CZ-2C R/B, 63127
Orbit data source: Space-Track
CZ-2C R/B, 63127 is space debris in SSO originally from a launch on Thu, 27 Feb 2025 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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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63127 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
~3,800 kg wet, ~3,800 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 3.6 m
Radar Cross Section
23.715 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 CZ-2C R/B
1 63127U 25040C 26119.20555259 .00011262 00000-0 31021-3 0 9994
2 63127 97.1690 230.6419 0012182 235.1544 124.8556 15.37227515 65141Epoch: 2026-04-29T04:55Z
TLE epoch observation values (Epoch: 2026-04-29T04:55:59.743Z)
Latitude
-0.00005°
Longitude
-60.52687°
Altitude
462.197 km
Speed
7.633 km/s
True Right ascension
15h 22m 34s
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
23:40:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.565 km
Perigee altitude
442.925 km
Semi-major axis
6,829.382 km
Eccentricity
0.00122
Inclination
97.169°
RAAN
230.6419°
Arg. of periapsis
235.1544°
True anomaly
124.97005°
Mean anomaly
124.8556°
Eccentric anomaly
124.91284°
Mean motion
3.84566 °/min
Orbital period
93.61 mins
BSTAR
0.00031021
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Other satellites on launch #40 in the year 2025 (2025-02-27 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-2C 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-29 19:34:24.495Z | 51.94° ENE | 2026-04-29 19:36:24.495Z | 97.064° ESE | 20.647° | 2026-04-29 19:38:24.495Z | 140.744° SSE |
| 4 mins | 2026-04-30 07:38:24.495Z | 186.913° SSW | 2026-04-30 07:39:24.495Z | 214.141° SW | 39.578° | 2026-04-30 07:42:24.495Z | 339.224° N |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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