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, 2.5 m
Radar Cross Section
2.173 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 FIRESAT0
1 63256U 25052AY 26193.13571181 .00000443 00000-0 47950-4 0 9994
2 63256 97.6935 83.7593 0001665 110.8498 249.2900 14.92976714 72316Epoch: 2026-07-12T03:15Z
TLE epoch observation values (Epoch: 2026-07-12T03:15:25.500Z)
Latitude
-0.00002°
Longitude
104.86413°
Altitude
592.116 km
Speed
7.564 km/s
True Right ascension
05h 35m 02s
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
22:00:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.834 km
Perigee altitude
584.515 km
Semi-major axis
6,963.811 km
Eccentricity
0.00017
Inclination
97.6935°
RAAN
83.7593°
Arg. of periapsis
110.8498°
True anomaly
249.27215°
Mean anomaly
249.29°
Eccentric anomaly
249.28108°
Mean motion
3.73485 °/min
Orbital period
96.39 mins
BSTAR
0.00004795
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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 | 2026-07-12 16:14:56.952Z | 140.056° SSE | 2026-07-12 16:18:56.952Z | 63.587° ENE | 31.655° | 2026-07-12 16:21:56.952Z | 7.551° NNE |
| 7 mins | 2026-07-13 05:33:56.952Z | 15.528° NNE | 2026-07-13 05:36:56.952Z | 76.329° E | 44.537° | 2026-07-13 05:40:56.952Z | 189.815° SSW |
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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