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

18 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 18 hours ago

0 CZ-4 DEB
1 26140U 99057AC  25199.22400729  .00003956  00000-0  71531-3 0  9998
2 26140  99.3497  88.7750 0143887 217.0770 265.6504 14.60569326325185

Epoch: 2025-07-18T05:22Z

TLE epoch observation values (Epoch: 2025-07-18T05:22:34.229Z)

Latitude

57.7749°

Longitude

-93.08801°

Altitude

710.188 km

Speed

7.501 km/s

True Right ascension

18h 55m 19s

True Declination

57° 37' 07"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

36.02099°

Longitude

65.84616°

Altitude

797.866 km

Speed

7.404 km/s

Apparent Right ascension

02h 59m 08s

Apparent Declination

0° 55' 41"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

11:51:38

Azimuth

301.715° NW

Elevation

-30.919°

Doppler factor

Orbital elements

Apogee altitude

790.152 km

Perigee altitude

586.793 km

Semi-major axis

7,066.609 km

Eccentricity

0.01439

Inclination

99.3497°

RAAN

88.775°

Arg. of periapsis

217.077°

True anomaly

264.00879°

Mean anomaly

265.6504°

Eccentric anomaly

264.82934°

Mean motion

3.65365 °/min

Orbital period

98.53 mins

BSTAR

0.00071531

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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.
4 mins	2025-07-19 04:27:05.210Z	62.798° ENE	2025-07-19 04:29:05.210Z	90.601° ESE	14.42°	2025-07-19 04:31:05.210Z	119.762° SE
7 mins	2025-07-19 06:04:05.210Z	355.667° N	2025-07-19 06:07:05.210Z	281.747° WNW	37.023°	2025-07-19 06:11:05.210Z	215.401° SW
6 mins	2025-07-19 15:30:05.210Z	104.764° ESE	2025-07-19 15:33:05.210Z	62.242° ENE	21.032°	2025-07-19 15:36:05.210Z	21.079° NNE
8 mins	2025-07-19 17:06:05.210Z	190.754° SSW	2025-07-19 17:10:05.210Z	262.384° W	35.982°	2025-07-19 17:14:05.210Z	329.254° NNW

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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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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