METHANESAT, 59101
Orbit data source: Space-Track
METHANESAT, 59101 is a payload satellite owned by MethaneSAT (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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Blue Canyon
Mission
Non-operational Amateur Earth Obs Sci
Bus & Motor
SATURN X-SAT, NANO-R3
Mass
362 kg wet, 326 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
2.251 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 METHANESAT
1 59101U 24043D 25292.28156160 .00007617 00000-0 67896-3 0 9998
2 59101 97.8158 57.9110 0011650 95.5776 264.6774 14.96236180 88609Epoch: 2025-10-19T06:45Z
TLE epoch observation values (Epoch: 2025-10-19T06:45:26.922Z)
Latitude
-0.00001°
Longitude
-71.45165°
Altitude
582.346 km
Speed
7.569 km/s
True Right ascension
03h 51m 38s
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
06:38:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.655 km
Perigee altitude
567.453 km
Semi-major axis
6,953.691 km
Eccentricity
0.00117
Inclination
97.8158°
RAAN
57.911°
Arg. of periapsis
95.5776°
True anomaly
264.54449°
Mean anomaly
264.6774°
Eccentric anomaly
264.61095°
Mean motion
3.743 °/min
Orbital period
96.18 mins
BSTAR
0.00067896
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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.METHANESAT 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 | 2025-10-19 21:46:43.461Z | 351.388° N | 2025-10-19 21:48:43.461Z | 305.941° NW | 35.412° | 2025-10-19 21:52:43.461Z | 214.167° SW |
| 6 mins | 2025-10-20 08:34:43.461Z | 171.022° S | 2025-10-20 08:36:43.461Z | 198.775° SSW | 44.197° | 2025-10-20 08:40:43.461Z | 345.743° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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