SZ-18 MODULE, 62077 (Decayed)
Orbit data source: Space-Track
SZ-18 MODULE, 62077 was a payload satellite owned by ZZHGB (CN) in LEO that was launched on Thu, 25 Apr 2024 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62077 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 SZ-18 MODULE
1 62077U 24078F 25169.73508573 .11307513 83951-5 12143-3 0 9990
2 62077 41.4466 328.7904 0008290 307.1589 179.4785 16.49966653 35671Epoch: 2025-06-18T17:38Z
TLE epoch observation values (Epoch: 2025-06-18T17:38:31.407Z)
Latitude
32.21343°
Longitude
-68.23736°
Altitude
145.532 km
Speed
7.821 km/s
True Right ascension
06h 54m 25s
True Declination
32° 02' 38"
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
18:24:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
147.149 km
Perigee altitude
136.339 km
Semi-major axis
6,519.881 km
Eccentricity
0.00083
Inclination
41.4466°
RAAN
328.7904°
Arg. of periapsis
307.1589°
True anomaly
179.47936°
Mean anomaly
179.4785°
Eccentric anomaly
179.47893°
Mean motion
4.12272 °/min
Orbital period
87.32 mins
BSTAR
0.00012143
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Other satellites on launch #78 in the year 2024 (2024-04-25 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.SZ-18 MODULE Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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