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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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, 0.3 m
Radar Cross Section
0.048 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 POSAT 2
1 63488U 25009DR 26256.16163416 .00010309 00000-0 55762-3 0 9995
2 63488 97.4781 329.6804 0005620 188.5867 171.5269 15.14840036 79958Epoch: 2026-09-13T03:52Z
TLE epoch observation values (Epoch: 2026-09-13T03:52:45.191Z)
Latitude
-0.00011°
Longitude
-80.66813°
Altitude
528.382 km
Speed
7.597 km/s
True Right ascension
21h 58m 43s
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
02:49:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
522.316 km
Perigee altitude
514.564 km
Semi-major axis
6,896.577 km
Eccentricity
0.00056
Inclination
97.4781°
RAAN
329.6804°
Arg. of periapsis
188.5867°
True anomaly
171.53638°
Mean anomaly
171.5269°
Eccentric anomaly
171.53164°
Mean motion
3.78959 °/min
Orbital period
95 mins
BSTAR
0.00055762
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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 | 2026-09-13 17:08:01.522Z | 41.846° NE | 2026-09-13 17:11:01.522Z | 96.768° ESE | 23.63° | 2026-09-13 17:14:01.522Z | 150.153° SSE |
| 5 mins | 2026-09-14 05:23:01.522Z | 195.513° SSW | 2026-09-14 05:25:01.522Z | 257.206° W | 48.852° | 2026-09-14 05:28:01.522Z | 332.817° NNW |
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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