CZ-4 DEB, 26126

Orbit data source: Space-Track

CZ-4 DEB, 26126 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/26126?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26126, 1999-057N

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1999-10-14 (27 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 CZ-4 DEB
1 26126U 99057N   26144.10152699  .00000777  00000-0  22348-3 0  9990
2 26126  98.6307 198.1234 0092962 249.5597 139.6425 14.45329962372286

Epoch: 2026-05-24T02:26Z

TLE epoch observation values (Epoch: 2026-05-24T02:26:11.931Z)

Latitude

29.56362°

Longitude

-85.04771°

Altitude

795.346 km

Speed

7.432 km/s

True Right ascension

12h 52m 50s

True Declination

29° 25' 01"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

01:38:42

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

804.217 km

Perigee altitude

671.909 km

Semi-major axis

7,116.2 km

Eccentricity

0.0093

Inclination

98.6307°

RAAN

198.1234°

Arg. of periapsis

249.5597°

True anomaly

140.32625°

Mean anomaly

139.6425°

Eccentric anomaly

139.98498°

Mean motion

3.61552 °/min

Orbital period

99.57 mins

BSTAR

0.00022348

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Other satellites on launch #57 in the year 1999 (1999-10-14 UTC)

CBERS 1 DEB, 30782 (Decayed)

CZ-4 DEB, 26653 (Decayed)

CZ-4 DEB, 35331

CZ-4 DEB, 26441 (Decayed)

CBERS 1 DEB, 35385 (Decayed)

CZ-4 DEB, 26182 (Decayed)

CZ-4 DEB, 26232 (Decayed)

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CZ-4 DEB Visibility forecast

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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.
5 mins	2026-05-24 17:50:02.188Z	332.539° NNW	2026-05-24 17:53:02.188Z	293.21° NW	16.679°	2026-05-24 17:55:02.188Z	266.609° W
8 mins	2026-05-25 03:21:02.188Z	153.346° SSE	2026-05-25 03:25:02.188Z	46.204° ENE	42.721°	2026-05-25 03:29:02.188Z	352.816° N
6 mins	2026-05-25 15:28:02.188Z	54.879° ENE	2026-05-25 15:31:02.188Z	99.083° ESE	19.779°	2026-05-25 15:34:02.188Z	139.214° SSE

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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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out CZ-4 DEB, 26126 on other resources

View CZ-4 DEB, 26126 on Heavens-Above

View CZ-4 DEB, 26126 on Keep Track

View CZ-4 DEB, 26126 on Celestrak

View CZ-4 DEB, 26126 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

CZ-4 DEB, 26126

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-05-24T02:26:11.931Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #57 in the year 1999 (1999-10-14 UTC)

CZ-4 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4 DEB, 26126 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago