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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   26251.24318086  .00000520  00000-0  54008-4 0  9995
2 40013  97.5691 122.7684 0002152  66.6203 293.5244 14.93909562650121
Epoch: 2026-09-08T05:50Z
TLE epoch observation values (Epoch: 2026-09-08T05:50:10.826Z)
Latitude
0.00002°
Longitude
47.9109°
Altitude
588.212 km
Speed
7.566 km/s
True Right ascension
08h 11m 04s
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
06:40:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.265 km
Perigee altitude
581.269 km
Semi-major axis
6,960.904 km
Eccentricity
0.00022
Inclination
97.5691°
RAAN
122.7684°
Arg. of periapsis
66.6203°
True anomaly
293.50179°
Mean anomaly
293.5244°
Eccentric anomaly
293.51309°
Mean motion
3.73719 °/min
Orbital period
96.33 mins
BSTAR
0.000054008
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