CZ-4 DEB, 26286

Orbit data source: Space-Track

CZ-4 DEB, 26286 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/26286?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26286, 1999-057FY

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: 1 day ago

TLE from 1 day ago

0 CZ-4 DEB
1 26286U 99057FY  25349.11190133  .00002359  00000-0  45591-3 0  9992
2 26286  98.4110  46.2744 0060982 103.4504 287.6005 14.63209201360283

Epoch: 2025-12-15T02:41Z

TLE epoch observation values (Epoch: 2025-12-15T02:41:08.274Z)

Latitude

30.07584°

Longitude

-82.91091°

Altitude

673.863 km

Speed

7.53 km/s

True Right ascension

02h 45m 33s

True Declination

29° 55' 31"

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

01:17:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

722.959 km

Perigee altitude

636.876 km

Semi-major axis

7,058.054 km

Eccentricity

0.0061

Inclination

98.411°

RAAN

46.2744°

Arg. of periapsis

103.4504°

True anomaly

286.93289°

Mean anomaly

287.6005°

Eccentric anomaly

287.26685°

Mean motion

3.66029 °/min

Orbital period

98.35 mins

BSTAR

0.00045591

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

CZ-4 DEB, 26426 (Decayed)

CBERS 1 DEB, 32073 (Decayed)

CZ-4 DEB, 26290 (Decayed)

CZ-4 DEB, 26336

CZ-4 DEB, 26654

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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.
7 mins	2025-12-16 03:17:33.850Z	133.308° SE	2025-12-16 03:21:33.850Z	69.488° E	28.971°	2025-12-16 03:24:33.850Z	13.077° NNE
5 mins	2025-12-16 04:56:33.850Z	225.957° WSW	2025-12-16 04:58:33.850Z	258.079° W	20.141°	2025-12-16 05:01:33.850Z	307.565° NW
7 mins	2025-12-16 16:52:33.850Z	15.337° NNE	2025-12-16 16:55:33.850Z	97.923° ESE	44.886°	2025-12-16 16:59:33.850Z	192.279° SSW

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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, 26286 on other resources

View CZ-4 DEB, 26286 on Heavens-Above

View CZ-4 DEB, 26286 on Keep Track

View CZ-4 DEB, 26286 on Celestrak

View CZ-4 DEB, 26286 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, 26286

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2025-12-15T02:41:08.274Z)

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, 26286 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago