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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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, 1.0 m
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 MUSAT2
1 59099U 24043B 26295.08475426 .00007994 00000-0 49646-3 0 9996
2 59099 97.8770 76.9742 0005903 261.6854 98.3705 15.09953203144239Epoch: 2026-10-22T02:02Z
TLE epoch observation values (Epoch: 2026-10-22T02:02:02.768Z)
Latitude
-0°
Longitude
15.93794°
Altitude
540.002 km
Speed
7.592 km/s
True Right ascension
05h 07m 53s
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
14:22:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
537.423 km
Perigee altitude
529.263 km
Semi-major axis
6,911.48 km
Eccentricity
0.00059
Inclination
97.877°
RAAN
76.9742°
Arg. of periapsis
261.6854°
True anomaly
98.43742°
Mean anomaly
98.3705°
Eccentric anomaly
98.40396°
Mean motion
3.77734 °/min
Orbital period
95.31 mins
BSTAR
0.00049646
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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 | 2026-10-22 21:41:42.680Z | 44.72° NE | 2026-10-22 21:44:42.680Z | 98.184° ESE | 22.272° | 2026-10-22 21:46:42.680Z | 137.129° SSE |
| 4 mins | 2026-10-22 23:17:42.680Z | 319.397° NNW | 2026-10-22 23:18:42.680Z | 296.563° NW | 24.175° | 2026-10-22 23:21:42.680Z | 239.62° WSW |
| 6 mins | 2026-10-23 09:58:42.680Z | 194.162° SSW | 2026-10-23 10:00:42.680Z | 244.179° WSW | 46.491° | 2026-10-23 10:04:42.680Z | 335.306° 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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