CZ-3A R/B, 26383

Orbit data source: Space-Track

CZ-3A R/B, 26383 is space debris in HEO originally from a launch on Sun, 25 Jun 2000 UTC launched from the Xichang Space Center, China (XSC). 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/26383?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26383, 2000-032B

Orbit

HEO

Last TLE update

1 day ago

Origin

China Aerospace Science and Technology Corporation (CASC) (CN / PRC)

Manufacturer

CALT

Mission

Spacecraft

Bus & Motor

CZ-3 STAGE 3, Unknown motor

Mass

~2,000 kg wet, 2,000 kg dry

Launch date (UTC)

2000-06-25 (25 years ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 7.5 m

Radar Cross Section

15.242 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 CZ-3A R/B
1 26383U 00032B   25128.68111907  .00015784  00000-0  15916-2 0  9997
2 26383  27.3379  40.4152 5849067 326.7150   7.4407  4.30246340286952

Epoch: 2025-05-08T16:20Z

Definitive object data (Epoch: 2025-05-08T16:20:48.687Z)

Latitude

0.00003°

Longitude

-71.55048°

Altitude

675.223 km

Speed

9.384 km/s

True Right ascension

02h 41m 36s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

19.62164°

Longitude

64.11831°

Altitude

17,756.321 km

Speed

2.841 km/s

Apparent Right ascension

11h 55m 34s

Apparent Declination

8° 19' 27"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

00:48:29

Azimuth

17.25° NNE

Elevation

-40.232°

Doppler factor

Orbital elements

Apogee altitude

18,935.65 km

Perigee altitude

251.644 km

Semi-major axis

15,971.784 km

Eccentricity

0.5849067

Inclination

27.3379°

RAAN

40.4152°

Arg. of periapsis

326.715°

True anomaly

33.55289°

Mean anomaly

7.4407°

Eccentric anomaly

17.54106°

Mean motion

1.07526 °/min

BSTAR

0.0015916

Orbital period

334.8 mins

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Other satellites on launch #32 in the year 2000 (2000-06-25 UTC)

FENGYUN 2B, 26382

FENGYUN 2B AKM, 26460

CZ-3A R/B 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.
76 mins	2025-05-09 20:20:58.700Z	186.678° SSW	2025-05-09 20:30:58.700Z	128.674° SE	28.841°	2025-05-09 21:36:58.700Z	80.728° E
254 mins	2025-05-10 02:12:58.700Z	266.622° W	2025-05-10 03:17:58.700Z	206.463° SW	42.034°	2025-05-10 06:26:58.700Z	153.113° SSE

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Check out CZ-3A R/B, 26383 on other resources

View CZ-3A R/B, 26383 on Heavens-Above

View CZ-3A R/B, 26383 on Keep Track

View CZ-3A R/B, 26383 on Celestrak

View CZ-3A R/B, 26383 on Gunter's Space Page

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