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: 5 hours ago
TLE from 5 hours ago
0 STRIX 2
1 62406U 24248A 26108.83963432 .00004874 00000-0 31829-3 0 9992
2 62406 97.6253 64.8757 0015973 171.1780 188.9732 15.08205433 72647Epoch: 2026-04-18T20:09Z
TLE epoch observation values (Epoch: 2026-04-18T20:09:04.405Z)
Latitude
0°
Longitude
-84.34536°
Altitude
555.672 km
Speed
7.578 km/s
True Right ascension
04h 19m 30s
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
08:06:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.723 km
Perigee altitude
527.627 km
Semi-major axis
6,916.812 km
Eccentricity
0.0016
Inclination
97.6253°
RAAN
64.8757°
Arg. of periapsis
171.178°
True anomaly
188.94471°
Mean anomaly
188.9732°
Eccentric anomaly
188.95895°
Mean motion
3.77298 °/min
Orbital period
95.42 mins
BSTAR
0.00031829
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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 | 2026-04-19 09:27:50.072Z | 33.303° NE | 2026-04-19 09:30:50.072Z | 105.204° ESE | 32.094° | 2026-04-19 09:33:50.072Z | 166.049° S |
| 4 mins | 2026-04-19 20:11:50.072Z | 103.537° ESE | 2026-04-19 20:13:50.072Z | 64.104° ENE | 19.406° | 2026-04-19 20:15:50.072Z | 28.004° NE |
| 5 mins | 2026-04-19 21:45:50.072Z | 216.787° SW | 2026-04-19 21:47:50.072Z | 258.457° W | 24.258° | 2026-04-19 21:50:50.072Z | 317.886° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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