FIRESAT0, 63256
Orbit data source: Space-Track
FIRESAT0, 63256 is a payload satellite owned by Muon Space (US) in SSO that was launched on Sat, 15 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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63256 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Muon Space
Mission
Operational Commercial Imaging
Bus & Motor
MUON, Unknown motor
Mass
135 kg wet, 132 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.7 m
Radar Cross Section
2.173 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 FIRESAT0
1 63256U 25052AY 25334.59978346 .00002008 00000-0 19788-3 0 9990
2 63256 97.7102 224.9099 0001338 80.9959 279.1412 14.93140268 38960Epoch: 2025-11-30T14:23Z
TLE epoch observation values (Epoch: 2025-11-30T14:23:41.290Z)
Latitude
-0.00006°
Longitude
-60.72345°
Altitude
591.048 km
Speed
7.565 km/s
True Right ascension
14h 59m 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
21:17:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.098 km
Perigee altitude
584.234 km
Semi-major axis
6,963.303 km
Eccentricity
0.00013
Inclination
97.7102°
RAAN
224.9099°
Arg. of periapsis
80.9959°
True anomaly
279.12606°
Mean anomaly
279.1412°
Eccentric anomaly
279.13363°
Mean motion
3.73525 °/min
Orbital period
96.38 mins
BSTAR
0.00019788
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Other satellites on launch #52 in the year 2025 (2025-03-15 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.FIRESAT0 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 | 2025-12-01 05:26:06.250Z | 22.808° NE | 2025-12-01 05:30:06.250Z | 121.196° SE | 38.682° | 2025-12-01 05:33:06.250Z | 176.138° S |
| 5 mins | 2025-12-01 16:17:06.250Z | 117.611° SE | 2025-12-01 16:19:06.250Z | 67.602° E | 28.69° | 2025-12-01 16:22:06.250Z | 11.258° NNE |
| 4 mins | 2025-12-01 17:53:06.250Z | 240.541° WSW | 2025-12-01 17:54:06.250Z | 258.046° W | 17.224° | 2025-12-01 17:57:06.250Z | 307.508° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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