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: 7 hours ago
TLE from 7 hours ago
0 FIRESAT0
1 63256U 25052AY 26175.17364426 .00001173 00000-0 11838-3 0 9996
2 63256 97.6960 66.1934 0000990 102.4115 257.7216 14.92933557 69634Epoch: 2026-06-24T04:10Z
TLE epoch observation values (Epoch: 2026-06-24T04:10:02.864Z)
Latitude
0.00006°
Longitude
91.34681°
Altitude
591.986 km
Speed
7.564 km/s
True Right ascension
04h 24m 46s
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
21:57:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.498 km
Perigee altitude
585.119 km
Semi-major axis
6,963.946 km
Eccentricity
0.0001
Inclination
97.696°
RAAN
66.1934°
Arg. of periapsis
102.4115°
True anomaly
257.71052°
Mean anomaly
257.7216°
Eccentric anomaly
257.71606°
Mean motion
3.73474 °/min
Orbital period
96.39 mins
BSTAR
0.00011838
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-24 17:10:06.881Z | 193.85° SSW | 2026-06-24 17:13:06.881Z | 279.707° WNW | 35.565° | 2026-06-24 17:16:06.881Z | 332.836° NNW |
| 5 mins | 2026-06-25 04:53:06.881Z | 48.988° ENE | 2026-06-25 04:55:06.881Z | 85.169° E | 22.845° | 2026-06-25 04:58:06.881Z | 143.939° SSE |
| 5 mins | 2026-06-25 06:29:06.881Z | 327.989° NNW | 2026-06-25 06:31:06.881Z | 286.775° WNW | 22.326° | 2026-06-25 06:34:06.881Z | 238.101° 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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