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: 8 hours ago
TLE from 8 hours ago
0 KORSAT-2
1 62377U 24247A 25298.10641028 .00006904 00000-0 58407-3 0 9998
2 62377 45.4085 206.5360 0007159 41.7749 318.3675 14.98692708 46297Epoch: 2025-10-25T02:33Z
TLE epoch observation values (Epoch: 2025-10-25T02:33:13.848Z)
Latitude
0.00003°
Longitude
134.4866°
Altitude
567.262 km
Speed
7.581 km/s
True Right ascension
13h 46m 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
06:17:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.432 km
Perigee altitude
567.48 km
Semi-major axis
6,950.593 km
Eccentricity
0.00072
Inclination
45.4085°
RAAN
206.536°
Arg. of periapsis
41.7749°
True anomaly
318.31296°
Mean anomaly
318.3675°
Eccentric anomaly
318.34024°
Mean motion
3.74551 °/min
Orbital period
96.12 mins
BSTAR
0.00058407
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-25 20:18:59.173Z | 192.108° SSW | 2025-10-25 20:21:59.173Z | 144.67° SSE | 21.62° | 2025-10-25 20:24:59.173Z | 92.411° ESE |
| 6 mins | 2025-10-25 21:59:59.173Z | 250.434° W | 2025-10-25 22:02:59.173Z | 40.153° NE | 43.367° | 2025-10-25 22:05:59.173Z | 63.75° ENE |
| 6 mins | 2025-10-25 23:40:59.173Z | 293.648° NW | 2025-10-25 23:43:59.173Z | 7.424° NNE | 32.106° | 2025-10-25 23:46:59.173Z | 61.712° ENE |
| 7 mins | 2025-10-26 01:21:59.173Z | 303.648° NW | 2025-10-26 01:24:59.173Z | 18.533° NNE | 37.449° | 2025-10-26 01:28:59.173Z | 90.641° ESE |
| 6 mins | 2025-10-26 03:02:59.173Z | 281.419° WNW | 2025-10-26 03:05:59.173Z | 195.474° SSW | 37.834° | 2025-10-26 03:08:59.173Z | 138.778° SSE |
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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