CZ-7A R/B, 66314
Orbit data source: Space-Track
CZ-7A R/B, 66314 is space debris 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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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 CZ-7A R/B
1 66314U 25250B 25308.78056345 .04554797 -13031-4 51460-3 0 9993
2 66314 19.9260 116.0532 3555489 130.5060 266.3968 8.58954420 196Epoch: 2025-11-04T18:44Z
TLE epoch observation values (Epoch: 2025-11-04T18:44:00.682Z)
Latitude
0.00001°
Longitude
150.7877°
Altitude
5,057.627 km
Speed
5.491 km/s
True Right ascension
07h 44m 12s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
17:57:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
7,280.099 km
Perigee altitude
115.222 km
Semi-major axis
10,075.797 km
Eccentricity
0.35555
Inclination
19.926°
RAAN
116.0532°
Arg. of periapsis
130.506°
True anomaly
229.52731°
Mean anomaly
266.3968°
Eccentric anomaly
247.56694°
Mean motion
2.14597 °/min
Orbital period
167.76 mins
BSTAR
0.0005146
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Other satellites on launch #250 in the year 2025 (2025-11-03 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.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. |
|---|---|---|---|---|---|---|---|
| 42 mins | 2025-11-08 09:50:35.925Z | 195.403° SSW | 2025-11-08 10:15:35.925Z | 162.515° S | 18.305° | 2025-11-08 10:32:35.925Z | 127.071° SE |
| 32 mins | 2025-11-08 12:56:35.925Z | 221.511° SW | 2025-11-08 13:18:35.925Z | 178.379° S | 24.131° | 2025-11-08 13:28:35.925Z | 131.025° SE |
| 12 mins | 2025-11-08 16:05:35.925Z | 232.263° WSW | 2025-11-08 16:12:35.925Z | 201.589° SSW | 17.926° | 2025-11-08 16:17:35.925Z | 157.238° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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