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 spacecraft
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
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 HADES-SA (SPINNYONE)
1 68446U 26067AG 26170.85664013 .00014903 00000-0 71102-3 0 9999
2 68446 97.4408 129.1130 0009324 75.2223 285.0044 15.19135217 12335Epoch: 2026-06-19T20:33Z
TLE epoch observation values (Epoch: 2026-06-19T20:33:33.707Z)
Latitude
-0.00001°
Longitude
-87.35705°
Altitude
509.884 km
Speed
7.61 km/s
True Right ascension
08h 36m 27s
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
07:13:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.84 km
Perigee altitude
499.003 km
Semi-major axis
6,883.558 km
Eccentricity
0.00093
Inclination
97.4408°
RAAN
129.113°
Arg. of periapsis
75.2223°
True anomaly
284.90117°
Mean anomaly
285.0044°
Eccentric anomaly
284.95279°
Mean motion
3.80035 °/min
Orbital period
94.73 mins
BSTAR
0.00071102
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 20:25:02.931Z | 115.16° SE | 2026-06-20 20:28:02.931Z | 59.971° ENE | 18.07° | 2026-06-20 20:30:02.931Z | 25.213° NE |
| 4 mins | 2026-06-20 22:00:02.931Z | 230.697° WSW | 2026-06-20 22:01:02.931Z | 254.29° W | 22.295° | 2026-06-20 22:04:02.931Z | 316.534° NNW |
| 5 mins | 2026-06-21 09:30:02.931Z | 47.894° ENE | 2026-06-21 09:32:02.931Z | 93.85° ESE | 25.061° | 2026-06-21 09:35:02.931Z | 154.707° 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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