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: 1 day ago
TLE from 1 day ago
0 HADES-SA (SPINNYONE)
1 68446U 26067AG 26247.59761519 .00010973 00000-0 48973-3 0 9997
2 68446 97.4466 204.8751 0007831 140.4162 219.7647 15.21522429 23992Epoch: 2026-09-04T14:20Z
TLE epoch observation values (Epoch: 2026-09-04T14:20:33.952Z)
Latitude
-0.00001°
Longitude
6.01449°
Altitude
508.483 km
Speed
7.607 km/s
True Right ascension
13h 39m 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
06:45:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.598 km
Perigee altitude
492.828 km
Semi-major axis
6,876.35 km
Eccentricity
0.00078
Inclination
97.4466°
RAAN
204.8751°
Arg. of periapsis
140.4162°
True anomaly
219.70734°
Mean anomaly
219.7647°
Eccentric anomaly
219.73602°
Mean motion
3.80633 °/min
Orbital period
94.58 mins
BSTAR
0.00048973
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-05 20:29:13.275Z | 109.227° ESE | 2026-09-05 20:31:13.275Z | 68.563° E | 19.623° | 2026-09-05 20:33:13.275Z | 28.694° NE |
| 4 mins | 2026-09-05 22:03:13.275Z | 228.384° WSW | 2026-09-05 22:05:13.275Z | 274.591° WNW | 20.73° | 2026-09-05 22:07:13.275Z | 312.165° NW |
| 4 mins | 2026-09-06 09:33:13.275Z | 60.84° ENE | 2026-09-06 09:34:13.275Z | 87.937° E | 25.516° | 2026-09-06 09:37:13.275Z | 154.556° SSE |
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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