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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Identifier
Orbit
Country
KR / 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: 14 hours ago
TLE from 14 hours ago
0 KORSAT-2
1 62377U 24247A 26094.00228640 .00000333 00000-0 45960-4 0 9994
2 62377 45.4115 92.3222 0008764 192.5690 167.4971 14.98834843 70435Epoch: 2026-04-04T00:03Z
TLE epoch observation values (Epoch: 2026-04-04T00:03:17.544Z)
Latitude
-0.00002°
Longitude
-100.82924°
Altitude
576.484 km
Speed
7.571 km/s
True Right ascension
06h 09m 17s
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
20:15:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.107 km
Perigee altitude
565.925 km
Semi-major axis
6,950.153 km
Eccentricity
0.00088
Inclination
45.4115°
RAAN
92.3222°
Arg. of periapsis
192.569°
True anomaly
167.51882°
Mean anomaly
167.4971°
Eccentric anomaly
167.50796°
Mean motion
3.74586 °/min
Orbital period
96.11 mins
BSTAR
0.00004596
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-05 01:49:22.488Z | 176.741° S | 2026-04-05 01:51:22.488Z | 143.84° SSE | 18.815° | 2026-04-05 01:54:22.488Z | 95.402° ESE |
| 6 mins | 2026-04-05 03:29:22.488Z | 243.377° WSW | 2026-04-05 03:32:22.488Z | 69.56° E | 43.605° | 2026-04-05 03:35:22.488Z | 65.759° ENE |
| 6 mins | 2026-04-05 05:10:22.488Z | 291.279° WNW | 2026-04-05 05:13:22.488Z | 8.395° NNE | 32.729° | 2026-04-05 05:16:22.488Z | 60.863° ENE |
| 6 mins | 2026-04-05 06:51:22.488Z | 304.275° NW | 2026-04-05 06:54:22.488Z | 18.686° NNE | 35.949° | 2026-04-05 06:57:22.488Z | 82.077° E |
| 6 mins | 2026-04-05 08:32:22.488Z | 285.283° WNW | 2026-04-05 08:35:22.488Z | 188.145° SSW | 40.815° | 2026-04-05 08:38:22.488Z | 132.323° SE |
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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