CZ-7A R/B, 66314

Orbit data source: Space-Track

CZ-7A R/B, 66314 is space debris in LEO originally from a launch on Mon, 03 Nov 2025 UTC launched from the Wenchang Satellite Launch Center (WSC). 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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https://www.satcat.com/sats-embedded/66314?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

66314, 2025-250B

Orbit

LEO

Country

CN / PRC

Related business

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

Manufacturer

CALT

Mission

Spacecraft

Bus & Motor

CZ-3A STAGE 3, Unknown motor

Mass

~2,800 kg wet, ~2,800 kg dry

Launch date (UTC)

2025-11-03 (1 month ago)

Launch vehicle

Unknown

Launch site

Wenchang Satellite Launch Center (WSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

RCS unknown

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 CZ-7A R/B
1 66314U 25250B   25338.49009442  .10512144 -37343-4  67590-3 0  9990
2 66314  19.9433  15.7377 1832158 313.6435  32.5639 12.24733305  3230

Epoch: 2025-12-04T11:45Z

TLE epoch observation values (Epoch: 2025-12-04T11:45:44.157Z)

Latitude

-0.00002°

Longitude

125.75786°

Altitude

441.365 km

Speed

8.173 km/s

True Right ascension

01h 02m 57s

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

13:38:09

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

3,034.284 km

Perigee altitude

119.34 km

Semi-major axis

7,954.949 km

Eccentricity

0.18322

Inclination

19.9433°

RAAN

15.7377°

Arg. of periapsis

313.6435°

True anomaly

46.39606°

Mean anomaly

32.5639°

Eccentric anomaly

39.19839°

Mean motion

3.05905 °/min

Orbital period

117.68 mins

BSTAR

0.0006759

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Other satellites on launch #250 in the year 2025 (2025-11-03 UTC)

OBJECT A, 66313

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CZ-7A 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	2025-12-06 06:25:52.065Z	185.32° SSW	2025-12-06 06:29:52.065Z	154.718° SSE	15.493°	2025-12-06 06:34:52.065Z	126.714° SE
17 mins	2025-12-06 08:24:52.065Z	217.259° SW	2025-12-06 08:31:52.065Z	169.28° S	24.413°	2025-12-06 08:41:52.065Z	125.056° SE
21 mins	2025-12-06 10:25:52.065Z	232.765° WSW	2025-12-06 10:34:52.065Z	185.342° SSW	24.719°	2025-12-06 10:46:52.065Z	138.657° SSE
17 mins	2025-12-06 12:29:52.065Z	233.666° WSW	2025-12-06 12:37:52.065Z	201.507° SSW	17.87°	2025-12-06 12:46:52.065Z	167.187° S

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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-7A R/B, 66314 on other resources

View CZ-7A R/B, 66314 on Heavens-Above

View CZ-7A R/B, 66314 on Keep Track

View CZ-7A R/B, 66314 on Celestrak

View CZ-7A R/B, 66314 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-7A R/B, 66314

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2025-12-04T11:45:44.157Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #250 in the year 2025 (2025-11-03 UTC)

CZ-7A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-7A R/B, 66314 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago