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: 19 hours ago
TLE from 19 hours ago
0 PUNCH-NFI00
1 63178U 25047A 25257.50332377 .00000472 00000-0 78952-4 0 9992
2 63178 97.9560 82.9176 0010547 330.3870 29.6741 14.74229764 27450Epoch: 2025-09-14T12:04Z
TLE epoch observation values (Epoch: 2025-09-14T12:04:47.173Z)
Latitude
0.00004°
Longitude
-92.00035°
Altitude
644.172 km
Speed
7.539 km/s
True Right ascension
05h 31m 40s
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
23:30:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.055 km
Perigee altitude
637.241 km
Semi-major axis
7,022.785 km
Eccentricity
0.00105
Inclination
97.956°
RAAN
82.9176°
Arg. of periapsis
330.387°
True anomaly
29.734°
Mean anomaly
29.6741°
Eccentric anomaly
29.70404°
Mean motion
3.6879 °/min
Orbital period
97.62 mins
BSTAR
0.000078952
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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 | 2025-09-15 12:38:22.364Z | 177.751° S | 2025-09-15 12:41:22.364Z | 233.725° WSW | 42.401° | 2025-09-15 12:45:22.364Z | 340.624° N |
| 5 mins | 2025-09-16 00:31:22.364Z | 58.138° ENE | 2025-09-16 00:33:22.364Z | 96.496° ESE | 23.06° | 2025-09-16 00:36:22.364Z | 145.663° SSE |
| 6 mins | 2025-09-16 02:07:22.364Z | 338.876° N | 2025-09-16 02:10:22.364Z | 279.724° WNW | 25.427° | 2025-09-16 02:13:22.364Z | 234.278° 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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