PUNCH-WFI02, 63181
Orbit data source: Space-Track
PUNCH-WFI02, 63181 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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63181 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, 1.9 m
Radar Cross Section
0.625 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 PUNCH-WFI02
1 63181U 25047D 25300.01484766 .00001216 00000-0 19305-3 0 9994
2 63181 97.9539 124.4413 0008842 203.9227 156.1572 14.73893133 33701Epoch: 2025-10-27T00:21Z
TLE epoch observation values (Epoch: 2025-10-27T00:21:22.837Z)
Latitude
-0.00001°
Longitude
83.47338°
Altitude
657.364 km
Speed
7.526 km/s
True Right ascension
08h 17m 45s
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
06:50:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.929 km
Perigee altitude
639.508 km
Semi-major axis
7,023.856 km
Eccentricity
0.00088
Inclination
97.9539°
RAAN
124.4413°
Arg. of periapsis
203.9227°
True anomaly
156.19812°
Mean anomaly
156.1572°
Eccentric anomaly
156.17766°
Mean motion
3.68706 °/min
Orbital period
97.64 mins
BSTAR
0.00019305
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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-WFI02 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 | 2025-10-27 11:53:21.861Z | 138.35° SSE | 2025-10-27 11:57:21.861Z | 62.327° ENE | 32.633° | 2025-10-27 12:00:21.861Z | 7.846° NNE |
| 4 mins | 2025-10-27 13:32:21.861Z | 241.589° WSW | 2025-10-27 13:34:21.861Z | 274.502° WNW | 16.974° | 2025-10-27 13:36:21.861Z | 303.662° NW |
| 7 mins | 2025-10-28 01:22:21.861Z | 10.491° NNE | 2025-10-28 01:25:21.861Z | 344.708° N | 44.25° | 2025-10-28 01:29:21.861Z | 196.727° SSW |
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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