QZS-7, 100270
Orbit data source: Space-Track
QZS-7, 100270 is a Japanese payload satellite in HEO 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: 1 day ago
TLE from 1 day ago
0 QZS-7
1 A0270U 26182A 26223.06669436 .00000005 00000-0 22541-3 0 9995
2 A0270 22.8828 292.4491 7210193 175.6988 198.3921 2.29772095 27Epoch: 2026-08-11T01:36Z
TLE epoch observation values (Epoch: 2026-08-11T01:36:02.392Z)
Latitude
0.00005°
Longitude
-51.07753°
Altitude
35,089.248 km
Speed
1.672 km/s
True Right ascension
19h 29m 53s
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
01:50:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,379.111 km
Perigee altitude
390.797 km
Semi-major axis
24,263.091 km
Eccentricity
0.72102
Inclination
22.8828°
RAAN
292.4491°
Arg. of periapsis
175.6988°
True anomaly
184.32375°
Mean anomaly
198.3921°
Eccentric anomaly
190.71285°
Mean motion
0.57428 °/min
Orbital period
626.87 mins
BSTAR
0.00022541
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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 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. |
|---|---|---|---|---|---|---|---|
| 77 mins | 2026-08-12 12:11:03.982Z | 268.148° W | 2026-08-12 13:21:03.982Z | 219.324° SW | 27.807° | 2026-08-12 13:28:03.982Z | 162.015° S |
| 554 mins | 2026-08-13 01:01:03.982Z | 178.883° S | 2026-08-13 09:54:03.982Z | 188.516° SSW | 40.299° | 2026-08-13 10:15:03.982Z | 113.761° SE |
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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