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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 (12 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: 9 hours ago

TLE from 9 hours ago
0 DEIMOS 2
1 40013U 14033D   26124.16991531  .00001008  00000-0  10071-3 0  9990
2 40013  97.5887   0.1957 0002274  88.7284 271.4197 14.93602435631152
Epoch: 2026-05-04T04:04Z
TLE epoch observation values (Epoch: 2026-05-04T04:04:40.682Z)
Latitude
-0.00002°
Longitude
76.96323°
Altitude
589.724 km
Speed
7.565 km/s
True Right ascension
00h 00m 46s
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
21:20:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.306 km
Perigee altitude
582.14 km
Semi-major axis
6,961.86 km
Eccentricity
0.00023
Inclination
97.5887°
RAAN
0.1957°
Arg. of periapsis
88.7284°
True anomaly
271.39365°
Mean anomaly
271.4197°
Eccentric anomaly
271.40667°
Mean motion
3.73642 °/min
Orbital period
96.35 mins
BSTAR
0.00010071
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