CZ-4 DEB, 28075

Orbit data source: Space-Track

CZ-4 DEB, 28075 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/28075?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28075, 1999-057NF

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

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago

0 CZ-4 DEB
1 28075U 99057NF  26142.13501043  .00000582  00000-0  17757-3 0  9999
2 28075  98.6211 206.2390 0094470 266.2197  92.8187 14.43351860730437

Epoch: 2026-05-22T03:14Z

TLE epoch observation values (Epoch: 2026-05-22T03:14:24.901Z)

Latitude

0°

Longitude

-82.13497°

Altitude

754.34 km

Speed

7.475 km/s

True Right ascension

13h 44m 57s

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

01:36:40

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

811.856 km

Perigee altitude

677.28 km

Semi-major axis

7,122.705 km

Eccentricity

0.00945

Inclination

98.6211°

RAAN

206.239°

Arg. of periapsis

266.2197°

True anomaly

93.89925°

Mean anomaly

92.8187°

Eccentric anomaly

93.35904°

Mean motion

3.61057 °/min

Orbital period

99.71 mins

BSTAR

0.00017757

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

CBERS 1 DEB, 30782 (Decayed)

CZ-4 DEB, 26653 (Decayed)

CZ-4 DEB, 35331

CZ-4 DEB, 26441 (Decayed)

CBERS 1 DEB, 35385 (Decayed)

CZ-4 DEB, 26182 (Decayed)

CZ-4 DEB, 26232 (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.
10 mins	2026-05-24 17:22:00.209Z	8.678° NNE	2026-05-24 17:27:00.209Z	287.152° WNW	43.417°	2026-05-24 17:32:00.209Z	203.207° SW
5 mins	2026-05-25 02:58:00.209Z	86.188° E	2026-05-25 03:00:00.209Z	58.288° ENE	17.429°	2026-05-25 03:03:00.209Z	22.476° NNE
9 mins	2026-05-25 04:34:00.209Z	183.766° SSW	2026-05-25 04:38:00.209Z	270.018° WNW	40.345°	2026-05-25 04:43:00.209Z	338.647° N

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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, 28075 on other resources

View CZ-4 DEB, 28075 on Heavens-Above

View CZ-4 DEB, 28075 on Keep Track

View CZ-4 DEB, 28075 on Celestrak

View CZ-4 DEB, 28075 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, 28075

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-05-22T03:14:24.901Z)

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, 28075 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago