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

14 hours ago

Origin

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

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 14 hours ago

0 CZ-4 DEB
1 26140U 99057AC  25151.66129956  .00005683  00000-0  10250-2 0  9993
2 26140  99.3537  35.1202 0148117   1.2969  55.6973 14.60059900318240

Epoch: 2025-05-31T15:52Z

TLE epoch observation values (Epoch: 2025-05-31T15:52:16.282Z)

Latitude

57.29556°

Longitude

-107.12805°

Altitude

644.593 km

Speed

7.572 km/s

True Right ascension

01h 21m 21s

True Declination

57° 08' 11"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-23.18557°

Longitude

84.27944°

Altitude

797.303 km

Speed

7.403 km/s

Apparent Right ascension

11h 32m 29s

Apparent Declination

-70° 00' 04"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

15:21:24

Azimuth

198.909° SSW

Elevation

-27.452°

Doppler factor

Orbital elements

Apogee altitude

794.81 km

Perigee altitude

585.425 km

Semi-major axis

7,068.254 km

Eccentricity

0.01481

Inclination

99.3537°

RAAN

35.1202°

Arg. of periapsis

1.2969°

True anomaly

Unknown

Mean anomaly

55.6973°

Eccentric anomaly

Unknown

Mean motion

3.65237 °/min

Orbital period

98.57 mins

BSTAR

0.001025

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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.
6 mins	2025-06-01 16:25:01.152Z	183.755° SSW	2025-06-01 16:27:01.152Z	224.661° SW	39.474°	2025-06-01 16:31:01.152Z	335.923° NNW
7 mins	2025-06-02 04:23:01.152Z	46.756° ENE	2025-06-02 04:26:01.152Z	95.214° ESE	26.641°	2025-06-02 04:30:01.152Z	154.574° SSE

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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