O3B FM8, 40082
Orbit data source: Space-Track
O3B FM8, 40082 is a payload satellite owned by O3B (JE) that was launched on Thu, 10 Jul 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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40082 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: 3 days ago
TLE from 3 days ago
0 O3B FM8
1 40082U 14038D 25259.28229155 -.00000029 00000-0 00000-0 0 9999
2 40082 0.0577 1.6769 0002520 173.0766 185.2492 5.00115828204246Epoch: 2025-09-16T06:46Z
TLE epoch observation values (Epoch: 2025-09-16T06:46:29.989Z)
Latitude
-0.00354°
Longitude
-97.09977°
Altitude
8,067.993 km
Speed
5.253 km/s
True Right ascension
00h 00m 00s
True Declination
0° 00' 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
17:40:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
8,072.583 km
Perigee altitude
8,065.302 km
Semi-major axis
14,447.079 km
Eccentricity
0.00025
Inclination
0.0577°
RAAN
1.6769°
Arg. of periapsis
173.0766°
True anomaly
185.24656°
Mean anomaly
185.2492°
Eccentric anomaly
185.24788°
Mean motion
1.24989 °/min
Orbital period
288.02 mins
BSTAR
0
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Other satellites on launch #38 in the year 2014 (2014-07-10 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 FM8 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. |
|---|---|---|---|---|---|---|---|
| 29 mins | 2025-09-19 00:48:37.317Z | 164.374° S | 2025-09-19 00:48:37.317Z | 164.374° S | 23.305° | 2025-09-19 01:17:37.317Z | 128.218° SE |
| 79 mins | 2025-09-19 05:59:37.317Z | 231.446° WSW | 2025-09-19 06:38:37.317Z | 179.77° S | 24.368° | 2025-09-19 07:18:37.317Z | 127.216° SE |
| 79 mins | 2025-09-19 11:59:37.317Z | 231.542° WSW | 2025-09-19 12:38:37.317Z | 179.817° S | 24.42° | 2025-09-19 13:18:37.317Z | 127.211° SE |
| 78 mins | 2025-09-19 17:59:37.317Z | 231.558° WSW | 2025-09-19 18:38:37.317Z | 179.775° S | 24.371° | 2025-09-19 19:17:37.317Z | 128.212° SE |
| 49 mins | 2025-09-19 23:59:37.317Z | 231.463° WSW | 2025-09-20 00:38:37.317Z | 179.728° S | 24.32° | 2025-09-20 00:48:37.317Z | 164.374° S |
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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