PHISAT 2, 60470
Orbit data source: Space-Track
PHISAT 2, 60470 is a UK payload satellite in SSO that was launched on Fri, 16 Aug 2024 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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60470 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
Open Cosmos
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
9 kg wet, 9 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.143 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 PHISAT 2
1 60470U 24149C 26173.47176180 .00005188 00000-0 17513-3 0 9992
2 60470 97.3752 252.6588 0001607 163.5207 196.6087 15.31121989102804Epoch: 2026-06-22T11:19Z
TLE epoch observation values (Epoch: 2026-06-22T11:19:20.219Z)
Latitude
-0°
Longitude
172.16736°
Altitude
476.625 km
Speed
7.627 km/s
True Right ascension
16h 50m 38s
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
10:53:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.514 km
Perigee altitude
468.313 km
Semi-major axis
6,847.55 km
Eccentricity
0.00016
Inclination
97.3752°
RAAN
252.6588°
Arg. of periapsis
163.5207°
True anomaly
196.60344°
Mean anomaly
196.6087°
Eccentric anomaly
196.60607°
Mean motion
3.83037 °/min
Orbital period
93.99 mins
BSTAR
0.00017513
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Other satellites on launch #149 in the year 2024 (2024-08-16 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.PHISAT 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-24 05:48:42.163Z | 207.079° SW | 2026-06-24 05:50:42.163Z | 268.63° W | 30.468° | 2026-06-24 05:53:42.163Z | 329.882° NNW |
| 4 mins | 2026-06-24 18:47:42.163Z | 328.098° NNW | 2026-06-24 18:48:42.163Z | 302.705° NW | 24.49° | 2026-06-24 18:51:42.163Z | 232.355° WSW |
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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