CZ-4 DEB, 26152

Orbit data source: Space-Track

CZ-4 DEB, 26152 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/26152?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26152, 1999-057AN

Orbit

SSO

Last TLE update

17 hours 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 17 hours ago

0 CZ-4 DEB
1 26152U 99057AN  25184.58810058  .00000047  00000-0  69648-4 0  9999
2 26152  99.1572 221.0195 0520972  98.5838  26.6928 13.38091997231523

Epoch: 2025-07-03T14:06Z

TLE epoch observation values (Epoch: 2025-07-03T14:06:51.89Z)

Latitude

51.05887°

Longitude

-81.10546°

Altitude

780.009 km

Speed

7.639 km/s

True Right ascension

03h 29m 51s

True Declination

50° 53' 28"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

15.78486°

Longitude

85.5098°

Altitude

1,036.193 km

Speed

7.375 km/s

Apparent Right ascension

11h 57m 16s

Apparent Declination

-15° 52' 07"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

19:22:27

Azimuth

270.923° WNW

Elevation

-26.32°

Doppler factor

Orbital elements

Apogee altitude

1,503.977 km

Perigee altitude

723.372 km

Semi-major axis

7,491.811 km

Eccentricity

0.0521

Inclination

99.1572°

RAAN

221.0195°

Arg. of periapsis

98.5838°

True anomaly

Unknown

Mean anomaly

26.6928°

Eccentric anomaly

Unknown

Mean motion

3.34706 °/min

Orbital period

107.56 mins

BSTAR

0.000069648

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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, 26150

CZ-4 DEB, 26151

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.
10 mins	2025-07-04 15:12:39.076Z	18.459° NNE	2025-07-04 15:17:39.076Z	124.299° SE	43.635°	2025-07-04 15:22:39.076Z	188.366° SSW
8 mins	2025-07-05 01:33:39.076Z	122.34° SE	2025-07-05 01:36:39.076Z	79.96° E	29.18°	2025-07-05 01:41:39.076Z	5.921° NNE
8 mins	2025-07-05 03:19:39.076Z	211.938° SW	2025-07-05 03:23:39.076Z	267.515° W	25.427°	2025-07-05 03:27:39.076Z	319.512° NNW

Authenticating...

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Check out CZ-4 DEB, 26152 on other resources

View CZ-4 DEB, 26152 on Heavens-Above

View CZ-4 DEB, 26152 on Keep Track

View CZ-4 DEB, 26152 on Celestrak

View CZ-4 DEB, 26152 on Gunter's Space Page

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