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 53807U 22111AL 24280.63841104 .00019500 00000-0 69650-3 0 9997
2 53807 53.2359 39.1349 0009104 75.7030 284.4981 15.28844194115264
| Epoch (UTC): | 06 October 2024 15:19:18 |
| Eccentricity: | 0.0009104 |
| inclination: | 53.2359° |
| perigee height: | 473 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 39.1349° |
| argument of perigee: | 75.7030° |
| revolutions per day: | 15.28844194 |
| mean anomaly at epoch: | 284.4981° |
| orbit number at epoch: | 11526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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