Environment Report

The latest Space Debris Environment Report issued by ESA's Space Debris Office is available here. The fifth edition has been released on 27/05/2021.

The AMOS 2019 keynote on the topic of the report by Dr. Francesca Letizia is available from these links: slides, transcript.

Environment Statistics

Last update: 05 January 2022

Space debris by the numbers

Number of rocket launches since the start of the space age in 1957
About 6170 (excluding failures)
Number of satellites these rocket launches have placed into Earth orbit
About 12450
Number of these still in space
About 7840
Number of these still functioning
About 4900
Number of debris objects regularly tracked by Space Surveillance Networks and maintained in their catalogue
About 30630
Estimated number of break-ups, explosions, collisions, or anomalous events resulting in fragmentation
More than 640
Total mass of all space objects in Earth orbit
More than 9800 tonnes
Number of debris objects estimated by statistical models to be in orbit
36500 objects greater than 10 cm
1000000 objects from greater than 1 cm to 10 cm
330 million objects from greater than 1 mm to 1 cm

Extended statistics

Here we would like to briefly address and summarise some facts on the space environment. This environment is understood to contain all man made objects, including fragments and elements thereof, which currently, or previously did, reside in an Earth bound orbit. Of specific interest is space debris, defined as all man made objects including fragments and elements thereof, in Earth orbit or reentering the atmosphere, that are non functional (IADC definition). Objects in the space environment can be categorised in two broad categories: The ones which can be traced back to a launch event and for which the nature can be identified, and the ones for which this is not (yet) possible. The later ones will be identified as Unidentified (UI), whereas the former can be further categorised in:

The taxonomy of objects in the space environment can be done based on type as before, but also via the orbital regime in which they reside. A catalogued object will refer to an object whose orbital elements are maintained for prolonged periods of time in a catalogue created by a space surveillance system. An asserted object will refer to an object which has not been reported by a space surveillance system but is known to exist in the space environment by design. Asserted objects include for example rocket bodies which perform a re-entry burn after inserting a payload into orbit prior to consistent detection or tracking by a space surveillance system. As such catalogued and asserted objects are not mutually exclusive and neither one is strictly contained within the other. Catalogued and asserted objects can be categorised in terms of their orbital elements for a given epoch. Orbital regimes used hereafter will be identified based on semi-major axis, eccentricity, inclination, perigee height and apogee height in the table below.

Orbital regime definitions
Orbital regime Description Limits
GEO Geostationary Orbit i < 25°, 35586 km < hp < 35986 km, 35586 km < ha < 35986 km
IGO Inclined Geosynchronous Orbit 37948 km < a < 46380 km, e < 0.25, 25° < i < 180°
EGO Extended Geostationary Orbit 37948 km < a < 46380 km, e < 0.25, i < 25°
NSO Navigation Satellites Orbit 50° < i < 70°, 18100 km < hp < 24300 km, 18100 km < ha < 24300 km
GTO GEO Transfer Orbit i < 90°, hp < 2000 km, 31570 km < ha < 40002 km
MEO Medium Earth Orbit 2000 km < hp < 31570 km, 2000 km < ha < 31570 km
GHO GEO-superGEO Crossing Orbits 31570 km < hp < 40002 km, ha > 40002 km
LEO Low Earth Orbit hp < 2000 km, ha < 2000 km
HAO High Altitude Earth Orbit hp > 40002 km, ha > 40002 km
MGO MEO-GEO Crossing Orbits 2000 km < hp < 31570 km, 31570 km < ha < 40002 km
HEO Highly Eccentric Earth Orbit hp < 31570 km, ha > 40002 km
LMO LEO-MEO Crossing Orbits hp < 2000 km, 2000 km < ha < 31570 km
UFO Undefined Orbit
ESO Escape Orbits

Fragmentation events are currently being categorised according to the assessed break-up cause:

Data presented hereafter will only relate to catalogued objects, and hence next to the increase of the space object population by human activity show the increase in availability of space surveillance networks. The abbreviation OCC (Orbit Control Capacity) will be used to identify Payload objects which can alter their orbit by means of applying demonstrated impulsive or continuous thrust. This thus include all conventional types of space propulsion but not technologies exploiting natural perturbations such as drag or solar sails. Rocket bodies, also described as Stages are all assumed to have OCC. Human spaceflight (HS) related missions are analysed separately, as they tend to skew results in terms of mass and count affected for the space environment and have generally a very high reliability. These mission include manned payloads as well as cargo payloads, but not the rocket bodies which bring them into orbit. An in-depth report will be available here soon.

Objects in Orbit

Objects in orbit count over time subdivided in object classes

Mass in orbit over time subdivided in object classes

Objects in orbit count over time subdivided in orbit classes

Mass in orbit over time subdivided in orbit classes

Reentered objects over time subdivided in object classes

Current number of orbiting objects per type and orbital regime
Orbital Regime PL PF PD PM RB RF RD RM UI Total
LEO 5961 7376 110 236 911 2588 134 617 72 18005
GEO 768 3 2 7 64 0 0 0 31 875
EGO 479 2 0 48 191 88 1 4 1694 2507
GTO 67 19 1 12 248 211 11 59 579 1207
NSO 275 0 0 1 92 0 0 2 11 381
MEO 66 3 5 53 20 45 1 3 283 479
LMO 87 156 5 47 234 788 20 226 980 2543
MGO 66 73 1 2 175 2185 5 0 814 3321
HEO 36 15 0 1 49 112 0 0 973 1186
Other 39 0 0 5 3 0 0 0 88 135
Total 7844 7647 124 412 1987 6017 172 911 5525 30639
Current mass (t) in orbit per object type and orbital regime
Orbital Regime PL PF PD PM RB RF RD RM UI Total
LEO 2152.8 1.5 1.0 12.5 1315.9 0.2 0.0 7.1 2.7 3493.8
GEO 2439.5 0.0 0.0 1.0 132.1 0.0 0.0 0.0 0.0 2572.6
EGO 782.6 0.0 0.0 4.9 354.3 0.0 0.0 0.1 0.0 1142.0
GTO 129.9 0.0 0.0 1.0 586.6 0.0 0.0 27.4 0.0 745.0
NSO 354.5 0.0 0.0 0.4 209.5 0.0 0.0 0.0 0.0 564.3
MEO 64.7 0.0 0.0 0.2 26.8 0.0 0.0 2.0 0.0 93.7
LMO 73.6 0.0 0.0 7.0 407.7 0.0 0.0 87.5 0.0 575.8
MGO 90.3 0.0 0.0 1.9 284.2 0.0 0.0 0.0 0.0 376.3
HEO 68.5 0.0 0.0 0.1 109.4 0.0 0.0 0.0 0.0 178.0
Other 70.1 0.0 0.0 0.1 5.5 0.0 0.0 0.0 0.0 75.7
Total 6226.5 1.5 1.0 29.1 3432.1 0.2 0.0 124.2 2.7 9817.3
Current cumulative cross sectional area (m²) in orbit per object type and orbital regime
Orbital Regime PL PF PD PM RB RF RD RM UI Total
LEO 31999.6 0.5 4.7 97.7 10801.7 2.6 0.0 289.7 8.5 43205.1
GEO 23730.3 0.0 23.6 8.4 1439.2 0.0 0.0 0.0 0.0 25201.5
EGO 10220.2 0.0 0.0 37.0 3916.9 0.0 0.0 1.2 0.0 14175.4
GTO 869.4 0.0 0.0 8.9 5745.4 0.0 0.0 865.7 0.0 7489.5
NSO 3096.2 0.0 0.0 0.8 1850.2 0.0 0.0 0.0 0.0 4947.3
MEO 933.2 0.0 0.0 10.3 265.5 0.0 0.0 15.3 0.0 1224.2
LMO 652.2 0.0 0.0 14.9 4585.8 0.0 0.0 1572.3 0.0 6825.2
MGO 901.1 0.0 0.0 14.5 3036.8 0.0 0.0 0.0 0.0 3952.4
HEO 826.2 0.0 0.0 0.1 1182.7 0.0 0.0 0.0 0.0 2009.1
Other 459.9 0.0 0.0 0.5 53.1 0.0 0.0 0.0 0.0 513.5
Total 73688.4 0.5 28.3 193.2 32877.5 2.6 0.0 2744.2 8.5 109543.1

Fragmentations in Orbit

Number of fragmentation events over time subdivided by fragmentation cause

Share of fragmentation causes over time

Missions to LEO and GEO

Launch traffic to LEO over time

Launch traffic to GEO over time