MUSAT2, 59099
Orbit data source: Space-Track
MUSAT2, 59099 is a payload satellite owned by Muon Space (US) in SSO that was launched on Mon, 04 Mar 2024 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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59099 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
67 kg wet, 67 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 MUSAT2
1 59099U 24043B 25288.31349199 .00010758 00000-0 78029-3 0 9999
2 59099 97.8300 57.5078 0008092 86.1249 274.0901 15.04081575 88221Epoch: 2025-10-15T07:31Z
TLE epoch observation values (Epoch: 2025-10-15T07:31:25.707Z)
Latitude
-0.00008°
Longitude
-79.43866°
Altitude
556.987 km
Speed
7.583 km/s
True Right ascension
03h 50m 01s
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
08:20:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
556.939 km
Perigee altitude
545.725 km
Semi-major axis
6,929.469 km
Eccentricity
0.00081
Inclination
97.83°
RAAN
57.5078°
Arg. of periapsis
86.1249°
True anomaly
273.9976°
Mean anomaly
274.0901°
Eccentric anomaly
274.04385°
Mean motion
3.76264 °/min
Orbital period
95.68 mins
BSTAR
0.00078029
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Other satellites on launch #43 in the year 2024 (2024-03-04 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.MUSAT2 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 | 2025-10-16 20:49:40.933Z | 48.091° ENE | 2025-10-16 20:52:40.933Z | 105.286° ESE | 20.698° | 2025-10-16 20:54:40.933Z | 140.894° SSE |
| 4 mins | 2025-10-16 22:25:40.933Z | 320.443° NNW | 2025-10-16 22:26:40.933Z | 298.062° NW | 22.357° | 2025-10-16 22:29:40.933Z | 240.417° WSW |
| 5 mins | 2025-10-17 09:09:40.933Z | 201.536° SSW | 2025-10-17 09:11:40.933Z | 263.418° W | 34.933° | 2025-10-17 09:14:40.933Z | 330.28° NNW |
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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