ION-MK01, 46274
Orbit data source: Space-Track
ION-MK01, 46274 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Thu, 03 Sep 2020 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). 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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46274 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ITRelated business
Manufacturer
D-ORBIT
Mission
Operational Commercial Technology
Bus & Motor
ION-SC, PM200
Mass
220 kg wet, 150 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.240 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 ION-MK01
1 46274U 20061C 25287.93145344 .00048189 00000-0 60060-3 0 9994
2 46274 97.2280 357.0519 0002742 115.2149 244.9392 15.59768069284767Epoch: 2025-10-14T22:21Z
TLE epoch observation values (Epoch: 2025-10-14T22:21:17.577Z)
Latitude
-0.00007°
Longitude
-1.98413°
Altitude
392.263 km
Speed
7.674 km/s
True Right ascension
23h 48m 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
10:33:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
387.088 km
Perigee altitude
383.379 km
Semi-major axis
6,763.37 km
Eccentricity
0.00027
Inclination
97.228°
RAAN
357.0519°
Arg. of periapsis
115.2149°
True anomaly
244.91074°
Mean anomaly
244.9392°
Eccentric anomaly
244.92497°
Mean motion
3.9021 °/min
Orbital period
92.26 mins
BSTAR
0.0006006
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Other satellites on launch #61 in the year 2020 (2020-09-03 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.ION-MK01 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-15 17:23:30.983Z | 24.587° NE | 2025-10-15 17:25:30.983Z | 76.22° E | 37.958° | 2025-10-15 17:28:30.983Z | 178.354° S |
| 5 mins | 2025-10-16 05:16:30.983Z | 202.204° SSW | 2025-10-16 05:18:30.983Z | 245.852° WSW | 24.657° | 2025-10-16 05:21:30.983Z | 324.285° NNW |
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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