DECAYED
Showing default

SMDC ONE 1.1, 38766 (Decayed)

Orbit data source: Space-Track

SMDC ONE 1.1, 38766 was a payload satellite owned by SMDC (US) in LEO that was launched on Thu, 13 Sep 2012 UTC via an ATLAS V 401 launch vehicle from the Air Force Western Test Range (AFWTR). 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.

Not visible in the next 10 days
Identifier
38766, 2012-048J
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
Duocomm Miltec
Mission
Decayed Defense Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2012-09-13 (14 years ago)
Launch vehicle
ATLAS V 401
Launch site
Air Force Western Test Range (AFWTR)
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: 9 months ago

TLE from 9 months ago
0 SMDC ONE 1.1
1 38766U 12048J   25227.49203623  .07519031  77217-5  10578-2 0  9990
2 38766  64.6036 272.5995 0019146 277.2324  82.6680 16.33883009 73487
Epoch: 2025-08-15T11:48Z
TLE epoch observation values (Epoch: 2025-08-15T11:48:31.930Z)
Latitude
Longitude
131.32561°
Altitude
182.664 km
Speed
7.798 km/s
True Right ascension
18h 10m 23s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
03:22:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
193.183 km
Perigee altitude
168.068 km
Semi-major axis
6,558.762 km
Eccentricity
0.00191
Inclination
64.6036°
RAAN
272.5995°
Arg. of periapsis
277.2324°
True anomaly
82.88567°
Mean anomaly
82.668°
Eccentric anomaly
82.77683°
Mean motion
4.08611 °/min
Orbital period
88.1 mins
BSTAR
0.0010578
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|