SAUDISAT 1A

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite SAUDISAT 1A at a glance.

Uptime

8990

Days in orbit

Revolutions

≈ 14.9

Per day

Orbit

LEO

Low Earth Orbit

Inclination

64.6

Latest

Satellite identification and parameters

Extended collection of information and parameters for SAUDISAT 1A.

Object identification

Identified? True

Debris? False

Object name: SAUDISAT 1A

International designator: 2000-057A

Object number (NORAD): 26545

Object ID (CCSDS): 26545

Country: SAUDI ARABIA (SAUD)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 96.545 minutes

Inclination: 64.5509 deg

SMA: 6971.312 km

Apoapsis: 594.123 km

Periapsis: 592.232 km

RAAN: 131.3599 deg

Eccentricy: 0.0001356

Argument of periapsis: 295.1906 deg

Mean anomaly: 64.9064 deg

Mean motion: 14.91526427 rev/day

Mean motion (dot): 0.00001951 rev/day2

B* drag term: 0.00020945 1/REarth

Two-line elements (TLE)

Creation date: May 8, 2025, 3:01 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 7, 2025, 9:18 a.m. UTC

TLE line 0: 0 SAUDISAT 1A

TLE line 1: 1 26545U 00057A 25127.38760729 .00001951 00000-0 20945-3 0 9992

TLE line 2: 2 26545 64.5509 131.3599 0001356 295.1906 64.9064 14.91526427332470

Live tracking on map

Real-time ground track for satellite SAUDISAT 1A.

In-orbit conjunctions

A list of the most updated potential collisions computed for object SAUDISAT 1A.

Target Orbit TCA Probability of collision Miss distance Type
SL-14 R/B LEO 2025-01-18 16:21:36 0.0006393702 771.0 (m) ROCKET BODY
COSMOS 2221 LEO 2024-12-14 19:19:57 0.02943818 55.0 (m) PAYLOAD
CZ-4C DEB SSO 2024-11-27 18:13:47 0.0003564212 370.0 (m) DEBRIS
CZ-6A DEB LEO 2024-10-14 12:42:18 0.0009802993 716.0 (m) DEBRIS

Associated space launch

Four small satellites were launched atop the Dnepr launch vehicle : MegSat 1, UniSat 1, TiungSat 1 as well as SaudiSat 1a and 1b. MegSat 1 is the second MegSat satellite. It is a LEO communications satellite. UniSat 1 is an Italian satellite developed and operated by GAUSS (La Sapienza University of Rome). TiungSAT-1 or MySat (Malaysian Satellite) is the first microsatellite for the Astronautic Technology (M) SDN. BHD. Company (ATSB) in Kuala Lumpur, Malaysia. Saudisat-1a and Saudisat-1b (Saudi Arabian Satellite) are the first Saudi Arabian micro satellites.

SAUDISAT 1A was lifted into orbit during the mission ‘Dnepr | SmallSat Rideshare’, on board a Dnepr space rocket.

The launch took place on Sept. 26, 2000, 10:05 a.m. from 109/95.

For more information about the launch, click the button.

Launch to space Dnepr | SmallSat Rideshare
Dnepr | SmallSat Rideshare

Agency: N/A

Status: Launch Successful

Launch date: Sept. 26, 2000, 10:05 a.m. UTC

Rocket: Dnepr

Launch pad: 109/95

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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