SAUDISAT 4
Launch
Launched on Jun 19, 2014 from 370/13, Russia aboard a Dnepr 1.
Dnepr 1 | Multipayload, 37 satellites. →Live · TLE epoch 2026-09-09 04:19 UTC
Orbit class
SSO — Sun-Synchronous (LEO at 96–102° inclination)
Operator
King Abdulaziz City for Science and Technology
Country
Saudi Arabia
Manufacturer
—
Launched
Jun 19, 2014
Mass
—
Apogee
666 km
Perigee
603 km
Inclination
97.77°
Period
1.62 h
Summary from Wikipedia (CC-BY-SA 4.0)
SaudiSat-4 is a Saudi Arabian micro-satellite launched in 2014. It was built by the National Satellite Technology Center at KACST.
Full article on Wikipedia →Altitude history
Apogee and perigee for SAUDISAT 4 across 103 days of archived orbital elements (104 element sets, one per day).
Trend
Stable
Change
-0.4 km
Rate
-0.00 km/day
Now
603 × 666 km
Apogee Perigee
Derived from our own archive of CelesTrak orbital elements, sampled every 3 hours. Short windows show drag and station-keeping; they are not a reentry prediction.
Launched with
21 other catalogued objects still in orbit from launch 2014-033 (Dnepr 1 | Multipayload, 37 satellites.).
- KAZEOSAT 2 · 40010
- PERSEUS-M2 · 40037
- PERSEUS-M1 · 40039
- POLYITAN-1 · 40042
- TIGRISAT · 40043
- LEMUR-1 · 40044
- AEROCUBE 6A · 40045
- AEROCUBE 6B · 40046
- HODOYOSHI-4 · 40011
- UNISAT-6 · 40012
- DEIMOS-2 · 40013
- BUGSAT-1 (TITA) · 40014
- HODOYOSHI-3 · 40015
- APRIZESAT 9 · 40018
- APRIZESAT 10 · 40019
- BRITE-CA1 (TORONTO) · 40020
- DUCHIFAT-1 · 40021
- NANOSATC-BR1 · 40024
- QB50P1 · 40025
- DTUSAT-2 · 40030
- QB50P2 · 40032
Sources & further reading
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