DUCHIFAT 1, 40021 (Decayed)
Orbit data source: Space-Track
DUCHIFAT 1, 40021 was a payload satellite owned by Herzliya (IL) in LEO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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40021 intel report (Beta)
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Identifier
Orbit
Country
IL / ISRARelated business
Manufacturer
Herzliya
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Ant, 0.3 m
Radar Cross Section
0.046 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 DUCHIFAT 1
1 40021U 14033M 26260.35376336 .11546644 29318-5 71988-3 0 9995
2 40021 98.0032 334.7798 0013138 273.3726 86.6069 16.40544584670300Epoch: 2026-09-17T08:29Z
TLE epoch observation values (Epoch: 2026-09-17T08:29:25.154Z)
Latitude
-0°
Longitude
-148.86722°
Altitude
167.09 km
Speed
7.806 km/s
True Right ascension
22h 19m 07s
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
23:57:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
169.781 km
Perigee altitude
152.598 km
Semi-major axis
6,539.326 km
Eccentricity
0.00131
Inclination
98.0032°
RAAN
334.7798°
Arg. of periapsis
273.3726°
True anomaly
86.7572°
Mean anomaly
86.6069°
Eccentric anomaly
86.68205°
Mean motion
4.10434 °/min
Orbital period
87.71 mins
BSTAR
0.00071988
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Other satellites on launch #33 in the year 2014 (2014-06-19 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.DUCHIFAT 1 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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