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: 15 hours ago
TLE from 15 hours ago
0 FIRESAT0
1 63256U 25052AY 26129.66318356 .00000766 00000-0 79280-4 0 9993
2 63256 97.7003 21.6733 0002070 71.3165 288.8279 14.92851604 62848Epoch: 2026-05-09T15:54Z
TLE epoch observation values (Epoch: 2026-05-09T15:54:59.059Z)
Latitude
-0.00004°
Longitude
-84.55016°
Altitude
591.629 km
Speed
7.564 km/s
True Right ascension
01h 26m 41s
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
15:09:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.506 km
Perigee altitude
584.622 km
Semi-major axis
6,964.201 km
Eccentricity
0.00021
Inclination
97.7003°
RAAN
21.6733°
Arg. of periapsis
71.3165°
True anomaly
288.80545°
Mean anomaly
288.8279°
Eccentric anomaly
288.81667°
Mean motion
3.73453 °/min
Orbital period
96.4 mins
BSTAR
0.00007928
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-10 16:12:19.688Z | 114.689° SE | 2026-05-10 16:14:19.688Z | 63.486° ENE | 28.065° | 2026-05-10 16:17:19.688Z | 10.703° NNE |
| 4 mins | 2026-05-10 17:48:19.688Z | 242.075° WSW | 2026-05-10 17:49:19.688Z | 260.176° W | 17.714° | 2026-05-10 17:52:19.688Z | 309.214° NW |
| 6 mins | 2026-05-11 05:30:19.688Z | 25.087° NE | 2026-05-11 05:32:19.688Z | 89.382° E | 42.572° | 2026-05-11 05:36:19.688Z | 184.084° 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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