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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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: 10 hours ago
TLE from 10 hours ago
0 PUNCH-WFI03
1 63180U 25047C 25340.24835550 .00001744 00000-0 27264-3 0 9992
2 63180 97.9491 163.8931 0011388 70.3818 289.8618 14.74009058 39639Epoch: 2025-12-06T05:57Z
TLE epoch observation values (Epoch: 2025-12-06T05:57:37.915Z)
Latitude
-0.00008°
Longitude
-0.79369°
Altitude
648.599 km
Speed
7.535 km/s
True Right ascension
10h 55m 34s
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
14:15:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.348 km
Perigee altitude
637.351 km
Semi-major axis
7,023.487 km
Eccentricity
0.00114
Inclination
97.9491°
RAAN
163.8931°
Arg. of periapsis
70.3818°
True anomaly
289.73901°
Mean anomaly
289.8618°
Eccentric anomaly
289.80041°
Mean motion
3.68735 °/min
Orbital period
97.63 mins
BSTAR
0.00027264
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-07 00:27:47.658Z | 42.132° NE | 2025-12-07 00:30:47.658Z | 87.679° E | 22.686° | 2025-12-07 00:33:47.658Z | 141.698° SSE |
| 5 mins | 2025-12-07 02:05:47.658Z | 331.431° NNW | 2025-12-07 02:07:47.658Z | 289.989° WNW | 25.489° | 2025-12-07 02:10:47.658Z | 237.812° WSW |
| 5 mins | 2025-12-07 11:26:47.658Z | 104.613° ESE | 2025-12-07 11:28:47.658Z | 71.687° E | 19.74° | 2025-12-07 11:31:47.658Z | 23.486° NE |
| 6 mins | 2025-12-07 13:02:47.658Z | 207.342° SW | 2025-12-07 13:05:47.658Z | 272.011° WNW | 29.01° | 2025-12-07 13:08:47.658Z | 323.567° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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