CZ-4 DEB, 26142

Orbit data source: Space-Track

CZ-4 DEB, 26142 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/26142?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26142, 1999-057AE

Orbit

SSO

Last TLE update

22 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 22 hours ago

0 CZ-4 DEB
1 26142U 99057AE  25191.47668214  .00000469  00000-0  30482-3 0  9990
2 26142  98.7670  89.1968 0298355 352.1190 185.4158 13.87384946277021

Epoch: 2025-07-10T11:26Z

TLE epoch observation values (Epoch: 2025-07-10T11:26:25.336Z)

Latitude

2.64692°

Longitude

169.35526°

Altitude

1,157.773 km

Speed

7.166 km/s

True Right ascension

17h 58m 24s

True Declination

2° 37' 55"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

65.9789°

Longitude

-170.04591°

Altitude

1,063.226 km

Speed

7.269 km/s

Apparent Right ascension

12h 21m 57s

Apparent Declination

40° 38' 24"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:54:36

Azimuth

332.906° NNW

Elevation

-2.745°

Doppler factor

Orbital elements

Apogee altitude

1,153.202 km

Perigee altitude

716.819 km

Semi-major axis

7,313.148 km

Eccentricity

0.02984

Inclination

98.767°

RAAN

89.1968°

Arg. of periapsis

352.119°

True anomaly

Unknown

Mean anomaly

185.4158°

Eccentric anomaly

Unknown

Mean motion

3.47046 °/min

Orbital period

103.73 mins

BSTAR

0.00030482

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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, 26140

CZ-4 DEB, 26141 (Decayed)

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.
8 mins	2025-07-11 16:08:52.485Z	117.057° SE	2025-07-11 16:12:52.485Z	60.95° ENE	23.71°	2025-07-11 16:16:52.485Z	11.233° NNE
8 mins	2025-07-11 17:51:52.485Z	206.623° SW	2025-07-11 17:54:52.485Z	259.638° W	30.413°	2025-07-11 17:59:52.485Z	329.381° NNW
8 mins	2025-07-12 04:44:52.485Z	57.166° ENE	2025-07-12 04:47:52.485Z	89.316° E	20.582°	2025-07-12 04:52:52.485Z	137.977° SSE
11 mins	2025-07-12 06:25:52.485Z	5.281° NNE	2025-07-12 06:30:52.485Z	289.353° WNW	42.704°	2025-07-12 06:36:52.485Z	208.271° SW

Authenticating...

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Check out CZ-4 DEB, 26142 on other resources

View CZ-4 DEB, 26142 on Heavens-Above

View CZ-4 DEB, 26142 on Keep Track

View CZ-4 DEB, 26142 on Celestrak

View CZ-4 DEB, 26142 on Gunter's Space Page

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