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 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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62078 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, 3.7 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 62078U 24218A 26084.76126927 .00006908 00000-0 28750-3 0 9998
2 62078 97.5410 99.8748 0043578 302.9539 56.7511 15.23210390 73757Epoch: 2026-03-25T18:16Z
TLE epoch observation values (Epoch: 2026-03-25T18:16:13.664Z)
Latitude
-0.00001°
Longitude
2.59793°
Altitude
482.919 km
Speed
7.633 km/s
True Right ascension
06h 39m 29s
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
10:33:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
523.075 km
Perigee altitude
463.188 km
Semi-major axis
6,871.269 km
Eccentricity
0.00436
Inclination
97.541°
RAAN
99.8748°
Arg. of periapsis
302.9539°
True anomaly
57.16997°
Mean anomaly
56.7511°
Eccentric anomaly
56.96041°
Mean motion
3.81055 °/min
Orbital period
94.47 mins
BSTAR
0.0002875
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-26 13:44:44.999Z | 14.792° NNE | 2026-03-26 13:48:44.999Z | 168.618° S | 42.158° | 2026-03-26 13:51:44.999Z | 189.104° SSW |
| 5 mins | 2026-03-27 00:22:44.999Z | 117.379° SE | 2026-03-27 00:24:44.999Z | 67.402° ENE | 25.504° | 2026-03-27 00:27:44.999Z | 11.479° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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