REORBITING STATISTICS OF GEOSTATIONARY OBJECTS IN THE YEARS 1997-2000 R. Jehn(1) and C. Hernandez´ (1) (1)European Space Operations Centre (ESOC), (1)Robert-Bosch-Str. 5, D-64293 Darmstadt, Germany, Email:
[email protected] ABSTRACT crease 300-400 km above GEO depending on spacecraft characteristics” [4]. At the same time, space agencies Based on orbital data in the DISCOS database the sit- like NASA, NASDA, RKA and ESA developed national uation in the geostationary ring is analysed. From 878 guidelines. All recommended an altitude increase of known objects, 305 are controlled inside their longitude more than 200 km above GEO. Finally in 1997, an in- slots, 353 are drifting above, below or through GEO, and ternational consensus was found within the Inter-Agency 125 are in a libration orbit (status of Jan. 2001). In the last Space Debris Coordination Committee (IADC). The rec- four years (1997-2000) 58 spacecraft reached end-of-life. ommended altitude increase (in km) is given as 20 of them were reorbited in compliance with the IADC recommendations, 16 were reorbited below this recom- mendation and 22 were abandoned without any end-of- H = 235 + 1000 C A=m life disposal manoeuvre. R (1) 1. INTRODUCTION C where R is the solar radiation pressure coefficient (usu- The geostationary ring is a valuable resource currently ally with a value between 1 and 2), A is the average cross- populated by some 300 operational satellites. Unlike in sectional area and m is the mass of the satellite [5]. low Earth orbit there is no atmospheric drag which will remove abandoned objects over time.