CZ-4 DEB, 26150

Orbit data source: Space-Track

CZ-4 DEB, 26150 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/26150?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26150, 1999-057AL

Orbit

SSO

Last TLE update

1 day ago

Origin

China National Space Administration (CN / PRC)

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

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 CZ-4 DEB
1 26150U 99057AL  25198.73824162  .00000552  00000-0  36316-3 0  9996
2 26150  99.1160 283.6732 0341499 253.4752 275.6379 13.81041466269214

Epoch: 2025-07-17T17:43Z

TLE epoch observation values (Epoch: 2025-07-17T17:43:04.075Z)

Latitude

14.57709°

Longitude

-95.51446°

Altitude

946.22 km

Speed

7.388 km/s

True Right ascension

07h 04m 12s

True Declination

14° 29' 45"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

10.92046°

Longitude

-94.93683°

Altitude

916.028 km

Speed

7.418 km/s

Apparent Right ascension

04h 31m 10s

Apparent Declination

-19° 41' 46"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:05:13

Azimuth

268.842° W

Elevation

-30.29°

Doppler factor

Orbital elements

Apogee altitude

1,207.929 km

Perigee altitude

706.912 km

Semi-major axis

7,335.558 km

Eccentricity

0.03415

Inclination

99.116°

RAAN

283.6732°

Arg. of periapsis

253.4752°

True anomaly

271.73018°

Mean anomaly

275.6379°

Eccentric anomaly

273.6853°

Mean motion

3.45457 °/min

Orbital period

104.21 mins

BSTAR

0.00036316

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

CBERS 1, 25940

CZ-4 DEB, 26138 (Decayed)

CZ-4 DEB, 26139 (Decayed)

CZ-4 DEB, 26140

CZ-4 DEB, 26141 (Decayed)

CZ-4 DEB, 26142

CZ-4 DEB, 26143

CZ-4 DEB, 26144 (Decayed)

CZ-4 DEB, 26145 (Decayed)

CZ-4 DEB, 26148 (Decayed)

CZ-4 DEB, 26149 (Decayed)

CZ-4 DEB, 26151

CZ-4 DEB, 26152

CZ-4 DEB, 26153 (Decayed)

CZ-4 DEB Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-19 03:50:38.837Z	89.76° E	2025-07-19 03:54:38.837Z	53.419° ENE	16.706°	2025-07-19 03:58:38.837Z	19.244° NNE
12 mins	2025-07-19 05:30:38.837Z	160.502° S	2025-07-19 05:36:38.837Z	13.492° NNE	44.379°	2025-07-19 05:42:38.837Z	347.582° N
7 mins	2025-07-19 07:16:38.837Z	241.743° WSW	2025-07-19 07:19:38.837Z	270.371° WNW	16.738°	2025-07-19 07:23:38.837Z	306.476° NW
11 mins	2025-07-19 18:11:38.837Z	24.628° NE	2025-07-19 18:16:38.837Z	87.271° E	40.095°	2025-07-19 18:22:38.837Z	178.4° S
8 mins	2025-07-19 19:55:38.837Z	340.517° N	2025-07-19 19:59:38.837Z	294.299° NW	22.759°	2025-07-19 20:03:38.837Z	251.013° W

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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Authenticating...

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Check out CZ-4 DEB, 26150 on other resources

View CZ-4 DEB, 26150 on Heavens-Above

View CZ-4 DEB, 26150 on Keep Track

View CZ-4 DEB, 26150 on Celestrak

View CZ-4 DEB, 26150 on Gunter's Space Page

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