OrbitGuard
14:32:00UTC

34454 · COSMOS 2251 DEB

debris — Iridium–Cosmos collision, 2009

Orbit

Apogee812km
Perigee498km
Inclination74.0°
RCS0.032m²

Characterization

Object type
debris
Origin
Iridium–Cosmos collision, 2009
Radar cross-section
0.032 m²
Active conjunctions
1

Derived elements

two-body · vis-viva
Semi-major axis7033.1km
Eccentricity0.02232
Period97.83min
Mean motion14.7190rev/day
Velocity at perigee7.698km/s
Velocity at apogee7.362km/s

LEO · computed from the catalogued apsides with μ = 398600.4418 km³/s² and R⊕ = 6378.137 km (WGS-84).

Secular perturbations

J2 oblateness
Nodal regression-1.9526deg/day
Apsidal rotation-2.1964deg/day

Ω̇ node · ω̇ argument of perigee, secular rates from the J2 term.

J2 is the dominant perturbation at this altitude. The plane precesses relative to the fleet's, so the encounter geometry walks through the catalogue rather than repeating.

Orbit determination

special perturbations
PropagatorSP
Epoch age0.2h
Observation arc6.5d
Inferred mass11.63kg
Ballistic coeff.165.2kg/m²
Covariance delivered
full 6x6

Special-perturbations fit — numerically integrated against a full force model, delivered with a covariance the screening pipeline can use directly.

Conjunctions against the fleet

1 active
EventPrimaryTCAMiss kmRel vel km/sPc
CJ-4471OG-2Meridian-2T−09:13:480.41214.814.6×10−4

Spacecraft: OG-2