Key statistics
Satellite MEGSAT 1 at a glance.
Uptime
9051
Days in orbit
Revolutions
≈ 15.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
64.6
Latest
Satellite identification and parameters
Extended collection of information and parameters for MEGSAT 1.
Object identification
Identified? True
Debris? False
Object name: MEGSAT 1
International designator: 2000-057B
Object number (NORAD): 26546
Object ID (CCSDS): 26546
Country: ITALY (IT)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 95.842 minutes
Inclination: 64.5515 deg
SMA: 6937.39 km
Apoapsis: 573.288 km
Periapsis: 545.222 km
RAAN: 95.1119 deg
Eccentricy: 0.0020228
Argument of periapsis: 310.9662 deg
Mean anomaly: 48.9703 deg
Mean motion: 15.02479666 rev/day
Mean motion (dot): 0.000024 rev/day2
B* drag term: 0.00019246 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 6:12 a.m. UTC
TLE line 0: 0 MEGSAT 1
TLE line 1: 1 26546U 00057B 25187.25874628 .00002400 00000-0 19246-3 0 9991
TLE line 2: 2 26546 64.5515 95.1119 0020228 310.9662 48.9703 15.02479666345636
Live tracking on map
Real-time ground track for satellite MEGSAT 1.
In-orbit conjunctions
There are no conjunctions computed for MEGSAT 1, at the moment. Check back to stay up to date, as we update our databases every day.
Go to all conjunctionsAssociated 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.
MEGSAT 1 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.
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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Latest news about this satellite
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