CZ-2C R/B, 62078
Orbit data source: Space-Track
CZ-2C R/B, 62078 is space debris in SSO originally from a launch on Sun, 24 Nov 2024 UTC via a CHANG ZHENG 2C launch vehicle 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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62078 intel report (Beta)
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Edit Public Description
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
Launch site
Object type
Shape & HBR
Cyl, 3.7 m
Radar Cross Section
23.715 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 CZ-2C R/B
1 62078U 24218A 25260.95214572 .00005177 00000-0 23827-3 0 9995
2 62078 97.5478 270.6562 0046977 239.8539 119.8036 15.19781036 45047Epoch: 2025-09-17T22:51Z
TLE epoch observation values (Epoch: 2025-09-17T22:51:05.39Z)
Latitude
-0.00005°
Longitude
-69.23697°
Altitude
525.78 km
Speed
7.591 km/s
True Right ascension
18h 02m 37s
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
03:39:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.802 km
Perigee altitude
471.146 km
Semi-major axis
6,881.611 km
Eccentricity
0.0047
Inclination
97.5478°
RAAN
270.6562°
Arg. of periapsis
239.8539°
True anomaly
120.26935°
Mean anomaly
119.8036°
Eccentric anomaly
120.03661°
Mean motion
3.80196 °/min
Orbital period
94.69 mins
BSTAR
0.00023827
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Other satellites on launch #218 in the year 2024 (2024-11-24 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-18 13:38:17.930Z | 11.153° NNE | 2025-09-18 13:41:17.930Z | 334.997° NNW | 44.867° | 2025-09-18 13:44:17.930Z | 194.603° SSW |
| 5 mins | 2025-09-19 00:17:17.930Z | 123.424° SE | 2025-09-19 00:19:17.930Z | 66.071° ENE | 30.668° | 2025-09-19 00:22:17.930Z | 7.72° NNE |
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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