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
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
MELCO
Mission
Operational Civil Nav/Com
Bus & Motor
DS-2000, LAPS-500?
Mass
4,900 kg wet, ~2,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 22.5 m
Radar Cross Section
39.598 m²
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 QZS-6
1 62876U 25023A 26002.33735750 -.00000224 00000-0 00000-0 0 9993
2 62876 0.0809 78.3338 0002073 210.3685 25.1880 1.00267450 3290Epoch: 2026-01-02T08:05Z
TLE epoch observation values (Epoch: 2026-01-02T08:05:47.688Z)
Latitude
-0.08691°
Longitude
90.48259°
Altitude
35,779.371 km
Speed
3.075 km/s
True Right ascension
20h 55m 38s
True Declination
0° 05' 13"
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
07:26:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,797.622 km
Perigee altitude
35,780.139 km
Semi-major axis
42,167.018 km
Eccentricity
0.00021
Inclination
0.0809°
RAAN
78.3338°
Arg. of periapsis
210.3685°
True anomaly
25.19811°
Mean anomaly
25.188°
Eccentric anomaly
25.19306°
Mean motion
0.25066 °/min
Orbital period
1,436.21 mins
BSTAR
0
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Other satellites on launch #23 in the year 2025 (2025-02-02 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.QZS-6 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. |
|---|---|---|---|---|---|---|---|
| QZS-6 is likely not visible in the next few days. |
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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
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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