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: 20 hours ago
TLE from 20 hours ago
0 PUNCH-NFI00
1 63178U 25047A 25311.46002391 .00001222 00000-0 19175-3 0 9993
2 63178 97.9529 135.8903 0011823 145.2170 214.9814 14.74364403 35409Epoch: 2025-11-07T11:02Z
TLE epoch observation values (Epoch: 2025-11-07T11:02:26.065Z)
Latitude
-0.00002°
Longitude
-76.62198°
Altitude
656.992 km
Speed
7.525 km/s
True Right ascension
09h 03m 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
03:15:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.523 km
Perigee altitude
635.918 km
Semi-major axis
7,022.357 km
Eccentricity
0.00118
Inclination
97.9529°
RAAN
135.8903°
Arg. of periapsis
145.217°
True anomaly
214.90382°
Mean anomaly
214.9814°
Eccentric anomaly
214.9426°
Mean motion
3.68824 °/min
Orbital period
97.61 mins
BSTAR
0.00019175
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-08 11:36:49.953Z | 121.477° SE | 2025-11-08 11:39:49.953Z | 74.157° E | 23.898° | 2025-11-08 11:42:49.953Z | 20.327° NNE |
| 5 mins | 2025-11-08 13:14:49.953Z | 227.149° WSW | 2025-11-08 13:16:49.953Z | 269.145° W | 24.53° | 2025-11-08 13:19:49.953Z | 318.1° NNW |
| 6 mins | 2025-11-09 01:05:49.953Z | 28.276° NE | 2025-11-09 01:07:49.953Z | 75.444° E | 40.469° | 2025-11-09 01:11:49.953Z | 179.833° S |
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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