CZ-4 DEB, 26140

Orbit data source: Space-Track

CZ-4 DEB, 26140 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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Iframe URL

https://www.satcat.com/sats-embedded/26140?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26140, 1999-057AC

Orbit

SSO

Last TLE update

10 hours ago

Origin

China National Space Administration (CN / PRC)

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

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 10 hours ago

0 CZ-4 DEB
1 26140U 99057AC  25191.60807249  .00002954  00000-0  53827-3 0  9995
2 26140  99.3510  80.1829 0143924 240.3570 181.2325 14.60508146324077

Epoch: 2025-07-10T14:35Z

TLE epoch observation values (Epoch: 2025-07-10T14:35:37.463Z)

Latitude

60.27653°

Longitude

-84.16743°

Altitude

803.499 km

Speed

7.403 km/s

True Right ascension

04h 14m 02s

True Declination

60° 07' 45"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

76.96534°

Longitude

-112.06211°

Altitude

798.886 km

Speed

7.411 km/s

Apparent Right ascension

01h 12m 11s

Apparent Declination

24° 17' 56"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:49:13

Azimuth

354.2° N

Elevation

-25.562°

Doppler factor

Orbital elements

Apogee altitude

790.378 km

Perigee altitude

586.962 km

Semi-major axis

7,066.807 km

Eccentricity

0.01439

Inclination

99.351°

RAAN

80.1829°

Arg. of periapsis

240.357°

True anomaly

Unknown

Mean anomaly

181.2325°

Eccentric anomaly

Unknown

Mean motion

3.65349 °/min

Orbital period

98.54 mins

BSTAR

0.00053827

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

CBERS 1, 25940

CZ-4 DEB, 26138 (Decayed)

CZ-4 DEB, 26139 (Decayed)

CZ-4 DEB, 26141 (Decayed)

CZ-4 DEB, 26142

CZ-4 DEB, 26143

CZ-4 DEB, 26144 (Decayed)

CZ-4 DEB, 26145 (Decayed)

CZ-4 DEB, 26148 (Decayed)

CZ-4 DEB, 26149 (Decayed)

CZ-4 DEB, 26150

CZ-4 DEB, 26151

CZ-4 DEB, 26152

CZ-4 DEB, 26153 (Decayed)

CZ-4 DEB Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-11 05:41:58.179Z	9.366° NNE	2025-07-11 05:44:58.179Z	315.694° NNW	44.012°	2025-07-11 05:48:58.179Z	202.116° SSW
4 mins	2025-07-11 15:09:58.179Z	77.52° E	2025-07-11 15:10:58.179Z	64.259° ENE	15.471°	2025-07-11 15:13:58.179Z	27.316° NE
9 mins	2025-07-11 16:43:58.179Z	175.535° S	2025-07-11 16:47:58.179Z	254.45° W	43°	2025-07-11 16:52:58.179Z	340.206° N

Authenticating...

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Check out CZ-4 DEB, 26140 on other resources

View CZ-4 DEB, 26140 on Heavens-Above

View CZ-4 DEB, 26140 on Keep Track

View CZ-4 DEB, 26140 on Celestrak

View CZ-4 DEB, 26140 on Gunter's Space Page

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