CZ-4 DEB, 26123

Orbit data source: Space-Track

CZ-4 DEB, 26123 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/26123?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26123, 1999-057K

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, 0.050 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

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

TLE from 20 hours ago

0 CZ-4 DEB
1 26123U 99057K   26277.01645566  .00001002  00000-0  18170-3 0  9994
2 26123  98.6622 295.7898 0052216 289.4506  70.1059 14.67916701406472

Epoch: 2026-10-04T00:23Z

TLE epoch observation values (Epoch: 2026-10-04T00:23:41.769Z)

Latitude

-0.00004°

Longitude

-82.84998°

Altitude

658.356 km

Speed

7.535 km/s

True Right ascension

19h 43m 09s

True Declination

0° 00' 00"

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

13:51:39

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

701.595 km

Perigee altitude

628.044 km

Semi-major axis

7,042.956 km

Eccentricity

0.00522

Inclination

98.6622°

RAAN

295.7898°

Arg. of periapsis

289.4506°

True anomaly

70.66979°

Mean anomaly

70.1059°

Eccentric anomaly

70.38772°

Mean motion

3.67207 °/min

Orbital period

98.04 mins

BSTAR

0.0001817

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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 01:03:03.603Z	151.412° SSE	2026-10-05 01:07:03.603Z	86.044° E	59.709°	2026-10-05 01:11:03.603Z	356.069° N
7 mins	2026-10-05 14:36:03.603Z	1.776° NNE	2026-10-05 14:39:03.603Z	304.006° NW	59.297°	2026-10-05 14:43:03.603Z	210.242° 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, 26123 on other resources

View CZ-4 DEB, 26123 on Heavens-Above

View CZ-4 DEB, 26123 on Keep Track

View CZ-4 DEB, 26123 on Celestrak

View CZ-4 DEB, 26123 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, 26123

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: 2026-10-04T00:23:41.769Z)

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, 26123 on other resources

Documentation

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