METOP SG-A, 65159
Orbit data source: Space-Track
METOP SG-A, 65159 is a payload satellite owned by EUMETSAT (ESA) in SSO that was launched on Wed, 13 Aug 2025 UTC via an ARIANE 62 launch vehicle from the French Guiana (FRGUI). 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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65159 intel report (Beta)
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Identifier
Orbit
Country
ESARelated business
Manufacturer
Airbus/Toulouse
Mission
Operational Civil Weather
Bus & Motor
METOP, AOCS
Mass
4,050 kg wet, 3,250 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 3.8 m
Radar Cross Section
32.163 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 METOP SG-A
1 65159U 25172A 26167.15332899 .00000049 00000-0 42000-4 0 9998
2 65159 98.6644 226.8998 0000902 93.8213 266.3067 14.21509720 43644Epoch: 2026-06-16T03:40Z
TLE epoch observation values (Epoch: 2026-06-16T03:40:47.624Z)
Latitude
-0.0001°
Longitude
-92.72807°
Altitude
823.211 km
Speed
7.441 km/s
True Right ascension
15h 07m 35s
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
07:22:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
818.055 km
Perigee altitude
816.757 km
Semi-major axis
7,195.543 km
Eccentricity
0.00009
Inclination
98.6644°
RAAN
226.8998°
Arg. of periapsis
93.8213°
True anomaly
266.29639°
Mean anomaly
266.3067°
Eccentric anomaly
266.30154°
Mean motion
3.55589 °/min
Orbital period
101.24 mins
BSTAR
0.000042
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Other satellites on launch #172 in the year 2025 (2025-08-13 UTC)
No other RSOs were in this launch
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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.METOP SG-A 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-21 03:44:03.922Z | 155.489° SSE | 2026-06-21 03:49:03.922Z | 47.269° ENE | 42.896° | 2026-06-21 03:53:03.922Z | 352.722° N |
| 7 mins | 2026-06-21 16:03:03.922Z | 44.618° NE | 2026-06-21 16:06:03.922Z | 87.758° E | 25.88° | 2026-06-21 16:10:03.922Z | 148.976° SSE |
| 8 mins | 2026-06-21 17:43:03.922Z | 347.097° N | 2026-06-21 17:46:03.922Z | 302.867° NW | 28.892° | 2026-06-21 17:51:03.922Z | 229.871° WSW |
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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