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 23851U 96024A 22222.14511257 .00000283 00000-0 22882-3 0 9994
2 23851 98.8866 169.5157 0008009 148.1279 212.0371 13.98129332341688
| Epoch (UTC): | 10 August 2022 03:28:57 |
| Eccentricity: | 0.0008009 |
| inclination: | 98.8866° |
| perigee height: | 894 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 169.5157° |
| argument of perigee: | 148.1279° |
| revolutions per day: | 13.98129332 |
| mean anomaly at epoch: | 212.0371° |
| orbit number at epoch: | 34168 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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