PUNCH-WFI01, 63179
Orbit data source: Space-Track
PUNCH-WFI01, 63179 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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63179 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: 11 hours ago
TLE from 11 hours ago
0 PUNCH-WFI01
1 63179U 25047B 26171.44887147 .00000395 00000-0 67085-4 0 9991
2 63179 97.9584 356.7151 0009423 159.2083 200.9511 14.74351923 68544Epoch: 2026-06-20T10:46Z
TLE epoch observation values (Epoch: 2026-06-20T10:46:22.495Z)
Latitude
0.00003°
Longitude
-73.54197°
Altitude
656.406 km
Speed
7.526 km/s
True Right ascension
23h 46m 51s
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
08:41:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.877 km
Perigee altitude
637.643 km
Semi-major axis
7,022.397 km
Eccentricity
0.00094
Inclination
97.9584°
RAAN
356.7151°
Arg. of periapsis
159.2083°
True anomaly
200.91253°
Mean anomaly
200.9511°
Eccentric anomaly
200.93181°
Mean motion
3.68821 °/min
Orbital period
97.61 mins
BSTAR
0.000067085
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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-WFI01 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 00:23:45.721Z | 48.823° ENE | 2026-06-21 00:26:45.721Z | 100.218° ESE | 21.571° | 2026-06-21 00:29:45.721Z | 146.008° SSE |
| 6 mins | 2026-06-21 02:00:45.721Z | 338.041° N | 2026-06-21 02:02:45.721Z | 300.445° NW | 26.176° | 2026-06-21 02:06:45.721Z | 231.321° WSW |
| 4 mins | 2026-06-21 11:22:45.721Z | 92.95° ESE | 2026-06-21 11:24:45.721Z | 57.331° ENE | 18.797° | 2026-06-21 11:26:45.721Z | 27.136° NE |
| 6 mins | 2026-06-21 12:57:45.721Z | 203.105° SW | 2026-06-21 13:00:45.721Z | 265.679° W | 30.836° | 2026-06-21 13:03:45.721Z | 323.174° NNW |
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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