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, 1.6 m
Radar Cross Section
10.556 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 PUNCH-NFI00
1 63178U 25047A 25261.03271478 .00000566 00000-0 93153-4 0 9993
2 63178 97.9560 86.3826 0010314 318.2938 41.7483 14.74234469 27975Epoch: 2025-09-18T00:47Z
TLE epoch observation values (Epoch: 2025-09-18T00:47:06.556Z)
Latitude
-0.0001°
Longitude
77.40517°
Altitude
645.19 km
Speed
7.538 km/s
True Right ascension
05h 45m 31s
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
21:17:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.877 km
Perigee altitude
637.39 km
Semi-major axis
7,022.77 km
Eccentricity
0.00103
Inclination
97.956°
RAAN
86.3826°
Arg. of periapsis
318.2938°
True anomaly
41.82707°
Mean anomaly
41.7483°
Eccentric anomaly
41.78768°
Mean motion
3.68791 °/min
Orbital period
97.62 mins
BSTAR
0.000093153
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-19 11:09:53.204Z | 91.322° ESE | 2025-09-19 11:11:53.204Z | 63.653° ENE | 13.403° | 2025-09-19 11:13:53.204Z | 35.995° NE |
| 7 mins | 2025-09-19 12:44:53.204Z | 184.711° SSW | 2025-09-19 12:47:53.204Z | 249.165° W | 39.892° | 2025-09-19 12:51:53.204Z | 337.188° NNW |
| 6 mins | 2025-09-20 00:36:53.204Z | 43.792° NE | 2025-09-20 00:39:53.204Z | 99.285° ESE | 26.104° | 2025-09-20 00:42:53.204Z | 151.108° SSE |
| 6 mins | 2025-09-20 02:13:53.204Z | 334.602° NNW | 2025-09-20 02:15:53.204Z | 300.645° NW | 22.697° | 2025-09-20 02:19:53.204Z | 237.567° WSW |
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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