CZ-4 DEB, 26122

Orbit data source: Space-Track

CZ-4 DEB, 26122 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/26122?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26122, 1999-057J

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, 0.2 m

Radar Cross Section

Small (<0.1 m²)

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

TLE from 8 hours ago

0 CZ-4 DEB
1 26122U 99057J   25349.90860483  .00001513  00000-0  11946-2 0  9997
2 26122  98.9170 128.8592 0525867 162.2560 319.1772 13.42603958255383

Epoch: 2025-12-15T21:48Z

TLE epoch observation values (Epoch: 2025-12-15T21:48:23.457Z)

Latitude

61.49045°

Longitude

-86.34163°

Altitude

821.81 km

Speed

7.59 km/s

True Right ascension

21h 42m 13s

True Declination

61° 20' 50"

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

04:21:36

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,489.942 km

Perigee altitude

703.771 km

Semi-major axis

7,474.993 km

Eccentricity

0.05259

Inclination

98.917°

RAAN

128.8592°

Arg. of periapsis

162.256°

True anomaly

315.03576°

Mean anomaly

319.1772°

Eccentric anomaly

317.12724°

Mean motion

3.35836 °/min

Orbital period

107.2 mins

BSTAR

0.0011946

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

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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.
12 mins	2025-12-16 08:04:35.436Z	120.939° SE	2025-12-16 08:11:35.436Z	58.951° ENE	26.3°	2025-12-16 08:16:35.436Z	10.289° NNE
13 mins	2025-12-16 09:49:35.436Z	182.458° SSW	2025-12-16 09:56:35.436Z	258.801° W	40.481°	2025-12-16 10:02:35.436Z	335.102° NNW
4 mins	2025-12-16 21:08:35.436Z	72.326° E	2025-12-16 21:09:35.436Z	86.45° E	14.904°	2025-12-16 21:12:35.436Z	127.003° SE
8 mins	2025-12-16 22:52:35.436Z	357.098° N	2025-12-16 22:56:35.436Z	276.907° WNW	35.06°	2025-12-16 23:00:35.436Z	218.234° 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, 26122 on other resources

View CZ-4 DEB, 26122 on Heavens-Above

View CZ-4 DEB, 26122 on Keep Track

View CZ-4 DEB, 26122 on Celestrak

View CZ-4 DEB, 26122 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, 26122

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: 2025-12-15T21:48:23.457Z)

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, 26122 on other resources

Documentation

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