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: 9 hours ago
TLE from 9 hours ago
0 POSAT 2
1 63488U 25009DR 25357.24971583 .00013615 00000-0 89605-3 0 9993
2 63488 97.5044 71.0281 0007296 37.0202 323.1529 15.07642309 40081Epoch: 2025-12-23T05:59Z
TLE epoch observation values (Epoch: 2025-12-23T05:59:35.447Z)
Latitude
0.00003°
Longitude
-110.90576°
Altitude
542.437 km
Speed
7.593 km/s
True Right ascension
04h 44m 06s
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
13:40:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.441 km
Perigee altitude
535.345 km
Semi-major axis
6,918.53 km
Eccentricity
0.00073
Inclination
97.5044°
RAAN
71.0281°
Arg. of periapsis
37.0202°
True anomaly
323.10273°
Mean anomaly
323.1529°
Eccentric anomaly
323.12782°
Mean motion
3.77157 °/min
Orbital period
95.45 mins
BSTAR
0.00089605
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-23 17:42:29.839Z | 22.997° NE | 2025-12-23 17:45:29.839Z | 80.798° E | 39.035° | 2025-12-23 17:49:29.839Z | 178.858° S |
| 4 mins | 2025-12-24 04:27:29.839Z | 103.977° ESE | 2025-12-24 04:28:29.839Z | 80.547° E | 23.703° | 2025-12-24 04:31:29.839Z | 18.633° NNE |
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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