DEIMOS 2, 40013
Orbit data source: Space-Track
DEIMOS 2, 40013 is a payload satellite owned by Elecnor Deimos (ES) in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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40013 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
ELDEC/SATREC
Mission
Operational Commercial Imaging
Bus & Motor
DEIMOS-2, Unknown motor
Mass
300 kg wet, 300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 3 Pan, 1.5 m
Radar Cross Section
2.520 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 DEIMOS 2
1 40013U 14033D 25287.92804906 .00002623 00000-0 26024-3 0 9991
2 40013 97.6122 165.6659 0002332 76.9030 283.2450 14.92584566601124Epoch: 2025-10-14T22:16Z
TLE epoch observation values (Epoch: 2025-10-14T22:16:23.438Z)
Latitude
-0.00002°
Longitude
167.8588°
Altitude
592.555 km
Speed
7.564 km/s
True Right ascension
11h 02m 39s
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
09:02:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.516 km
Perigee altitude
585.267 km
Semi-major axis
6,965.028 km
Eccentricity
0.00023
Inclination
97.6122°
RAAN
165.6659°
Arg. of periapsis
76.903°
True anomaly
283.21899°
Mean anomaly
283.245°
Eccentric anomaly
283.23199°
Mean motion
3.73387 °/min
Orbital period
96.41 mins
BSTAR
0.00026024
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Other satellites on launch #33 in the year 2014 (2014-06-19 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.DEIMOS 2 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-15 16:05:41.823Z | 173.165° S | 2025-10-15 16:08:41.823Z | 214.136° SW | 43.36° | 2025-10-15 16:12:41.823Z | 343.966° N |
| 5 mins | 2025-10-16 05:25:41.823Z | 335.789° NNW | 2025-10-16 05:27:41.823Z | 282.418° WNW | 30.092° | 2025-10-16 05:30:41.823Z | 226.075° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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