CZ-4 DEB, 26151

Orbit data source: Space-Track

CZ-4 DEB, 26151 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/26151?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26151, 1999-057AM

Orbit

SSO

Last TLE update

16 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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 16 hours ago

0 CZ-4 DEB
1 26151U 99057AM  25199.85272102 -.00000033  00000-0  80376-5 0  9994
2 26151  99.4173 161.8400 0610162 239.6307 143.9844 13.18655728214901

Epoch: 2025-07-18T20:27Z

TLE epoch observation values (Epoch: 2025-07-18T20:27:55.096Z)

Latitude

27.1167°

Longitude

-86.88671°

Altitude

1,575.659 km

Speed

6.901 km/s

True Right ascension

10h 27m 57s

True Declination

26° 59' 30"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-49.59409°

Longitude

87.37482°

Altitude

750.946 km

Speed

7.702 km/s

Apparent Right ascension

17h 13m 08s

Apparent Declination

-69° 57' 57"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

00:54:39

Azimuth

206.297° SW

Elevation

-45.68°

Doppler factor

Orbital elements

Apogee altitude

1,648.78 km

Perigee altitude

725.567 km

Semi-major axis

7,565.31 km

Eccentricity

0.06102

Inclination

99.4173°

RAAN

161.84°

Arg. of periapsis

239.6307°

True anomaly

147.85338°

Mean anomaly

143.9844°

Eccentric anomaly

145.94224°

Mean motion

3.2984 °/min

Orbital period

109.14 mins

BSTAR

0.0000080376

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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, 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.
15 mins	2025-07-19 20:06:58.102Z	122.248° SE	2025-07-19 20:14:58.102Z	56.765° ENE	31.279°	2025-07-19 20:21:58.102Z	2.807° NNE
16 mins	2025-07-19 21:53:58.102Z	183.125° SSW	2025-07-19 22:01:58.102Z	271.033° WNW	40.961°	2025-07-19 22:09:58.102Z	337.463° NNW
11 mins	2025-07-20 09:24:58.102Z	34.576° NE	2025-07-20 09:30:58.102Z	95.631° ESE	29.612°	2025-07-20 09:35:58.102Z	153.132° SSE
11 mins	2025-07-20 11:12:58.102Z	357.98° N	2025-07-20 11:18:58.102Z	286.593° WNW	35.078°	2025-07-20 11:23:58.102Z	229.012° WSW

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, 26151 on other resources

View CZ-4 DEB, 26151 on Heavens-Above

View CZ-4 DEB, 26151 on Keep Track

View CZ-4 DEB, 26151 on Celestrak

View CZ-4 DEB, 26151 on Gunter's Space Page

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