MIMAN, 52900
Orbit data source: Space-Track
MIMAN, 52900 is a payload satellite owned by Yonsei U (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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52900 intel report (Beta)
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Identifier
Orbit
Country
KR / SKORRelated business
Manufacturer
Yonsei U
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, 0.2 m
Radar Cross Section
0.039 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 MIMAN
1 52900U 22065G 26171.33376383 .00000375 00000-0 84546-4 0 9990
2 52900 98.2265 313.8001 0008018 25.7705 334.3894 14.61846294210900Epoch: 2026-06-20T08:00Z
TLE epoch observation values (Epoch: 2026-06-20T08:00:37.194Z)
Latitude
-0.00005°
Longitude
-74.90475°
Altitude
685.097 km
Speed
7.517 km/s
True Right ascension
20h 55m 12s
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
02:14:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
689.961 km
Perigee altitude
678.636 km
Semi-major axis
7,062.436 km
Eccentricity
0.0008
Inclination
98.2265°
RAAN
313.8001°
Arg. of periapsis
25.7705°
True anomaly
334.34965°
Mean anomaly
334.3894°
Eccentric anomaly
334.36953°
Mean motion
3.65689 °/min
Orbital period
98.44 mins
BSTAR
0.000084546
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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.MIMAN 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 | 2026-06-22 21:22:54.993Z | 48.181° ENE | 2026-06-22 21:25:54.993Z | 89.698° E | 18.773° | 2026-06-22 21:28:54.993Z | 134.759° SE |
| 7 mins | 2026-06-22 23:00:54.993Z | 347.128° N | 2026-06-22 23:03:54.993Z | 281.88° WNW | 32.202° | 2026-06-22 23:07:54.993Z | 221.593° SW |
| 4 mins | 2026-06-23 08:27:54.993Z | 92.835° ESE | 2026-06-23 08:29:54.993Z | 59.025° ENE | 18.861° | 2026-06-23 08:31:54.993Z | 28.951° NE |
| 7 mins | 2026-06-23 10:03:54.993Z | 202.253° SSW | 2026-06-23 10:06:54.993Z | 269.517° W | 32.508° | 2026-06-23 10:10:54.993Z | 330.954° NNW |
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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