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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 JINJUSAT-1B
1 63210U 25052A 26083.43982330 .00016488 00000-0 55666-3 0 9995
2 63210 97.4091 340.2089 0004803 49.8735 310.2927 15.30745150 57121Epoch: 2026-03-24T10:33Z
TLE epoch observation values (Epoch: 2026-03-24T10:33:20.733Z)
Latitude
0.00009°
Longitude
-0.04495°
Altitude
474.565 km
Speed
7.63 km/s
True Right ascension
22h 40m 50s
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
05:10:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.829 km
Perigee altitude
467.25 km
Semi-major axis
6,848.676 km
Eccentricity
0.00048
Inclination
97.4091°
RAAN
340.2089°
Arg. of periapsis
49.8735°
True anomaly
310.2507°
Mean anomaly
310.2927°
Eccentric anomaly
310.2717°
Mean motion
3.82942 °/min
Orbital period
94.01 mins
BSTAR
0.00055666
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-25 05:56:20.058Z | 11.366° NNE | 2026-03-25 05:59:20.058Z | 334.304° NNW | 44.948° | 2026-03-25 06:02:20.058Z | 193.772° SSW |
| 4 mins | 2026-03-25 16:31:20.058Z | 112.189° ESE | 2026-03-25 16:32:20.058Z | 87.254° E | 24.24° | 2026-03-25 16:35:20.058Z | 16.397° NNE |
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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