Key statistics
Satellite MACSAT at a glance.
Uptime
629
Days in orbit
Revolutions
≈ 15.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.6
Latest
Satellite identification and parameters
Extended collection of information and parameters for MACSAT.
Object identification
Identified? True
Debris? False
Object name: MACSAT
International designator: 2023-155J
Object number (NORAD): 58024
Object ID (CCSDS): 58024
Country: LUXEMBOURG (LUXE)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 94.939 minutes
Inclination: 97.6096 deg
SMA: 6893.776 km
Apoapsis: 517.338 km
Periapsis: 513.944 km
RAAN: 255.3912 deg
Eccentricy: 0.0002462
Argument of periapsis: 174.2295 deg
Mean anomaly: 185.8966 deg
Mean motion: 15.16760554 rev/day
Mean motion (dot): 0.00005942 rev/day2
B* drag term: 0.00030623 1/REarth
Two-line elements (TLE)
Creation date: June 29, 2025, 2:41 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 28, 2025, 10:19 p.m. UTC
TLE line 0: 0 MACSAT
TLE line 1: 1 58024U 23155J 25179.92997176 .00005942 00000-0 30623-3 0 9996
TLE line 2: 2 58024 97.6096 255.3912 0002462 174.2295 185.8966 15.16760554 94713
Live tracking on map
Real-time ground track for satellite MACSAT.
In-orbit conjunctions
There are no conjunctions computed for MACSAT, at the moment. Check back to stay up to date, as we update our databases every day.
Go to all conjunctionsAssociated space launch
THEOS-2 is Thailand’s first Earth observation satellite. Built by Airbus Defense and Space and based on the Astrobus-S platform, it is designed for optical measurements with a ground resolution of approximately 1 meter. TRITON or FORMOSAT-7R is an additional satellite by NSPO added to the joint Taiwanese-US FORMOSAT 7 / COSMIC-2 constellation for collecting atmospheric data for weather prediction and for ionosphere, climate and gravity research. Its GNSS Reflectometry payload can be used to calculate the wind speed over sea surfaces. Cubesats: PROBA-V-CC (Project for On-Board Autonomy - Vegetation - Companion CubeSat) (12U) is a mission that will fly a scaled-down version of the vegetation-monitoring instrument aboard the Earth-observing PROBA-V to conduct combined experimental observations with its predecessor. PRETTY (Passive REflecTomeTry and dosimetrY) (3U) flies a GPS/Galileo signal reflectometer and radiation monitor for Graz University of Technology of Austria. MACSAT (6U) is an In-orbit demonstration (IoD) missionto demonstrate IoT communication over 5G for OQTech. CSC-1 and 2 (6U) contains 7 different experimental payloads from various institutions being flown by ISISPACE/ISL. N3SS (Nanosat 3U pour la Surveillance du Spectre) (3U) is a demonstration system for detecting and localize radio-frequency jammers on civil spectrum for the French CNES. ESTCUBE-2 is a technology demonstration mission with multiple scientific payloads for University of Tartu of Estonia. ANSER LEADER/FOLLOWER 1/2 (Advanced Nanosatellite Systems for Earth observation Research) is a cluster of 3 Earth observing cubesats with panchromatic and hyperspectral cameras for Spain's INTA for monitoring the quality of inland (reservoirs) water over the Iberian Peninsula.
MACSAT was lifted into orbit during the mission ‘Vega | THEOS-2, TRITON & others’, on board a Vega space rocket.
The launch took place on Oct. 9, 2023, 1:36 a.m. from Ariane Launch Area 1 (ELV).
For more information about the launch, click the button.

Vega | THEOS-2, TRITON & others
Agency: Arianespace
Status: Launch Successful
Launch date: Oct. 9, 2023, 1:36 a.m. UTC
Rocket: Vega
Launch pad: Ariane Launch Area 1 (ELV)
Location: Guiana Space Centre, French Guiana
...
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Two Vega VV23 Payloads Failed to Deploy
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Arianespace Launch Europe’s Final Mission of 2023 Aboard Vega
Arianespace launched a Vega rocket in the early hours of 9 October, carrying two primary payloads and ten small secondary payloads. The VV23 flight was Europe’s third and final mission of 2023. The Avio-built Vega rocket was launched from the Guiana Space...

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