KORSAT-2, 62377
Orbit data source: Space-Track
KORSAT-2, 62377 is a payload satellite owned by DAPA (KR) in LEO that was launched on Sat, 21 Dec 2024 UTC via an FALCON 9 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.
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62377 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SKORRelated business
Manufacturer
KAI
Mission
Operational Defense Radar Imaging
Bus & Motor
CAS500?, Unknown motor
Mass
~800 kg wet, ~750 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Box + 3 Pan, 3.0 m
Radar Cross Section
10.467 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 KORSAT-2
1 62377U 24247A 26036.49033836 .00008046 00000-0 67250-3 0 9998
2 62377 45.4109 30.6067 0012082 251.7349 108.2215 14.98944934 61805Epoch: 2026-02-05T11:46Z
TLE epoch observation values (Epoch: 2026-02-05T11:46:05.234Z)
Latitude
0.00001°
Longitude
78.44309°
Altitude
572.833 km
Speed
7.575 km/s
True Right ascension
02h 02m 25s
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
08:19:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.073 km
Perigee altitude
563.279 km
Semi-major axis
6,949.813 km
Eccentricity
0.00121
Inclination
45.4109°
RAAN
30.6067°
Arg. of periapsis
251.7349°
True anomaly
108.35294°
Mean anomaly
108.2215°
Eccentric anomaly
108.28723°
Mean motion
3.74614 °/min
Orbital period
96.1 mins
BSTAR
0.0006725
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Other satellites on launch #247 in the year 2024 (2024-12-21 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.KORSAT-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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-06 07:23:12.171Z | 297.683° NW | 2026-02-06 07:27:12.171Z | 23.072° NE | 42.171° | 2026-02-06 07:31:12.171Z | 101.9° ESE |
| 6 mins | 2026-02-06 09:05:12.171Z | 270.081° WNW | 2026-02-06 09:08:12.171Z | 202.27° SSW | 28.087° | 2026-02-06 09:11:12.171Z | 154.533° SSE |
| 6 mins | 2026-02-07 02:22:12.171Z | 219.525° SW | 2026-02-07 02:25:12.171Z | 125.113° SE | 38.569° | 2026-02-07 02:28:12.171Z | 73.958° E |
| 6 mins | 2026-02-07 04:03:12.171Z | 280.575° WNW | 2026-02-07 04:05:12.171Z | 325.988° NNW | 36.357° | 2026-02-07 04:09:12.171Z | 59.985° ENE |
| 6 mins | 2026-02-07 05:44:12.171Z | 304.086° NW | 2026-02-07 05:47:12.171Z | 18.333° NNE | 32.559° | 2026-02-07 05:50:12.171Z | 72.455° E |
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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