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: 6 days ago
TLE from 6 days ago
0 O3B FM7
1 40080U 14038B 25282.78892903 -.00000018 00000-0 00000-0 0 9993
2 40080 0.0612 3.4383 0004195 211.0834 145.4569 5.00115384205358Epoch: 2025-10-09T18:56Z
TLE epoch observation values (Epoch: 2025-10-09T18:56:03.468Z)
Latitude
-0.00062°
Longitude
57.34147°
Altitude
8,069.37 km
Speed
5.253 km/s
True Right ascension
00h 00m 00s
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
13:11:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
8,075.011 km
Perigee altitude
8,062.89 km
Semi-major axis
14,447.088 km
Eccentricity
0.00042
Inclination
0.0612°
RAAN
3.4383°
Arg. of periapsis
211.0834°
True anomaly
145.48415°
Mean anomaly
145.4569°
Eccentric anomaly
145.47052°
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 | 2025-10-15 21:34:10.566Z | 232.089° WSW | 2025-10-15 22:13:10.566Z | 180.661° SSW | 24.308° | 2025-10-15 22:53:10.566Z | 127.797° SE |
| 78 mins | 2025-10-16 03:35:10.566Z | 231.014° WSW | 2025-10-16 04:13:10.566Z | 180.643° SSW | 24.36° | 2025-10-16 04:53:10.566Z | 127.779° SE |
| 78 mins | 2025-10-16 09:35:10.566Z | 231.109° WSW | 2025-10-16 10:14:10.566Z | 179.188° S | 24.428° | 2025-10-16 10:53:10.566Z | 127.821° SE |
| 78 mins | 2025-10-16 15:35:10.566Z | 231.185° WSW | 2025-10-16 16:13:10.566Z | 180.767° SSW | 24.376° | 2025-10-16 16:53:10.566Z | 127.839° 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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