°

Mean anomaly

238.9807°

Eccentric anomaly

238.54352°

Mean motion

3.60186 °/min

Orbital period

99.95 mins

BSTAR

0.00021677

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

CZ-4 DEB, 26292 (Decayed)

CZ-4 DEB, 26131 (Decayed)

CZ-4 DEB, 26279 (Decayed)

CZ-4 DEB, 26435 (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.
6 mins	2026-02-06 15:00:42.790Z	51.47° ENE	2026-02-06 15:03:42.790Z	92.825° ESE	18.282°	2026-02-06 15:06:42.790Z	135.127° SSE
7 mins	2026-02-06 16:39:42.790Z	351.289° N	2026-02-06 16:42:42.790Z	292.051° WNW	33.975°	2026-02-06 16:46:42.790Z	222.226° SW
7 mins	2026-02-07 02:13:42.790Z	116.588° SE	2026-02-07 02:16:42.790Z	72.934° E	25.88°	2026-02-07 02:20:42.790Z	13.686° NNE
7 mins	2026-02-07 03:52:42.790Z	210.096° SW	2026-02-07 03:55:42.790Z	263.392° W	29.939°	2026-02-07 03:59:42.790Z	323.592° 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, 26338 on other resources

View CZ-4 DEB, 26338 on Heavens-Above

View CZ-4 DEB, 26338 on Keep Track

View CZ-4 DEB, 26338 on Celestrak

View CZ-4 DEB, 26338 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, 26338

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 hours ago

TLE from 6 hours ago

TLE epoch observation values (Epoch: 2026-02-05T23:43:53.561Z)

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, 26338 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 6 hours ago