DMC 3-FM2, 40716
Orbit data source: Space-Track
DMC 3-FM2, 40716 is a payload satellite owned by DMCii (UK) in SSO that was launched on Fri, 10 Jul 2015 UTC via a PSLV-XL launch vehicle from the Sirharikota (SRI). 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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40716 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
SSTL (Astrium)
Mission
Operational Commercial Imaging
Bus & Motor
SSTL-300S1, Unknown motor
Mass
447 kg wet, 435 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hept Cyl + Cyl, 1.3 m
Radar Cross Section
2.356 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 DMC 3-FM2
1 40716U 15032B 26306.89056244 .00000078 00000-0 14810-4 0 9997
2 40716 97.6278 168.1421 0005488 336.2270 23.8692 14.85866431610508Epoch: 2026-11-02T21:22Z
TLE epoch observation values (Epoch: 2026-11-02T21:22:24.594Z)
Latitude
-0.00001°
Longitude
165.37854°
Altitude
610.397 km
Speed
7.556 km/s
True Right ascension
11h 12m 34s
True Declination
0° 00' 00"
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
02:15:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
611.723 km
Perigee altitude
604.055 km
Semi-major axis
6,986.026 km
Eccentricity
0.00055
Inclination
97.6278°
RAAN
168.1421°
Arg. of periapsis
336.227°
True anomaly
23.89466°
Mean anomaly
23.8692°
Eccentric anomaly
23.88193°
Mean motion
3.71705 °/min
Orbital period
96.85 mins
BSTAR
0.00001481
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Other satellites on launch #32 in the year 2015 (2015-07-10 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.DMC 3-FM2 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-03 13:42:19.602Z | 92.117° ESE | 2026-11-03 13:44:19.602Z | 62.732° ENE | 14.061° | 2026-11-03 13:46:19.602Z | 34.311° NE |
| 6 mins | 2026-11-03 15:17:19.602Z | 194.079° SSW | 2026-11-03 15:19:19.602Z | 240.917° WSW | 49.084° | 2026-11-03 15:23:19.602Z | 334.983° NNW |
| 6 mins | 2026-11-04 03:03:19.602Z | 46.262° ENE | 2026-11-04 03:06:19.602Z | 106.56° ESE | 27.583° | 2026-11-04 03:09:19.602Z | 153.597° SSE |
| 5 mins | 2026-11-04 04:39:19.602Z | 334.343° NNW | 2026-11-04 04:41:19.602Z | 300.033° NW | 23.632° | 2026-11-04 04:44:19.602Z | 245.78° WSW |
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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