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 25476U 98053B 24357.52332529 .00002463 00000-0 86295-3 0 9999
2 25476 45.0086 21.8393 0002090 354.8854 5.1972 14.37439951372207
| Epoch (UTC): | 22 December 2024 12:33:35 |
| Eccentricity: | 0.0002090 |
| inclination: | 45.0086° |
| perigee height: | 765 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 21.8393° |
| argument of perigee: | 354.8854° |
| revolutions per day: | 14.37439951 |
| mean anomaly at epoch: | 5.1972° |
| orbit number at epoch: | 37220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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