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: 19 hours ago
TLE from 19 hours ago
0 PUNCH-WFI02
1 63181U 25047D 26308.92024314 .00000396 00000-0 67020-4 0 9998
2 63181 97.9564 131.5231 0010710 90.3995 269.8442 14.74475831 88792Epoch: 2026-11-04T22:05Z
TLE epoch observation values (Epoch: 2026-11-04T22:05:09.007Z)
Latitude
0.00009°
Longitude
116.07392°
Altitude
649.856 km
Speed
7.533 km/s
True Right ascension
08h 46m 05s
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
13:12:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.387 km
Perigee altitude
636.346 km
Semi-major axis
7,022.003 km
Eccentricity
0.00107
Inclination
97.9564°
RAAN
131.5231°
Arg. of periapsis
90.3995°
True anomaly
269.72147°
Mean anomaly
269.8442°
Eccentric anomaly
269.78284°
Mean motion
3.68852 °/min
Orbital period
97.6 mins
BSTAR
0.00006702
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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 | 2026-11-06 00:43:01.386Z | 29.491° NE | 2026-11-06 00:47:01.386Z | 106.588° ESE | 41.151° | 2026-11-06 00:50:01.386Z | 164.004° S |
| 4 mins | 2026-11-06 02:22:01.386Z | 312.859° NW | 2026-11-06 02:23:01.386Z | 296.003° NW | 18.068° | 2026-11-06 02:26:01.386Z | 252.529° W |
| 6 mins | 2026-11-06 11:42:01.386Z | 118.605° SE | 2026-11-06 11:44:01.386Z | 75.601° E | 33.437° | 2026-11-06 11:48:01.386Z | 7.486° NNE |
| 5 mins | 2026-11-06 13:19:01.386Z | 233.171° WSW | 2026-11-06 13:21:01.386Z | 268.426° W | 21.037° | 2026-11-06 13:24:01.386Z | 313.311° NW |
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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