CZ-4 DEB, 26125

Orbit data source: Space-Track

CZ-4 DEB, 26125 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/26125?theme=dark&initialShowStats=false

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Identifier

26125, 1999-057M

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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago

0 CZ-4 DEB
1 26125U 99057M   26226.06957355  .00000568  00000-0  25612-3 0  9992
2 26125  99.2135 266.0919 0237084 120.9277 272.0251 14.12343279350960

Epoch: 2026-08-14T01:40Z

TLE epoch observation values (Epoch: 2026-08-14T01:40:11.154Z)

Latitude

29.85731°

Longitude

-86.76907°

Altitude

853.073 km

Speed

7.43 km/s

True Right ascension

17h 23m 06s

True Declination

29° 42' 40"

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

03:05:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,019.889 km

Perigee altitude

677.222 km

Semi-major axis

7,226.692 km

Eccentricity

0.02371

Inclination

99.2135°

RAAN

266.0919°

Arg. of periapsis

120.9277°

True anomaly

269.30819°

Mean anomaly

272.0251°

Eccentric anomaly

270.6668°

Mean motion

3.53292 °/min

Orbital period

101.9 mins

BSTAR

0.00025612

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

CZ-4 DEB, 26327 (Decayed)

CZ-4 DEB, 26237 (Decayed)

CZ-4 DEB, 26270 (Decayed)

CZ-4 DEB, 35325 (Decayed)

CZ-4 DEB, 26323

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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	2026-08-14 15:42:05.032Z	14.103° NNE	2026-08-14 15:46:05.032Z	11.595° NNE	44.884°	2026-08-14 15:50:05.032Z	195.622° SSW
6 mins	2026-08-15 01:30:05.032Z	99.036° ESE	2026-08-15 01:32:05.032Z	72.234° E	19.406°	2026-08-15 01:36:05.032Z	18.876° NNE
8 mins	2026-08-15 03:09:05.032Z	190.199° SSW	2026-08-15 03:13:05.032Z	264.344° W	36.805°	2026-08-15 03:17:05.032Z	330.483° 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, 26125 on other resources

View CZ-4 DEB, 26125 on Heavens-Above

View CZ-4 DEB, 26125 on Keep Track

View CZ-4 DEB, 26125 on Celestrak

View CZ-4 DEB, 26125 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, 26125

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-08-14T01:40:11.154Z)

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, 26125 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago