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: 5 hours ago
TLE from 5 hours ago
0 DEIMOS 2
1 40013U 14033D 25342.62574198 .00003913 00000-0 38213-3 0 9993
2 40013 97.6069 218.5617 0000969 95.3799 264.7531 14.92948213609289Epoch: 2025-12-08T15:01Z
TLE epoch observation values (Epoch: 2025-12-08T15:01:04.107Z)
Latitude
-0.00004°
Longitude
-84.32749°
Altitude
591.858 km
Speed
7.564 km/s
True Right ascension
14h 34m 14s
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
18:36:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.434 km
Perigee altitude
585.084 km
Semi-major axis
6,963.896 km
Eccentricity
0.0001
Inclination
97.6069°
RAAN
218.5617°
Arg. of periapsis
95.3799°
True anomaly
264.74204°
Mean anomaly
264.7531°
Eccentric anomaly
264.74757°
Mean motion
3.73478 °/min
Orbital period
96.39 mins
BSTAR
0.00038213
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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 | 2025-12-09 04:27:02.405Z | 23.326° NE | 2025-12-09 04:31:02.405Z | 115.585° SE | 38.068° | 2025-12-09 04:34:02.405Z | 174.165° S |
| 5 mins | 2025-12-09 15:18:02.405Z | 118.092° SE | 2025-12-09 15:20:02.405Z | 72.44° E | 27.583° | 2025-12-09 15:23:02.405Z | 13.837° NNE |
| 4 mins | 2025-12-09 16:54:02.405Z | 237.034° WSW | 2025-12-09 16:56:02.405Z | 274.241° WNW | 18.138° | 2025-12-09 16:58:02.405Z | 306.508° NW |
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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