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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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, 5.5 m
Radar Cross Section
2.251 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 METHANESAT
1 59101U 24043D 26304.09260200 .00001097 00000-0 96506-4 0 9990
2 59101 97.8627 76.0149 0009749 276.1196 83.8915 14.98596971145008Epoch: 2026-10-31T02:13Z
TLE epoch observation values (Epoch: 2026-10-31T02:13:20.812Z)
Latitude
-0.00007°
Longitude
3.27491°
Altitude
573.564 km
Speed
7.574 km/s
True Right ascension
05h 04m 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
07:45:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.017 km
Perigee altitude
561.473 km
Semi-major axis
6,946.382 km
Eccentricity
0.00097
Inclination
97.8627°
RAAN
76.0149°
Arg. of periapsis
276.1196°
True anomaly
84.0026°
Mean anomaly
83.8915°
Eccentric anomaly
83.94705°
Mean motion
3.74891 °/min
Orbital period
96.03 mins
BSTAR
0.000096506
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-31 22:00:26.330Z | 6.375° NNE | 2026-10-31 22:04:26.330Z | 274.415° WNW | 66.148° | 2026-10-31 22:07:26.330Z | 205.169° SW |
| 6 mins | 2026-11-01 08:48:26.330Z | 154.618° SSE | 2026-11-01 08:51:26.330Z | 35.344° NE | 63.467° | 2026-11-01 08:54:26.330Z | 353.828° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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