OrbitGuard
14:32:00UTC

Fleet GNSS Downlink

onboard · OrbitGuard fleet ephemeris

Last delivery1m
Expected cadence5m
Objects tracked6
Observations 24h8,640
Statenominal
Age against cadence20%

80% of the delivery interval remaining.

Observation and orbit determination

CCSDS OEM (operator ephemeris)
Fit span24h
1σ position8m
Observations 24h8,640
Obs per object1440.0
Measurement types
GNSS pseudorange · carrier phase
Delivered product
CCSDS OEM (operator ephemeris)

GNSS ephemeris downlinked from the fleet itself. This is the primary state for every OrbitGuard spacecraft; catalogue data covers only the secondary.

Range and angles constrain radial position well but leave along-track error to be inferred from arc length, so the covariance ellipsoid stays elongated along the velocity vector. A short fit span compounds this — there is not enough arc to separate drag from geometry.

Conjunctions screened by this source

0 active

No active conjunctions are currently sourced from this network.