PUNCH-WFI01, 63179
Orbit data source: Space-Track
PUNCH-WFI01, 63179 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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63179 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-WFI01
1 63179U 25047B 25308.45504697 .00000947 00000-0 15196-3 0 9997
2 63179 97.9552 132.8868 0009186 171.2078 188.9293 14.73913276 34955Epoch: 2025-11-04T10:55Z
TLE epoch observation values (Epoch: 2025-11-04T10:55:16.058Z)
Latitude
-0.00001°
Longitude
-74.87193°
Altitude
657.993 km
Speed
7.525 km/s
True Right ascension
08h 51m 32s
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
17:43:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.107 km
Perigee altitude
639.202 km
Semi-major axis
7,023.792 km
Eccentricity
0.00092
Inclination
97.9552°
RAAN
132.8868°
Arg. of periapsis
171.2078°
True anomaly
188.91298°
Mean anomaly
188.9293°
Eccentric anomaly
188.92114°
Mean motion
3.68711 °/min
Orbital period
97.64 mins
BSTAR
0.00015196
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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-WFI01 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 | 2025-11-05 00:32:16.116Z | 40.679° NE | 2025-11-05 00:35:16.116Z | 87.209° E | 24.017° | 2025-11-05 00:39:16.116Z | 153.127° SSE |
| 5 mins | 2025-11-05 02:10:16.116Z | 329.972° NNW | 2025-11-05 02:12:16.116Z | 290.202° WNW | 24.007° | 2025-11-05 02:15:16.116Z | 239.914° WSW |
| 5 mins | 2025-11-05 11:31:16.116Z | 106.247° ESE | 2025-11-05 11:33:16.116Z | 72.02° E | 21.314° | 2025-11-05 11:36:16.116Z | 22.385° NNE |
| 6 mins | 2025-11-05 13:07:16.116Z | 209.917° SW | 2025-11-05 13:10:16.116Z | 271.103° WNW | 27.709° | 2025-11-05 13:13:16.116Z | 321.704° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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