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: 10 hours ago
TLE from 10 hours ago
0 PUNCH-WFI03
1 63180U 25047C 26095.25439011 .00000903 00000-0 14401-3 0 9998
2 63180 97.9547 281.6403 0011033 48.3723 311.8428 14.74272363 57312Epoch: 2026-04-05T06:06Z
TLE epoch observation values (Epoch: 2026-04-05T06:06:19.305Z)
Latitude
-0.00011°
Longitude
-3.50257°
Altitude
645.307 km
Speed
7.538 km/s
True Right ascension
18h 46m 33s
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
21:58:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.261 km
Perigee altitude
636.765 km
Semi-major axis
7,022.65 km
Eccentricity
0.0011
Inclination
97.9547°
RAAN
281.6403°
Arg. of periapsis
48.3723°
True anomaly
311.74853°
Mean anomaly
311.8428°
Eccentric anomaly
311.79567°
Mean motion
3.68801 °/min
Orbital period
97.61 mins
BSTAR
0.00014401
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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 | 2026-04-06 00:36:31.078Z | 39.965° NE | 2026-04-06 00:39:31.078Z | 95.273° ESE | 28.068° | 2026-04-06 00:43:31.078Z | 160.597° S |
| 4 mins | 2026-04-06 02:14:31.078Z | 321.162° NNW | 2026-04-06 02:16:31.078Z | 282.873° WNW | 20.713° | 2026-04-06 02:18:31.078Z | 250.925° W |
| 5 mins | 2026-04-06 11:35:31.078Z | 103.578° ESE | 2026-04-06 11:37:31.078Z | 61.242° ENE | 23.908° | 2026-04-06 11:40:31.078Z | 14.828° NNE |
| 5 mins | 2026-04-06 13:11:31.078Z | 221.067° SW | 2026-04-06 13:13:31.078Z | 258.345° W | 23.87° | 2026-04-06 13:16:31.078Z | 313.294° 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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