SNUGLITE-II, 52899
Orbit data source: Space-Track
SNUGLITE-II, 52899 is a payload satellite owned by SNU (KR) in SSO that was launched on Tue, 21 Jun 2022 UTC via an NURI launch vehicle from the Naro Space Center, South Korea (NSC). 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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52899 intel report (Beta)
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Identifier
Orbit
Country
KR / SKORRelated business
Manufacturer
SNU
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Rod, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 SNUGLITE-II
1 52899U 22065F 26171.37922855 .00000681 00000-0 13817-3 0 9994
2 52899 98.2207 316.2040 0007803 23.7444 336.4117 14.64352373211468Epoch: 2026-06-20T09:06Z
TLE epoch observation values (Epoch: 2026-06-20T09:06:05.346Z)
Latitude
-0.00004°
Longitude
-88.91297°
Altitude
677.099 km
Speed
7.521 km/s
True Right ascension
21h 04m 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
21:35:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
681.736 km
Perigee altitude
670.727 km
Semi-major axis
7,054.369 km
Eccentricity
0.00078
Inclination
98.2207°
RAAN
316.204°
Arg. of periapsis
23.7444°
True anomaly
336.37589°
Mean anomaly
336.4117°
Eccentric anomaly
336.3938°
Mean motion
3.66316 °/min
Orbital period
98.28 mins
BSTAR
0.00013817
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Other satellites on launch #65 in the year 2022 (2022-06-21 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.SNUGLITE-II 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-22 22:21:14.216Z | 21.367° NNE | 2026-06-22 22:25:14.216Z | 122.491° SE | 41.699° | 2026-06-22 22:29:14.216Z | 182.935° SSW |
| 7 mins | 2026-06-23 09:23:14.216Z | 149.759° SSE | 2026-06-23 09:26:14.216Z | 102.72° ESE | 39.777° | 2026-06-23 09:30:14.216Z | 357.49° 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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