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 5918U 72022B 24358.00054945 .00000255 00000-0 14514-3 0 9995
2 5918 81.2363 189.3613 0058223 170.0703 190.1631 14.06186247703816
| Epoch (UTC): | 23 December 2024 00:00:47 |
| Eccentricity: | 0.0058223 |
| inclination: | 81.2363° |
| perigee height: | 830 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 189.3613° |
| argument of perigee: | 170.0703° |
| revolutions per day: | 14.06186247 |
| mean anomaly at epoch: | 190.1631° |
| orbit number at epoch: | 70381 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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