CLARITY-1, 63227 (Decayed)
Orbit data source: Space-Track
CLARITY-1, 63227 was an American payload satellite in LEO that was launched on Sat, 15 Mar 2025 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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63227 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
ALBEDO
Mission
Decayed Commercial Imaging
Bus & Motor
ALBEDO, Unknown motor
Mass
530 kg wet, 485 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl, 1.1 m
Radar Cross Section
2.290 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 CLARITY-1
1 63227U 25052T 26161.15767168 .09211707 26169-5 12257-3 0 9997
2 63227 97.3825 82.7091 0009598 247.2263 112.8028 16.48960409 70590Epoch: 2026-06-10T03:47Z
TLE epoch observation values (Epoch: 2026-06-10T03:47:02.833Z)
Latitude
0.00005°
Longitude
127.42744°
Altitude
147.769 km
Speed
7.816 km/s
True Right ascension
05h 30m 50s
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
04:57:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
145.125 km
Perigee altitude
132.615 km
Semi-major axis
6,517.007 km
Eccentricity
0.00096
Inclination
97.3825°
RAAN
82.7091°
Arg. of periapsis
247.2263°
True anomaly
112.90414°
Mean anomaly
112.8028°
Eccentric anomaly
112.85348°
Mean motion
4.12545 °/min
Orbital period
87.26 mins
BSTAR
0.00012257
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.CLARITY-1 Visibility
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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. |
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| This satellite is decayed. |
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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