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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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Identifier
40013, 2014-033D
Orbit
SSO
Country
Flag of ESES / SPN
Related business
Manufacturer
ELDEC/SATREC
Mission
Operational Commercial Imaging
Bus & Motor
DEIMOS-2, Unknown motor
Mass
300 kg wet, 300 kg dry
Launch date (UTC)
2014-06-19 (11 years ago)
Launch vehicle
DNEPR
Launch site
Orenburg, Russia (OREN)
Object type
Payload
Rocket body
Debris
Shape & HBR
Hex Cyl + 3 Pan, 1.5 m
Radar Cross Section
2.520 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 DEIMOS 2
1 40013U 14033D   25334.85088322  .00002127  00000-0  21046-3 0  9990
2 40013  97.6073 211.0427 0000741  73.6976 286.4326 14.92885027608123
Epoch: 2025-11-30T20:25Z
TLE epoch observation values (Epoch: 2025-11-30T20:25:16.310Z)
Latitude
0.00007°
Longitude
-165.23408°
Altitude
591.847 km
Speed
7.564 km/s
True Right ascension
14h 04m 10s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
00:27:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.472 km
Perigee altitude
585.44 km
Semi-major axis
6,964.093 km
Eccentricity
0.00007
Inclination
97.6073°
RAAN
211.0427°
Arg. of periapsis
73.6976°
True anomaly
286.42446°
Mean anomaly
286.4326°
Eccentric anomaly
286.42853°
Mean motion
3.73462 °/min
Orbital period
96.4 mins
BSTAR
0.00021046
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