POSAT 2, 63488
Orbit data source: Space-Track
POSAT 2, 63488 is a Portuguese payload satellite in SSO that was launched on Tue, 14 Jan 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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63488 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
PT / PORRelated business
Manufacturer
LUSO
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
0.048 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 POSAT 2
1 63488U 25009DR 25297.28814587 .00005101 00000-0 35254-3 0 9992
2 63488 97.5113 12.5525 0006239 225.1649 134.9072 15.06151231 31056Epoch: 2025-10-24T06:54Z
TLE epoch observation values (Epoch: 2025-10-24T06:54:55.803Z)
Latitude
0°
Longitude
-124.11521°
Altitude
554.095 km
Speed
7.583 km/s
True Right ascension
00h 50m 12s
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
20:31:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.282 km
Perigee altitude
540.644 km
Semi-major axis
6,923.1 km
Eccentricity
0.00062
Inclination
97.5113°
RAAN
12.5525°
Arg. of periapsis
225.1649°
True anomaly
134.95781°
Mean anomaly
134.9072°
Eccentric anomaly
134.93251°
Mean motion
3.76784 °/min
Orbital period
95.55 mins
BSTAR
0.00035254
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.POSAT 2 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-25 05:21:48.275Z | 178.943° S | 2025-10-25 05:24:48.275Z | 253.376° W | 42.121° | 2025-10-25 05:27:48.275Z | 338.941° N |
| 6 mins | 2025-10-25 18:33:48.275Z | 345.41° N | 2025-10-25 18:35:48.275Z | 305.34° NW | 28.954° | 2025-10-25 18:39:48.275Z | 222.201° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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