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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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: 16 hours ago
TLE from 16 hours ago
0 FIRESAT0
1 63256U 25052AY 26083.41259627 .00001159 00000-0 11762-3 0 9997
2 63256 97.7059 336.4086 0001506 108.7536 251.3847 14.92729373 55943Epoch: 2026-03-24T09:54Z
TLE epoch observation values (Epoch: 2026-03-24T09:54:08.317Z)
Latitude
-0.00003°
Longitude
5.98333°
Altitude
592.809 km
Speed
7.563 km/s
True Right ascension
22h 25m 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
06:58:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.494 km
Perigee altitude
585.396 km
Semi-major axis
6,964.582 km
Eccentricity
0.00015
Inclination
97.7059°
RAAN
336.4086°
Arg. of periapsis
108.7536°
True anomaly
251.36835°
Mean anomaly
251.3847°
Eccentric anomaly
251.37652°
Mean motion
3.73423 °/min
Orbital period
96.41 mins
BSTAR
0.00011762
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.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 | 2026-03-25 05:46:09.630Z | 9.025° NNE | 2026-03-25 05:50:09.630Z | 230.905° WSW | 43.371° | 2026-03-25 05:53:09.630Z | 198.763° SSW |
| 7 mins | 2026-03-25 16:36:09.630Z | 151.816° SSE | 2026-03-25 16:39:09.630Z | 70.702° E | 41.461° | 2026-03-25 16:43:09.630Z | 354.835° N |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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