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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 PUNCH-WFI02
1 63181U 25047D 26305.05211700 .00000359 00000-0 61497-4 0 9997
2 63181 97.9566 127.7233 0010675 101.2385 259.0025 14.74472470 88220Epoch: 2026-11-01T01:15Z
TLE epoch observation values (Epoch: 2026-11-01T01:15:02.908Z)
Latitude
0.00005°
Longitude
68.61215°
Altitude
651.277 km
Speed
7.531 km/s
True Right ascension
08h 30m 53s
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
13:43:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.373 km
Perigee altitude
636.381 km
Semi-major axis
7,022.014 km
Eccentricity
0.00107
Inclination
97.9566°
RAAN
127.7233°
Arg. of periapsis
101.2385°
True anomaly
258.88245°
Mean anomaly
259.0025°
Eccentric anomaly
258.94247°
Mean motion
3.68851 °/min
Orbital period
97.6 mins
BSTAR
0.000061497
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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 | 2026-11-02 00:37:45.811Z | 33.725° NE | 2026-11-02 00:41:45.811Z | 111.679° ESE | 35.059° | 2026-11-02 00:44:45.811Z | 160.927° S |
| 5 mins | 2026-11-02 02:15:45.811Z | 326.16° NNW | 2026-11-02 02:17:45.811Z | 292.19° WNW | 20.379° | 2026-11-02 02:20:45.811Z | 247.704° W |
| 5 mins | 2026-11-02 11:36:45.811Z | 111.609° ESE | 2026-11-02 11:38:45.811Z | 69.528° E | 29.594° | 2026-11-02 11:41:45.811Z | 15.966° NNE |
| 5 mins | 2026-11-02 13:13:45.811Z | 233.464° WSW | 2026-11-02 13:15:45.811Z | 273.171° WNW | 23.771° | 2026-11-02 13:18:45.811Z | 317.576° 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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