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 09982U 77012F 24357.52154669 .00000136 00000-0 45183-3 0 9998
2 09982 65.8964 153.7826 1708836 61.2217 314.9577 10.80864950887721
| Epoch (UTC): | 22 December 2024 12:31:01 |
| Eccentricity: | 0.1708836 |
| inclination: | 65.8964° |
| perigee height: | 786 km |
| apogee height: | 3739 km |
| right ascension of ascending node: | 153.7826° |
| argument of perigee: | 61.2217° |
| revolutions per day: | 10.80864950 |
| mean anomaly at epoch: | 314.9577° |
| orbit number at epoch: | 88772 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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