OrbitGuard
14:32:00UTC

99214 · UNCHARACTERIZED OBJECT

unknown — Unattributed — 3 optical tracks

Orbit

Apogee728km
Perigee691km
Inclination98.1°
RCS—

Characterization

Object type
unknown
Origin
Unattributed — 3 optical tracks
Radar cross-section
uncharacterized
Active conjunctions
1

No radar cross-section on file. Area-to-mass ratio is unmodelled, which is why any Pc estimate against this object carries a wide confidence band.

Derived elements

two-body · vis-viva
Semi-major axis7087.6km
Eccentricity0.00261
Period98.97min
Mean motion14.5496rev/day
Velocity at perigee7.519km/s
Velocity at apogee7.480km/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 regression0.9706deg/day
Apsidal rotation-3.1023deg/day

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

The node regresses at 0.9856 deg/day, so this orbit is sun-synchronous — its geometry against the fleet's own sun-synchronous planes repeats rather than drifting apart, which is why repeat conjunctions with this object are common.

Orbit determination

general perturbations
PropagatorSGP4
Epoch age1.2h
Observation arc0.3d
Inferred mass—
Ballistic coeff.—
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. With no radar cross-section on file, neither mass nor drag response can be inferred at all — the covariance is a floor assumption, not a measurement.

Conjunctions against the fleet

1 active
EventPrimaryTCAMiss kmRel vel km/sPc
CJ-4451OG-5HalcyonT−64:00:000.9608.723.3×10−5

Spacecraft: OG-5