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: 11 hours ago
TLE from 11 hours ago
0 PUNCH-WFI03
1 63180U 25047C 26171.40376359 .00000402 00000-0 68107-4 0 9992
2 63180 97.9545 356.3850 0010674 151.5467 208.6326 14.74353397 68531Epoch: 2026-06-20T09:41Z
TLE epoch observation values (Epoch: 2026-06-20T09:41:25.174Z)
Latitude
-0.00005°
Longitude
-57.58877°
Altitude
656.802 km
Speed
7.526 km/s
True Right ascension
23h 45m 32s
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
07:21:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.751 km
Perigee altitude
636.76 km
Semi-major axis
7,022.392 km
Eccentricity
0.00107
Inclination
97.9545°
RAAN
356.385°
Arg. of periapsis
151.5467°
True anomaly
208.57406°
Mean anomaly
208.6326°
Eccentric anomaly
208.60332°
Mean motion
3.68821 °/min
Orbital period
97.61 mins
BSTAR
0.000068107
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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 | 2026-06-21 00:55:29.820Z | 24.852° NE | 2026-06-21 00:59:29.820Z | 125.074° SE | 38.117° | 2026-06-21 01:02:29.820Z | 175.136° S |
| 7 mins | 2026-06-21 11:53:29.820Z | 136.162° SSE | 2026-06-21 11:56:29.820Z | 69.266° E | 34.614° | 2026-06-21 12:00:29.820Z | 1.652° NNE |
| 4 mins | 2026-06-21 13:31:29.820Z | 240.454° WSW | 2026-06-21 13:33:29.820Z | 271.307° WNW | 15.692° | 2026-06-21 13:35:29.820Z | 300.397° NW |
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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