CZ-4 DEB, 27678

Orbit data source: Space-Track

CZ-4 DEB, 27678 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/27678?theme=dark&initialShowStats=false

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Identifier

27678, 1999-057MS

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: 2 days ago

TLE from 2 days ago

0 CZ-4 DEB
1 27678U 99057MS  26224.35698161  .00000049  00000-0  32730-4 0  9997
2 27678  98.8332 265.7271 0106062 215.0599 157.2406 14.33932341265169

Epoch: 2026-08-12T08:34Z

TLE epoch observation values (Epoch: 2026-08-12T08:34:03.211Z)

Latitude

12.57194°

Longitude

174.42603°

Altitude

850.917 km

Speed

7.392 km/s

True Right ascension

17h 35m 00s

True Declination

12° 30' 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

03:04:27

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

851.638 km

Perigee altitude

699.886 km

Semi-major axis

7,153.899 km

Eccentricity

0.01061

Inclination

98.8332°

RAAN

265.7271°

Arg. of periapsis

215.0599°

True anomaly

157.7051°

Mean anomaly

157.2406°

Eccentric anomaly

157.47341°

Mean motion

3.58698 °/min

Orbital period

100.36 mins

BSTAR

0.00003273

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

CZ-4 DEB, 26327 (Decayed)

CZ-4 DEB, 26237 (Decayed)

CZ-4 DEB, 26270 (Decayed)

CZ-4 DEB, 35325 (Decayed)

CZ-4 DEB, 26323

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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.
7 mins	2026-08-14 14:42:08.962Z	45.951° ENE	2026-08-14 14:46:08.962Z	100.231° ESE	19.66°	2026-08-14 14:49:08.962Z	140.205° SSE
7 mins	2026-08-14 16:22:08.962Z	349.591° N	2026-08-14 16:25:08.962Z	290.861° WNW	33.426°	2026-08-14 16:29:08.962Z	224.121° SW
8 mins	2026-08-15 01:58:08.962Z	120.997° SE	2026-08-15 02:01:08.962Z	77.188° E	28.748°	2026-08-15 02:06:08.962Z	6.545° NNE
8 mins	2026-08-15 03:37:08.962Z	209.299° SW	2026-08-15 03:41:08.962Z	272.697° WNW	27.803°	2026-08-15 03:45:08.962Z	323.521° NNW

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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, 27678 on other resources

View CZ-4 DEB, 27678 on Heavens-Above

View CZ-4 DEB, 27678 on Keep Track

View CZ-4 DEB, 27678 on Celestrak

View CZ-4 DEB, 27678 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, 27678

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-08-12T08:34:03.211Z)

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, 27678 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago