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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ISO8601 Format

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 (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 27678U 99057MS  26083.34310337  .00000155  00000-0  68658-4 0  9991
2 27678  98.8477 121.6025 0105660 269.6117 152.9011 14.33880624244954

Epoch: 2026-03-24T08:14Z

TLE epoch observation values (Epoch: 2026-03-24T08:14:04.131Z)

Latitude

61.83974°

Longitude

159.4495°

Altitude

856.838 km

Speed

7.395 km/s

True Right ascension

06h 59m 09s

True Declination

61° 41' 54"

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

15:44:29

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

851.525 km

Perigee altitude

700.345 km

Semi-major axis

7,154.072 km

Eccentricity

0.01057

Inclination

98.8477°

RAAN

121.6025°

Arg. of periapsis

269.6117°

True anomaly

153.44622°

Mean anomaly

152.9011°

Eccentric anomaly

153.1743°

Mean motion

3.58685 °/min

Orbital period

100.37 mins

BSTAR

0.000068658

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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, 26754 (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.
9 mins	2026-03-25 14:40:21.607Z	33.248° NE	2026-03-25 14:45:21.607Z	106.046° ESE	29.588°	2026-03-25 14:49:21.607Z	160.257° S
7 mins	2026-03-25 16:21:21.607Z	337.605° N	2026-03-25 16:24:21.607Z	287.463° WNW	26.241°	2026-03-25 16:28:21.607Z	236.228° WSW
9 mins	2026-03-26 01:56:21.607Z	138.896° SSE	2026-03-26 02:00:21.607Z	66.776° ENE	37.025°	2026-03-26 02:05:21.607Z	357.874° N
6 mins	2026-03-26 03:37:21.607Z	233.99° WSW	2026-03-26 03:39:21.607Z	261.612° W	19.683°	2026-03-26 03:43:21.607Z	312.19° NW

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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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-03-24T08:14:04.131Z)

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: 1 day ago