HADES-SA (SPINNYONE), 68446
Orbit data source: Space-Track
HADES-SA (SPINNYONE), 68446 is a payload satellite owned by Hydra Space (ES) in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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68446 intel report (Beta)
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Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
Hydra Space
Mission
Operational Amateur Communications
Bus & Motor
POCKETQUBE 1P, Unknown motor
Mass
0.25 kg wet, 0.25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Ant, 14.5 m
Radar Cross Section
0.006 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 HADES-SA (SPINNYONE)
1 68446U 26067AG 26216.41502510 .00018624 00000-0 84972-3 0 9998
2 68446 97.4433 174.0499 0003870 264.4967 95.5827 15.20663115 19253Epoch: 2026-08-04T09:57Z
TLE epoch observation values (Epoch: 2026-08-04T09:57:38.168Z)
Latitude
-0.00003°
Longitude
71.65676°
Altitude
507.19 km
Speed
7.61 km/s
True Right ascension
11h 36m 11s
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
12:36:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.468 km
Perigee altitude
498.144 km
Semi-major axis
6,878.943 km
Eccentricity
0.00039
Inclination
97.4433°
RAAN
174.0499°
Arg. of periapsis
264.4967°
True anomaly
95.62683°
Mean anomaly
95.5827°
Eccentric anomaly
95.60477°
Mean motion
3.80418 °/min
Orbital period
94.63 mins
BSTAR
0.00084972
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.HADES-SA (SPINNYONE) 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 | 2026-08-06 09:54:03.895Z | 21.434° NNE | 2026-08-06 09:57:03.895Z | 94.707° ESE | 40.855° | 2026-08-06 10:00:03.895Z | 179.067° S |
| 4 mins | 2026-08-06 20:33:03.895Z | 107.414° ESE | 2026-08-06 20:35:03.895Z | 61.266° ENE | 21.321° | 2026-08-06 20:37:03.895Z | 23.131° NE |
| 4 mins | 2026-08-06 22:07:03.895Z | 234.877° WSW | 2026-08-06 22:08:03.895Z | 255.69° W | 19.001° | 2026-08-06 22:11:03.895Z | 312.73° NW |
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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