View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 23405U 94077B 22148.82508850 .00000079 00000-0 65265-4 0 9998
2 23405 70.9835 16.7728 0000815 143.6156 216.5022 14.15255625421112
| Epoch (UTC): | 28 May 2022 19:48:07 |
| Eccentricity: | 0.0000815 |
| inclination: | 70.9835° |
| perigee height: | 841 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 16.7728° |
| argument of perigee: | 143.6156° |
| revolutions per day: | 14.15255625 |
| mean anomaly at epoch: | 216.5022° |
| orbit number at epoch: | 42111 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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