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KOMPSAT 3A, 40536

Orbit data source: Space-Track

KOMPSAT 3A, 40536 is a payload satellite in SSO that was launched on Wed, 25 Mar 2015 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
40536, 2015-014A
Orbit
SSO
Last TLE update
6 hours ago
Origin
Manufacturer
AP Aerospace
Mission
Operational Civil Imaging
Bus & Motor
KOMPSAT, AOCS?
Mass
1,112 kg wet, 1,039 kg dry
Launch date (UTC)
2015-03-25 (10 years ago)
Launch vehicle
DNEPR
Launch site
Orenburg, Russia (OREN)
Object type
Payload
Rocket body
Debris
Shape & HBR
Hex Cyl + 3 Pan, 6.5 m
Radar Cross Section
9.888 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 6 hours ago
0 KOMPSAT 3A
1 40536U 15014A   25152.55338679  .00033914  00000-0  94500-3 0  9991
2 40536  97.6560 117.7909 0005864 111.7576 248.4292 15.36696954563074
Epoch: 2025-06-01T13:16Z
TLE epoch observation values (Epoch: 2025-06-01T13:16:52.618Z)
Latitude
-0.00004°
Longitude
28.2939°
Altitude
460.466 km
Speed
7.636 km/s
True Right ascension
07h 51m 09s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-63.84739°
Longitude
-167.25464°
Altitude
483.043 km
Speed
7.621 km/s
Apparent Right ascension
17h 31m 04s
Apparent Declination
-53° 08' 32"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
04:43:26
Azimuth
207.566° SW
Elevation
-74.488°
Doppler factor
1
Orbital elements
Apogee altitude
456.845 km
Perigee altitude
448.834 km
Semi-major axis
6,830.976 km
Eccentricity
0.00059
Inclination
97.656°
RAAN
117.7909°
Arg. of periapsis
111.7576°
True anomaly
Unknown
Mean anomaly
248.4292°
Eccentric anomaly
Unknown
Mean motion
3.84432 °/min
Orbital period
93.64 mins
BSTAR
0.000945
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Other satellites on launch #14 in the year 2015 (2015-03-25 UTC)

KOMPSAT 3A Visibility forecast

Observer location: undefined°, undefined°

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 mins2025-06-01 21:13:51.407Z135.779° SSE2025-06-01 21:16:51.407Z60.265° ENE28.77°2025-06-01 21:18:51.407Z13.448° NNE
4 mins2025-06-02 10:10:51.407Z46.464° ENE2025-06-02 10:12:51.407Z121.015° SE30.48°2025-06-02 10:14:51.407Z164.043° S
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