CZ-4 DEB, 26194

Orbit data source: Space-Track

CZ-4 DEB, 26194 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/26194?theme=dark&initialShowStats=false

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Identifier

26194, 1999-057CG

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, 0.2 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

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

TLE from 1 day ago

0 CZ-4 DEB
1 26194U 99057CG  26276.40396977  .00001160  00000-0  19035-3 0  9999
2 26194  98.1947 236.7446 0041777 351.2680 161.2484 14.72106529660831

Epoch: 2026-10-03T09:41Z

TLE epoch observation values (Epoch: 2026-10-03T09:41:42.988Z)

Latitude

27.06805°

Longitude

-96.59904°

Altitude

685.564 km

Speed

7.501 km/s

True Right ascension

04h 03m 46s

True Declination

26° 55' 39"

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

09:55:54

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

680.783 km

Perigee altitude

622.049 km

Semi-major axis

7,029.553 km

Eccentricity

0.00418

Inclination

98.1947°

RAAN

236.7446°

Arg. of periapsis

351.268°

True anomaly

161.40154°

Mean anomaly

161.2484°

Eccentric anomaly

161.32504°

Mean motion

3.68258 °/min

Orbital period

97.76 mins

BSTAR

0.00019035

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

CBERS 1 DEB, 32078 (Decayed)

CZ-4 DEB, 26195 (Decayed)

CBERS 1 DEB, 34216 (Decayed)

CBERS 1 DEB, 34218 (Decayed)

CZ-4 DEB, 35320

CBERS 1 DEB, 30780 (Decayed)

CZ-4 DEB, 26344 (Decayed)

CZ-4 DEB, 26423 (Decayed)

CZ-4 DEB, 26349 (Decayed)

CZ-4 DEB, 26318 (Decayed)

CZ-4 DEB, 26351

CZ-4 DEB, 35333 (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	2026-10-04 21:00:56.578Z	142.777° SSE	2026-10-04 21:04:56.578Z	65.762° ENE	44.903°	2026-10-04 21:08:56.578Z	0.335° NNE
9 mins	2026-10-05 10:29:56.578Z	9.15° NNE	2026-10-05 10:33:56.578Z	333.972° NNW	68.14°	2026-10-05 10:38:56.578Z	200.283° 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, 26194 on other resources

View CZ-4 DEB, 26194 on Heavens-Above

View CZ-4 DEB, 26194 on Keep Track

View CZ-4 DEB, 26194 on Celestrak

View CZ-4 DEB, 26194 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, 26194

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: 2026-10-03T09:41:42.988Z)

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, 26194 on other resources

Documentation

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