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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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: 18 hours ago
TLE from 18 hours ago
0 PUNCH-WFI03
1 63180U 25047C 26257.45723740 .00000364 00000-0 62420-4 0 9991
2 63180 97.9568 80.8755 0008825 238.1534 121.8816 14.74428558 81213Epoch: 2026-09-14T10:58Z
TLE epoch observation values (Epoch: 2026-09-14T10:58:25.311Z)
Latitude
-0.00003°
Longitude
-77.16722°
Altitude
653.257 km
Speed
7.529 km/s
True Right ascension
05h 23m 30s
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
21:09:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.214 km
Perigee altitude
637.82 km
Semi-major axis
7,022.154 km
Eccentricity
0.00088
Inclination
97.9568°
RAAN
80.8755°
Arg. of periapsis
238.1534°
True anomaly
121.96742°
Mean anomaly
121.8816°
Eccentric anomaly
121.92452°
Mean motion
3.6884 °/min
Orbital period
97.6 mins
BSTAR
0.00006242
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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 | 2026-09-15 11:32:24.194Z | 125.198° SE | 2026-09-15 11:36:24.194Z | 57.846° ENE | 27.423° | 2026-09-15 11:39:24.194Z | 13.353° NNE |
| 5 mins | 2026-09-15 13:10:24.194Z | 224.071° SW | 2026-09-15 13:12:24.194Z | 262.039° W | 26.253° | 2026-09-15 13:15:24.194Z | 314.144° NW |
| 7 mins | 2026-09-16 01:01:24.194Z | 23.971° NE | 2026-09-16 01:04:24.194Z | 121.972° SE | 63.825° | 2026-09-16 01:08:24.194Z | 183.382° 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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