DIDO 3, 46284 (Decayed)
Orbit data source: Space-Track
DIDO 3, 46284 was a payload satellite owned by Space Pharma (IL) in LEO 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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46284 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ISRARelated business
SpacePharma (CH)Manufacturer
Space Pharma
Mission
Decayed Commercial Microgravity
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, Unknown HBR
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 DIDO 3
1 46284U 20061N 25081.48766028 .07487664 24492-5 76787-3 0 9996
2 46284 97.2679 159.5651 0011148 273.5907 86.4116 16.37766130252652Epoch: 2025-03-22T11:42Z
TLE epoch observation values (Epoch: 2025-03-22T11:42:13.848Z)
Latitude
-0.00006°
Longitude
163.77539°
Altitude
174.555 km
Speed
7.802 km/s
True Right ascension
10h 38m 15s
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
12:30:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
175.855 km
Perigee altitude
161.258 km
Semi-major axis
6,546.693 km
Eccentricity
0.00111
Inclination
97.2679°
RAAN
159.5651°
Arg. of periapsis
273.5907°
True anomaly
86.53911°
Mean anomaly
86.4116°
Eccentric anomaly
86.47535°
Mean motion
4.09742 °/min
Orbital period
87.86 mins
BSTAR
0.00076787
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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.DIDO 3 Visibility
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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. |
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| This satellite is decayed. |
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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