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: 6 hours ago
TLE from 6 hours ago
0 PUNCH-WFI03
1 63180U 25047C 26035.45772789 .00001041 00000-0 16527-3 0 9991
2 63180 97.9513 222.9527 0009091 230.6142 129.4262 14.74161060 48503Epoch: 2026-02-04T10:59Z
TLE epoch observation values (Epoch: 2026-02-04T10:59:07.689Z)
Latitude
-0.00004°
Longitude
-76.45336°
Altitude
654.888 km
Speed
7.528 km/s
True Right ascension
14h 51m 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
18:44:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.251 km
Perigee altitude
638.482 km
Semi-major axis
7,023.004 km
Eccentricity
0.00091
Inclination
97.9513°
RAAN
222.9527°
Arg. of periapsis
230.6142°
True anomaly
129.50661°
Mean anomaly
129.4262°
Eccentric anomaly
129.46641°
Mean motion
3.68773 °/min
Orbital period
97.62 mins
BSTAR
0.00016527
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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 | 2026-02-05 00:35:31.295Z | 34.491° NE | 2026-02-05 00:39:31.295Z | 101.147° ESE | 27.381° | 2026-02-05 00:42:31.295Z | 153.903° SSE |
| 5 mins | 2026-02-05 02:13:31.295Z | 332.724° NNW | 2026-02-05 02:15:31.295Z | 299.145° NW | 21.377° | 2026-02-05 02:18:31.295Z | 247.931° W |
| 6 mins | 2026-02-05 11:34:31.295Z | 113.284° SE | 2026-02-05 11:36:31.295Z | 79.029° E | 23.575° | 2026-02-05 11:40:31.295Z | 13.629° NNE |
| 5 mins | 2026-02-05 13:11:31.295Z | 223.434° SW | 2026-02-05 13:13:31.295Z | 263.649° W | 24.974° | 2026-02-05 13:16:31.295Z | 316.125° 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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