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

7 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 7 hours ago

0 CZ-4 DEB
1 26142U 99057AE  25199.66834060  .00000481  00000-0  31291-3 0  9996
2 26142  98.7657  96.8977 0297784 329.7611  59.5223 13.87394880278207

Epoch: 2025-07-18T16:02Z

TLE epoch observation values (Epoch: 2025-07-18T16:02:24.627Z)

Latitude

31.91722°

Longitude

-85.9034°

Altitude

836.229 km

Speed

7.491 km/s

True Right ascension

06h 05m 39s

True Declination

31° 45' 53"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

50.1417°

Longitude

110.45677°

Altitude

1,149.984 km

Speed

7.18 km/s

Apparent Right ascension

21h 43m 41s

Apparent Declination

12° 21' 58"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:13:52

Azimuth

41.995° NE

Elevation

-27.167°

Doppler factor

Orbital elements

Apogee altitude

1,152.749 km

Perigee altitude

717.203 km

Semi-major axis

7,313.113 km

Eccentricity

0.02978

Inclination

98.7657°

RAAN

96.8977°

Arg. of periapsis

329.7611°

True anomaly

62.51833°

Mean anomaly

59.5223°

Eccentric anomaly

61.01477°

Mean motion

3.47048 °/min

Orbital period

103.73 mins

BSTAR

0.00031291

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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.
9 mins	2025-07-19 04:37:16.112Z	48.523° ENE	2025-07-19 04:41:16.112Z	85.838° E	19.236°	2025-07-19 04:46:16.112Z	133.799° SE
12 mins	2025-07-19 06:19:16.112Z	7.868° NNE	2025-07-19 06:24:16.112Z	311.045° NW	43.524°	2025-07-19 06:31:16.112Z	204.268° SW
5 mins	2025-07-19 08:04:16.112Z	319.593° NNW	2025-07-19 08:06:16.112Z	300.977° NW	13.764°	2025-07-19 08:09:16.112Z	275.239° WNW
8 mins	2025-07-19 16:16:16.112Z	117.508° SE	2025-07-19 16:19:16.112Z	71.696° E	28.342°	2025-07-19 16:24:16.112Z	6.477° NNE
7 mins	2025-07-19 17:59:16.112Z	218.019° SW	2025-07-19 18:02:16.112Z	270.768° WNW	28.01°	2025-07-19 18:06:16.112Z	322.781° 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, 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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