UNHA 3 R/B, 39027
Orbit data source: Space-Track
UNHA 3 R/B, 39027 is space debris in SSO originally from a launch on Wed, 12 Dec 2012 UTC launched from the Yunsong, Dprk (YUN). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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39027 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / NKORRelated business
North Korean Committee for the Space Science and Technology (KP)Manufacturer
KCST
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 0.9 m
Radar Cross Section
0.459 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 UNHA 3 R/B
1 39027U 12072B 25249.30110095 .00141202 00000-0 73310-3 0 9991
2 39027 97.5421 258.0364 0017256 114.2938 246.0134 15.80386638674306Epoch: 2025-09-06T07:13Z
TLE epoch observation values (Epoch: 2025-09-06T07:13:35.122Z)
Latitude
0.00002°
Longitude
164.00316°
Altitude
337.237 km
Speed
7.704 km/s
True Right ascension
17h 12m 08s
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
20:08:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
337.807 km
Perigee altitude
314.669 km
Semi-major axis
6,704.375 km
Eccentricity
0.00173
Inclination
97.5421°
RAAN
258.0364°
Arg. of periapsis
114.2938°
True anomaly
245.8329°
Mean anomaly
246.0134°
Eccentric anomaly
245.92313°
Mean motion
3.95372 °/min
Orbital period
91.05 mins
BSTAR
0.0007331
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Other satellites on launch #72 in the year 2012 (2012-12-12 UTC)
UNHA 3 R/B Visibility
Observer location: undefined°, undefined°
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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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