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OPTOS, 39420

Orbit data source: Space-Track

OPTOS, 39420 is a payload satellite owned by INTA (ES) in SSO that was launched on Thu, 21 Nov 2013 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
39420, 2013-066E
Orbit
SSO
Country
Flag of ESES / SPN
Related business
Manufacturer
INTA
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2013-11-21 (12 years ago)
Launch vehicle
DNEPR
Launch site
Orenburg, Russia (OREN)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.075 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 OPTOS
1 39420U 13066E   26037.57354600  .00001948  00000-0  28546-3 0  9992
2 39420  97.7002 269.4652 0118682  72.6369 288.7779 14.71943594652309
Epoch: 2026-02-06T13:45Z
TLE epoch observation values (Epoch: 2026-02-06T13:45:54.374Z)
Latitude
0.00001°
Longitude
-73.72084°
Altitude
631.906 km
Speed
7.556 km/s
True Right ascension
17h 57m 51s
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
02:42:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
735.346 km
Perigee altitude
568.478 km
Semi-major axis
7,030.049 km
Eccentricity
0.01187
Inclination
97.7002°
RAAN
269.4652°
Arg. of periapsis
72.6369°
True anomaly
287.48423°
Mean anomaly
288.7779°
Eccentric anomaly
288.13167°
Mean motion
3.68218 °/min
Orbital period
97.77 mins
BSTAR
0.00028546
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