PUNCH-NFI00, 63178
Orbit data source: Space-Track
PUNCH-NFI00, 63178 is a payload satellite owned by JPL (US) 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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
BAEB
Mission
Operational Civil Astronomy
Bus & Motor
SPHEREX, Unknown motor
Mass
502 kg wet, 502 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: 13 hours ago
TLE from 13 hours ago
0 PUNCH-NFI00
1 63178U 25047A 25308.47386865 .00000914 00000-0 14532-3 0 9990
2 63178 97.9532 132.9588 0011660 154.3452 205.8337 14.74355772 34961Epoch: 2025-11-04T11:22Z
TLE epoch observation values (Epoch: 2025-11-04T11:22:22.251Z)
Latitude
-0.00006°
Longitude
-81.59428°
Altitude
657.586 km
Speed
7.525 km/s
True Right ascension
08h 51m 50s
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
20:35:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.436 km
Perigee altitude
636.06 km
Semi-major axis
7,022.385 km
Eccentricity
0.00117
Inclination
97.9532°
RAAN
132.9588°
Arg. of periapsis
154.3452°
True anomaly
205.77555°
Mean anomaly
205.8337°
Eccentric anomaly
205.80462°
Mean motion
3.68822 °/min
Orbital period
97.61 mins
BSTAR
0.00014532
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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 | 2025-11-05 00:58:52.038Z | 26.497° NE | 2025-11-05 01:01:52.038Z | 78.629° E | 37.424° | 2025-11-05 01:05:52.038Z | 174.199° S |
| 6 mins | 2025-11-05 11:56:52.038Z | 133.597° SE | 2025-11-05 11:59:52.038Z | 64.574° ENE | 33.608° | 2025-11-05 12:02:52.038Z | 7.283° NNE |
| 4 mins | 2025-11-05 13:34:52.038Z | 241.587° WSW | 2025-11-05 13:36:52.038Z | 273.548° WNW | 16.232° | 2025-11-05 13:38:52.038Z | 302.496° 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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