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: 13 hours ago
TLE from 13 hours ago
0 DUCHIFAT 1
1 40021U 14033M 26033.07430414 .00044386 00000-0 91807-3 0 9998
2 40021 98.0708 75.4178 0005664 190.6627 169.4501 15.45659878634765Epoch: 2026-02-02T01:46Z
TLE epoch observation values (Epoch: 2026-02-02T01:46:59.877Z)
Latitude
-0.00003°
Longitude
-83.6065°
Altitude
436.336 km
Speed
7.648 km/s
True Right ascension
05h 01m 40s
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
16:07:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
430.256 km
Perigee altitude
422.547 km
Semi-major axis
6,804.539 km
Eccentricity
0.00057
Inclination
98.0708°
RAAN
75.4178°
Arg. of periapsis
190.6627°
True anomaly
169.46198°
Mean anomaly
169.4501°
Eccentric anomaly
169.45604°
Mean motion
3.86674 °/min
Orbital period
93.1 mins
BSTAR
0.00091807
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-03 02:47:14.476Z | 170.977° S | 2026-02-03 02:49:14.476Z | 324.143° NNW | 43.425° | 2026-02-03 02:51:14.476Z | 344.406° N |
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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