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, 0.3 m
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 MUSAT2
1 59099U 24043B 26174.95503330 .00005031 00000-0 32529-3 0 9996
2 59099 97.8605 313.7643 0006051 316.8432 43.2321 15.08664691126117Epoch: 2026-06-23T22:55Z
TLE epoch observation values (Epoch: 2026-06-23T22:55:14.877Z)
Latitude
0.00002°
Longitude
57.83313°
Altitude
540.291 km
Speed
7.594 km/s
True Right ascension
20h 55m 03s
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
06:19:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.465 km
Perigee altitude
533.096 km
Semi-major axis
6,915.417 km
Eccentricity
0.00061
Inclination
97.8605°
RAAN
313.7643°
Arg. of periapsis
316.8432°
True anomaly
43.27962°
Mean anomaly
43.2321°
Eccentric anomaly
43.25586°
Mean motion
3.77412 °/min
Orbital period
95.39 mins
BSTAR
0.00032529
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-24 21:46:04.084Z | 27.078° NE | 2026-06-24 21:50:04.084Z | 119.614° SE | 33.558° | 2026-06-24 21:53:04.084Z | 170.881° S |
| 4 mins | 2026-06-25 08:31:04.084Z | 96.775° ESE | 2026-06-25 08:32:04.084Z | 74.838° E | 21.065° | 2026-06-25 08:35:04.084Z | 19.495° NNE |
| 4 mins | 2026-06-25 10:05:04.084Z | 228.296° WSW | 2026-06-25 10:07:04.084Z | 273.088° WNW | 21.583° | 2026-06-25 10:09:04.084Z | 310.443° NW |
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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