CZ-3C R/B, 65487
Orbit data source: Space-Track
CZ-3C R/B, 65487 is space debris in HEO originally from a launch on Fri, 05 Sep 2025 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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65487 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3C 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
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 CZ-3C R/B
1 65487U 25196B 25251.41819693 .00025655 00000-0 33348-2 0 9995
2 65487 28.4934 20.6057 6976947 130.0484 315.6750 2.68841397 106Epoch: 2025-09-08T10:02Z
TLE epoch observation values (Epoch: 2025-09-08T10:02:12.214Z)
Latitude
0.00003°
Longitude
-117.68199°
Altitude
13,947.152 km
Speed
4.58 km/s
True Right ascension
01h 22m 22s
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
00:37:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
30,718.63 km
Perigee altitude
227.614 km
Semi-major axis
21,851.259 km
Eccentricity
0.69769
Inclination
28.4934°
RAAN
20.6057°
Arg. of periapsis
130.0484°
True anomaly
230.15357°
Mean anomaly
315.675°
Eccentric anomaly
275.91271°
Mean motion
0.67194 °/min
Orbital period
535.76 mins
BSTAR
0.0033348
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Other satellites on launch #196 in the year 2025 (2025-09-05 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-3C 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. |
|---|---|---|---|---|---|---|---|
| 59 mins | 2025-09-17 07:52:07.648Z | 169.569° S | 2025-09-17 08:19:07.648Z | 156.451° SSE | 31.98° | 2025-09-17 08:51:07.648Z | 101.362° ESE |
| 143 mins | 2025-09-18 05:29:07.648Z | 199.833° SSW | 2025-09-18 07:52:07.648Z | 211.674° SW | 16.22° | 2025-09-18 07:52:07.648Z | 211.674° SW |
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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