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, 3.0 m
Radar Cross Section
2.251 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 METHANESAT
1 59101U 24043D 26106.27202012 .00000930 00000-0 84221-4 0 9993
2 59101 97.8351 237.0562 0009610 212.4677 147.5955 14.97833286115386Epoch: 2026-04-16T06:31Z
TLE epoch observation values (Epoch: 2026-04-16T06:31:42.538Z)
Latitude
0.00001°
Longitude
-65.29299°
Altitude
582.283 km
Speed
7.566 km/s
True Right ascension
15h 48m 13s
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
09:25:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.284 km
Perigee altitude
563.929 km
Semi-major axis
6,948.744 km
Eccentricity
0.00096
Inclination
97.8351°
RAAN
237.0562°
Arg. of periapsis
212.4677°
True anomaly
147.65445°
Mean anomaly
147.5955°
Eccentric anomaly
147.62498°
Mean motion
3.747 °/min
Orbital period
96.08 mins
BSTAR
0.000084221
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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 | 2026-04-17 08:18:42.782Z | 143.912° SSE | 2026-04-17 08:21:42.782Z | 85.611° E | 36.001° | 2026-04-17 08:25:42.782Z | 0.314° NNE |
| 6 mins | 2026-04-17 21:35:42.782Z | 12.394° NNE | 2026-04-17 21:37:42.782Z | 2.523° NNE | 44.945° | 2026-04-17 21:41:42.782Z | 193.903° SSW |
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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