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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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: 22 hours ago
TLE from 22 hours ago
0 DEIMOS 2
1 40013U 14033D 26172.53738174 .00001554 00000-0 15187-3 0 9995
2 40013 97.5819 46.8723 0001408 60.2856 299.8504 14.93736204638372Epoch: 2026-06-21T12:53Z
TLE epoch observation values (Epoch: 2026-06-21T12:53:49.782Z)
Latitude
-0.00005°
Longitude
-56.32135°
Altitude
588.86 km
Speed
7.566 km/s
True Right ascension
03h 07m 29s
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
21:57:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.287 km
Perigee altitude
582.327 km
Semi-major axis
6,961.444 km
Eccentricity
0.00014
Inclination
97.5819°
RAAN
46.8723°
Arg. of periapsis
60.2856°
True anomaly
299.8364°
Mean anomaly
299.8504°
Eccentric anomaly
299.8434°
Mean motion
3.73675 °/min
Orbital period
96.34 mins
BSTAR
0.00015187
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 14:46:36.484Z | 108.103° ESE | 2026-06-22 14:48:36.484Z | 73.085° E | 19.867° | 2026-06-22 14:51:36.484Z | 22.19° NNE |
| 6 mins | 2026-06-22 16:21:36.484Z | 212.435° SW | 2026-06-22 16:24:36.484Z | 277.156° WNW | 25.322° | 2026-06-22 16:27:36.484Z | 324.088° NNW |
| 5 mins | 2026-06-23 04:04:36.484Z | 43.561° NE | 2026-06-23 04:06:36.484Z | 99.909° ESE | 33.233° | 2026-06-23 04:09:36.484Z | 164.276° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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