Scenarios:
Orbital Shadow Cone Geometry
Sun → Moon → Earth
Umbra (Total Shadow)
Penumbra (Partial)
Earth
Moon
Observer Sky Vantage Projection
Obscuration: 100.0%
Totality: Solar Corona Active
Moon Orbit Phase Angle: 0.0° (New Moon)
Totality (C2 → C3)
Orbital Parameters
Direct Control
Primary Alignment
Solar Eclipse
Lunar Distance ($d_{moon}$)
363,300 km (Perigee)
Perigee creates Total Solar; Apogee creates Annular "Ring of Fire".
Orbital Plane Node Tilt ($i$)
0.00° (Node Crossing)
Moon's 5.14° tilt causes shadows to miss Earth most new/full moons.
Observer Track Offset
0.0° (Centerline)
Distance from the centerline changes totality into partial eclipse.
Geometric Telemetry
Calculated
Angular Ratio
1.034
θ Moon / θ Sun
Umbra Cone Length
375,800 km
Reaches Earth? YES
Shadow Footprint
198 km
Path of Totality
Eclipse Category
Total Solar
Duration ~ 4m 28s
Geometric Principle: In this configuration, the Moon is near perigee so its apparent angular diameter ($33.1'$) exceeds the Sun's ($31.9'$), allowing the Umbra shadow cone to reach Earth's surface and create a Total Solar Eclipse with full coronal visibility along the central track.