PUNCH-WFI03, 63180
Orbit data source: Space-Track
PUNCH-WFI03, 63180 is an American payload satellite in SSO that was launched on Wed, 12 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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63180 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SWRI
Mission
Operational Civil Astronomy
Bus & Motor
PUNCH, Unknown motor
Mass
64 kg wet, 64 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 0.5 m
Radar Cross Section
0.625 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 PUNCH-WFI03
1 63180U 25047C 25257.56000271 .00000488 00000-0 82136-4 0 9992
2 63180 97.9538 82.7935 0009720 340.8629 19.2213 14.73783116 27452Epoch: 2025-09-14T13:26Z
TLE epoch observation values (Epoch: 2025-09-14T13:26:24.234Z)
Latitude
0.00001°
Longitude
-112.58474°
Altitude
645.578 km
Speed
7.539 km/s
True Right ascension
05h 31m 10s
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
21:24:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.896 km
Perigee altitude
639.241 km
Semi-major axis
7,024.205 km
Eccentricity
0.00097
Inclination
97.9538°
RAAN
82.7935°
Arg. of periapsis
340.8629°
True anomaly
19.25801°
Mean anomaly
19.2213°
Eccentric anomaly
19.23965°
Mean motion
3.68678 °/min
Orbital period
97.65 mins
BSTAR
0.000082136
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Other satellites on launch #47 in the year 2025 (2025-03-12 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.PUNCH-WFI03 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 | 2025-09-15 12:22:38.566Z | 162.638° S | 2025-09-15 12:25:38.566Z | 144.207° SSE | 43.339° | 2025-09-15 12:29:38.566Z | 349.671° N |
| 4 mins | 2025-09-16 00:16:38.566Z | 72.614° E | 2025-09-16 00:17:38.566Z | 88.957° E | 16.981° | 2025-09-16 00:20:38.566Z | 133.131° SE |
| 7 mins | 2025-09-16 01:51:38.566Z | 351.001° N | 2025-09-16 01:54:38.566Z | 290.856° WNW | 33.09° | 2025-09-16 01:58:38.566Z | 220.31° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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