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: 22 hours ago
TLE from 22 hours ago
0 CLARITY-1
1 63227U 25052T 25256.44791112 .00013985 00000-0 14639-3 0 9995
2 63227 97.4395 152.6119 0008218 85.2046 275.0152 15.64511494 28033Epoch: 2025-09-13T10:44Z
TLE epoch observation values (Epoch: 2025-09-13T10:44:59.52Z)
Latitude
0.00003°
Longitude
-1.31723°
Altitude
377.313 km
Speed
7.684 km/s
True Right ascension
10h 10m 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
00:49:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
377.099 km
Perigee altitude
366.005 km
Semi-major axis
6,749.689 km
Eccentricity
0.00082
Inclination
97.4395°
RAAN
152.6119°
Arg. of periapsis
85.2046°
True anomaly
274.92138°
Mean anomaly
275.0152°
Eccentric anomaly
274.96829°
Mean motion
3.91397 °/min
Orbital period
91.98 mins
BSTAR
0.00014639
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-14 17:34:40.126Z | 193.544° SSW | 2025-09-14 17:36:40.126Z | 238.319° WSW | 29.16° | 2025-09-14 17:39:40.126Z | 329.539° NNW |
| 4 mins | 2025-09-15 06:17:40.126Z | 353.052° N | 2025-09-15 06:19:40.126Z | 256.651° W | 36.092° | 2025-09-15 06:21:40.126Z | 210.302° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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