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Table 1

Geometric circumstances of the OE observations performed by VIR.

Cube SCET number α coverage [deg] i⟩ [deg] e⟩ [deg] SR [km pix−1]
V546731788 0.630–1.310 60.7 61.6 5.0
V546732290 0.644–1.344 56.5 57.3 5.0
V546733092 0.009–1.506 31.0 31.6 5.0
V546733894 0.006–1.560 34.9 35.4 5.0
V546734698 0.244–1.655 32.1 32.7 5.0
V546735500 0.010–1.639 43.0 43.6 5.0
V546736302 0.404–1.011 64.9 65.5 5.0
V546742558 2.101–2.732 40.7 42.7 4.9
V546743360 2.450–2.967 47.8 50.3 4.9
V546744162 2.815–3.201 56.6 59.5 4.9
V546749758 3.234–3.680 33.8 36.1 4.9
V546750560 3.832–4.124 47.8 51.3 4.9
V546751362 2.697–4.479 40.4 42.1 4.8
V546759118 4.753–5.215 29.7 31.9 4.8
V546759920 4.944–5.904 51.7 56.9 4.8
V546760722 4.396–5.668 36.4 35.9 4.8
V546762658 4.862–6.466 39.8 42.8 4.8
V546763460 5.158–5.651 30.6 30.2 4.7
V546764262 6.072–6.490 39.3 44.5 4.8
I546730582 0.091–1.624 32.5 33.1 5.0

Notes. For each cube, the SCET (spacecraft elapsed time) number (V and I prefix indicate visible and infrared observations, respectively), the phase angle α coverage, the average incidence i and emission e angles, and the spatial resolution (SR) are reported.

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