OPTUS 10, 40146
Orbit data source: Space-Track
OPTUS 10, 40146 is a payload satellite owned by SingTel Optus (AU) in GEO that was launched on Thu, 11 Sep 2014 UTC via an ARIANE 5ECA 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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40146 intel report (Beta)
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Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
SS/Loral (MDA)
Mission
Operational Commercial Communications
Bus & Motor
LS-1300LL, R-4D
Mass
3,970 kg wet, ~2,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 12.4 m
Radar Cross Section
38.560 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OPTUS 10
1 40146U 14054A 26257.17835721 -.00000156 00000-0 00000-0 0 9998
2 40146 0.0943 30.1658 0002041 139.2274 43.9942 1.00271351 43920Epoch: 2026-09-14T04:16Z
TLE epoch observation values (Epoch: 2026-09-14T04:16:50.062Z)
Latitude
0.01567°
Longitude
156.0283°
Altitude
35,779.98 km
Speed
3.075 km/s
True Right ascension
14h 13m 35s
True Declination
0° 00' 56"
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
03:49:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,796.393 km
Perigee altitude
35,779.181 km
Semi-major axis
42,165.924 km
Eccentricity
0.0002
Inclination
0.0943°
RAAN
30.1658°
Arg. of periapsis
139.2274°
True anomaly
44.01045°
Mean anomaly
43.9942°
Eccentric anomaly
44.00232°
Mean motion
0.25067 °/min
Orbital period
1,436.16 mins
BSTAR
0
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Other satellites on launch #54 in the year 2014 (2014-09-11 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.OPTUS 10 Visibility
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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. |
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| OPTUS 10 is likely not visible in the next few days. |
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40146 neighbors
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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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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