O3B FM9, 40351
Orbit data source: Space-Track
O3B FM9, 40351 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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40351 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: 20 hours ago
TLE from 20 hours ago
0 O3B FM9
1 40351U 14083D 25292.15800669 -.00000026 00000-0 00000-0 0 9993
2 40351 0.0498 6.6718 0002722 201.9889 151.3290 5.00115803198006Epoch: 2025-10-19T03:47Z
TLE epoch observation values (Epoch: 2025-10-19T03:47:31.778Z)
Latitude
-0.00229°
Longitude
-84.76106°
Altitude
8,067.819 km
Speed
5.253 km/s
True Right ascension
00h 00m 00s
True Declination
0° 00' 08"
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
18:30:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
8,072.875 km
Perigee altitude
8,065.01 km
Semi-major axis
14,447.08 km
Eccentricity
0.00027
Inclination
0.0498°
RAAN
6.6718°
Arg. of periapsis
201.9889°
True anomaly
151.34396°
Mean anomaly
151.329°
Eccentric anomaly
151.33648°
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 FM9 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. |
|---|---|---|---|---|---|---|---|
| 80 mins | 2025-10-20 02:47:13.890Z | 232.529° WSW | 2025-10-20 03:27:13.890Z | 179.892° S | 24.355° | 2025-10-20 04:07:13.890Z | 127.305° SE |
| 79 mins | 2025-10-20 08:48:13.890Z | 231.607° WSW | 2025-10-20 09:27:13.890Z | 179.96° S | 24.414° | 2025-10-20 10:07:13.890Z | 127.32° SE |
| 79 mins | 2025-10-20 14:48:13.890Z | 231.667° WSW | 2025-10-20 15:27:13.890Z | 179.97° S | 24.385° | 2025-10-20 16:07:13.890Z | 127.337° SE |
| 79 mins | 2025-10-20 20:48:13.890Z | 231.601° WSW | 2025-10-20 21:27:13.890Z | 179.902° S | 24.325° | 2025-10-20 22:07:13.890Z | 127.322° 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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