CZ-4 DEB, 26654

Orbit data source: Space-Track

CZ-4 DEB, 26654 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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https://www.satcat.com/sats-embedded/26654?theme=dark&initialShowStats=false

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Identifier

26654, 1999-057LL

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 (26 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: 20 hours ago

TLE from 20 hours ago

0 CZ-4 DEB
1 26654U 99057LL  26083.75672212  .00007961  00000-0  13041-2 0  9998
2 26654  98.6427 191.2765 0081078 307.0725  52.3085 14.68868517338461

Epoch: 2026-03-24T18:09Z

TLE epoch observation values (Epoch: 2026-03-24T18:09:40.791Z)

Latitude

0.00004°

Longitude

96.62673°

Altitude

633.038 km

Speed

7.56 km/s

True Right ascension

12h 45m 06s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

19:31:38

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

718.851 km

Perigee altitude

604.694 km

Semi-major axis

7,039.91 km

Eccentricity

0.00811

Inclination

98.6427°

RAAN

191.2765°

Arg. of periapsis

307.0725°

True anomaly

53.04826°

Mean anomaly

52.3085°

Eccentric anomaly

52.67792°

Mean motion

3.67445 °/min

Orbital period

97.97 mins

BSTAR

0.0013041

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

CZ-4 DEB, 26458 (Decayed)

CZ-4 DEB, 26343 (Decayed)

CZ-4 DEB, 26651 (Decayed)

CZ-4 DEB, 35328 (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.
8 mins	2026-03-25 19:15:52.807Z	37.659° NE	2026-03-25 19:19:52.807Z	99.547° ESE	26.763°	2026-03-25 19:23:52.807Z	157.711° S
6 mins	2026-03-25 20:53:52.807Z	339.089° N	2026-03-25 20:56:52.807Z	285.453° WNW	25.407°	2026-03-25 20:59:52.807Z	239.838° WSW
6 mins	2026-03-26 06:16:52.807Z	114.594° SE	2026-03-26 06:19:52.807Z	57.438° ENE	24.95°	2026-03-26 06:22:52.807Z	12.948° NNE
6 mins	2026-03-26 07:53:52.807Z	218.811° SW	2026-03-26 07:55:52.807Z	254.287° W	24.317°	2026-03-26 07:59:52.807Z	319.798° NNW

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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, 26654 on other resources

View CZ-4 DEB, 26654 on Heavens-Above

View CZ-4 DEB, 26654 on Keep Track

View CZ-4 DEB, 26654 on Celestrak

View CZ-4 DEB, 26654 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, 26654

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 20 hours ago

TLE from 20 hours ago

TLE epoch observation values (Epoch: 2026-03-24T18:09:40.791Z)

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, 26654 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 20 hours ago