To set the orbit so that it uses the data entered above, click here. Not available because the solar system bodies that ship with Starry Night can not be changed.
To set the orbit so that it uses the data entered above, click here.
Enter the second line of the NASA two line data here by selecting all, then pasting. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter the second line of the NASA two line data here by selecting all, then pasting.
Enter the first line of the NASA two line data here by selecting all, then pasting. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter the first line of the NASA two line data here by selecting all, then pasting.
Enter orbit’s revolution here. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter orbit’s revolution here.
Enter orbit’s decay rate here. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter orbit’s decay rate here.
Enter orbit’s mean motion here. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter orbit’s mean motion here.
Enter orbit’s mean anomaly here. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter orbit’s mean anomaly here.
Enter orbit’s argument of perigee here. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter orbit’s argument of perigee here.
Enter orbit’s eccentricity here. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter orbit’s eccentricity here.
Enter the right ascension of the orbit’s ascending node here. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter the right ascension of the orbit’s ascending node here.
Enter orbit’s inclination here. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter orbit’s inclination here.
Enter the AMSAT element set for the object here. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter the AMSAT element set for the object here.
Enter the data’s epoch here. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter the data’s epoch here.
Enter the AMSAT catalogue number for the object here. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter the AMSAT catalogue number for the object here.
To change the orbit’s mean anomaly, use this slider. Not available because the solar system bodies that ship with Starry Night can not be changed.
To change the orbit’s mean anomaly, use this slider.
To change the mean distance from the orbit to the body being orbited, use this slider. Not available because the solar system bodies that ship with Starry Night can not be changed.
To change the mean distance from the orbit to the body being orbited, use this slider.
Enter the data’s epoch here. Not available because the solar system bodies that ship with Starry Night can not be changed.
Enter the data’s epoch here.
Use this slider to select the point in the orbit at which pericentre occurs. Not available because the solar system bodies that ship with Starry Night can not be changed.
Use this slider to select the point in the orbit at which pericentre occurs.
Use this slider to select a time at which the object will be at the orbit’s pericentre. Not available because the solar system bodies that ship with Starry Night can not be changed.
Use this slider to select a time at which the object will be at the orbit’s pericentre.
To change the distance from the orbit’s pericentre to the body being orbited, use this slider. Not available because the solar system bodies that ship with Starry Night can not be changed.
To change the distance from the orbit’s pericentre to the body being orbited, use this slider.
To change the orbit’s ascending node, use this slider. Not available because the solar system bodies that ship with Starry Night can not be changed.
To change the orbit’s ascending node, use this slider.
To change the orbit’s tilt on an axis through its nodes, use this slider. Not available because the solar system bodies that ship with Starry Night can not be changed.
To change the orbit’s tilt on an axis through its nodes, use this slider.
To change the orbit’s eccentricity, use this slider. Not available because the solar system bodies that ship with Starry Night can not be changed.
To change the orbit’s eccentricity, use this slider.
Use this popup to select a reference plane for the data. Not available because the solar system bodies that ship with Starry Night can not be changed.
Use this popup to select a reference plane for the data.
Use this popup to select the format to use when editing or viewing the object’s orbital elements
