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 24925U 97048A 24358.15751134 .00000788 00000-0 85489-4 0 9990
2 24925 86.3355 216.6423 0008717 60.3230 299.8861 14.86689348479218
| Epoch (UTC): | 23 December 2024 03:46:48 |
| Eccentricity: | 0.0008717 |
| inclination: | 86.3355° |
| perigee height: | 602 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 216.6423° |
| argument of perigee: | 60.3230° |
| revolutions per day: | 14.86689348 |
| mean anomaly at epoch: | 299.8861° |
| orbit number at epoch: | 47921 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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