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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Identifier
Orbit
Country
IL / 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: 10 hours ago
TLE from 10 hours ago
0 DUCHIFAT 1
1 40021U 14033M 26124.09577514 .00074568 00000-0 10193-2 0 9997
2 40021 98.0515 177.3522 0005133 210.7680 149.3273 15.57185713648875Epoch: 2026-05-04T02:17Z
TLE epoch observation values (Epoch: 2026-05-04T02:17:54.972Z)
Latitude
-0°
Longitude
-79.11674°
Altitude
401.919 km
Speed
7.668 km/s
True Right ascension
11h 49m 24s
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
20:15:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
396.228 km
Perigee altitude
389.277 km
Semi-major axis
6,770.889 km
Eccentricity
0.00051
Inclination
98.0515°
RAAN
177.3522°
Arg. of periapsis
210.768°
True anomaly
149.35729°
Mean anomaly
149.3273°
Eccentric anomaly
149.3423°
Mean motion
3.8956 °/min
Orbital period
92.41 mins
BSTAR
0.0010193
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-04 16:43:42.309Z | 358.779° N | 2026-05-04 16:46:42.309Z | 263.246° W | 34.369° | 2026-05-04 16:48:42.309Z | 215.249° SW |
| 4 mins | 2026-05-05 03:07:42.309Z | 120.593° SE | 2026-05-05 03:08:42.309Z | 90.076° ESE | 27.515° | 2026-05-05 03:11:42.309Z | 8.335° 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 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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