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

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

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 16 hours ago

0 CZ-4 DEB
1 26152U 99057AN  25132.62230571  .00000606  00000-0  55875-3 0  9990
2 26152  99.1602 173.9494 0519261 227.6729 262.7209 13.38064110224521

Epoch: 2025-05-12T14:56Z

Definitive object data (Epoch: 2025-05-12T14:56:07.213Z)

Latitude

54.498°

Longitude

-87.71593°

Altitude

1,194.383 km

Speed

7.228 km/s

True Right ascension

00h 27m 47s

True Declination

54° 20' 41"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

29.7574°

Longitude

74.61282°

Altitude

1,492.815 km

Speed

6.941 km/s

Apparent Right ascension

08h 17m 51s

Apparent Declination

-1° 49' 38"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

14:59:19

Azimuth

275.283° WNW

Elevation

-9.112°

Doppler factor

Orbital elements

Apogee altitude

1,502.805 km

Perigee altitude

724.753 km

Semi-major axis

7,491.916 km

Eccentricity

0.0519261

Inclination

99.1602°

RAAN

173.9494°

Arg. of periapsis

227.6729°

True anomaly

256.87686°

Mean anomaly

262.7209°

Eccentric anomaly

259.79284°

Mean motion

3.34699 °/min

BSTAR

0.00055875

Orbital period

107.56 mins

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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.
8 mins	2025-05-13 14:16:41.413Z	47.622° ENE	2025-05-13 14:20:41.413Z	87.305° E	19.517°	2025-05-13 14:24:41.413Z	131.485° SE
11 mins	2025-05-13 16:01:41.413Z	6.094° NNE	2025-05-13 16:07:41.413Z	286.877° WNW	41.39°	2025-05-13 16:12:41.413Z	212.981° SW
8 mins	2025-05-14 00:34:41.413Z	81.191° E	2025-05-14 00:38:41.413Z	50.587° ENE	16.889°	2025-05-14 00:42:41.413Z	21.036° NNE
15 mins	2025-05-14 02:15:41.413Z	151.755° SSE	2025-05-14 02:22:41.413Z	84.638° E	43.409°	2025-05-14 02:30:41.413Z	351.036° N
12 mins	2025-05-14 04:03:41.413Z	219.622° SW	2025-05-14 04:09:41.413Z	270.793° WNW	24.747°	2025-05-14 04:15:41.413Z	319.213° 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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