O3B FM20, 44112
Orbit data source: Space-Track
O3B FM20, 44112 is a payload satellite owned by O3B SES (JE) that was launched on Thu, 04 Apr 2019 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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44112 intel report (Beta)
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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 FM20
1 44112U 19020A 26223.18188966 -.00000025 00000-0 00000+0 0 9993
2 44112 0.0537 353.9748 0002329 146.2945 219.7443 5.00115539134327Epoch: 2026-08-11T04:21Z
TLE epoch observation values (Epoch: 2026-08-11T04:21:55.266Z)
Latitude
0.00064°
Longitude
-25.13413°
Altitude
8,066.959 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
12:42:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
8,072.313 km
Perigee altitude
8,065.583 km
Semi-major axis
14,447.085 km
Eccentricity
0.00023
Inclination
0.0537°
RAAN
353.9748°
Arg. of periapsis
146.2945°
True anomaly
219.72724°
Mean anomaly
219.7443°
Eccentric anomaly
219.73577°
Mean motion
1.24989 °/min
Orbital period
288.02 mins
BSTAR
0
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Other satellites on launch #20 in the year 2019 (2019-04-04 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 FM20 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 | 2026-08-12 02:22:13.854Z | 232.284° WSW | 2026-08-12 03:02:13.854Z | 179.479° S | 24.322° | 2026-08-12 03:41:13.854Z | 128.068° SE |
| 78 mins | 2026-08-12 08:23:13.854Z | 231.297° WSW | 2026-08-12 09:02:13.854Z | 179.536° S | 24.368° | 2026-08-12 09:41:13.854Z | 128.043° SE |
| 78 mins | 2026-08-12 14:23:13.854Z | 231.385° WSW | 2026-08-12 15:02:13.854Z | 179.55° S | 24.416° | 2026-08-12 15:41:13.854Z | 128.019° SE |
| 78 mins | 2026-08-12 20:23:13.854Z | 231.378° WSW | 2026-08-12 21:02:13.854Z | 179.493° S | 24.37° | 2026-08-12 21:41:13.854Z | 128.044° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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