26588 · ARIANE 40 DEB
debris — Ariane 4 H-10 stage, 1996
Orbit
Apogee812km
Perigee704km
Inclination98.8°
RCS0.062m²
Characterization
- Object type
- debris
- Origin
- Ariane 4 H-10 stage, 1996
- Radar cross-section
- 0.062 m²
- Active conjunctions
- 0
Derived elements
two-body · vis-viva
Semi-major axis7136.1km
Eccentricity0.00757
Period99.99min
Mean motion14.4015rev/day
Velocity at perigee7.530km/s
Velocity at apogee7.417km/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 regression1.0291deg/day
Apsidal rotation-2.9697deg/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
general perturbations
PropagatorSGP4
Epoch age21.7h
Observation arc6.6d
Inferred mass31.36kg
Ballistic coeff.229.9kg/m²
- Covariance delivered
- none
General-perturbations fit — an SGP4 mean-element set. The analytic theory carries no formal covariance, so screening substitutes a modelled one and the resulting Pc is correspondingly softer.
Conjunctions against the fleet
0 active
This object is in the screening catalog but has no active conjunctions against the fleet.