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QPS-SAR-20, 101257

Orbit data source: Space-Track

QPS-SAR-20, 101257 is a Japanese payload satellite in LEO that was launched on Mon, 02 Nov 2026 UTC launched from the Rocket Lab Launch Complex (RLLC). 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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Identifier
101257, 2026-247A
Orbit
LEO
Country
Flag of JPJP / JPN
Related business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-11-02 (2 days ago)
Launch vehicle
Unknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 QPS-SAR-20
1 A1257U 26247A   26307.91976113  .00000146  00000-0  27916-4 0  9991
2 A1257  42.0133 220.0481 0009119 280.6182  79.3615 14.96876515   186
Epoch: 2026-11-03T22:04Z
TLE epoch observation values (Epoch: 2026-11-03T22:04:27.361Z)
Latitude
-0.00005°
Longitude
-154.24147°
Altitude
575.059 km
Speed
7.576 km/s
True Right ascension
14h 40m 11s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
05:55:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.98 km
Perigee altitude
572.293 km
Semi-major axis
6,956.773 km
Eccentricity
0.00091
Inclination
42.0133°
RAAN
220.0481°
Arg. of periapsis
280.6182°
True anomaly
79.46422°
Mean anomaly
79.3615°
Eccentric anomaly
79.41286°
Mean motion
3.74051 °/min
Orbital period
96.24 mins
BSTAR
0.000027916
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Other satellites on launch #247 in the year 2026 (2026-11-02 UTC)

Documentation

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