O3B FM12, 40350
Orbit data source: Space-Track
O3B FM12, 40350 is a payload satellite owned by O3B (JE) that was launched on Thu, 18 Dec 2014 UTC via a SOYUZ-ST-B 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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40350 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / O3BRelated business
Manufacturer
Thales Alenia
Mission
Operational Commercial Communications
Bus & Motor
PRISMA?, LS-400 AOCS?
Mass
700 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 6.0 m
Radar Cross Section
21.980 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 O3B FM12
1 40350U 14083C 25300.72647980 -.00000017 00000-0 00000-0 0 9990
2 40350 0.0505 4.7202 0002814 208.1248 147.1446 5.00115851198291Epoch: 2025-10-27T17:26Z
TLE epoch observation values (Epoch: 2025-10-27T17:26:07.854Z)
Latitude
-0.00053°
Longitude
62.14302°
Altitude
8,067.781 km
Speed
5.253 km/s
True Right ascension
23h 59m 59s
True Declination
0° 00' 02"
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
06:37:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
8,073.007 km
Perigee altitude
8,064.877 km
Semi-major axis
14,447.079 km
Eccentricity
0.00028
Inclination
0.0505°
RAAN
4.7202°
Arg. of periapsis
208.1248°
True anomaly
147.16209°
Mean anomaly
147.1446°
Eccentric anomaly
147.15335°
Mean motion
1.24989 °/min
Orbital period
288.02 mins
BSTAR
0
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Other satellites on launch #83 in the year 2014 (2014-12-18 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.O3B FM12 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. |
|---|---|---|---|---|---|---|---|
| 79 mins | 2025-10-28 13:59:06.114Z | 232.49° WSW | 2025-10-28 14:39:06.114Z | 179.708° S | 24.389° | 2025-10-28 15:18:06.114Z | 128.158° SE |
| 78 mins | 2025-10-28 20:00:06.114Z | 231.435° WSW | 2025-10-28 20:39:06.114Z | 179.639° S | 24.323° | 2025-10-28 21:18:06.114Z | 128.141° SE |
| 78 mins | 2025-10-29 02:00:06.114Z | 231.367° WSW | 2025-10-29 02:39:06.114Z | 179.619° S | 24.351° | 2025-10-29 03:18:06.114Z | 128.117° SE |
| 79 mins | 2025-10-29 08:00:06.114Z | 231.43° WSW | 2025-10-29 08:39:06.114Z | 179.687° S | 24.416° | 2025-10-29 09:19:06.114Z | 127.15° SE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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