The spacecraft was deployed into a heliosynchronous orbit.
Draconic period T_dr = 101.30655 min (6078,3921 sec);
Average altitude A_avg = 832.22 (827-836) km;
Mean altitude anomaly: 815-850 km;
Inclination I = 98.786 degrees;
Eccentricity å = 0.00112;
Local time on equator on the ascending part of the orbit LT = 8.93 hours;
Multiplicity: 14 days
Revolutions per Day: 14.21429;
Duration of the illuminated part of the orbit: 74.5 min;
Longitude of the ascending node: 134 degrees;
Interval between revolutions: -25.327 degrees

Detailed information on the mission.

Full data archive for science team members.

Atmospheric UV and IR flashes and relativistic electron fluxes measured at the moment of maximum UV luminosity during the given minute