CZ-4 DEB, 26143

Orbit data source: Space-Track

CZ-4 DEB, 26143 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/26143?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26143, 1999-057AF

Orbit

SSO

Last TLE update

2 days 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 2 days ago

0 CZ-4 DEB
1 26143U 99057AF  25198.40555755  .00000220  00000-0  21403-3 0  9994
2 26143  98.9532 187.3715 0475938 255.5492 281.9986 13.47232159242631

Epoch: 2025-07-17T09:44Z

TLE epoch observation values (Epoch: 2025-07-17T09:44:00.172Z)

Latitude

7.68264°

Longitude

-72.88958°

Altitude

1,027.168 km

Speed

7.367 km/s

True Right ascension

00h 34m 19s

True Declination

7° 38' 20"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-80.74069°

Longitude

-178.69692°

Altitude

777.04 km

Speed

7.631 km/s

Apparent Right ascension

23h 30m 33s

Apparent Declination

-66° 47' 41"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

12:25:04

Azimuth

168.567° S

Elevation

-62.062°

Doppler factor

Orbital elements

Apogee altitude

1,434.666 km

Perigee altitude

724.771 km

Semi-major axis

7,457.855 km

Eccentricity

0.04759

Inclination

98.9532°

RAAN

187.3715°

Arg. of periapsis

255.5492°

True anomaly

276.60512°

Mean anomaly

281.9986°

Eccentric anomaly

279.30758°

Mean motion

3.36994 °/min

Orbital period

106.83 mins

BSTAR

0.00021403

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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, 26142

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.
13 mins	2025-07-19 00:08:26.642Z	201.544° SSW	2025-07-19 00:14:26.642Z	262.918° W	32.797°	2025-07-19 00:21:26.642Z	329.424° NNW
11 mins	2025-07-19 11:23:26.642Z	31.948° NE	2025-07-19 11:29:26.642Z	103.375° ESE	33.58°	2025-07-19 11:34:26.642Z	161.442° S
11 mins	2025-07-19 13:08:26.642Z	356.12° N	2025-07-19 13:14:26.642Z	293.863° NW	31.768°	2025-07-19 13:19:26.642Z	235.915° WSW
10 mins	2025-07-19 21:36:26.642Z	98.055° ESE	2025-07-19 21:41:26.642Z	52.499° ENE	22.457°	2025-07-19 21:46:26.642Z	12.692° NNE
14 mins	2025-07-19 23:19:26.642Z	170.079° S	2025-07-19 23:25:26.642Z	269.12° W	44.645°	2025-07-19 23:33:26.642Z	344.341° N

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, 26143 on other resources

View CZ-4 DEB, 26143 on Heavens-Above

View CZ-4 DEB, 26143 on Keep Track

View CZ-4 DEB, 26143 on Celestrak

View CZ-4 DEB, 26143 on Gunter's Space Page

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