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 14781U 84021B 24261.47967091 .00008188 00000-0 90967-3 0 9993
2 14781 97.7153 228.0633 0009605 124.6638 235.5485 14.87407528162208
| Epoch (UTC): | 17 September 2024 11:30:43 |
| Eccentricity: | 0.0009605 |
| inclination: | 97.7153° |
| perigee height: | 599 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 228.0633° |
| argument of perigee: | 124.6638° |
| revolutions per day: | 14.87407528 |
| mean anomaly at epoch: | 235.5485° |
| orbit number at epoch: | 16220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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