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: 19 hours ago
TLE from 19 hours ago
0 CLARITY-1
1 63227U 25052T 25318.25575338 .00052151 00000-0 51300-3 0 9997
2 63227 97.4312 217.7091 0003103 95.2415 264.9199 15.65850214 37690Epoch: 2025-11-14T06:08Z
TLE epoch observation values (Epoch: 2025-11-14T06:08:17.092Z)
Latitude
0.00001°
Longitude
72.03601°
Altitude
374.132 km
Speed
7.685 km/s
True Right ascension
14h 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
21:37:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
369.794 km
Perigee altitude
365.608 km
Semi-major axis
6,745.838 km
Eccentricity
0.00031
Inclination
97.4312°
RAAN
217.7091°
Arg. of periapsis
95.2415°
True anomaly
264.88448°
Mean anomaly
264.9199°
Eccentric anomaly
264.90219°
Mean motion
3.91732 °/min
Orbital period
91.9 mins
BSTAR
0.000513
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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 | 2025-11-15 05:42:26.763Z | 46.694° ENE | 2025-11-15 05:44:26.763Z | 92.938° ESE | 19.393° | 2025-11-15 05:46:26.763Z | 143.032° SSE |
| 4 mins | 2025-11-15 17:33:26.763Z | 172.484° S | 2025-11-15 17:35:26.763Z | 332.868° NNW | 40.394° | 2025-11-15 17:37:26.763Z | 345.473° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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