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 21820U 91086B 24254.79145793 .00003080 00000-0 60738-3 0 9997
2 21820 82.5665 358.4301 1567702 150.2803 219.7497 11.95422115422107
| Epoch (UTC): | 10 September 2024 18:59:41 |
| Eccentricity: | 0.1567702 |
| inclination: | 82.5665° |
| perigee height: | 435 km |
| apogee height: | 2968 km |
| right ascension of ascending node: | 358.4301° |
| argument of perigee: | 150.2803° |
| revolutions per day: | 11.95422115 |
| mean anomaly at epoch: | 219.7497° |
| orbit number at epoch: | 42210 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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