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: 11 hours ago
TLE from 11 hours ago
0 SAUDISAT 4
1 40016U 14033G 25334.66949578 .00000830 00000-0 11701-3 0 9997
2 40016 97.7292 123.0767 0045137 1.3823 358.7506 14.79134440616725Epoch: 2025-11-30T16:04Z
TLE epoch observation values (Epoch: 2025-11-30T16:04:04.435Z)
Latitude
0.00003°
Longitude
172.27819°
Altitude
603.442 km
Speed
7.575 km/s
True Right ascension
08h 12m 18s
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
00:27:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
660.721 km
Perigee altitude
597.463 km
Semi-major axis
7,007.229 km
Eccentricity
0.00451
Inclination
97.7292°
RAAN
123.0767°
Arg. of periapsis
1.3823°
True anomaly
358.73926°
Mean anomaly
358.7506°
Eccentric anomaly
358.74494°
Mean motion
3.70019 °/min
Orbital period
97.29 mins
BSTAR
0.00011701
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-01 10:03:01.721Z | 165.405° S | 2025-12-01 10:06:01.721Z | 158.673° S | 43.713° | 2025-12-01 10:10:01.721Z | 348.37° N |
| 4 mins | 2025-12-01 21:54:01.721Z | 66.394° ENE | 2025-12-01 21:56:01.721Z | 99.526° ESE | 17.51° | 2025-12-01 21:58:01.721Z | 129.319° SE |
| 7 mins | 2025-12-01 23:29:01.721Z | 350.338° N | 2025-12-01 23:32:01.721Z | 292.165° WNW | 32.446° | 2025-12-01 23:36:01.721Z | 221.223° SW |
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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