CZ-4 DEB, 26265

Orbit data source: Space-Track

CZ-4 DEB, 26265 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/26265?theme=dark&initialShowStats=false

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Identifier

26265, 1999-057FB

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: 8 hours ago

TLE from 8 hours ago

0 CZ-4 DEB
1 26265U 99057FB  26277.43706111  .00000597  00000-0  18035-3 0  9999
2 26265  98.6241 345.4831 0094718 227.4386 197.5709 14.43717503390579

Epoch: 2026-10-04T10:29Z

TLE epoch observation values (Epoch: 2026-10-04T10:29:22.079Z)

Latitude

63.44034°

Longitude

157.44504°

Altitude

821.531 km

Speed

7.415 km/s

True Right ascension

21h 51m 40s

True Declination

63° 18' 13"

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

12:28:49

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

810.818 km

Perigee altitude

675.911 km

Semi-major axis

7,121.502 km

Eccentricity

0.00947

Inclination

98.6241°

RAAN

345.4831°

Arg. of periapsis

227.4386°

True anomaly

197.2469°

Mean anomaly

197.5709°

Eccentric anomaly

197.40854°

Mean motion

3.61148 °/min

Orbital period

99.68 mins

BSTAR

0.00018035

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

CZ-4 DEB, 26126

CZ-4 DEB, 26125

CZ-4 DEB, 26195 (Decayed)

CBERS 1 DEB, 30780 (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.
4 mins	2026-10-04 19:05:26.792Z	325.579° NNW	2026-10-04 19:07:26.792Z	301.311° NW	13.533°	2026-10-04 19:09:26.792Z	276.246° WNW
9 mins	2026-10-05 04:36:26.792Z	164.585° S	2026-10-05 04:40:26.792Z	1.074° NNE	86.031°	2026-10-05 04:45:26.792Z	346.919° N
6 mins	2026-10-05 16:44:26.792Z	49.463° ENE	2026-10-05 16:47:26.792Z	100.496° ESE	27.424°	2026-10-05 16:50:26.792Z	146.9° SSE
7 mins	2026-10-05 18:22:26.792Z	346.449° N	2026-10-05 18:25:26.792Z	299.961° NW	31.547°	2026-10-05 18:29:26.792Z	234.51° WSW

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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, 26265 on other resources

View CZ-4 DEB, 26265 on Heavens-Above

View CZ-4 DEB, 26265 on Keep Track

View CZ-4 DEB, 26265 on Celestrak

View CZ-4 DEB, 26265 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, 26265

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-10-04T10:29:22.079Z)

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, 26265 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago