CZ-4 DEB, 28068

Orbit data source: Space-Track

CZ-4 DEB, 28068 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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https://www.satcat.com/sats-embedded/28068?theme=dark&initialShowStats=false

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Identifier

28068, 1999-057MY

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, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 CZ-4 DEB
1 28068U 99057MY  26083.62542508  .00001916  00000-0  45447-3 0  9999
2 28068  98.5029 147.8924 0080226 139.6582 221.0603 14.53213299671924

Epoch: 2026-03-24T15:00Z

TLE epoch observation values (Epoch: 2026-03-24T15:00:36.726Z)

Latitude

0.00001°

Longitude

100.63898°

Altitude

761.253 km

Speed

7.451 km/s

True Right ascension

09h 51m 34s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

22:47:21

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

769.161 km

Perigee altitude

655.393 km

Semi-major axis

7,090.414 km

Eccentricity

0.00802

Inclination

98.5029°

RAAN

147.8924°

Arg. of periapsis

139.6582°

True anomaly

220.46098°

Mean anomaly

221.0603°

Eccentric anomaly

220.76019°

Mean motion

3.63526 °/min

Orbital period

99.03 mins

BSTAR

0.00045447

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

CZ-4 DEB, 26343 (Decayed)

CZ-4 DEB, 26651 (Decayed)

CZ-4 DEB, 26657 (Decayed)

CZ-4 DEB, 26173 (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.
6 mins	2026-03-25 18:01:04.290Z	344.66° N	2026-03-25 18:04:04.290Z	299.057° NW	23.159°	2026-03-25 18:07:04.290Z	245.846° WSW
6 mins	2026-03-26 03:31:04.290Z	121.043° SE	2026-03-26 03:34:04.290Z	59.923° ENE	29.258°	2026-03-26 03:37:04.290Z	11.258° NNE
6 mins	2026-03-26 05:09:04.290Z	222.204° SW	2026-03-26 05:12:04.290Z	271.681° WNW	22.083°	2026-03-26 05:15:04.290Z	314.53° NW
7 mins	2026-03-26 17:10:04.290Z	12.922° NNE	2026-03-26 17:13:04.290Z	3.523° NNE	44.734°	2026-03-26 17:17:04.290Z	195.194° SSW

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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, 28068 on other resources

View CZ-4 DEB, 28068 on Heavens-Above

View CZ-4 DEB, 28068 on Keep Track

View CZ-4 DEB, 28068 on Celestrak

View CZ-4 DEB, 28068 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, 28068

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-03-24T15:00:36.726Z)

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, 28068 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago