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: 15 hours ago
TLE from 15 hours ago
0 PUNCH-WFI03
1 63180U 25047C 25310.03941473 .00001084 00000-0 17278-3 0 9999
2 63180 97.9511 134.2661 0010521 158.3531 201.8124 14.73918575 35185Epoch: 2025-11-06T00:56Z
TLE epoch observation values (Epoch: 2025-11-06T00:56:45.432Z)
Latitude
-0.00005°
Longitude
74.57335°
Altitude
658.464 km
Speed
7.524 km/s
True Right ascension
08h 57m 03s
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
12:15:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.027 km
Perigee altitude
638.248 km
Semi-major axis
7,023.774 km
Eccentricity
0.00105
Inclination
97.9511°
RAAN
134.2661°
Arg. of periapsis
158.3531°
True anomaly
201.76766°
Mean anomaly
201.8124°
Eccentric anomaly
201.79002°
Mean motion
3.68712 °/min
Orbital period
97.64 mins
BSTAR
0.00017278
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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 | 2025-11-07 00:20:33.912Z | 46.894° ENE | 2025-11-07 00:23:33.912Z | 91.376° ESE | 19.282° | 2025-11-07 00:26:33.912Z | 138.461° SSE |
| 6 mins | 2025-11-07 01:57:33.912Z | 345.897° N | 2025-11-07 02:00:33.912Z | 285.769° WNW | 29.208° | 2025-11-07 02:03:33.912Z | 230.821° WSW |
| 4 mins | 2025-11-07 11:20:33.912Z | 85.384° E | 2025-11-07 11:21:33.912Z | 68.788° E | 17.169° | 2025-11-07 11:24:33.912Z | 24.992° NE |
| 6 mins | 2025-11-07 12:55:33.912Z | 201.554° SSW | 2025-11-07 12:58:33.912Z | 279.065° WNW | 33.073° | 2025-11-07 13:01:33.912Z | 328.88° 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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