JINJUSAT-1B, 63210
Orbit data source: Space-Track
JINJUSAT-1B, 63210 is a South Korean payload satellite in SSO that was launched on Sat, 15 Mar 2025 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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63210 intel report (Beta)
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Identifier
Orbit
Country
KR / SKORRelated business
Manufacturer
KTL
Mission
Operational Civil Imaging
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.025 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 JINJUSAT-1B
1 63210U 25052A 26264.69606325 .00011866 00000-0 33776-3 0 9994
2 63210 97.3861 161.7026 0005267 94.7775 265.4070 15.36257753 84909Epoch: 2026-09-21T16:42Z
TLE epoch observation values (Epoch: 2026-09-21T16:42:19.864Z)
Latitude
-0.0001°
Longitude
-89.45234°
Altitude
460.59 km
Speed
7.636 km/s
True Right ascension
10h 46m 48s
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
17:13:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.729 km
Perigee altitude
450.532 km
Semi-major axis
6,832.268 km
Eccentricity
0.00053
Inclination
97.3861°
RAAN
161.7026°
Arg. of periapsis
94.7775°
True anomaly
265.34684°
Mean anomaly
265.407°
Eccentric anomaly
265.37692°
Mean motion
3.84323 °/min
Orbital period
93.67 mins
BSTAR
0.00033776
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.JINJUSAT-1B 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-23 06:47:36.538Z | 329.014° NNW | 2026-09-23 06:49:36.538Z | 276.967° WNW | 24.151° | 2026-09-23 06:51:36.538Z | 237.105° WSW |
| 5 mins | 2026-09-23 17:18:36.538Z | 167.306° S | 2026-09-23 17:20:36.538Z | 347.575° N | 76.87° | 2026-09-23 17:23:36.538Z | 348.133° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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