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 22148.89576816 .00000087 00000-0 69124-4 0 9999
2 23405 70.9834 16.6242 0000818 143.7868 216.3310 14.15255665420857
| Epoch (UTC): | 28 May 2022 21:29:54 |
| Eccentricity: | 0.0000818 |
| inclination: | 70.9834° |
| perigee height: | 841 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 16.6242° |
| argument of perigee: | 143.7868° |
| revolutions per day: | 14.15255665 |
| mean anomaly at epoch: | 216.3310° |
| orbit number at epoch: | 42085 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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