Orbit auxiliary information (gaiadr2.aux_sso_orbits)
The table has 14099 rows, 19 columns.
Description
Auxiliary information on asteroid orbits and basic photometric parameters. Ready to ingest the astorb data base: ftp://cdsarc.u-strasbg.fr/pub/cats/B/astorb/astorb.html
Attribution
If you have used Gaia data in your research, please use the following acknowledgement:
This work has made use of data from the European Space Agency (ESA) mission Gaia (http://www.cosmos.esa.int/gaia), processed by the Gaia Data Processing and Analysis Consortium (DPAC, http://www.cosmos.esa.int/web/gaia/dpac/consortium). Funding for the DPAC has been provided by national institutions, in particular the institutions participating in the Gaia Multilateral Agreement.
More information can be found on the credit and citation instructions page.
Columns
Name | Type | UCD | Unit | Description |
---|---|---|---|---|
solution_id | long | meta.version |
Solution Identifier |
|
number_mp | long | meta.id |
Asteroid MPC number |
|
designation | char |
meta.id meta.main |
MPC name |
|
mag_h | double | phot.mag | Magnitude[mag] |
absolute magnitude |
slope_g | double | stat.fit.param |
slope parameter |
|
code | int | meta.code.status |
object specific flags |
|
obs_arc | long | time.interval | Time[day] |
arc spanned by the observations |
obs_num | long | meta.number |
number of observations used |
|
osc_epoch | char | time.epoch | Time[yyyymmdd] |
epoch of osculation |
orb_m | double | src.orbital.meanAnomaly | Angle[deg] |
mean anomaly |
omega | double | src.orbital.periastron | Angle[deg] |
argument of perihelion |
node_omega | double | src.orbital.node | Angle[deg] |
longitude of ascending node |
inclination | double | src.orbital.inclination | Angle[deg] |
orbit inclination |
eccentricity | double | src.orbital.eccentricity |
orbit eccentricity |
|
a | double |
src.orbital phys.size.smajAxis |
Length & Distance[AU] |
semimajor axis |
orb_date | char | time.processing | Time[yyyymmdd] |
date of orbit computation |
ceu | double |
src.orbital stat.error |
Angle[arcsec] |
current orbit uncertainty |
ceu_rate | double |
arith.rate src.orbital stat.error |
Angular Velocity[mas/s] |
rate of change of the orbit uncertainty |
ceu_epoch | char | time | Time[yyyymmdd] |
date of the CEU |