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, 0.5 m
Radar Cross Section
0.625 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 PUNCH-WFI02
1 63181U 25047D 25257.44704888 .00000482 00000-0 81340-4 0 9995
2 63181 97.9560 82.6790 0009362 355.6444 4.4681 14.73781250 27437Epoch: 2025-09-14T10:43Z
TLE epoch observation values (Epoch: 2025-09-14T10:43:45.023Z)
Latitude
-0.00004°
Longitude
-71.92452°
Altitude
645.474 km
Speed
7.539 km/s
True Right ascension
05h 30m 42s
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
23:31:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.65 km
Perigee altitude
639.498 km
Semi-major axis
7,024.211 km
Eccentricity
0.00094
Inclination
97.956°
RAAN
82.679°
Arg. of periapsis
355.6444°
True anomaly
4.47647°
Mean anomaly
4.4681°
Eccentric anomaly
4.47228°
Mean motion
3.68678 °/min
Orbital period
97.65 mins
BSTAR
0.00008134
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-15 11:19:59.658Z | 100.551° ESE | 2025-09-15 11:21:59.658Z | 70.873° E | 16.782° | 2025-09-15 11:24:59.658Z | 26.348° NE |
| 6 mins | 2025-09-15 12:55:59.658Z | 199.757° SSW | 2025-09-15 12:58:59.658Z | 274.517° WNW | 33.527° | 2025-09-15 13:01:59.658Z | 328.304° NNW |
| 6 mins | 2025-09-16 00:47:59.658Z | 40.486° NE | 2025-09-16 00:50:59.658Z | 112.12° ESE | 31.581° | 2025-09-16 00:53:59.658Z | 162.864° S |
| 5 mins | 2025-09-16 02:24:59.658Z | 326.014° NNW | 2025-09-16 02:26:59.658Z | 293.383° NW | 18.468° | 2025-09-16 02:29:59.658Z | 249.755° W |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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