PUNCH-NFI00, 63178
Orbit data source: Space-Track
PUNCH-NFI00, 63178 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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63178 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
Cyl + Cone + 2 Pan, 1.9 m
Radar Cross Section
10.556 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 PUNCH-NFI00
1 63178U 25047A 26098.46292230 .00000547 00000-0 89274-4 0 9996
2 63178 97.9569 285.1612 0011678 28.9962 331.1893 14.74698113 57808Epoch: 2026-04-08T11:06Z
TLE epoch observation values (Epoch: 2026-04-08T11:06:36.486Z)
Latitude
-0.00007°
Longitude
-78.21575°
Altitude
641.935 km
Speed
7.541 km/s
True Right ascension
19h 00m 38s
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
04:57:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.36 km
Perigee altitude
634.961 km
Semi-major axis
7,021.297 km
Eccentricity
0.00117
Inclination
97.9569°
RAAN
285.1612°
Arg. of periapsis
28.9962°
True anomaly
331.12473°
Mean anomaly
331.1893°
Eccentric anomaly
331.15702°
Mean motion
3.68907 °/min
Orbital period
97.59 mins
BSTAR
0.000089274
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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-NFI00 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 | 2026-04-09 00:42:53.733Z | 33.727° NE | 2026-04-09 00:46:53.733Z | 113.577° SE | 30.251° | 2026-04-09 00:49:53.733Z | 161.868° S |
| 5 mins | 2026-04-09 02:20:53.733Z | 324.954° NNW | 2026-04-09 02:22:53.733Z | 290.908° WNW | 19.005° | 2026-04-09 02:25:53.733Z | 247.48° WSW |
| 5 mins | 2026-04-09 11:41:53.733Z | 110.271° ESE | 2026-04-09 11:43:53.733Z | 65.982° ENE | 26.4° | 2026-04-09 11:46:53.733Z | 14.313° NNE |
| 5 mins | 2026-04-09 13:17:53.733Z | 222.032° SW | 2026-04-09 13:19:53.733Z | 255.055° W | 21.244° | 2026-04-09 13:22:53.733Z | 308.661° NW |
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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