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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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 26275.01127085 .00000282 00000-0 49954-4 0 9997
2 63179 97.9601 98.4503 0008688 186.5135 173.5963 14.74440431 83803Epoch: 2026-10-02T00:16Z
TLE epoch observation values (Epoch: 2026-10-02T00:16:13.801Z)
Latitude
0.00006°
Longitude
83.65344°
Altitude
656.007 km
Speed
7.526 km/s
True Right ascension
06h 33m 48s
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
05:25:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.08 km
Perigee altitude
637.878 km
Semi-major axis
7,022.116 km
Eccentricity
0.00087
Inclination
97.9601°
RAAN
98.4503°
Arg. of periapsis
186.5135°
True anomaly
173.60739°
Mean anomaly
173.5963°
Eccentric anomaly
173.60185°
Mean motion
3.68843 °/min
Orbital period
97.6 mins
BSTAR
0.000049954
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-10-02 11:47:51.045Z | 138.059° SSE | 2026-10-02 11:51:51.045Z | 65.806° ENE | 39.133° | 2026-10-02 11:55:51.045Z | 3.249° NNE |
| 4 mins | 2026-10-02 13:26:51.045Z | 240.363° WSW | 2026-10-02 13:28:51.045Z | 273.627° WNW | 18.328° | 2026-10-02 13:30:51.045Z | 303.382° NW |
| 7 mins | 2026-10-03 01:16:51.045Z | 11.273° NNE | 2026-10-03 01:19:51.045Z | 333.476° NNW | 83.856° | 2026-10-03 01:23:51.045Z | 195.573° 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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