CZ-4B R/B, 25942

Orbit data source: Space-Track

CZ-4B R/B, 25942 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/25942?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

25942, 1999-057C

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-4 STAGE 3, Unknown motor

Mass

~1,000 kg wet, ~1,000 kg dry

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

Cyl, 2.5 m

Radar Cross Section

14.536 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 CZ-4B R/B
1 25942U 99057C   26037.07939815  .00000527  00000-0  17951-3 0  9992
2 25942  98.7422  87.1735 0094944 245.4154 113.7117 14.38316754376742

Epoch: 2026-02-06T01:54Z

TLE epoch observation values (Epoch: 2026-02-06T01:54:20.000Z)

Latitude

0.00006°

Longitude

-77.63226°

Altitude

794.815 km

Speed

7.442 km/s

True Right ascension

05h 48m 41s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

17:43:28

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

828.984 km

Perigee altitude

693.417 km

Semi-major axis

7,139.338 km

Eccentricity

0.00949

Inclination

98.7422°

RAAN

87.1735°

Arg. of periapsis

245.4154°

True anomaly

114.70305°

Mean anomaly

113.7117°

Eccentric anomaly

114.20785°

Mean motion

3.59796 °/min

Orbital period

100.06 mins

BSTAR

0.00017951

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

CZ-4 DEB, 26455 (Decayed)

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CZ-4B R/B 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.
9 mins	2026-02-06 15:50:48.633Z	22.58° NE	2026-02-06 15:54:48.633Z	74.096° E	40.059°	2026-02-06 15:59:48.633Z	180.297° SSW
5 mins	2026-02-06 17:31:48.633Z	323.431° NNW	2026-02-06 17:33:48.633Z	296.503° NW	16.467°	2026-02-06 17:36:48.633Z	259.738° W
9 mins	2026-02-07 03:04:48.633Z	158.737° S	2026-02-07 03:08:48.633Z	26.665° NE	43.941°	2026-02-07 03:13:48.633Z	348.997° N
7 mins	2026-02-07 15:14:48.633Z	46.98° ENE	2026-02-07 15:17:48.633Z	90.835° ESE	23.812°	2026-02-07 15:21:48.633Z	148.705° SSE

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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-4B R/B, 25942 on other resources

View CZ-4B R/B, 25942 on Heavens-Above

View CZ-4B R/B, 25942 on Keep Track

View CZ-4B R/B, 25942 on Celestrak

View CZ-4B R/B, 25942 on Gunter's Space Page

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CZ-4B R/B, 25942

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-02-06T01:54:20.000Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

CZ-4B R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4B R/B, 25942 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago