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: 8 hours ago

TLE from 8 hours ago

0 CZ-4 DEB
1 28068U 99057MY  25350.97654693  .00001451  00000-0  35044-3 0  9998
2 28068  98.5219  48.7534 0080663  78.8999 282.1253 14.52757214657744

Epoch: 2025-12-16T23:26Z

TLE epoch observation values (Epoch: 2025-12-16T23:26:13.654Z)

Latitude

-0.00007°

Longitude

-28.65651°

Altitude

708.042 km

Speed

7.508 km/s

True Right ascension

03h 15m 00s

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

06:38:13

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

770.968 km

Perigee altitude

656.558 km

Semi-major axis

7,091.9 km

Eccentricity

0.00807

Inclination

98.5219°

RAAN

48.7534°

Arg. of periapsis

78.8999°

True anomaly

281.21971°

Mean anomaly

282.1253°

Eccentric anomaly

281.67269°

Mean motion

3.63412 °/min

Orbital period

99.06 mins

BSTAR

0.00035044

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

CZ-4 DEB, 26438 (Decayed)

CZ-4 DEB, 26123

CZ-4 DEB, 28073

CBERS 1 DEB, 30790 (Decayed)

CZ-4 DEB, 26458 (Decayed)

CZ-4 DEB, 26333

CZ-4 DEB, 27536

CZ-4 DEB, 26171 (Decayed)

CBERS 1 DEB, 32070 (Decayed)

CBERS 1 DEB, 34207 (Decayed)

CZ-4 DEB, 26455 (Decayed)

CZ-4 DEB, 26308 (Decayed)

CZ-4 DEB, 26433 (Decayed)

CBERS 1 DEB, 30784 (Decayed)

CZ-4 DEB, 26242 (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.
8 mins	2025-12-17 16:31:53.578Z	25.255° NE	2025-12-17 16:35:53.578Z	85.048° E	36.676°	2025-12-17 16:39:53.578Z	171.912° S
7 mins	2025-12-18 03:40:53.578Z	142.088° SSE	2025-12-18 03:43:53.578Z	54.821° ENE	38.82°	2025-12-18 03:47:53.578Z	356.22° 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, 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: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2025-12-16T23:26:13.654Z)

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: 8 hours ago