PUNCH-WFI02, 63181
Orbit data source: Space-Track
PUNCH-WFI02, 63181 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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63181 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: 2 days ago
TLE from 2 days ago
0 PUNCH-WFI02
1 63181U 25047D 25312.50622954 .00001307 00000-0 20668-3 0 9999
2 63181 97.9530 136.6960 0009739 163.2800 196.8731 14.73924852 35540Epoch: 2025-11-08T12:08Z
TLE epoch observation values (Epoch: 2025-11-08T12:08:58.232Z)
Latitude
-0.00004°
Longitude
-93.48149°
Altitude
658.129 km
Speed
7.525 km/s
True Right ascension
09h 06m 47s
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
08:42:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.458 km
Perigee altitude
638.777 km
Semi-major axis
7,023.755 km
Eccentricity
0.00097
Inclination
97.953°
RAAN
136.696°
Arg. of periapsis
163.28°
True anomaly
196.84075°
Mean anomaly
196.8731°
Eccentric anomaly
196.85692°
Mean motion
3.68714 °/min
Orbital period
97.64 mins
BSTAR
0.00020668
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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-WFI02 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 | 2025-11-10 13:08:37.699Z | 204.245° SW | 2025-11-10 13:12:37.699Z | 273.237° WNW | 26.061° | 2025-11-10 13:15:37.699Z | 321.028° NNW |
| 6 mins | 2025-11-11 01:01:37.699Z | 30.705° NE | 2025-11-11 01:03:37.699Z | 75.267° E | 38.752° | 2025-11-11 01:07:37.699Z | 176.622° S |
| 7 mins | 2025-11-11 11:58:37.699Z | 137.757° SSE | 2025-11-11 12:01:37.699Z | 71.784° E | 35.336° | 2025-11-11 12:05:37.699Z | 1.349° NNE |
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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