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 25977U 99064A 24276.40117067 .00005342 00000-0 63348-3 0 9996
2 25977 98.2256 151.5795 0001348 37.7104 322.4204 14.84958506607522
| Epoch (UTC): | 02 October 2024 09:37:41 |
| Eccentricity: | 0.0001348 |
| inclination: | 98.2256° |
| perigee height: | 613 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 151.5795° |
| argument of perigee: | 37.7104° |
| revolutions per day: | 14.84958506 |
| mean anomaly at epoch: | 322.4204° |
| orbit number at epoch: | 60752 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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