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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 16 hours ago
TLE from 16 hours ago
0 JINJUSAT-1B
1 63210U 25052A 25287.81051516 .00016377 00000-0 67679-3 0 9999
2 63210 97.4225 180.4432 0002114 201.2382 158.8768 15.24068938 32601Epoch: 2025-10-14T19:27Z
TLE epoch observation values (Epoch: 2025-10-14T19:27:08.509Z)
Latitude
-0.00003°
Longitude
-134.93585°
Altitude
498.033 km
Speed
7.615 km/s
True Right ascension
12h 01m 46s
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
05:51:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.996 km
Perigee altitude
489.092 km
Semi-major axis
6,868.681 km
Eccentricity
0.00021
Inclination
97.4225°
RAAN
180.4432°
Arg. of periapsis
201.2382°
True anomaly
158.88553°
Mean anomaly
158.8768°
Eccentric anomaly
158.88116°
Mean motion
3.8127 °/min
Orbital period
94.42 mins
BSTAR
0.00067679
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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 | 2025-10-15 16:05:14.382Z | 109.917° ESE | 2025-10-15 16:07:14.382Z | 75.86° E | 16.492° | 2025-10-15 16:09:14.382Z | 36.574° NE |
| 4 mins | 2025-10-15 17:39:14.382Z | 220.236° SW | 2025-10-15 17:41:14.382Z | 270.891° WNW | 24.178° | 2025-10-15 17:43:14.382Z | 313.918° NW |
| 4 mins | 2025-10-16 05:08:14.382Z | 64.089° ENE | 2025-10-16 05:09:14.382Z | 87.428° E | 21.246° | 2025-10-16 05:12:14.382Z | 147.728° SSE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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