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 is defined by the following mean orbital elements,
1 53462U 98067UB 23068.08779678 .11260875 12411-4 73372-3 0 9999
2 53462 51.6110 79.8349 0001728 245.2836 114.8011 16.40891195 32706
| Epoch (UTC): | 09 March 2023 02:06:25 |
| Eccentricity: | 0.0001728 |
| inclination: | 51.6110° |
| perigee height: | 162 km |
| apogee height: | 164 km |
| right ascension of ascending node: | 79.8349° |
| argument of perigee: | 245.2836° |
| revolutions per day: | 16.40891195 |
| mean anomaly at epoch: | 114.8011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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