QZS-6, 62876
Orbit data source: Space-Track
QZS-6, 62876 is a Japanese payload satellite in GEO that was launched on Sun, 02 Feb 2025 UTC via a H3-22S launch vehicle from the Tanegashima Space Center (TNSTA). 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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62876 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 QZS-6
1 62876U 25023A 25242.86558821 -.00000230 00000-0 00000-0 0 9995
2 62876 0.0571 313.0559 0001313 178.6712 249.6921 1.00273872 2049
Epoch: 2025-08-30T20:46Z
TLE epoch observation values (Epoch: 2025-08-30T20:46:26.821Z)
Latitude
0.03648°
Longitude
90.49532°
Altitude
35,787.439 km
Speed
3.075 km/s
True Right ascension
01h 25m 36s
True Declination
0° 02' 11"
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
20:48:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,792.617 km
Perigee altitude
35,781.544 km
Semi-major axis
42,165.217 km
Eccentricity
0.00013
Inclination
0.0571°
RAAN
313.0559°
Arg. of periapsis
178.6712°
True anomaly
249.67799°
Mean anomaly
249.6921°
Eccentric anomaly
249.68505°
Mean motion
0.25068 °/min
Orbital period
1,436.12 mins
BSTAR
0
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Other satellites on launch #23 in the year 2025 (2025-02-02 UTC)
QZS-6 Visibility
Observer location: undefined°, undefined°
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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62876 neighbors
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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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