SAUDISAT 4, 40016
Orbit data source: Space-Track
SAUDISAT 4, 40016 is a payload satellite owned by KACST (SA) 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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40016 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SAUDRelated business
Manufacturer
KACST
Mission
Operational Civil Technology
Bus & Motor
SAUDISAT, Unknown motor
Mass
100 kg wet, 100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.275 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 SAUDISAT 4
1 40016U 14033G 25286.29880746 .00001535 00000-0 21108-3 0 9998
2 40016 97.7252 76.5883 0045822 155.4357 204.9052 14.78995638609572Epoch: 2025-10-13T07:10Z
TLE epoch observation values (Epoch: 2025-10-13T07:10:16.964Z)
Latitude
-0°
Longitude
-53.08597°
Altitude
664.691 km
Speed
7.509 km/s
True Right ascension
05h 06m 21s
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
11:12:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
661.641 km
Perigee altitude
597.42 km
Semi-major axis
7,007.668 km
Eccentricity
0.00458
Inclination
97.7252°
RAAN
76.5883°
Arg. of periapsis
155.4357°
True anomaly
204.68522°
Mean anomaly
204.9052°
Eccentric anomaly
204.7951°
Mean motion
3.69984 °/min
Orbital period
97.3 mins
BSTAR
0.00021108
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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.SAUDISAT 4 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 | 2025-10-13 22:22:08.963Z | 39.321° NE | 2025-10-13 22:25:08.963Z | 96.275° ESE | 27.188° | 2025-10-13 22:28:08.963Z | 153.926° SSE |
| 4 mins | 2025-10-14 00:00:08.963Z | 315.67° NNW | 2025-10-14 00:01:08.963Z | 296.517° NW | 19.418° | 2025-10-14 00:04:08.963Z | 247.151° WSW |
| 5 mins | 2025-10-14 09:19:08.963Z | 101.448° ESE | 2025-10-14 09:21:08.963Z | 60.837° ENE | 22.724° | 2025-10-14 09:24:08.963Z | 15.919° NNE |
| 5 mins | 2025-10-14 10:55:08.963Z | 224.087° SW | 2025-10-14 10:57:08.963Z | 266.634° W | 25.546° | 2025-10-14 11:00:08.963Z | 318.41° NNW |
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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