QZS-7, 100270
Orbit data source: Space-Track
QZS-7, 100270 is a Japanese payload satellite in GEO that was launched on Mon, 10 Aug 2026 UTC launched 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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100270 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
MELCO
Mission
Operational spacecraft
Bus & Motor
DS-2000, LAPS-500?
Mass
4,900 kg wet, ~2,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
BOX + 2 PAN, 12.7 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 QZS-7
1 A0270U 26182A 26249.55715484 .00000060 00000-0 00000-0 0 9996
2 A0270 2.9771 300.9841 0074610 358.6689 70.6093 1.00285937 319Epoch: 2026-09-06T13:22Z
TLE epoch observation values (Epoch: 2026-09-06T13:22:18.178Z)
Latitude
2.78411°
Longitude
-175.17181°
Altitude
35,678.085 km
Speed
3.082 km/s
True Right ascension
00h 44m 13s
True Declination
2° 46' 53"
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
13:13:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,098.264 km
Perigee altitude
35,469.125 km
Semi-major axis
42,161.831 km
Eccentricity
0.00746
Inclination
2.9771°
RAAN
300.9841°
Arg. of periapsis
358.6689°
True anomaly
71.41825°
Mean anomaly
70.6093°
Eccentric anomaly
71.01353°
Mean motion
0.25071 °/min
Orbital period
1,435.95 mins
BSTAR
0
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Other satellites on launch #182 in the year 2026 (2026-08-10 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-7 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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| QZS-7 is likely not visible in the next few days. |
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100270 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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