CZ-4 DEB, 26155

Orbit data source: Space-Track

CZ-4 DEB, 26155 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/26155?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26155, 1999-057AR

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, 0.071 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago

0 CZ-4 DEB
1 26155U 99057AR  26277.44384440  .00004552  00000-0  76028-3 0  9996
2 26155  98.5270 347.0440 0118541 152.2258 273.0452 14.65853724385418

Epoch: 2026-10-04T10:39Z

TLE epoch observation values (Epoch: 2026-10-04T10:39:08.156Z)

Latitude

62.74323°

Longitude

157.29739°

Altitude

681.638 km

Speed

7.524 km/s

True Right ascension

22h 00m 52s

True Declination

62° 36' 05"

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

13:49:35

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

754.99 km

Perigee altitude

587.858 km

Semi-major axis

7,049.561 km

Eccentricity

0.01185

Inclination

98.527°

RAAN

347.044°

Arg. of periapsis

152.2258°

True anomaly

271.6878°

Mean anomaly

273.0452°

Eccentric anomaly

272.36659°

Mean motion

3.66691 °/min

Orbital period

98.18 mins

BSTAR

0.00076028

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

CZ-4 DEB, 26315 (Decayed)

CZ-4 DEB, 35319

CBERS 1 DEB, 30780 (Decayed)

CZ-4 DEB, 27806

CZ-4 DEB, 26344 (Decayed)

CZ-4 DEB, 26423 (Decayed)

CZ-4 DEB, 26449

CZ-4 DEB, 29039

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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	2026-10-05 04:29:59.309Z	153.905° SSE	2026-10-05 04:33:59.309Z	83.646° E	65.574°	2026-10-05 04:37:59.309Z	354.3° N
6 mins	2026-10-05 18:03:59.309Z	356.191° N	2026-10-05 18:06:59.309Z	276.394° WNW	48.923°	2026-10-05 18:09:59.309Z	216.107° SW

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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, 26155 on other resources

View CZ-4 DEB, 26155 on Heavens-Above

View CZ-4 DEB, 26155 on Keep Track

View CZ-4 DEB, 26155 on Celestrak

View CZ-4 DEB, 26155 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, 26155

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-10-04T10:39:08.156Z)

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, 26155 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 9 hours ago