STRIX 2, 62406
Orbit data source: Space-Track
STRIX 2, 62406 is a payload satellite owned by Synspective (JP) in SSO that was launched on Sat, 21 Dec 2024 UTC via an ELECTRON launch vehicle 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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62406 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
Synspective
Mission
Operational Commercial Radar Imaging
Bus & Motor
STRIX, Unknown motor
Mass
150 kg wet, 150 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
1.052 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STRIX 2
1 62406U 24248A 26171.52148274 .00004444 00000-0 28501-3 0 9993
2 62406 97.6290 127.1424 0014604 330.8529 29.1882 15.08934642 82090Epoch: 2026-06-20T12:30Z
TLE epoch observation values (Epoch: 2026-06-20T12:30:56.108Z)
Latitude
-0.00013°
Longitude
30.67372°
Altitude
533.705 km
Speed
7.601 km/s
True Right ascension
08h 28m 34s
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
08:43:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
546.542 km
Perigee altitude
526.346 km
Semi-major axis
6,914.581 km
Eccentricity
0.00146
Inclination
97.629°
RAAN
127.1424°
Arg. of periapsis
330.8529°
True anomaly
29.26994°
Mean anomaly
29.1882°
Eccentric anomaly
29.22906°
Mean motion
3.7748 °/min
Orbital period
95.37 mins
BSTAR
0.00028501
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Other satellites on launch #248 in the year 2024 (2024-12-21 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.STRIX 2 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 09:47:08.047Z | 23.224° NE | 2026-06-21 09:49:08.047Z | 68.888° E | 41.645° | 2026-06-21 09:53:08.047Z | 183.854° SSW |
| 5 mins | 2026-06-21 20:30:08.047Z | 116.115° SE | 2026-06-21 20:32:08.047Z | 64.246° ENE | 26.892° | 2026-06-21 20:35:08.047Z | 10.433° NNE |
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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