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: 14 hours ago
TLE from 14 hours ago
0 METHANESAT
1 59101U 24043D 25321.90446396 .00005206 00000-0 46215-3 0 9997
2 59101 97.8199 87.5032 0010560 4.4679 355.6634 14.96557973 93031Epoch: 2025-11-17T21:42Z
TLE epoch observation values (Epoch: 2025-11-17T21:42:25.686Z)
Latitude
-0.00006°
Longitude
64.69797°
Altitude
573.262 km
Speed
7.578 km/s
True Right ascension
05h 50m 00s
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
08:49:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.898 km
Perigee altitude
567.214 km
Semi-major axis
6,952.693 km
Eccentricity
0.00106
Inclination
97.8199°
RAAN
87.5032°
Arg. of periapsis
4.4679°
True anomaly
355.65424°
Mean anomaly
355.6634°
Eccentric anomaly
355.65882°
Mean motion
3.74381 °/min
Orbital period
96.16 mins
BSTAR
0.00046215
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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 | 2025-11-18 20:44:26.132Z | 35.426° NE | 2025-11-18 20:48:26.132Z | 109.14° ESE | 25.703° | 2025-11-18 20:51:26.132Z | 157.204° SSE |
| 4 mins | 2025-11-18 22:21:26.132Z | 323.3° NNW | 2025-11-18 22:23:26.132Z | 284.228° WNW | 19.521° | 2025-11-18 22:25:26.132Z | 250.611° W |
| 4 mins | 2025-11-19 07:34:26.132Z | 95.373° ESE | 2025-11-19 07:36:26.132Z | 58.294° ENE | 17.375° | 2025-11-19 07:38:26.132Z | 26.824° NE |
| 6 mins | 2025-11-19 09:08:26.132Z | 206.823° SW | 2025-11-19 09:11:26.132Z | 276.246° WNW | 27.764° | 2025-11-19 09:14:26.132Z | 325.933° 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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