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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Identifier

26151, 1999-057AM

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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago

0 CZ-4 DEB
1 26151U 99057AM  26036.79576407  .00001153  00000-0  11273-2 0  9993
2 26151  99.4425 344.2475 0610270 116.7330 278.5839 13.19087009241520

Epoch: 2026-02-05T19:05Z

TLE epoch observation values (Epoch: 2026-02-05T19:05:54.015Z)

Latitude

27.96333°

Longitude

-83.20995°

Altitude

1,150.455 km

Speed

7.3 km/s

True Right ascension

22h 36m 49s

True Declination

27° 49' 43"

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

07:36:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,647.112 km

Perigee altitude

723.937 km

Semi-major axis

7,563.661 km

Eccentricity

0.06103

Inclination

99.4425°

RAAN

344.2475°

Arg. of periapsis

116.733°

True anomaly

271.60676°

Mean anomaly

278.5839°

Eccentric anomaly

275.10116°

Mean motion

3.29948 °/min

Orbital period

109.11 mins

BSTAR

0.0011273

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

CZ-4 DEB, 26292 (Decayed)

CZ-4 DEB, 26131 (Decayed)

CZ-4 DEB, 26279 (Decayed)

CZ-4 DEB, 26435 (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.
7 mins	2026-02-06 08:18:23.290Z	47.698° ENE	2026-02-06 08:22:23.290Z	105.657° ESE	20.451°	2026-02-06 08:25:23.290Z	144.039° SSE
6 mins	2026-02-06 10:07:23.290Z	339.038° N	2026-02-06 10:09:23.290Z	300.122° NW	28.956°	2026-02-06 10:13:23.290Z	232.865° WSW
6 mins	2026-02-06 18:48:23.290Z	92.231° ESE	2026-02-06 18:51:23.290Z	58.739° ENE	17.664°	2026-02-06 18:54:23.290Z	25.148° NE
11 mins	2026-02-06 20:32:23.290Z	174.913° S	2026-02-06 20:38:23.290Z	258.357° W	42.852°	2026-02-06 20:43:23.290Z	338.233° N

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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, 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

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

CZ-4 DEB, 26151

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-02-05T19:05:54.015Z)

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, 26151 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago