Note that in the description below, "height" means the orbit semi-major-axis
minus the Earth equatorial radius; equivalently, it is the average
of the perigee and apogee values: (p+a)/2.
The columns in the catalog are:
Event type | meaning |
---|---|
Aerodyn | Aerodyamic breakup due to low perigee approaching reentry |
ASAT | Destruction by antisatellite weapon |
Coll | Collision with another orbiting object |
Coolant | Frozen coolant blobs leaked from orbital nuclear reactor |
Batt | Battery explosion |
Burn | Broke up during rocket firing |
Destruct | Deliberate self-destruction with onboard explosive |
Disint | Structural disintegration (e.g. balloon breakup) |
Deploy | objects are not debris, but deliberately deployed (notably, see the West Ford dipoles) |
Insul | Possible insulation shedding - debris generation continues over a period of time |
Resid | Propellant-related breakup, usually ignition of residual propellant |
Sep/Coll | Collision with parent object during separation |
Slag | suspected solid rocket motor slag released during rocket firing |
Tumble | Structural disintegration due to tumbling or spin |
Release | deliberate non-destructive release of sub-objects |
Unk | Unknown |
In a debris cloud whose parent was in a circular orbit at height h,
the initial orbits of the debris objects usually
have either their apogee or their perigee equal to h. I make a histogram
of these apogee and perigee values (lumped together) and find the mode of that
histogram (in km). This ApseMode value is often a good estimate of the height at
which the debris event occurred.