CLARITY-1, 63227
Orbit data source: Space-Track
CLARITY-1, 63227 is an American payload satellite in SSO 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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ALBEDO
Mission
Operational 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 CLARITY-1
1 63227U 25052T 25346.98429307 .00065824 00000-0 56448-3 0 9991
2 63227 97.4315 248.1105 0004014 87.5480 272.6241 15.69193480 42199Epoch: 2025-12-12T23:37Z
TLE epoch observation values (Epoch: 2025-12-12T23:37:22.921Z)
Latitude
-0.00002°
Longitude
171.84692°
Altitude
364.238 km
Speed
7.691 km/s
True Right ascension
16h 32m 26s
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
16:29:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.811 km
Perigee altitude
355.403 km
Semi-major axis
6,736.244 km
Eccentricity
0.0004
Inclination
97.4315°
RAAN
248.1105°
Arg. of periapsis
87.548°
True anomaly
272.57815°
Mean anomaly
272.6241°
Eccentric anomaly
272.60113°
Mean motion
3.92569 °/min
Orbital period
91.7 mins
BSTAR
0.00056448
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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 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 | 2025-12-13 18:07:43.640Z | 213.474° SW | 2025-12-13 18:09:43.640Z | 279.925° WNW | 23.497° | 2025-12-13 18:11:43.640Z | 323.153° NNW |
| 4 mins | 2025-12-14 06:47:43.640Z | 344.351° N | 2025-12-14 06:48:43.640Z | 313.478° NW | 30.728° | 2025-12-14 06:51:43.640Z | 214.795° SW |
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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