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, 0.5 m
Radar Cross Section
0.625 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 PUNCH-WFI01
1 63179U 25047B 25257.46914462 .00000485 00000-0 81782-4 0 9998
2 63179 97.9581 82.8533 0008897 351.4079 8.6975 14.73782441 27440Epoch: 2025-09-14T11:15Z
TLE epoch observation values (Epoch: 2025-09-14T11:15:34.095Z)
Latitude
-0.00007°
Longitude
-79.72646°
Altitude
645.849 km
Speed
7.538 km/s
True Right ascension
05h 31m 24s
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
23:29:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.32 km
Perigee altitude
639.821 km
Semi-major axis
7,024.208 km
Eccentricity
0.00089
Inclination
97.9581°
RAAN
82.8533°
Arg. of periapsis
351.4079°
True anomaly
8.71293°
Mean anomaly
8.6975°
Eccentric anomaly
8.70522°
Mean motion
3.68678 °/min
Orbital period
97.65 mins
BSTAR
0.000081782
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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 | 2025-09-15 11:50:16.290Z | 131.272° SE | 2025-09-15 11:53:16.290Z | 78.555° E | 29.87° | 2025-09-15 11:57:16.290Z | 7.005° NNE |
| 5 mins | 2025-09-15 13:28:16.290Z | 232.449° WSW | 2025-09-15 13:30:16.290Z | 265.864° W | 18.846° | 2025-09-15 13:33:16.290Z | 311.095° NW |
| 7 mins | 2025-09-16 01:19:16.290Z | 14.369° NNE | 2025-09-16 01:22:16.290Z | 164.585° S | 44.745° | 2025-09-16 01:26:16.290Z | 192.382° 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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