MTG-I2, 100530
Orbit data source: Space-Track
MTG-I2, 100530 is a payload satellite owned by EUMETSAT (ESA) in GEO that was launched on Thu, 27 Aug 2026 UTC launched 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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100530 intel report (Beta)
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Identifier
Orbit
Country
ESARelated business
Manufacturer
Thales Alenia
Mission
Operational spacecraft
Bus & Motor
MTG, S400 X2
Mass
3,800 kg wet, ~2,500 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
BOX + 2 PAN, 5.0 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 MTG-I2
1 A0530U 26198A 26248.14836412 .00000062 00000-0 00000-0 0 9993
2 A0530 1.0191 301.4746 0012857 264.6956 194.7576 1.00597412 130Epoch: 2026-09-05T03:33Z
TLE epoch observation values (Epoch: 2026-09-05T03:33:38.659Z)
Latitude
0.98801°
Longitude
3.21753°
Altitude
35,747.158 km
Speed
3.074 km/s
True Right ascension
02h 43m 33s
True Declination
0° 59' 13"
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
10:28:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,750.724 km
Perigee altitude
35,642.533 km
Semi-major axis
42,074.765 km
Eccentricity
0.00129
Inclination
1.0191°
RAAN
301.4746°
Arg. of periapsis
264.6956°
True anomaly
194.72013°
Mean anomaly
194.7576°
Eccentric anomaly
194.73886°
Mean motion
0.25148 °/min
Orbital period
1,431.5 mins
BSTAR
0
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Other satellites on launch #198 in the year 2026 (2026-08-27 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.MTG-I2 Visibility
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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. |
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| MTG-I2 is likely not visible in the next few days. |
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100530 neighbors
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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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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