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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Identifier
Orbit
Country
SA / 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
0.195 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 SAUDISAT 4
1 40016U 14033G 26297.15028400 .00000451 00000-0 66016-4 0 9991
2 40016 97.7779 78.9925 0044984 15.5354 344.7227 14.79680902665148Epoch: 2026-10-24T03:36Z
TLE epoch observation values (Epoch: 2026-10-24T03:36:24.537Z)
Latitude
-0.00001°
Longitude
-7.67034°
Altitude
602.947 km
Speed
7.574 km/s
True Right ascension
05h 15m 58s
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
17:53:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
658.881 km
Perigee altitude
595.854 km
Semi-major axis
7,005.504 km
Eccentricity
0.0045
Inclination
97.7779°
RAAN
78.9925°
Arg. of periapsis
15.5354°
True anomaly
344.58614°
Mean anomaly
344.7227°
Eccentric anomaly
344.65449°
Mean motion
3.70155 °/min
Orbital period
97.26 mins
BSTAR
0.000066016
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-24 23:38:31.674Z | 334.692° NNW | 2026-10-24 23:41:31.674Z | 292.247° WNW | 17.157° | 2026-10-24 23:43:31.674Z | 262.365° W |
| 5 mins | 2026-10-25 08:58:31.674Z | 116.331° SE | 2026-10-25 09:00:31.674Z | 70.732° E | 31.573° | 2026-10-25 09:03:31.674Z | 13.783° NNE |
| 4 mins | 2026-10-25 10:35:31.674Z | 240.202° WSW | 2026-10-25 10:36:31.674Z | 258.459° W | 19.853° | 2026-10-25 10:39:31.674Z | 308.813° NW |
| 7 mins | 2026-10-25 22:22:31.674Z | 16.779° NNE | 2026-10-25 22:25:31.674Z | 51.327° ENE | 70.591° | 2026-10-25 22:29:31.674Z | 187.626° SSW |
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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