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.