O3B FM7, 40080
Orbit data source: Space-Track
O3B FM7, 40080 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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40080 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: 11 hours ago
TLE from 11 hours ago
0 O3B FM7
1 40080U 14038B 25258.00250108 -.00000026 00000-0 00000-0 0 9995
2 40080 0.0598 4.5067 0004032 189.5505 165.9323 5.00115468204117Epoch: 2025-09-15T00:03Z
TLE epoch observation values (Epoch: 2025-09-15T00:03:36.093Z)
Latitude
-0.00623°
Longitude
4.88621°
Altitude
8,070.025 km
Speed
5.252 km/s
True Right ascension
00h 00m 00s
True Declination
0° 00' 22"
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
04:08:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
8,074.774 km
Perigee altitude
8,063.124 km
Semi-major axis
14,447.086 km
Eccentricity
0.0004
Inclination
0.0598°
RAAN
4.5067°
Arg. of periapsis
189.5505°
True anomaly
165.94353°
Mean anomaly
165.9323°
Eccentric anomaly
165.93791°
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 FM7 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 | 2025-09-15 15:34:21.176Z | 231.986° WSW | 2025-09-15 16:13:21.176Z | 180.462° SSW | 24.407° | 2025-09-15 16:53:21.176Z | 127.622° SE |
| 78 mins | 2025-09-15 21:35:21.176Z | 230.925° WSW | 2025-09-15 22:13:21.176Z | 180.364° SSW | 24.329° | 2025-09-15 22:53:21.176Z | 127.613° SE |
| 78 mins | 2025-09-16 03:35:21.176Z | 230.817° WSW | 2025-09-16 04:13:21.176Z | 180.335° SSW | 24.332° | 2025-09-16 04:53:21.176Z | 127.608° SE |
| 78 mins | 2025-09-16 09:35:21.176Z | 230.88° WSW | 2025-09-16 10:13:21.176Z | 180.434° SSW | 24.41° | 2025-09-16 10:53:21.176Z | 127.618° 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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