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

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 26142U 99057AE  25151.64694984  .00000765  00000-0  47871-3 0  9997
2 26142  98.7710  51.7492 0299324 100.4017 336.6431 13.87325837271507

Epoch: 2025-05-31T15:31Z

TLE epoch observation values (Epoch: 2025-05-31T15:31:36.466Z)

Latitude

73.28864°

Longitude

-101.277°

Altitude

750.56 km

Speed

7.588 km/s

True Right ascension

01h 24m 02s

True Declination

73° 11' 37"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-22.861°

Longitude

106.31805°

Altitude

993.89 km

Speed

7.33 km/s

Apparent Right ascension

14h 17m 34s

Apparent Declination

-74° 00' 56"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

15:37:13

Azimuth

185.926° SSW

Elevation

-24.725°

Doppler factor

Orbital elements

Apogee altitude

1,154.125 km

Perigee altitude

716.313 km

Semi-major axis

7,313.356 km

Eccentricity

0.02993

Inclination

98.771°

RAAN

51.7492°

Arg. of periapsis

100.4017°

True anomaly

Unknown

Mean anomaly

336.6431°

Eccentric anomaly

Unknown

Mean motion

3.47031 °/min

Orbital period

103.74 mins

BSTAR

0.00047871

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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.
6 mins	2025-06-01 07:19:46.972Z	336.516° NNW	2025-06-01 07:22:46.972Z	290.685° WNW	21.49°	2025-06-01 07:25:46.972Z	248.881° W
8 mins	2025-06-01 17:15:46.972Z	164.576° S	2025-06-01 17:19:46.972Z	359.478° N	44.958°	2025-06-01 17:23:46.972Z	346.557° N
7 mins	2025-06-02 05:50:46.972Z	31.478° NE	2025-06-02 05:53:46.972Z	89.954° E	37.907°	2025-06-02 05:57:46.972Z	172.09° S

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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