DUCHIFAT 1, 40021
Orbit data source: Space-Track
DUCHIFAT 1, 40021 is a payload satellite owned by Herzliya (IL) in SSO 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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Edit Public Description
Identifier
Orbit
Country
Unknown / ISRARelated business
Manufacturer
Herzliya
Mission
Operational 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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 DUCHIFAT 1
1 40021U 14033M 25287.88735590 .00032649 00000-0 95497-3 0 9998
2 40021 98.0889 313.8035 0006144 217.9019 142.1791 15.35187437617809Epoch: 2025-10-14T21:17Z
TLE epoch observation values (Epoch: 2025-10-14T21:17:47.549Z)
Latitude
0.00001°
Longitude
-29.31396°
Altitude
466.775 km
Speed
7.631 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
00:08:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.54 km
Perigee altitude
453.14 km
Semi-major axis
6,835.477 km
Eccentricity
0.00061
Inclination
98.0889°
RAAN
313.8035°
Arg. of periapsis
217.9019°
True anomaly
142.22225°
Mean anomaly
142.1791°
Eccentric anomaly
142.20068°
Mean motion
3.84052 °/min
Orbital period
93.74 mins
BSTAR
0.00095497
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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 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 | 2025-10-15 15:03:25.229Z | 359.76° N | 2025-10-15 15:06:25.229Z | 284.508° WNW | 36.769° | 2025-10-15 15:09:25.229Z | 212.302° SW |
| 4 mins | 2025-10-16 01:36:25.229Z | 136.359° SSE | 2025-10-16 01:38:25.229Z | 42.759° NE | 35.951° | 2025-10-16 01:40:25.229Z | 1.986° NNE |
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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